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flying+range

  • 81 kortdistanseflying

    subst. short range flying

    Norsk-engelsk ordbok > kortdistanseflying

  • 82 kortdistanseflyvning

    subst. (Riksmål, eg. kortdistanseflyging) short range flying

    Norsk-engelsk ordbok > kortdistanseflyvning

  • 83 в зависимости от

    1. against
    2. in terms of

    держащийся вдали; отдаление отkeeping off

    3. subject to

    корка, отслоившаяся от мякишаflying top crust

    обувь, предохраняющая от скольженияsafety toe shoes

    4. vers
    5. versus
    6. with

    идти наравне; идти в ногу; не отставать отkeep pace with

    7. depending of

    отказываться от, расторгатьdeclare off

    отрываться от земли; стартоватьlift off

    8. depending on
    9. depending upon

    Русско-английский большой базовый словарь > в зависимости от

  • 84 дисплей с растром телевизионного типа

    Русско-английский большой базовый словарь > дисплей с растром телевизионного типа

  • 85 пол

    1. м. floor
    2. margin
    3. dale
    4. с. field

    переменное поле — variable field; alternating field

    тормозящее поле — retarding field; brake field

    лётное поле, аэродромflying field

    Синонимический ряд:
    пустотелый (прил.) пустой; пустотелый
    Антонимический ряд:

    Русско-английский большой базовый словарь > пол

  • 86 high

    [haɪ]
    1. adjective
    1) at, from, or reaching up to, a great distance from ground-level, sea-level etc:

    a dive from the high diving-board.

    عالٍ
    2) having a particular height:

    My horse is fifteen hands high.

    ذو ارتفاع، أرتِفاعُهُ
    3) great; large; considerable:

    The child has a high fever/temperature.

    عظيم، عالٍ
    4) most important; very important:

    a high official.

    الأهَم
    5) noble; good:

    high ideals.

    نبيل، رفيع، جيِّد
    6) (of a wind) strong:

    The wind is high tonight.

    قوي
    7) (of sounds) at or towards the top of a (musical) range:

    a high note.

    نغمة عاليَه
    8) (of voices) like a child's voice (rather than like a man's):

    He still speaks in a high voice.

    عالي الصوت
    9) (of food, especially meat) beginning to go bad.
    تالِف
    10) having great value:

    Aces and kings are high cards.

    ذو قيمة عاليَه
    2. adverb
    at, or to, a great distance from ground-level, sea-level etc:

    He'll rise high in his profession.

    على ارتفاع عالٍ

    Arabic-English dictionary > high

  • 87 крен


    roll, aileron (ail)
    (канал автопилота)
    - (маневр)roll
    поворот самолета вокруг продольной оси, при котором между поперечной осью и горизонтальной плоскостью образуется угол. — the act of rolling: rotational or oscillatory movement of an aircraft about а longitudinal axis.
    - (угол относительно продопьной оси самолета) (рис. 135) — bank, angle of roll when the aircraft is banked in a turn toward a selected heading, the bank indicator and heading pointer are displaced on the same side of the lubber line.
    -, внешний — outside /outer/ roll
    крен при отрицательном угле атаки, — а roll executed while flying in the negative angle of attack range.
    - внутренний — inside /inner/ roll
    -, левый (правый) — left (right) bank, roll to the left (right)
    -, наружный — outside /outer/ roll
    - при разворотеbank in turn
    движение no к. — rolling motion
    демпфирование к. — roll damping
    момент к. — rolling moment
    неустойчивость no к. — roll instability
    ошибка no к. — roll error
    положение по к. — roll attitude
    разворот с к....° — turn with bank of...deg., deg. bank(ed) turn
    реакция no к. — roll response
    с к...градусов — with -degree bank
    устойчивость по к. — rolling stability
    управление по к. — roll control
    вводить в к. — roll, bank
    входить в к. — roll
    выполнять к. — bank, roll bank (or roll) the aircraft to keep the roll command bar centered.
    выполнять левый (правый) к. для выдерживания командной курсовой стрелки (пкп) в нулевом (среднем) положении — roll left (right) to keep the roll command bar centered
    выполнять левый (правый) к. до момента обнуления командной курсовой стрелки (пкп) — roll left (right) until the roll command bar centers
    выставлять самолет в линию горизонтального полета без к. — position the aircraft at wingslevel, wing-level the airplane

    Русско-английский сборник авиационно-технических терминов > крен

  • 88 нагрузка


    load
    - (нервно-психическая и физическая)workload
    -, асимметричная — unsymmetrical load
    асимметричная нагрузка на самолет может возникнуть при отказе критического двигателя. — the airplane must be designed for unsymmetrical loads resulting from the failure of the critical engine.
    -, аэродинамическая — aerodynamic load
    -, безопасная — safe load
    -, боковая — side load
    для случая боковой нагрузки предполагается что самолет находится в горизонтальном положении при условии касания земли только колесами основных опор. — for the side load condition, the airplane is assumed to be in the level attitude with only the main wheels contacting the ground.
    -, вертикальная — vertical load
    -, вибрационная — vibration load
    -, воздушная — air load
    -, вызванная отказом двигателя, асимметричная — unsymmetrical load due to engine failure
    - генератораgenerator load
    -, гидравлическая — hydraulic load
    -, гироскопическая — gyroscopic load
    -, десантная — air-delivery load
    -, десантная (парашютная) — paradrop load
    -, динамическая — dynamic load
    нагрузка, возникающая при воздействии положительного (ипи отрицательного) ускорения на конструкцию ла. — any load due to acceleration (or deceleration) of an aircraft, and therefore proportional to its mass.
    -, динамическая, при полном вытягивании строп парашюта до наполнения купола — (parachute) deployment shock load the load which occurs when the rigging lines become taut prior to inflation of the canopy.
    -, динамическая, при раскрытии купола парашюта — (parachute) opening shock load

    maximum load developed during rapid inflation of the canopy.
    -, длительная — permanent load
    -, допускаемая прочностью самолета — load not exceeding airplane structural limitations
    -, допустимая — allowable load
    -, знакопеременная — alternate load
    -, индуктивная (эл.) — inductive load
    -, инерционная — inertia load
    -, коммерческая bес пассажиров, груза и багажа. — payload (p/l) weight of passengers, cargo, and baggage.
    - коммерческая, располагаемая — payload available
    -, максимальная коммерческая — maximum payload
    разность между максимальным расчетным весом без топлива и весом пустого снаряженного ла. — maximum design zero fuel weight minus operational empty weight.
    -, максимальная предельная радиальная (на колесо) — maximum radial limit load (rating of each wheel)
    -, максимальная статическая (на колесо) — maximum static load (rating of each wheel)
    -, маневренная — maneuvering load
    -, минимальная расчетная — minimum design load
    при определении минимальных расчетных нагрузок необходимо учитывать влияние возможных усталостных нагрузок и нагрузок от трения и заклинивания. — the minimum design loads must provide а rugged system for service use, including consideration of fatigua, jamming and friction loads.
    -, моментная (напр. поворотного срезного болта водила) — torque load
    - на вал (ротор)shaft (rotor) load
    - на генераторgenerator load
    - на гермокабину (от избыточного давления)pressurized cabin pressure differential load
    конструкция самолета допжна выдерживать полетные нагрузки в сочетании с нагрузками от избыточного давления в гермокабине. — the airplane structure must be strong enough to withstand the flight loads combined with pressure differential loads.
    - на двигательpower load on engine

    prevent too sudden and great power load being thrown on the engine.
    - на единицу площадиload per unit area
    - на колесоwheel load
    - на колонку (или штурвал, ручку) при продольном yправлении — elevator pressure (felt when deflecting control column (wheel or stick)
    - на конструкцию, выраженная в единицах ускорения (статическая и динамическая) — (static and dynamic) loads on structure expressed in g units
    - на крыло, удельная — wing loading
    часть веса самолета, приходящаяся на единицу поверхности крыла и равная частномy от деления полетного веса самолета на площадь крыла. — wing loading is gross weight of aeroplane divided by gross wing area.
    - на лопасть, удельная — blade loading
    - на моторамуload on engine mount
    - на мотораму, боковая — side load on engine mount
    - на мощность, удельная часть веса самолета, приходящаяся на единицу силы тяги, развиваемой его силовой установкой при нормальном режиме работы. — power loading the gross weight of an aircraft divided by the horsepower of the engine(s).
    - на орган управления (усилие)control pressure
    - на орган управления, пропорциональная величине отклонения поверхности управнения — control pressure proportional to amount of control surface deflection
    - на орган управления (штурвал, колонку, ручку управления, педали), создаваемая загрузочным механизмом — control pressure created by feel unit /or spring/
    - на орган управления (штурвал, колонку или педали), создаваемая отклоняемой поверхностью управления — control pressure created by control surface
    - на педали при путевом управленииrudder pressure (felt when deflecting pedals)
    - на площадь, сметаемую несущим винтом — rotor disc loading
    величина подъемной силы (тяги) несущего винта, деленная на площадь ометаемую винтом. — the thrust of the rotor divided by the rotor disc area.
    - на поверхность управления — control surface load, backpressure on control surface
    - на поверхность управления от порыва ветраcontrol surface gust load
    - на поверхность управления, удельная — control surface loading the mean normal force per unit area carried by an aerofoil.
    - на полfloor load
    - на пол, удельная — floor loading
    -, направленная к продольной оси самолета, боковая — inward acting side load
    -, направленная от продольной оси самолета, боковая — outward acting side load
    - на размах, удельная — span loading
    полетный вес самолета, деленный на квадрат размаха крыла. — the gross weight of an airplane divided by the square of the span.
    - на растяжение — tensile load /stress, strain/
    - на руль высоты (усилие при отклонении)backpressure on elevator
    - на руль направления (усилие при отклонении)backpressure on rudder
    - на сжатиеcompression load
    - на систему управленияcontrol system load
    максимальные и минимальные усилия летчика, прикладываемые к органам управления (в условиях полета) и передаваемые в точку крепления проводки управления к рычагу поверхности управления. — the maximum and minimum pilot forces are assumed to act at the appropriate control grips or pads (in a manner simulating flight conditions) and to be reacted at the attachment of the control system to control surface horn.
    - на скручиваниеtorsional load
    - на срезshear load
    - на тягу, удельная — thrust loading
    отношение веса реактивного самолета к тяге, развиваемой его двигателем (двигателями), — the weight-thrust ratio of а jet aircraft expressed as gross weight (in kg) divided by thrust (in kg).
    - на шасси при посадкеground load on the landing gear at touch-down
    - на шину (колеса)load on tire
    - на штурвал (ручку) при управлении no кренуaileron pressure (felt when deflecting control wheel (or stick)
    - на элерон (усилие при отклонении)backpressure on aileron
    -, номинальная (эл.) — rated load
    -, нормальная — normal load
    -, нормальная эксплуатационная (в системах управления) — normal operating load control system load that can be obtained in normal operation.
    -, ограниченная весом, коммерческая (платная) — weight limited payload (wlp)
    коммерческая нагрузка, oграниченная одним наиболее перечисленных ниже): — payload as restricted by the most critical of the following:
    1. взлетным весом снаряженного самолета за вычетом веса пустого снаряженного самолета и минимального запаса расходуемого топлива. — 1. operational takeoff weight minus operational empty weight minus minimum usable fuel.
    2. посадочным весом снаряженного самолета за вычетом веса пустого снаряженнаго самолета и анз топлива. — 2. operational landing weight minus operational empty weight minus flight reserve fuel.
    3. ограничениями по использованию отсеков. данная нагрузка не должна превышать макс. коммерческую нагрузку. — 3. compartment and other related limits. (it must not exceed maximum payload).
    -, ограниченная объемом, коммерческая (платная) — space limited payload (slp)
    нагрузка, ограниченная числом мест, объемными и другими пределами кабины, грузовых и багажных отсеков, — payload as restricted by seating,volumetric, and other related limits of the cabin, cargo, and baggage compartments. (it must not exceed maximum payload).
    -, омическая (эл.) — resistive load
    -, осевая — axial load
    -, основная — basic load
    - от встречного порыва (ветpa)load resulting from encountering head-on gust
    - от заклинивания (подвижных элементов)jamming load
    - от избыточного давления (в гермокабине)pressure differential load
    - от порыва (ветра)gust load
    случай нагружения конструкции самолета, особенного крыла, в результате воздействия на самолет вертикальных и горизонтальных воздушных течений (порывов), — the load condition which is imposed on an airplane, especially the wings, as a result of the airplane's flying into vertical or horizontal air currents.
    - от тренияfriction load
    -, параллельная линия шарниров (узлов подвески поверхностей управления). — load parallel to (control surface) hinge line
    -, переменная (по величине) — varying load, load of variable magnitude
    -, пиковая — peak load
    -, платная (коммерческая) — payload (p/l)
    beс пассажиров, груза и багажа. — weight of passengers, cargo, and baggage.
    -, повторная — repeated load
    расчеты и испытания конструкции должны продемонстрировать ее способность выдерживать повторные переменные нагрузки возможные при эксплуатации. — the structure must be shown by analysis, tests, or both, to be able to withstand the repeated load of variable magnitude expected in service.
    -, погонная — load per unit length
    -, полезная — payload (p/l)
    вес пассажиров, груза, багажа — weight of passengers, cargo, and baggage.
    -, полезная — useful load
    разность между взлетным весом снаряженного и весом пустого снаряженного ла. (включает: коммерческую нагрузку, вырабатываемые топливо и др. жидкости, не входящие в состав снаряжения ла). — difference between operational takeoff weight and operational empty weight. (it includes payload, usable fuel, and other usable fluids not included as operational items).
    -, полетная — flight load
    отношение составляющей аэродинамической силы (действующей перпендикулярно продольной оси самолета) к весу самолета. — flight load factors represent the ratio of the aerodynamic force component (acting normal to the assumed longitudinal axis of the airplane) to the weight of the airplane.
    -, полная — full load
    включает вес экипажа, снаряжения, топлива и полезной нагрузки.
    -, постоянная — permanent load
    - предельная, разрушающая (по терминологии икао) — ultimate load
    -, продольная — longitudinal load
    -, равномерная — uniform load
    -, радиальная эксплуатационная (на каждое колесо шасcи) — radial limit load (rating of each wheel)
    -, разрушающая (расчетная) — ultimate load
    нагрузка, в результате которой возникает, или может возникнуть на основании расчетов, разрушение элемента конструкции. — the load which will, or is computed to, cause failure in any structural member.
    -, разрушающая (способная вызывать разрушение) — destructive load
    торможение может привести к появлению разрушающей нагрузки на переднее колесо. — braking can cause destructive loads on nosewheel.
    -, распределенная — distributed load
    -, рассредоточенная — distributed load
    -, расчетная — ultimate load
    расчетная нагрузка опрелеляется как произведение эксплуатационной нагрузки на коэффициент безопасности. — ultimate load is the limit load multiplied by the prescribed factor of safety.
    -, расчетная (по терминологии икао) — proof load
    -, расчетная (по усилиям в системе управления) — design load design loads are accepted in the absence of a rational analysis.
    -, скручивающая — torsional load
    -, служебная — operational items /load/
    включает экипаж, парашюты, кислородное оборудование экипажа, масло для двигателей и невырабатываемое топливо. — includes: crew, parachutes, crew's oxygen equipment, engine oil, unusable fuel.
    -, служебная (стандартная) — standard items
    служебная нагрузка может включать: нерасходуемые топливо и жидкости, масло для двигателей, огнетушители, аварийное кислородное оборудоавние, конструкции в буфете, дополнительное электронное оборудование. — may include, unusable fuel and other fluids, engine oil, toilet fluid, fire extinguishers, emergency oxygen equipment, structure in galley, buffet, supplementary electronic equipment.
    - снаряженного (самолета)operational load
    -, сосредоточенная — concentrated load
    -, статическая — static load
    постоянно действующая нагрузка, постепенно возрастающая от нуля до своего максимума при нулевом ускорении. — а stationary load or one that is gradually increased from zero to its maximum. it is an unaccelerated basic load.
    -, суммарная — total load
    -, ударная — impact load
    -, уравновешивающая — balancing load
    -, усталостная — fatigue load
    -, фрикционная — friction load
    -, центробежная (на ротор) — centrifugal loading (on rotor)
    -, частичная — partial load
    -, чрезмерная — overload(ing)
    -, эксплуатационная — limit load
    максимальная нагрузка, воздействующая на самолет в эксплуатации, — the strength requirements are specified in terms of limit loads (the maximum loads to be expected in service).
    -, эксплуатационная нормальная (на систему управления) — normal operating load, load obtained in normal operationtained in normal operation
    -, электрическая — (electrical) load
    весовая отдача по полезной н. — useful load-to-takeoff weight ratio
    зависимость платной н. от дальности полета — payload-range curve
    под н. — under load
    при установившемся режиме работы с полной н. — at steady full-load conditions
    распределение н. — load distribution
    точка приложения н. — point of load application
    характеристика н. — load characteristic
    включать (эл.) н. — activate load
    включать (эл.) н. на генератор, (аккумулятор) — apply load to (generator, battery)
    воспринимать н. — take up load
    выдерживать н. — withstand /support/ load
    испытывать h. — be subjected to load
    нести h. — carry load
    передавать н. — transmit load
    подключать (эл.) н. к... — apply load to...
    прикладывать — apply load to...
    работать без н. (об электродвигателе, преобразователе) — run unloaded
    сбрасывать (эл.) н. — deactivate load
    снимать н. (руля высоты) — relieve elevator pressure, adjust elevator trim tab, relieve pressure by adjusting elevator trim control
    создавать (маханическую) н. — impose load on...
    устанавливать за счет платной h. — install (smth) with payload penalty

    Русско-английский сборник авиационно-технических терминов > нагрузка

  • 89 устройство


    device
    (агрегат, приспособление)
    - автоматического поиска записи программы (магнитофона)automatic program locate device (apld)
    - автоматическое навигационное — automatic navigation device the dr computer is a part of the automatic navigation device.
    - автоматическое навигационное(ану) — dead reckoning computer, dr computer (dr cmptr)
    входные параметры: путевая скорость, угол сноса и карты, ивс, скорость и направление ветра для определения места ла. — in its traditional form the dr computer uses the ground and airspeed data, drift angle, wind speed and direction.
    - автономное (автоматическое) навигационное (ану) — dead-reckoning computer, dr computer
    - автостабилизирующее (вертолета)automatic stabilization installation
    - алфавитно (-буквенно) цифровое печатающее (ацпу)alpha-numerical printer
    -, антенносогласующее (асу) — antenna coupler
    - арифметическое (ау)arithmetic unit
    -, арретирующее (арретир) — caging device
    -, блокирующее (блокировочное, для отключения и удержания в нерабочем положении оборудования при нарушении его нормальной работы) — lockout /locking-out/ device used to shut down ал@ hold an equipment out of service on occurrence of abnormal conditions.
    -, блокирующее — interlock
    устройство, включаемое срабатыванием другого устройства, находящимся с первым в прямой взаимосвязи, для управления данного или связанного с ним устройств, — а device actuated by operation of some other device with which it is directly associated, to govern succeeding operations of the same or allied devices.
    -, бортовое погрузочное (бпу) — (airborne) cargo handling device
    специальная каретка со стропами, перемещающаяся пo потолочным рельсам в грузовой кабине. — cargo handling device carriage moving along rails in cargo compartment.
    - ввода (в уст-ве ввода и индикации)insertion device
    - ввода/вывода (увв, для эвм) — input/output device (in-out device)

    transfer of data between the program and input/output devices.
    - ввода и индикации (уви инерциальной навигационной системы) — control display unit (c/du, cdu)
    - вентилятора (гтд), реверсивное — fan reverser
    -, весоизмерительное — balance (for weighing)
    -, взлетно-посадочное (шасси) — landing gear
    -, визуальное сигнальное (аварийной сигнализации) — visual warning device
    - внутрисамолетной связи для техобслуживания — ground service interphone system, ground crew interphone system
    -, входное (двиг.) — engine air inlet section

    it is directly attached to the front flange of the engine.
    - выдержки времени (реле)time delay relay
    -, выключающее (эл.) — tripping device
    механическое или электромагнитное ус-во для размыкания аэс. — а mechanical or electromagnetic device used for opening (turning off) a circuit breaker.
    -, выпрямительное (ву) — rectifier (rect)
    -, выпрямительное (трансформаторное) (ву) — transformer rectifier unit (tru)
    -, выхлопное (двиг.) — exhaust unit
    -, выходное (двиг. в реактивном сопле за турбиной) — exhaust unit
    -, вычислительное (ву) — computer (cmptr)
    -,вычислительное(системы ссос) — gpws computer
    -,вычислительное,директорное — steering computer command input signals are provided to the steering computer.
    -, вычислительное, канала крена (системы сау) — roll computer
    -, вычислительное, канала курса (сау) — yaw computer
    -, вычислительное, канала тангажа (сау) — pitch computer
    - горизонтирования (гироплатформы) — (platform) levelling unit /device/
    -, девиационное (магнит. компаса) (рис.80) — compass compensator
    -, декодирующее (дешифратор) — decoder
    устройство для декодирования кодовых сигналов. — a device for decoding а series of coded signals.
    -, демпфирующее — damper
    - для воспроизведения записи с магнитной лентыtape reproducer
    - для выдачи бумажных полотенецpaper towel dispenser
    - для выдачи бумажных салфеток для лица (напр., для удаления косметики) — facial tissue dispenser
    - для выдачи бумажных стаканчиковpaper cup dispenser
    - для выдачи гигиенических пакетовmotion sickness bag dispenser
    - для выдачи гигиенических салфетокsanitary napkin dispenser
    - для выдачи роликовой туалетной бумагиtoilet tissue roll paper dispenser
    - для записи речиvoice recorder
    устройство для записи переговоров членов экипажа. — that portion of the system used to record crew member conversation.
    - для контейнерной загрузки (ла)unit load device (uld)
    - для определения отношения давлений (тяги) двигателя, вычислительное — engine pressure ratio computer used to determine engine rating for all modes of operation.
    - для предотвращений возникновения земного резонанса (вертолета)ground resonance prevention device
    - для тарировки высотомера (см. устройство, тарировочное) — altimeter calibrator
    - для тарировки указателя воздушной скорости (см. устройство, тарировочное) — airspeed calibrator
    - для увеличения подъемной силыhigh-lift device
    - для форсирования тягиthrust augmentor
    - для хранения и выдачи полотенец (в туалете)towel dispenser
    - для хранения и выдачи салфетокnapkin dispenser
    -, дозирующее — metering device
    -, дозирующее (насоса-регулятора двигателя) — throttle valve
    -, долговременное запоминающее (дзу) (постоянной информации) — permanent data storage unit (pdsu)
    -, загрузочное (в системе управления ла) — load feel unit
    -, задерживающее посадочное — arrester gear
    -, запальное — igniter
    устройство, непосредственно служащее для зажигания топлива (горючей смеси) в камере сгорания. — a device used to ignite fuel/air mixture in combustion chamber.
    -, запоминающее — storage /unit/, memory
    -, запоминающее ("блок памяти") — data storage unit (dsu) used to store information.
    -, запоминающее (блок памяти параметров полета) — flight data storage unit (fdsu)
    -, запоминающее ("память" доплеровского измерителя путевой скорости и сноса) — doppler memory (unit)
    в случае отсутствия подачи сигналов, запоминающее устройство фиксирует последние замеры путевой скорости и сноса ла для выдачи их на индикацию. — under conditions of signal loss, the ground speed and drift indication last measured will continue to be displayed indefinitely.
    -, запорно-редуцирующее — shut-off/pressure reducing valve
    -, защитное (в агрегате, системе) — protection /protective/ device
    -, защитное (снаряжение) — protective device
    защитные очки, маски, резиновые перчатки. — use protective devices, such as goggles, face masks, and rubber gloves.
    - защитное, катапультного кресла — ejection seat guard
    - защиты (эл. сети) — circuit protection device
    - защиты (эл. цепи) от повыщенного (или пониженного) напряжения — overvoltage (or undervoltage) protection device
    - защиты (эл. цепи) от пониженной (или повышенной) частоты — underfrequency (or overfrequency) protection device
    - защиты (эл.) сети, повторного включения — resettable circuit protective /protection/ device
    устройство должно размыкать цепь независимо от положения органов управления (выключателей, переключателей) при перегрузке и неисправности данной цепи. — each resettable circuit protective device must be designed so that, when an overload or circuit fault exists, it will open the circuit regardless of the position of the operating control.
    -, звуковое сигнальное (аварийной сигнализации) — audio warning device
    -, имитирующие — simulator
    устройство, имитирующее систему или явление. — а device which represents а system ог phenomenon.
    - индикации выставки (навигационной системы) — align display unit (adu) panel set mode selector of the adu panel to trim lat, trim long, align nav.
    - индикации и сигнализации углов атаки и перегрузок — angle-of-attack and acceleration indicating/warding system
    -, инициирующее (вызывающее срабатывание пиромеханизмов) — initiator
    - и работа (раздел ртэ)construction and operation
    -, кодирующее (шифратор) — coder
    -, коммутационное — switching device, switch gear
    электрическое или механическое устройство, служащее дпя включения и/или выключения цепи (системы), — any device or mechanism, either electrical or mechanical, which can place another device or circuit in an operating or nonoperating state.
    -, коммутационное (соединительная или распределительная коробка) — junction box (jb)
    -, коммутирующее (ук, плата для размещения радиоэлементов напр., диодов, резисторов и т.п.) — circuit board
    - контроляmonitor
    -, контрольно-записывающее (типа кз для регистрации высоты, скорости, перегрузки) — altitude, airspeed and acceleration recorder, height-velocity-g recorder (hvg rcdr)
    -, коррекционное (гироскопического прибора) — erection mechanism
    -, ламельное (для приведения штока рулевого агрегата автопилота при выключенных режимах) — switching (contact) device
    -, лекальное (коррекционного механизма) — cam strip
    -, множительное (ум) — multiplier
    -, моделирующее — simulator
    -, монтажное (амортизированная рама, платформа) — shockmount
    -, наборное (частоты арм) — band selector switch
    -, навигационно-вычислительное (нву, навигационный координатор) состав: пу, задатчики зпу и угла карты, планшет, задатчик ветра. — dead-reckoning navigation system (drns) system incorporates: control panel, dtk and chart angle selectors, roller map and wind selector.
    -, навигационное вычислительнoe (доплеровского оборудования) (рис.82) — (doppler) navigation computer the doppler navigator provides outputs of velocity along and across heading to a navigation computer.
    -, навигационное вычислительное, цифроаналоговое — navigation analog-digital computer
    - навигационное, координаторное (типа ану, нву) — dead reckoning navigation system (drns)
    - натяга (ножного) привязного ремня (на катапультном кресле) — (lap) strap /belt/ retractor
    -, обеспечивающее плавучесть сухопутного самолета при аварийной посадке на воду. — flotation gear an emergency gear attached to а landplane to permit alighting on the water, and to provide buoyancy when resting on the surface of the water.
    - обменаexchange device
    -, оперативное запоминающее (озу) (переменной информации) — random-access memory (ram), working (data) storage unit (wdsu)
    - определения аэродинамических поправок (к показаниям указателя скорости, высотомеров) (уоап) — position error correction (determination) device
    -, осветительное (лампа) — light
    - пеленгаторноеdirection finder
    - первого каскада компрессоpa, входное — lp compressor air inlet section
    -, переходное (переходник) — adapter
    -, переходное (наружной подвески - для крепления к пилону) — store adapter shoe
    -, переходное (соединяющее двигатель с удлинительной трубой или трубу с соплом) — transition section
    -, погрузочно-разгрузочное — cargo handling device
    -, подпорное (в гидравлической системе) — intensifier
    - полупроводниковое.-, постоянное запоминяющее (пзу) — semiconductor device read-only memory (rom), permanent storage unit

    computer storage device which retains the stored data indefinitely.
    -, постоянное запоминающее (внешнее) — permanent storage (unit)
    - предотвращающее перекладку рычага управления шасси в убранное положение на земле — landing gear control lever antiretraction device
    -, предохранительное — safety device
    -, предохранительное (напр., колпачок на выключателе) — guard check switch guard down and safetied.
    - предупредительной тряски штурвала при приближении к критическому углу атаки — stick shaker turn off stall warn switch if alpha off light is illuminated to prevent stick shaker action resulting from a false stall warning due to alpha probe icing.
    -, преобразующее (в системе мсрп) — converter
    - приемопеленгаторноеdirection-finder receiver
    -, приемопеленгаторное (арк) — direction finder
    -, программное (временное) — timer
    -, противообледенительное — anti-icer, de-icer
    -, противообледенительное воздушно-тепловое — hot air anti-icer
    -, противоюзовое — anti-skid device
    -, пусковое (pc или cc) — missile launcher
    -, пылезащитное (пзу, на воздухозаборник двигателя вертолета) — dust protection device (dust prot)
    -, развязывающее (эл.) — decoupler
    -, раздаточное (см. устройство для выдачи) — dispenser
    -, распределительное — distributor
    -, распределительное (эл. сети) — distribution panel (р)
    -, распределительное (распределительная коробка зл. сети) — junction box (jb)
    -, распределительное (панель азс) (напр. ру25) — circuit breaker panel, св panel, (св pnl, р) (р25)
    - распределительное (эл. шина) — bus
    -, распределительное (положение переключателя ру (шин), напр. ру1,ру2 и т.д.) — bus (1, 2) the bus selector switch is set in bus 1 position.
    -, распределительное (ру, распределительная шина) (рис.91) — distribution bus
    шина, запитываемая от питательной магистрали для дальнейшего распределения электропитания по фидерам и цепям. — а conductor connected to the (supply) mains from which electric power is taken to circuits and/or feeders.
    -, распределительное переменного тока (панель азс) — ac power circuit breaker panel
    -, распределительное постоянного тока (панель азс) — dc power circuit breaker panel
    -, распределительное хвостового (хру) (панель азс) — tail circuit breaker panel
    -, распределительное центральное (цру, панель азс) — main circuit breaker panel, main св panel
    -, распределительное центральное (цру, коробка) — main junction box (mjb)
    -, распределительное, центральное (цру, шина) — main distribution bus
    -, реверсивное (двигателя) — thrust reverser
    устройство для изменения направления тяги двигателя на обратно (рис.53). — a device for redirecting the engine exhaust to an opposite direction.
    -, реверсивное, включено — thrust reverser deployed (reverser dplyd, rvsr dpld)
    при включенном ру продолжать полет на пониженной скорости. — if reverser is deployed, continue (flying) at reduced speed.
    -, реверсивное выключено — thrust reverser stowed (reverser stwd, rvsr stwd)
    при невозможности выключения ру необходимо как можно скорее совершить посадку. — if reverser cannot be stowed, land as soon as practical.
    -, реверсивно-тормозное (рту) комбинация створок реверса тяги и тормозных щитков. — thrust/air brakes
    - реверсирования тяги, основное — primary thrust reverser
    - регистрации, бортовое — (flight data) recorder
    - регистрации звуковой информации в кабине экипажаcockpit voice recorder (cvr)
    - регистрации высоты прибop для записи (изменений) высоты по времени полета. — altitude /height/ recorder an instrument by which variation in height is recorded against time.
    -, регулировочное — adjusting device, adjuster
    -, рулежно-демпфирующее (передней опоры шасси) — nosewheel steering/damping control valve (and follow-up assembly)
    - самоконтроля (встроенное) — (built-in, integral) self-test feature
    -, самолетное громкоговорящее (сгу) — passenger /public/ address system (pa)
    сгу предназначено для оповещения пассажиров через громкоговорители. — used to make voice announcements to the passengers over cabin loud speakers.
    -, самолетное переговорное (спу) — interphone system int, intph, intercommunication system (ics, intcom)
    оборудование, обеспечивающее связь между членами экипажа внутри самолета и с техническим персоналом на земле. — that portion of the system which is used by flight and ground personnel to communicate between areas on the aircraft.
    -, самолетное переговорное вспомогательное для связи с бортпроводниками и наземным обслуживающим персоналом. — service interphone system
    - самолетное переговорное громкоговорящее (спгу = сгу + спу) — interphone /intercom/ and passenger /public/ address system (int/pa)
    для связи между членами экипажа и обращения к пассажирам через громкоговорители. — used by the crew members to communicate, and to address the passengers over cabin loud speakers.
    - сброса (показаний прибора)(instrument reading) reset knob
    -, светотехническое (арматура) — light
    - связи (в ацбс) — coupler, coupling device
    -, сигнальное (для подачи сигнала бедствия в случае аварийной посадки) — long-range signaling device
    - смотровое, оптическое — optical viewer
    наблюдение за механическим указателем положения шасси осуществляется посредством смотрового оптического устройства. — the nose gear (mechanical) indicators can be seen through an optical viewer in aft bulkhead.
    -, согласующее (системы регистрации параметров полета) — signal conditioning unit
    -, сопрягающее/сопряжения / (блоков, систем) — interface
    -, сравнивающее (блок сравнения данных) — comparator
    ус-тва и цепь для сравнения информации, поступающей из двух источников. — a device (in computer operations) or circuit for comparing information from two sources.
    -, стопорное (арретирующее) — caging device
    -, стопорное (фиксатор) — lock, latch
    - счисления пути, вычислительное — dead-reckoning computer dr computer outputs are latitude and longitude.
    -, тарировочное (калибратор) — calibrator
    - тарировочное (высотомера)altimeter calibrator
    устройство для определения инструментальной погрешности высотомера. — an apparatus for measuring the instrument errors of an altimeter.
    -, тарировочное (указателя воздушной скорости) — airspeed calibrator an apparatus for measuring the instrument errors of an airspeed indicator.
    -, термокомпенсационное (напр., трубопровода) — thermal compensator
    -, тормозное (тормоз) — brake
    -, тормозное (специальное) к спец. тормозным устройствам относятся: устройства реверсирования тяги, возд. тормоза, спойлеры, реверсивные возд. винты. — deceleration device special deceleration (or retardation) devices include thrust reversers, air brakes, spoilers, ground fine and reverse pitch propellers.
    -, трансформаторно-выпрямительное (ву) — transformer-rectifier unit (tr, t/r, tru, xfmr-rect)
    - управляющее вычислительное (системы автоматического управления ла)steering computer
    - усилительно-выпрямительное (уву)transformer rectifier unit (tru)
    -, форсажное (форсажная камера) — afterburner
    -, форсажное (пд) — augmentor
    выхлопная система пд включает форсажное устройство. — exhaust system for reciproсating engines includes augmentors.
    -, фронтовое, двигателя (между двигателем и удлинительной трубой) — jet pipe transition section
    -, фронтовое, реактивного сопла (между удлинительной трубой и pc) — jet /propelling/ nozzle transition section
    -, центральное распределительное (панель) — main distribution panel
    -, центральное, распределительное (цру, коробка эл. сети) — main junction box (mjb)
    -, центральное распределительное (цру, шина) — main distribution bus
    шина между источником питания и распределительными шинами (рис.91). — a conductor connected between а generating source and distribution busses.
    -, центральное, распределительное (центральный распределительный энергоузел) — main distribution center wires extending from а generator bus to the main distribution center.
    -, цифровое вычислительное — digital computer
    вычислительное ус-во обрабатывающее и выдающее информацию в цифровой форме. — a computer which operates with information represented in а digital form.
    - часового типа (таймер) — timer, clockwork timing device
    -, электромагнитное стопорное (рулевого агрегата автопилота) — solenoid brake
    -, электромеханическое — electromechanical device
    гироскоп является точным электромеханическим устройством. — a gyroscope is а delicate electromechanical device.
    выполнять свою функцию (о защитном у.) — serve its purpose
    срабатывать (о защитном у.) — operate, become actuated, come into action

    Русско-английский сборник авиационно-технических терминов > устройство

  • 90 Anschütz, Ottomar

    [br]
    b. 1846 Lissa, Prussia (now Leszno, Poland) d. 1907
    [br]
    German photographer, chronophotographer ana inventor.
    [br]
    The son of a commercial photographer, Anschütz entered the business in 1868 and developed an interest in the process of instantaneous photography. The process was very difficult with the contemporary wet-plate process, but with the introduction of the much faster dry plates in the late 1870s he was able to make progress. Anschütz designed a focal plane shutter capable of operating at speeds up to 1/1000 of a second in 1883, and patented his design in 1888. it involved a vertically moving fabric roller-blind that worked at a fixed tension but had a slit the width of which could be adjusted to alter the exposure time. This design was adopted by C.P.Goerz, who from 1890 manufactures a number of cameras that incorporated it.
    Anschütz's action pictures of flying birds and animals attracted the attention of the Prussian authorities, and in 1886 the Chamber of Deputies authorized financial support for him to continue his work, which had started at the Hanover Military Institute in October 1885. Inspired by the work of Eadweard Muybridge in America, Anschütz had set up rows of cameras whose focal-plane shutters were released in sequence by electromagnets, taking twenty-four pictures in about three-quarters of a second. He made a large number of studies of the actions of people, animals and birds, and at the Krupp artillery range at Meppen, near Essen, he recorded shells in flight. His pictures were reproduced, and favourably commented upon, in scientific and photographic journals.
    To bring the pictures to the public, in 1887 he created the Electro-Tachyscope. The sequence negatives were printed as 90 x 120 mm transparencies and fixed around the circumference of a large steel disc. This was rotated in front of a spirally wound Geissler tube, which produced a momentary brilliant flash of light when a high voltage from an induction coil was applied to it, triggered by contacts on the steel disc. The flash duration, about 1/1000 of a second, was so short that it "froze" each picture as it passed the tube. The pictures succeeded each other at intervals of about 1/30 of a second, and the observer saw an apparently continuously lit moving picture. The Electro-Tachyscope was shown publicly in Berlin at the Kulturministerium from 19 to 21 March 1887; subsequently Siemens \& Halske manufactured 100 machines, which were shown throughout Europe and America in the early 1890s. From 1891 his pictures were available for the home in the form of the Tachyscope viewer, which used the principle of the zoetrope: sequence photographs were printed on long strips of thin card, perforated with narrow slots between the pictures. Placed around the circumference of a shallow cylinder and rotated, the pictures could be seen in life-like movement when viewed through the slots.
    In November 1894 Anschütz displayed a projector using two picture discs with twelve images each, which through a form of Maltese cross movement were rotated intermittently and alternately while a rotating shutter allowed each picture to blend with the next so that no flicker occurred. The first public shows, given in Berlin, were on a screen 6×8 m (20×26 ft) in size. From 22 February 1895 they were shown regularly to audiences of 300 in a building on the Leipzigstrasse; they were the first projected motion pictures seen in Germany.
    [br]
    Further Reading
    J.Deslandes, 1966, Histoire comparée du cinéma, Vol. I, Paris. B.Coe, 1992, Muybridge and the Chronophotographers, London.
    BC

    Biographical history of technology > Anschütz, Ottomar

  • 91 Cockerill, William

    SUBJECT AREA: Textiles
    [br]
    b. 1759 Lancashire, England
    d. 1832 near Aix-la-Chapelle, France (now Aachen, Germany)
    [br]
    English (naturalized Belgian c. 1810) engineer, inventor and an important figure in the European textile machinery industry.
    [br]
    William Cockerill began his career in Lancashire by making "roving billies" and flying shuttles. He was reputed to have an extraordinary mechanical genius and it is said that he could make models of almost any machine. He followed in the footsteps of many other enterprising British engineers when in 1794 he went to St Petersburg in Russia, having been recommended as a skilful artisan to the Empress Catherine II. After her death two years later, her successor Paul sent Cockerill to prison because he failed to finish a model within a certain time. Cockerill, however, escaped to Sweden where he was commissioned to construct the locks on a public canal. He attempted to introduce textile machinery of his own invention but was unsuccessful and so in 1799 he removed to Verviers, Belgium, where he established himself as a manufacturer of textile machinery. In 1802 he was joined by James Holden, who before long set up his own machine-building business. In 1807 Cockerill moved to Liège where, with his three sons (William Jnr, Charles James and John), he set up factories for the construction of carding machines, spinning frames and looms for the woollen industry. He secured for Verviers supremacy in the woollen trade and introduced at Liège an industry of which England had so far possessed the monopoly. His products were noted for their fine craftsmanship, and in the heyday of the Napoleonic regime about half of his output was sold in France. In 1813 he imported a model of a Watt steam-engine from England and so added another range of products to his firm. Cockerill became a naturalized Belgian subject c. 1810, and a few years later he retired from the business in favour of his two younger sons, Charles James and John (b. 30 April 1790 Haslingden, Lancashire, England; d. 19 June 1840 Warsaw, Poland), but in 1830 at Andenne he converted a vast factory formerly used for calico printing into a paper mill. Little is known of his eldest son William, but the other two sons expanded the enterprise, setting up a woollen factory at Berlin after 1815 and establishing at Seraing-on-the-Meuse in 1817 blast furnaces, an iron foundry and a machine workshop which became the largest on the European continent. William Cockerill senior died in 1832 at the Château du Behrensberg, the residence of his son Charles James, near Aix-la-Chapelle.
    [br]
    Further Reading
    W.O.Henderson, 1961, The Industrial Revolution on the Continent, Manchester (a good account of the spread of the Industrial Revolution in Germany, France and Russia).
    RTS / RLH

    Biographical history of technology > Cockerill, William

  • 92 Douglas, Donald Wills

    SUBJECT AREA: Aerospace
    [br]
    b. 6 April 1892 Brooklyn, New York, USA
    d. 1 February 1981 Palm Springs, California, USA
    [br]
    American aircraft designer best known for bis outstanding airliner', the DC-3.
    [br]
    In 1912 Donald Douglas went to the Massachusetts Institute of Technology to study aeronautical engineering. After graduating in this relatively new subject he joined the Glenn L.Martin Company as Chief Engineer. In 1920 he founded the Davis-Douglas Company in California to build an aircraft capable of flying across America non-stop: unfortunately, the Cloudster failed to achieve its target. Douglas reorganized the company in 1921 as the Douglas Company (later it became the Douglas Aircraft Company). In 1924 a team of US Army personnel made the first round-the-world flight in specially designed Douglas World Cruisers, a feat which boosted Douglas's reputation considerably. This reputation was further enhanced by his airliner, designed in 1935, that revolutionized air travel: the Douglas Commercial 3, or DC-3, of which some 13,000 were built. A series of piston-engined airliners followed, culminating in the DC-7. Meanwhile, in the military field, Douglas aircraft played a major part in the Second World War. In the jet age Douglas continued to produce a wide range of successful civil and military aircraft, and the company also moved into the rocket and guided missile business. In 1966 Donald W. Douglas was still Chairman of the company, with Donald W.Douglas Jr as President. In 1967 the company merged with the McDonnell Aircraft Company to become the giant McDonnell Douglas Corporation.
    [br]
    Principal Honours and Distinctions
    American Institute of Aeronautics and Astronautics; Daniel Guggenheim Medal 1939.
    Bibliography
    1935, "The development and reliability of the modern multi-engined airliner", Journal of the Royal Aeronautical Society, London (lecture).
    Further Reading
    B.Yenne, 1985, McDonnell Douglas: A Tale of Two Giants, London (pays some attention to both Douglas and McDonnell, but also covers the history of the companies and the aircraft they produced).
    René J.Francillon, 1979, McDonnell Douglas Aircraft since 1920, London; 1988, 2nd edn (a comprehensive history of the company's aircraft).
    JDS

    Biographical history of technology > Douglas, Donald Wills

  • 93 Junkers, Hugo

    SUBJECT AREA: Aerospace
    [br]
    b. 3 February 1859 Rheydt, Germany
    d. 3 February 1935 Munich, Germany
    [br]
    German aircraft designer, pioneer of all-metal aircraft, including the world's first real airliner.
    [br]
    Hugo Junkers trained as an engineer and in 1895 founded the Junkers Company, which manufactured metal products including gas-powered hot-water heaters. He was also Professor of Thermodynamics at the high school in Aachen. The visits to Europe by the Wright brothers in 1908 and 1909 aroused his interest in flight, and in 1910 he was granted a patent for a flying wing, i.e. no fuselage and a thick wing which did not require external bracing wires. Using his sheet-metal experience he built the more conventional Junkers J 1 entirely of iron and steel. It made its first flight in December 1915 but was rather heavy and slow, so Junkers turned to the newly available aluminium alloys and built the J 4 bi-plane, which entered service in 1917. To stiffen the thin aluminium-alloy skins, Junkers used corrugations running fore and aft, a feature of his aircraft for the next twenty years. Incidentally, in 1917 the German authorities persuaded Junkers and Fokker to merge, but the Junkers-Fokker Company was short-lived.
    After the First World War Junkers very rapidly converted to commercial aviation, and in 1919 he produced a single-engined low-wing monoplane capable of carrying four passengers in an enclosed cabin. The robust all-metal F 13 is generally accepted as being the world's first airliner and over three hundred were built and used worldwide: some were still in service eighteen years later. A series of low-wing transport aircraft followed, of which the best known is the Ju 52. The original version had a single engine and first flew in 1930; a three-engined version flew in 1932 and was known as the Ju 52/3m. This was used by many airlines and served with the Luftwaffe throughout the Second World War, with almost five thousand being built.
    Junkers was always ready to try new ideas, such as a flap set aft of the trailing edge of the wing that became known as the "Junkers flap". In 1923 he founded a company to design and manufacture stationary diesel engines and aircraft petrol engines. Work commenced on a diesel aero-engine: this flew in 1929 and a successful range of engines followed later. Probably the most spectacular of Junkers's designs was his G 38 airliner of 1929. This was the world's largest land-plane at the time, with a wing span of 44 m (144 ft). The wing was so thick that some of the thirty-four passengers could sit in the wing and look out through windows in the leading edge. Two were built and were frequently seen on European routes.
    [br]
    Bibliography
    1923, "Metal aircraft construction", Journal of the Royal Aeronautical Society, London.
    Further Reading
    G.Schmitt, 1988, Hugh Junkers and His Aircraft, Berlin.
    1990, Jane's Fighting Aircraft of World War I, London: Jane's (provides details of Junkers's aircraft).
    P. St J.Turner and H.J.Nowarra, 1971, Junkers: An Aircraft Album, London.
    JDS

    Biographical history of technology > Junkers, Hugo

  • 94 Leonardo da Vinci

    [br]
    b. 15 April 1452 Vinci, near Florence, Italy,
    d. 2 May 1519 St Cloux, near Amboise, France.
    [br]
    Italian scientist, engineer, inventor and artist.
    [br]
    Leonardo was the illegitimate son of a Florentine lawyer. His first sixteen years were spent with the lawyer's family in the rural surroundings of Vinci, which aroused in him a lifelong love of nature and an insatiable curiosity in it. He received little formal education but extended his knowledge through private reading. That gave him only a smattering of Latin, a deficiency that was to be a hindrance throughout his active life. At sixteen he was apprenticed in the studio of Andrea del Verrochio in Florence, where he received a training not only in art but in a wide variety of crafts and technical arts.
    In 1482 Leonardo went to Milan, where he sought and obtained employment with Ludovico Sforza, later Duke of Milan, partly to sculpt a massive equestrian statue of Ludovico but the work never progressed beyond the full-scale model stage. He did, however, complete the painting which became known as the Virgin of the Rocks and in 1497 his greatest artistic achievement, The Last Supper, commissioned jointly by Ludovico and the friars of Santa Maria della Grazie and painted on the wall of the monastery's refectory. Leonardo was responsible for the court pageants and also devised a system of irrigation to supply water to the plains of Lombardy. In 1499 the French army entered Milan and deposed Leonardo's employer. Leonardo departed and, after a brief visit to Mantua, returned to Florence, where for a time he was employed as architect and engineer to Cesare Borgia, Duke of Romagna. Around 1504 he completed another celebrated work, the Mona Lisa.
    In 1506 Leonardo began his second sojourn in Milan, this time in the service of King Louis XII of France, who appointed him "painter and engineer". In 1513 Leonardo left for Rome in the company of his pupil Francesco Melzi, but his time there was unproductive and he found himself out of touch with the younger artists active there, Michelangelo above all. In 1516 he accepted with relief an invitation from King François I of France to reside at the small château of St Cloux in the royal domain of Amboise. With the pension granted by François, Leonardo lived out his remaining years in tranquility at St Cloux.
    Leonardo's career can hardly be regarded as a success or worthy of such a towering genius. For centuries he was known only for the handful of artistic works that he managed to complete and have survived more or less intact. His main activity remained hidden until the nineteenth and twentieth centuries, during which the contents of his notebooks were gradually revealed. It became evident that Leonardo was one of the greatest scientific investigators and inventors in the history of civilization. Throughout his working life he extended a searching curiosity over an extraordinarily wide range of subjects. The notes show careful investigation of questions of mechanical and civil engineering, such as power transmission by means of pulleys and also a form of chain belting. The notebooks record many devices, such as machines for grinding and polishing lenses, a lathe operated by treadle-crank, a rolling mill with conical rollers and a spinning machine with pinion and yard divider. Leonardo made an exhaustive study of the flight of birds, with a view to designing a flying machine, which obsessed him for many years.
    Leonardo recorded his observations and conclusions, together with many ingenious inventions, on thousands of pages of manuscript notes, sketches and drawings. There are occasional indications that he had in mind the publication of portions of the notes in a coherent form, but he never diverted his energy into putting them in order; instead, he went on making notes. As a result, Leonardo's impact on the development of science and technology was virtually nil. Even if his notebooks had been copied and circulated, there were daunting impediments to their understanding. Leonardo was left-handed and wrote in mirror-writing: that is, in reverse from right to left. He also used his own abbreviations and no punctuation.
    At his death Leonardo bequeathed his entire output of notes to his friend and companion Francesco Melzi, who kept them safe until his own death in 1570. Melzi left the collection in turn to his son Orazio, whose lack of interest in the arts and sciences resulted in a sad period of dispersal which endangered their survival, but in 1636 the bulk of them, in thirteen volumes, were assembled and donated to the Ambrosian Library in Milan. These include a large volume of notes and drawings compiled from the various portions of the notebooks and is now known as the Codex Atlanticus. There they stayed, forgotten and ignored, until 1796, when Napoleon's marauding army overran Italy and art and literary works, including the thirteen volumes of Leonardo's notebooks, were pillaged and taken to Paris. After the war in 1815, the French government agreed to return them but only the Codex Atlanticus found its way back to Milan; the rest remained in Paris. The appendix to one notebook, dealing with the flight of birds, was later regarded as of sufficient importance to stand on its own. Four small collections reached Britain at various times during the seventeenth and eighteenth centuries; of these, the volume in the Royal Collection at Windsor Castle is notable for its magnificent series of anatomical drawings. Other collections include the Codex Leicester and Codex Arundel in the British Museum in London, and the Madrid Codices in Spain.
    Towards the end of the nineteenth century, Leonardo's true stature as scientist, engineer and inventor began to emerge, particularly with the publication of transcriptions and translations of his notebooks. The volumes in Paris appeared in 1881–97 and the Codex Atlanticus was published in Milan between 1894 and 1904.
    [br]
    Principal Honours and Distinctions
    "Premier peintre, architecte et mécanicien du Roi" to King François I of France, 1516.
    Further Reading
    E.MacCurdy, 1939, The Notebooks of Leonardo da Vinci, 2 vols, London; 2nd edn, 1956, London (the most extensive selection of the notes, with an English translation).
    G.Vasari (trans. G.Bull), 1965, Lives of the Artists, London: Penguin, pp. 255–271.
    C.Gibbs-Smith, 1978, The Inventions of Leonardo da Vinci, Oxford: Phaidon. L.H.Heydenreich, Dibner and L. Reti, 1981, Leonardo the Inventor, London: Hutchinson.
    I.B.Hart, 1961, The World of Leonardo da Vinci, London: Macdonald.
    LRD / IMcN

    Biographical history of technology > Leonardo da Vinci

  • 95 McKay, Hugh Victor

    [br]
    b. c. 1866 Drummartin, Victoria, Australia
    d. 21 May 1926 Australia
    [br]
    Australian inventor and manufacturer of harvesting and other agricultural equipment.
    [br]
    A farmer's son, at the age of 17 McKay developed modifications to the existing stripper harvester and created a machine that would not only strip the seed from standing corn, but was able to produce a threshed, winnowed and clean sample in one operation. The prototype was produced in 1884 and worked well on the two acres of wheat that had been set aside on the family farm. By arrangement with a Melbourne plough maker, five machines were made and sold for the 1885 season. In 1886 the McKay Harvester Company was formed, with offices at Ballarat, from which the machines, built by various companies, were sold. The business expanded quickly, selling sixty machines in 1888, and eventually rising to the production of nearly 2,000 harvesters in 1905. The name "Sunshine" was given to the harvester, and the "Sun" prefix was to appear on all other implements produced by the company as it diversified its production interests. In 1902 severe drought reduced machinery sales and left 2,000 harvesters unsold. McKay was forced to look to export markets to dispose of his surplus machines. By 1914 a total of 10,000 machines were being exported annually. During the First World War McKay was appointed to the Business Board of the Defence Department. Increases in the scale of production resulted in the company moving to Melbourne, where it was close to the port of entry of raw materials and was able to export the finished article more readily. In 1909 McKay produced one of the first gas-engined harvesters, but its cost prevented it from being more than an experimental prototype. By this time McKay was the largest agricultural machinery manufacturer in the Southern hemisphere, producing a wide range of implements, including binders. In 1916 McKay hired Headlie Taylor, who had developed a machine capable of harvesting fallen crops. The jointly developed machine was a major success, coming as it did in what would otherwise have been a disastrous Australian harvest. Further developments included the "Sun Auto-header" in 1923, the first of the harvesting machines to adopt the "T" configuration to be seen on modern harvesters. The Australian market was expanding fast and a keen rivalry developed between McKay and Massey Harris. Confronted by the tariff regulations with which the Australian Government had protected its indigenous machinery industry since 1906, Massey Harris sold all its Australian assets to the H.V. McKay company in 1930. Twenty-three years later Massey Ferguson acquired the old Sunshine works and was still operating from there in the 1990s.
    Despite a long-running history of wage disputes with his workforce, McKay established a retiring fund as well as a self-help fund for distressed cases. Before his death he created a charitable trust and requested that some funds should be made available for the "aerial experiments" which were to lead to the establishment of the Flying Doctor Service.
    [br]
    Principal Honours and Distinctions
    CBE.
    Further Reading
    Graeme Quick and Wesley Buchele, 1978, The Grain Harvesters, American Society of Agricultural Engineers (devotes a chapter to the unique development of harvesting machinery which took place in Australia).
    AP

    Biographical history of technology > McKay, Hugh Victor

  • 96 Muybridge, Eadweard

    [br]
    b. 9 April 1830 Kingston upon Thames, England
    d. 8 May 1904 Kingston upon Thames, England
    [br]
    English photographer and pioneer of sequence photography of movement.
    [br]
    He was born Edward Muggeridge, but later changed his name, taking the Saxon spelling of his first name and altering his surname, first to Muygridge and then to Muybridge. He emigrated to America in 1851, working in New York in bookbinding and selling as a commission agent for the London Printing and Publishing Company. Through contact with a New York daguerreotypist, Silas T.Selleck, he acquired an interest in photography that developed after his move to California in 1855. On a visit to England in 1860 he learned the wet-collodion process from a friend, Arthur Brown, and acquired the best photographic equipment available in London before returning to America. In 1867, under his trade pseudonym "Helios", he set out to record the scenery of the Far West with his mobile dark-room, christened "The Flying Studio".
    His reputation as a photographer of the first rank spread, and he was commissioned to record the survey visit of Major-General Henry W.Halleck to Alaska and also to record the territory through which the Central Pacific Railroad was being constructed. Perhaps because of this latter project, he was approached by the President of the Central Pacific, Leland Stanford, to attempt to photograph a horse trotting at speed. There was a long-standing controversy among racing men as to whether a trotting horse had all four hooves off the ground at any point; Stanford felt that it did, and hoped than an "instantaneous" photograph would settle the matter once and for all. In May 1872 Muybridge photographed the horse "Occident", but without any great success because the current wet-collodion process normally required many seconds, even in a good light, for a good result. In April 1873 he managed to produce some better negatives, in which a recognizable silhouette of the horse showed all four feet above the ground at the same time.
    Soon after, Muybridge left his young wife, Flora, in San Francisco to go with the army sent to put down the revolt of the Modoc Indians. While he was busy photographing the scenery and the combatants, his wife had an affair with a Major Harry Larkyns. On his return, finding his wife pregnant, he had several confrontations with Larkyns, which culminated in his shooting him dead. At his trial for murder, in February 1875, Muybridge was acquitted by the jury on the grounds of justifiable homicide; he left soon after on a long trip to South America.
    He again took up his photographic work when he returned to North America and Stanford asked him to take up the action-photography project once more. Using a new shutter design he had developed while on his trip south, and which would operate in as little as 1/1,000 of a second, he obtained more detailed pictures of "Occident" in July 1877. He then devised a new scheme, which Stanford sponsored at his farm at Palo Alto. A 50 ft (15 m) long shed was constructed, containing twelve cameras side by side, and a white background marked off with vertical, numbered lines was set up. Each camera was fitted with Muybridge's highspeed shutter, which was released by an electromagnetic catch. Thin threads stretched across the track were broken by the horse as it moved along, closing spring electrical contacts which released each shutter in turn. Thus, in about half a second, twelve photographs were obtained that showed all the phases of the movement.
    Although the pictures were still little more than silhouettes, they were very sharp, and sequences published in scientific and photographic journals throughout the world excited considerable attention. By replacing the threads with an electrical commutator device, which allowed the release of the shutters at precise intervals, Muybridge was able to take series of actions by other animals and humans. From 1880 he lectured in America and Europe, projecting his results in motion on the screen with his Zoopraxiscope projector. In August 1883 he received a grant of $40,000 from the University of Pennsylvania to carry on his work there. Using the vastly improved gelatine dry-plate process and new, improved multiple-camera apparatus, during 1884 and 1885 he produced over 100,000 photographs, of which 20,000 were reproduced in Animal Locomotion in 1887. The subjects were animals of all kinds, and human figures, mostly nude, in a wide range of activities. The quality of the photographs was extremely good, and the publication attracted considerable attention and praise.
    Muybridge returned to England in 1894; his last publications were Animals in Motion (1899) and The Human Figure in Motion (1901). His influence on the world of art was enormous, over-turning the conventional representations of action hitherto used by artists. His work in pioneering the use of sequence photography led to the science of chronophotography developed by Marey and others, and stimulated many inventors, notably Thomas Edison to work which led to the introduction of cinematography in the 1890s.
    [br]
    Bibliography
    1887, Animal Locomotion, Philadelphia.
    1893, Descriptive Zoopraxography, Pennsylvania. 1899, Animals in Motion, London.
    Further Reading
    1973, Eadweard Muybridge: The Stanford Years, Stanford.
    G.Hendricks, 1975, Muybridge: The Father of the Motion Picture, New York. R.Haas, 1976, Muybridge: Man in Motion, California.
    BC

    Biographical history of technology > Muybridge, Eadweard

  • 97 сверхзвуковой

    Русско-английский словарь по информационным технологиям > сверхзвуковой

  • 98 большой

    амортизатор с большим ходом штока
    long-stroke shock strut
    аэродинамическая труба больших скоростей
    high-speed wind tunnel
    большой шаг
    1. coarse pitch
    2. high pitch вертолет большой грузоподъемности с внешней подвеской
    flying crane helicopter
    воздушное судно большой вместимости
    high-capacity aircraft
    воздушное судно большой дальности полетов
    long-distance aircraft
    воздушное судно для полетов на большой высоте
    high-altitude aircraft
    воздушные перевозки большой протяженности
    long-haul service
    воздушные перевозки с большим количеством промежуточных остановок
    multistop service
    воздушный винт с большим шагом
    high-pitch propeller
    в режиме большого шага
    in coarse pitch
    датчик предупреждения больших углов атаки
    stall warning device
    двигатель с большим ресурсом
    longer-lived engine
    диапазон больших скоростей
    high-speed range
    канал большого шага
    coarse-pitch passage
    маршрут большой протяженности
    long-stage route
    радиолокатор с большой разрешающей способностью
    fine grain radar
    топливный коллектор большого газа
    high-speed fuel manifold
    упор большого шага
    1. high-pitch stop
    (лопасти воздушного винта) 2. coarse pitch stop (лопасти воздушного винта)

    Русско-английский авиационный словарь > большой

  • 99 визуальный

    аэродромные визуальные средства
    aerodrome visual aids
    визуальная навигация
    visual navigation
    визуальная ориентировка
    1. visual orientation
    2. visual reference визуальная оценка расстояния в полете
    distance assessment
    визуальная посадка
    visual landing
    визуальная посадка по наземным ориентирам
    visually judged landing
    визуальная сигнализация
    visual warning
    визуальное наблюдение
    direct observation
    визуальное опознавание
    visual identification
    визуальное определение местоположения
    visual fixing
    визуальное управление
    visual guidance
    визуальное управление стыковкой
    visual docking guidance
    визуальные метеорологические условия
    visual meteorological conditions
    визуальные наблюдения
    visual observations
    визуальные навигационные средства
    navigation visual aids
    визуальные средства
    visual means
    визуальные средства захода на посадку
    visual aids to approach
    визуальный заход на посадку
    1. contact approach
    2. visual approach визуальный заход на посадку по упрощенной схеме
    abbreviated visual approach
    визуальный контакт в полете
    flight visual contact
    визуальный контроль
    visual monitoring
    визуальный контрольный ориентир
    visual reference point
    визуальный маяк
    visual beacon
    визуальный ориентир в полете
    flight visual cue
    визуальный осмотр
    visual inspection
    визуальный пеленг
    visual bearing
    визуальный полет
    1. contact flight
    2. visual flight визуальный полет по кругу
    visual circling
    визуальный прибор
    paravisual director
    визуальный сигнал
    visual signal
    визуальный указатель
    1. visual guide
    2. visual indicator визуальный указатель выпуска шасси
    visual downlock indicator
    визуальный указатель глиссады
    visual approach indicator
    воздушное пространство с запретом визуальных полетов
    visual exempted airspace
    высота перехода к визуальному полету
    break-off height
    дальность визуального обнаружения
    visual detection range
    зона ожидания для визуальных полетов
    visual holding point
    квалификационная отметка о допуске к визуальным полетам
    visual flying rating
    код визуального сигнала земля - воздух
    ground-air visual signal code
    навигация по визуальным ориентирам
    contact navigation
    наземные визуальные средства
    visual ground aids
    наземный визуальный сигнал
    visual ground signal
    ориентир для визуальной ориентировки
    visual pinpoint
    ошибка при визуальном определении местоположения
    observation error
    полет с визуальной ориентировкой
    visual contact flight
    посадка с визуальной ориентировкой
    contact landing
    правила визуального полета
    1. contact flight rules
    2. visual flight rules система визуального управления стыковкой с телескопическим трапом
    visual docking guidance system
    система визуальной индикации глиссады
    visual approach slope indicator system
    система контроля за работой визуальных средств
    system of monitoring visual aids
    (на аэродроме) средство визуального аварийного оповещения
    visual warning device
    схема визуального захода на посадку
    visual approach streamline
    схема визуального полета по кругу
    visual circling procedure
    упрощенная система визуальной индикации
    abbreviated visual indicator system
    (глиссады)

    Русско-английский авиационный словарь > визуальный

  • 100 горизонтальный

    горизонтальный прил
    lateral
    балансировка в горизонтальном полете
    horizontal trim
    время горизонтального полета
    level flight time
    выдерживать горизонтальное положение
    keep level
    выполнение горизонтального полета
    level flying
    горизонтальная составляющая
    horizontal component
    горизонтальная составляющая сдвига ветра
    horizontal wind shear
    горизонтальное оперение
    tail plane
    горизонтальное положение
    level attitude
    горизонтальное хвостовое оперение
    1. stabilizing fin
    2. horizontal tail горизонтальное эшелонирование
    horisontal separation
    горизонтальный полет
    1. level flight
    2. horizontal flight 3. level горизонтальный полет на крейсерском режиме
    level cruise
    горизонтальный разворот
    level turn
    горизонтальный шарнир
    flapping hinge
    дальность горизонтального полета
    horizontal range
    двигатель горизонтальной коррекции
    leveling torque motor
    измерение при горизонтальном пролете
    single level overflight measurement
    механизм горизонтальной коррекции
    gyro leveling mechanism
    несущее горизонтальное оперение
    lifting tailplane
    оставаться в горизонтальном положении
    remain level
    отклонение от линии горизонтального полета
    deviation from the level flight
    переводить воздушное судно в горизонтальный полет
    put the aircraft over
    переход в режим горизонтального полета
    puchover
    скорость горизонтального полета
    level-flight speed
    траектория горизонтального полета
    1. horizontal flight path
    2. level flight path

    Русско-английский авиационный словарь > горизонтальный

См. также в других словарях:

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