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61 missile
ракета; реактивный снаряд, см. тж. rocketatomic(-armed, -capable, -equipped, -tipped) missile — ракета с ядерной боевой частью
delayed impact space missile — орбитальная [космическая] ракета с запрограммированным по времени отделением головной или боевой части
ECM carrying missile — ракета радиопротиводействия, ракета — постановщик помех; противорадиолокационная ракета
infrared(-guided, -homing) missile — ракета с тепловой головкой самонаведения
land-based(-borne, -launched) missile — ракета, запускаемая с земли, ракета наземного базирования
liquid(-fuel, -fueled, -propellant) missile — ракета с ЖРД, жидкостная ракета
lock a missile on the target — наводить ракету на цель; захватывать цель головкой самонаведения ракеты
nuclear(-armed, -capability) missile — ракета с ядерной боевой частью
place missile on target — накрывать [поражать] цель ракетой
production(-line, -type) missile — серийная ракета, ракета серийного образца
rocket(-powered, -propelled) missile — ракета
solid(-fueled, -propellant) missile — твердотопливная ракета, ракета с РДТТ
trigger off a missile — производить пуск ракеты; подрывать ракету или боевую часть ракеты
warm up the missile — подготавливать ракету к пуску; прогревать аппаратуру ракеты
— - ship missile -
62 Wallis, Sir Barnes Neville
[br]b. 26 September 1887 Ripley, Derbyshire, Englandd. 30 October 1979 Leatherhead, Surrey, England[br]English aeronautical designer and inventor.[br]Wallis was apprenticed first at Thames Engineering Works, and then, in 1908, at John Samuel White's shipyard at Cowes. In 1913, the Government, spurred on by the accelerating development of the German Zeppelins (see Zeppelin, Ferdinand von), ordered an airship from Vickers; Wallis was invited to join the design team. Thus began his long association with aeronautical design and with Vickers. This airship, and the R80 that followed it, were successfully completed, but the military lost interest in them.In 1924 the Government initiated a programme for the construction of two airships to settle once and for all their viability for long-dis-tance air travel. The R101 was designed by a Government-sponsored team, but the R100 was designed by Wallis working for a subsidiary of Vickers. The R100 took off on 29 July 1930 for a successful round trip to Canada, but the R101 crashed on its first flight on 4 October, killing many of its distinguished passengers. The shock of this disaster brought airship development in Britain to an abrupt end and forced Wallis to direct his attention to aircraft.In aircraft design, Wallis is known for his use of geodesic construction, which combined lightness with strength. It was applied first to the single-engined "Wellesley" and then the twin-en-gined "Wellington" bomber, which first flew in 1936. With successive modifications, it became the workhorse of RAF Bomber Command during the Second World War until the autumn of 1943, when it was replaced by four-engined machines. In other areas, it remained in service until the end of the war and, in all, no fewer than 11,461 were built.Wallis is best known for his work on bomb design, first the bouncing bomb that was used to breach the Möhne and Eder dams in the Ruhr district of Germany in 1943, an exploit immortalized in the film Dambusters. Encouraged by this success, the authorities then allowed Wallis to realize an idea he had long urged, that of heavy, penetration bombs. In the closing stages of the war, Tallboy, of 12,000 lb (5,400 kg), and the 10-ton Grand Slam were used to devastating effect.After the Second World War, Wallis returned to aeronautical design and was given his own department at Vickers to promote his ideas, principally on variable-geometry or swing-wing aircraft. Over the next thirteen years he battled towards the prototype stage of this revolutionary concept. That never came, however; changing conditions and requirements and increasing costs led to the abandonment of the project. Bit-terly disappointed, Wallis continued his researches into high-speed aircraft until his retirement from Vickers (by then the British Aircraft Corporation), in 1971.[br]Principal Honours and DistinctionsKnighted 1968. FRS 1945.Further ReadingJ.Morpurgo, 1972, Barnes Wallis: A Biography, London: Longman (a readable account, rather biased in Wallis's favour).C.J.Heap, 1987, The Papers of Sir Barnes Wallis (1887–1979) in the Science Museum Library, London: Science Museum; with a biographical introd. by L.R.Day.LRDBiographical history of technology > Wallis, Sir Barnes Neville
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63 двигатель
- (газотурбинный, поршневой, тепловой) — engine
- (гидравлический, пневматический, электрический) — motor
-, авиационный — aircraft engine
двигатель, используемый или предназначенный к использованию в авиации для перемещения и (или) поддержания ла, на котором он установлен, в воздухе (рис. 46). — an engine that is used or intended to be used in propelting or lifting aircraft.
- аналогичной конструкции — engine of identical design and сonstruction
- без наддува (ид) — unsupercharged engine
-, безредукторный — direct-drive engine
-, безредукторный винто-вентиляторный (незакопоченный) — unducted fan engine (udf)
винтовентиляторы вращаются непосредственно силовой (свободной) турбиной с противоположным вращением рабочих колес. — fans are driven directly by a counter-rotating turbine, eliminating complexity of a reduction gearbox.
-, бензиновый — gasoline engine
-, боковой (рис. 13) — side engine
- в подвесной мотогондоле — pod engine
-, вентиляторный, с противоположным вращением вентиляторов — contrafan engine
- вертикальной наводки, приводной (стрелкового вооружения) — (gun) elevation drive motor
-, винто-вентиляторный (тввд) — prop-fan engine
-, включенный (работающий) — operating/running/engine
-, внешний (по отношению к фюзеляжу) (рис. 44) — outboard engine
- внутреннего сгорания — internal-combustion engine
-, внутренний (по отношению к наружному двигателю) (рис. 44) — inboard engine
- воздушного охлаждения (пд) — air-cooled engine
двигатель, у которого отвод тепла от цилиндров производится воздухом, непосредственно обдувающим их. — an engine whose running temperature is controlled by means of air cooled cylinders.
-, вспомогательный (всу) — auxiliary power unit (apu)
-, выключенный — shutdown engine
-, выключенный (неработающий) — inoperative engine
-, высокооборотный — high-speed engine
-, высотный — high-altitude engine
-, газотурбинный (гтд) — turbine engine
-, газотурбинный (вертолетныи) — helicopter turboshaft engine
-,газотурбинный-энергоузел (стартер-энергоузел) — turbine-starter - auxiliary power unit, starter - apu
- (-) генератор — motor-generator
устройство для преобразования одного вида эл. энергии в другую (напр., переменный ток в постоянный). — а motor-generator combination for converting one kind of electric power to another (e.g. ас to dc)
- горизонтальной наводки, приводной (стрелкового вооружения) — (gun) azimuth drive motor
- двухвальной схемы (турбовальный) — two-shaft turbine engine
-, двухвальный турбовинтовой — two-shaft turboprop engine
-, двухвальный турбореактивный — two-shaft /-rotor, -spool/turbojet engine
-, двухкаскадный — two-rotor /-shaft, -spool/ engine, twin-spool engine
двухвальный турбореактивный двигатель называется также двухроторным или двухкаскадным двигателем. — а two-rotor engine is a twoshaft or two-spool engine with lp and hp compressors and hp and lp turbines.
-, двухкаскадный, двухконтурный, (турбореактивный) — two-rotor /twin-spool/ by-pass turbo-jet engine
-, двухкаскадный, турбовальный, газотурбинный, со свободной турбиной — two-rotor /twin-spool/ turboshaft engine with free-power turbine
-, двухкаскадный, турбовентиляторвый с устройством отклонения направления тяги — two-rotor /twin-spool/ turbofan engine with thrust deflector system
-, двухконтурный — by-pass /bypass/ engine
гтд, в котором, помимо основного внутреннего (первого) контура, имеется наружный (второй) контур, представляющий собой канал кольцевого сечения, оканчивающийся у реактивного сопла. — in а by-pass engine, a part of the air leaving the lp cornpressor is dueted through the by-pass duct around the engine main duct to the exhaust unit to be exhausted to the atmosphere.
-, двухконтурный с дожиганиem во втором контуре — duct-burning by-pass engine
-, двухконтурный со смешиванием потоков наружного и и внутренного контуров — by-pass exhaust mixing engine
-, двухроторный — two-rotor engine
- двухрядная звезда (пд) — double-row radial engine
двигатель, у которого цнлиндры расположены двумя рядами радиально относительнo одного oбщего коленчатоro вала. — an engine having two rows of cylinders arranged radially around а common crankshaft. the corresponding front and rear cylinders may or may not be in line.
-, двухтактный (пд) — two-cycle engine
-, дозвуковой — subsonic engine
-, доработанный по модификации (1705) — engine incorporating mod. (1705), post-mod. (1705) engine
-, звездообразный — radial engine
поршневой двигатель с радиальным расположением цилиндров, оси которых лежат в одной, двух или нескольких плоскостях, перпендикулярных к оси коленчатого вала — an engine having stationary cylinders arranged radially around а commom crankshaft.
-, звездообразный двухрядный — double-row radial engine
-, звездообразный однорядный — single-row radial engine
-, исполнительный (эл.) — (electric) actuator, servo motor
-, исполнительный, канала курса (крена или тангажа) (гироплатформы) — azimuth (roll or pitch) servornotor
-, карбюраторный (пд) — carburetor engine
-, коррекционный (гироскопического прибора) — erection torque motor
-, критический — critical engine
двигатель, отказ которого вызывает наиболее неблагоприятные изменения в поведении самолета, управляемости и избытке тяги. — "critical engineп means the engine whose failure would most adversely affect the performance or handling qualities of an aircraft.
-, крыльевой (установленный на крыле) — wing engine
- левого вращения — engine of lh rotation
-, маломощный — low-powered engine
-, многорядный (пд) — multirow engine
-, многорядный звездообразный — multirow radial engine
-, модифицированный — modified engine
- модульной конструкции — module-construction engine
lp compressor - module i, hp compressor - module 2, etc.
-, мощный — high-powered engine
-, недоработанный no модификацин (1705) — engine not incorporating mod. (1705), pre-mod. (1705) engine
-, незакапоченный — uncowled engine
- непосредственного впрыска (пд) — fuel injection engine
-, неработающий — inoperative engine
-, одновальный (гтд) — single-shaft /single-rotor/ turbine engine
-, одновальный двухконтурный — single-shaft /single-rotor/ bypass engine
-, одновальный турбовентиляторный — single-shaft /single-rotor/ turbofan engine
-, одновальный турбовинтовой — single-shaft turboprop engine
-, одновальный турбореактивный — single-shaft /single-rotor/turbojet engine
-, однорядный (пд) — single-row engine
-, опытный — prototype engine
двигатель определенного тиna, еще не прошедший типовые государственные испытания. — the tirst engine of a type and arrangement not approved previously, to be submitted for type approval test.
-, основной — main engine
-, оставшийся (продолжающий работать) — remaining engine
-, отказавший — inoperative/failed/ engine
- отработки (эл., исполнительный) — servomotor
- отработки следящей системы — servo loop drive motor
- подтяга (патронной ленты) — ammunition booster torque motor
-, поперечный коррекционный (авиагоризонта) — roll erection torque motor
-, поршневой (пд) — reciprocating engine
- правого вращения — engine of rh rotation
-, продольный коррекционный (авиагоризонта) — pitch erection torque motor
-, прямоточный — ramjet engine
двигатель без механического компрессора, в котором сжатие воздуха обеспечивается поступательным движением самого двигателя. — а jet engine with no meehanical compressor, and using the air for combustion compressed by forward motion of the engine.
- работающий — operating engine
-, работающий с перебоями — rough engine
двигатель, работающий с неисправной системой зажигания или подачи топлива (рабочей смеси) — an engine that is running or firing unevenly, usually due to а faulty condition in either the fuel or ignition systems.
- рамы крена (гироплатформы — roll-gimbal servomotor
- рамы курса (гироплатформы — azimuth-gimbal servomotor
- рамы тангажа (гироплатформы) — pitch-gimbal servomotor
-, реактивный — jet-engine
двигатель, в котором энергия топлива преобразуется в кинетическую энергию газовой струи, вытекающей из двигателя, a получающаяся за счет этого сила реакции нenоcредственно используется как сила тяги для перемещения летательного аппарата. — an aircraft engine that derives all or most of its thrust by reaction to its ejection of combustion products (or heated air) in a jet and that obtains oxygen from the atmosphere for the combustion of its fuel.
-, реактивный, пульсирующий — pulse jet (engine)
применяется для непосредственного вращения несущеro винта вертолета. — pulse jets are designed for helicopter rotor propulsion.
-, ремонтный — overhauled engine
серийный двигатель, отремонтированный или восстановленный до состояния, удовлетворяющего требованиям серийного стандарта, и пригодный для дальнейшей эксплуатации в течение установленного межремонтного ресурса. — an engine which has been repaired or reconditioned to а standard rendering it eligible for the complete overhaul life agreed by the national authority.
- с внешним смесеобразованием (пд) — carburetor engine
двигатель внутреннего сгорания, у которого горючая смесь образуется вне рабочего цилиндра. — an engine in which the fuel/air mixture is formed in the carburetor.
- с внутренним смесеобразованием — fuel-injection engine
двигатель, у которого горючая смесь образуется внутри рабочего цилиндра. — an engine in which fuel is directly injected into the cylinders.
- с водяным охлаждением (пд) — water-cooled engine
- с высокой степенью сжатия — high-compression engine
- с нагнетателем (пд) — supercharged engine
- с наддувом (пд) с осевым компрессором (пд) — supercharged engine axial-flom turbine engine
- с передним расположением вентилятора — front fan turbine engine
- с противоточной камерой сгорания (гтд) — reverse-flow turbine engine
- с редуктором — engine with reduction gear
- с форсажной камерой (гтд). двигатель с дополнительным сжиганием топлива в специальной камере за турбиной — engine with afterburner, afterburning engine, reheat(ed) engine, engine with thrust augmentor
- с форсированной (взлетной) мощностью — engine with augmented (takeoff) power rating
- с центробежным компрессором (гтд) — radial-flow turbine engine
-, серийный — series engine
двигатель, изготовляемый в серийном производстве и соответствующий опытному двигателю, принятому при государственных испытаниях для серийного производства. — an engine essentially identiin design, in materials, and in methods of construction, with one which has been approved previously.
- со свободной турбиной — free-luroine engine
двигатель с двумя турбинами, валы которых кинематически не связаны. одна из турбин обычно служит для привода компрессора, а другая используется для передачи полезной работы потребителю, например, воздушному (или несущему) винту. — the engine with two turbines whose shafts are not mechanically coupled. one turbine drives the compressor, and the other free turbine drives the propeller or rotor.
- следящей системы по внутреннему крену (гироплатформы) — inner roll gimbal servomotor
- следящей системы по наружному крену (гироплатформы) — outer roll gimbal servomotor
- следящей системы по курсу (гироплатформы) — azimuth gimbal servomotor
- следящей системы по тангажу (гироплатформы) — pitch gimbal servomotor
-, собственно — engine itself
-, средний (рис. 44) — center engine
- стабилизации гироплатформы — stable platform-stabilization servomotor/servo/
-, стартовый (работающий при взлете) — booster
-, стартовый твердотопливный — solid propellant booster
-, трехкаскадный, турбореактивный, с передним вентилятором — three-rotor /triple-spool, triple shaft/ front fan turbo-jet engine
-, турбовентиляторный — turbofan engine
двухконтурный турбореактивный двигатель, в котором часть воздуха выбрасывается за первыми ступенями компрессора низкого давления, а остальная часть воздуха за кнд поступает в основной контур с камерами сгорания. — in the turbofan engine a part of the air bypassed and exhausted to atmosphere after the first (two) stages of lp compressor. about half of the thrust is produced by the fan exhaust.
-, турбовентиляторный (с дожиганием в вентиляторном контуре) — duct-burning turbofan engine
-, турбовинтовентиляторный — (turbo) propfan engine, unducted fan engine (ufe)
-, турбовинтовой (твд) — turboprop engine
газотурбинный двигатель, в котором тепло превращается в кинетическую энергию реактивной струи и в механическую работу на валу двигателя, которая используется для вращения воздушного винта. — а turboprop engine is a turbine engine driving the propeller and developing an additional propulsive thrust by reaction to ejection of combustion products.
-, "турбовинтовой" (вертолетный, с отбором мощности на вал) — turboshaft engine
-, турбовинтовой, с толкающим винтом — pusher-turboprop engine
-, турбопрямоточный — turbo/ram jet engine
комбинация из турбореактивного (до м-з) и прямоточного (для больших чисел м). — combines а turbo-jet engine (for speeds up to mach 3) and ram jet engine for higher mach numbers.
-,турбо-ракетный — turbo-rocket engine
аналог турбопрямоточному двигателю с автономным кислородным питанием, — а turbo/ram jet engine with its own oxygen to provide combustion.
-, турбореактивный — turbojet engine
газотурбинный двигатель (с приводом компрессора от турбин), в котором тепло превращается только в кинетическую энергию реактивной струи. — a jet engine incorporating a turbine-driven air compressor to take in and compress the air for the combustion of fuel, the gases of combustion being used both to rotate the turbine and to create a thrust-producing jet.
-, установленный в мотогондоле — nacelle-mounted engine
-, установленный в подвесной мотогондоле — pod engine
-, четырехтактный (поршневой — four-cycle engine
за два оборота коленчатого вала происходит четыре хода поршня в каждом цилиндре, по одному такту на ход. такт 1 - впуск всасывание рабочей смеси в цилиндр), такт 2 - матке рабочей смеси, такт 3 - рабочий ход (зажигание смеси), такт 4 - выхлоп (выпуск отработанных газов из цилиндра в атмосферу) — a common type of engine which requires two revolutions of the crankshaft (four strokes of the piston) to complete the four events of (1) admission of or forcing the charged mixture of combustible gas into the cylinder, (2) compression of the charge, (3) ignition and burning of the charge, which develops pressure (power) acting on the piston and (4) exhaust or expulsion of the charge from the cylinder.
-, шаговой (эл.) — step-servo motor
-, электрический — electric motor
устройство, преобразующее электрическую энергию во вращательное механическое движение. — device which converts electrical energy into rotating mechanical energy.
- (-) энергоузел, газотурбинный (ггдэ) — turbine starter /auxiliary power unit, starter/ apu
для запуска основн. двигателей, хол. прокрутки (стартерный режим) и привода агрегатов самолета при неработающих двигателях (режим энергоузла), имеет свой электростартер.
в зоне д. — in the region of the engine
выбег д. — engine run-down
гонка д. — engine run
данные д. — engine data
заливка д. (пд перед запуском) — engine priming
замена д. — engine replacement /change/
запуск д. — engine start
испытание д. — engine test
мощность д. — engine power
на входе в д. — at /in/ inlet to the engine
обороты д. — engine speed /rpm, rpm/
опробование д. — engine ground test
опробование д. в полете — in-flight engine test
опробование д. на земле — engine ground test
останов д. (выключение) — engine shutdown
остановка д. (отказ) — engine failure
остановка д. (выбег) — run down
остановка д. вслествие недостатка масла (топлива) — engine failure due to oil (fuel) starvation
отказ д. — engine failure
перебои в работе д. — rough engine operation
подогрев д. — engine heating
проба д. (на земле) — engine ground test
прогрев д. — engine warm-up
прокрутка д. (холодная) — engine cranking /motoring/
работа д. — engine operation
разгон д. — engine acceleration
стоянка д. (период, в течение которого двигатель не работает) — engine shutdown. one hundred starts must be made of which 25 starts must be preceded by at least a two-hour engine shutdown.
тряска д. — engine vibration
тяга д. — engine thrust
установка д. — engine installation
шум д. — engine noise
вывешивать д. с помощью лебедки — support weight of the engine by a hoist
выводить д. на требуемые обороты % — accelerate the engine to a required speed of %
выключать д. — shut down the engine
глушить д. — shut down the engine
гонять д. — run the engine
заливать д. (пд) — prim the engine
заменять д. — replace the engine
запускать д. — start the engine
запускать д. в воздухе — (re)start the engine
испытывать д. — test the engine
опробовать д. на земле — ground test the engine
останавливать д. — shut down the engine
подвешивать д. — mount the engine
поднимать д. подъемником — hoist the engine
подогревать д. — heat the engine
проворачивать д. на... оборотов — turn the engine... revolutions
прогревать д. (на оборотах...%) — warm up the engine (at a speed of... %)
продопжать полет на (двух) д. — continue flight on (two) engines
разгоняться на одном д. — accelerate with one engine operating
разгоняться при неработающем критическом д. — accelerate with the critical епgine inoperative
сбавлять (убирать) обороты (работающего) д. — decelerate the engine
увеличивать обороты (работающего) д. — accelerate the engine
устанавливать д. — install the engineРусско-английский сборник авиационно-технических терминов > двигатель
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64 Wankel, Felix
[br]b. 13 August 1902 Lahr, Black Forest, Germanyd. 9 October 1988 Lindau, Bavaria, Germany[br]German internal combustion engineer, inventor of the Wankel rotary engine.[br]Wankel was first employed at the German Aeronautical Research Establishment, where he worked on rotary valves and valve sealing techniques in the early 1930s and during the Second World War. In 1951 he joined NSU Motorenwerk AG, a motor manufacturer based at Neckarsulm, near Stuttgart, and began work on his rotary engine; the idea for this had first occurred to Wankel as early as 1929. He had completed his first design by 1954, and in 1957 his first prototype was tested. The Wankel engine has a three-pointed rotor, like a prism of an equilateral triangle but with the sides bowed outwards. This rotor is geared to a driveshaft and rotates within a closely fitting and slightly oval-shaped chamber so that, on each revolution, the power stroke is applied to each of the three faces of the rotor as they pass a single spark plug. Two or more rotors may be mounted coaxially, their power strokes being timed sequentially. The engine has only two moving parts, the rotor and the output shaft, making it about a quarter less in weight compared with a conventional piston engine; however, its fuel consumption is high and its exhaust emissions are relatively highly pollutant. The average Wankel engine speed is 5,500 rpm. The first production car to use a Wankel engine was the NSU Ro80, though this was preceded by the experimental NSU Spyder prototype, an open two-seater. The Japanese company Mazda is the only other automobile manufacturer to have fitted a Wankel engine to a production car, although licences were taken by Alfa Romeo, Peugeot- Citroën, Daimler-Benz, Rolls-Royce, Toyota, Volkswagen-Audi (the company that bought NSU in the mid-1970s) and many others; Daimler-Benz even produced a Mercedes C-111 prototype with a three-rotor Wankel engine. The American aircraft manufacturer Curtiss-Wright carried out research for a Wankel aero-engine which never went into production, but the Austrian company Rotax produced a motorcycle version of the Wankel engine which was fitted by the British motorcycle manufacturer Norton to a number of its models.While Wankel became director of his own research establishment at Lindau, on Lake Constance in southern Germany, Mazda continued to improve the rotary engine and by the time of Wankel's death the Mazda RX-7 coupé had become a successful, if not high-selling, Wankel -engined sports car.[br]Further ReadingN.Faith, 1975, Wankel: The Curious Story Behind the Revolutionary Rotary Engine, New York: Stein \& Day.IMcN -
65 EAP
1) Военный термин: Emergency Action Procedures, Enterprise Architecture Plan, effective air path, emergency action procedure, experimental aircraft program, experimental aircraft prototype, Economically Active Population2) Техника: Event Assessment Panel, experimental activity proposal3) Религия: Evidences of Answered Prayer4) Бухгалтерия: Estimated Adjusted Price5) Страхование: estimated annual premium6) Оптика: electro-absorption avalanche photodiode7) Сокращение: Electronic Assembly Plant, Emergency Action Plan (2004), Emergency Action Plan, Experimental Aircraft Programme8) Университет: Education Abroad Program, English For Academic Purposes9) Физиология: Eber Associated Protein, Estrus Associated Protein10) Вычислительная техника: Extensible Authentication Protocol (Cisco, Verschluesselung, RADIUS, WPA)11) Иммунология: Equine Assisted Psychotherapy12) Связь: Extensible Authentication Protocol13) Космонавтика: Environment Assessment Programme (UNEP)14) Транспорт: Employee Assistance Program15) Деловая лексика: Employee Assistance Plan, Enterprise Analytic Portal, employee assistance programme (This gives your employees telephone access to confidential advice and face-to-face counselling if necessary, and protects the business from personal injury claims.)16) Нефтегазовая техника Equivalent Air Pressure17) Образование: Early Access Program, Emea Academic Program, Employee Alcoholism Program18) Сетевые технологии: Enhanced Authentication Protocol, Enterprise Architecture Planning, открытый протокол аутентификации (extensible authentication protocol)19) ЕБРР: environmental action plan20) Электротехника: emergency action program21) Имена и фамилии: Edgar Allen Poe, Elvis Aaron Presley22) Должность: Executive Administrative And Professional23) Правительство: Engineering Access Permit -
66 Mikoyan, Artem Ivanovich
SUBJECT AREA: Aerospace[br]b. 5 August 1905 Sanain, Armeniad. 9 December 1970 Moscow, Russia[br]Armenian aircraft designer.[br]Mikoyan graduated from the Zhukovsky Military Aircraft Academy in 1936. His first major design project was in response to an official requirement, issued in December 1940, for a single-engined fighter with performance equating to those then in service with the British, French and German air forces. In conjunction with M.L. Gurevich, a mathematician, and in a bare four months, he produced a flying prototype, with a top speed of 401 mph (645 km/h), that entered service as the MiG-1 in 1941. The Mikoyan and Gurevich MiG-3 and MiG-5 followed, and they then designed the MiG-7 high-altitude fighter; however, the latter never came into service on account of the decline of the German air force.The Second World War MiG fighters were characterized by high speed, good protection and armament, but they had poor manoeuvrability. In 1945, however, Mikoyan began to study Western developments in jet-powered aircraft. The result was a series of jet fighters, beginning with the MiG-9A, through the MiG-11, to the MiG-15 that gave the Allied air forces such a shock when it first appeared during the Korean War. The last in the series in which Mikoyan himself was involved was the MiG-23, which entered service in 1967. The MiG series lived on after both his and Gurevich's (1976) deaths, with one of the latest models being the MiG-31.[br]Principal Honours and DistinctionsDeputy to the Supreme Soviet 1950, 1954, 1958. Corresponding Member of the Soviet Academy of Sciences 1953. Member of the Council of Nationalities 1962. Three Stalin Prizes and other decorations.CMBiographical history of technology > Mikoyan, Artem Ivanovich
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67 разработка опытного образца
Разработка опытного образцаOther military aircraft are in various stages of preliminary design of prototype development.Advanced development amounts to the development of prototype hardware for testing.Русско-английский научно-технический словарь переводчика > разработка опытного образца
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68 phase
фаза; стадия, этап; фазировать, синхронизировать по фазеatmospheric phase of launch — ркт. атмосферный этап или участок выведения
heliocentric phase of the mission — ксм. этап полёта по гелиоцентрической траектории
phase of the hop — разг. этап полёта
— phase in -
69 engine
1) двигатель
2) машина-двигатель
3) мотостроительный
4) скоропечатный
5) мотор
6) механизм
7) орудие
8) инструмент
9) локомотив
10) моторный
– accelerate the engine
– air-breathing jet engine
– air-cooled engine
– aircraft engine
– altitude engine
– arc-heating jet engine
– atmospheric jet engine
– augmented engine
– axial engine
– basic engine
– beam engine
– birotary engine
– boat engine
– build up engine
– bypass engine
– carburetor engine
– carburettor engine
– compound engine
– compression-ignition engine
– cowl engine
– crank engine
– cross-head engine
– crosshead engine
– crude oil engine
– cruise engine
– decelerate the engine
– diaphragm engine
– diesel engine
– double-acting engine
– double-row engine
– ducted-fan engine
– electric engine
– engine bay
– engine bed
– engine block
– engine brake
– engine braking
– engine break-away
– engine capacity
– engine case
– engine control
– engine cowling
– engine cycle
– engine department
– engine flameout
– engine frame
– engine hatch
– engine is dead
– engine is generating
– engine is running
– engine misses
– engine motoring
– engine mounting
– engine nacelle
– engine performance
– engine pings
– engine press
– engine reconditioning
– engine relay
– engine room
– engine rpm indicator
– engine shutdown
– engine smokes
– engine speed
– engine stalls
– engine support
– engine telegraph
– engine throttle
– engine torque
– engine tune-up
– engine works
– engine yard
– explosion engine
– flood engine
– flush engine
– four-cycle engine
– four-stroke engine
– free-piston engine
– fuel-injection engine
– fuel-pump engine
– gas turbine jet engine
– gas-turbine engine
– gasoline engine
– geared engine
– heat engine
– heavy-oil engine
– high-speed engine
– hoist engine
– hot-bulb engine
– hydraulic engine
– hydrojet engine
– in-line engine
– industrial engine
– ion rocket jet engine
– jet engine
– jet engine fuel
– left-hand engine
– lift engine
– liquid-cooled engine
– liquid-propellant jet engine
– loop-scavenged engine
– low-compression engine
– low-speed engine
– marine engine
– micro engine
– multibank engine
– multicrank engine
– multinozzle engine
– multipropellant engine
– multirow engine
– non-reversible engine
– nuclear engine
– outboard engine
– overhauled engine
– overhead engine
– piston engine
– plate-measuring engine
– pod-type engine
– power of an engine
– prime engine
– production engine
– prototype engine
– pulsejet engine
– racing of engine
– radial engine
– ramjet engine
– relight engine
– restart of engine
– rev up engine
– reversible engine
– revving-up engine
– right-hand engine
– rocket engine
– rotary-piston engine
– run in engine
– self-ignition engine
– semidiesel engine
– short-stroke engine
– sing-acting engine
– spark-ignition engine
– stand-by engine
– start engine
– starting engine
– steam engine
– steering engine
– supercharged engine
– supercompression engine
– sustainer engine
– switch engine
– tear-down of engine
– traction engine
– tune engine
– turbo-ramjet engine
– turbocharged engine
– turbojet engine
– turboprop engine
– turborocket engine
– turboshaft engine
– two-cycle engine
– two-stroke engine
– uncooled engine
– unsupercharged engine
– variable-stroke engine
– vectored-thrust engine
– Vee of engine
– Wankel engine
– water-cooled engine
aircraft engine mechanic — <aeron.> авиамоторист
back-pressure steam engine — паровая машина с противодавлением
bipropellant rocket engine — < rocket> двигатель двухкомпонентный
diesel locomotive engine — < railways> двигатель тепловозный
engine is installed as a unit — двигатель устанавливается в сборе
hybrid rocket engine — < rocket> двигатель ракетный комбинированный
jet engine starter system — <engin.> турбостартер
liquid-fuel rocket engine — <cosm.> двигатель реактивный жидкостный
liquid-propellant rocket engine — жидкостный ракетный двигатель
monopropellant rocket engine — < rocket> двигатель ракетный однокомпонентный
solid-propellant rocket engine — < rocket> двигатель ракетный твердотопливный
spontaneous ignition engine — < rocket> двигатель самореагирующий
twin ramjet engine — <engin.> двигатель прямоточнный спаренный
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70 PASS
1) Компьютерная техника: Print Analyzer Savings Solutions3) Американизм: Post Approval Surveillance System, Procurement Automated Source System, Proof Of Age Standards Scheme5) Военный термин: PACOM ADP Server Site, PACOM IPAC Intelligence Computer System Analyst Support System, Photo Interpretation Analyst Support System, parked aircraft sentry system, passive aircraft surveillance system, patrol advanced surveillance system, penetration aids/strike system, position and surveying system, precision angulation and support system, pressurized air start system, prototype artillery subsystem6) Техника: Personal Alert Safety System, post-accident sampling system, precision auto collimating solar sensor, programmed access/security system7) Юридический термин: Peer Assistance Support Scheme8) Статистика: Power Analysis and Sample Size9) Автомобильный термин: personalized automotive security system10) Грубое выражение: Polite And So Sexy11) Радио: Pressures Applications Solenoids Sensors12) Сокращение: Passive & Active Sensor Subsystem, Postal Application and Scheduling System (2001, employment test system), passage, passenger, Personal Access Satellite System (NASA)13) Университет: Patron Satisfaction Survey, Program And Semester Switch14) Физиология: Post Abortion Stress Syndrome15) Школьное выражение: Princeton Alternative Secondary School16) Экология: Programmable Atmospheric Sampling Control17) Образование: Parents Assuring Student Success, Partners At School Sharing, Partnership For Achieving Student Success, Peer Assisted Study Session, Practice Assessment Strengthen Skills, Preparatory Academic Skills For Students, Preventing Alcohol Sales To Students, Profile Of Achievement And School Success, Program For Academic Skills And Success, Program For Academic Student Success, Project Attendance For Secondary Schools, Pull Aim Squeeze And Sweep18) Должность: Professional Airways System Specialist19) НАСА: Primary Avionics Software System -
71 PATS
1) Военный термин: passive angle tracking system, personnel assistance teams, personnel in an awaiting training status, preacademic training student, primary aircraft training system3) Юридический термин: Personal Anti Theft System4) Автомобильный термин: (Passive Anti-Theft System) пассивная противоугонная система5) Сокращение: Portable Acoustic Tracking System, Precision Attack Targeting System (USAFR), Precision Attack Targeting System, Precision Automated Tracking Station, Precision Automatic Tracking System, Prototype Automatic Target Screener6) Транспорт: Passenger Assistant Training Scheme, Passive Anti Theft System, Precision Automated Tracking System7) Деловая лексика: Partly Assisted Trading System8) НАСДАК: International Superconductor -
72 pass
1) Компьютерная техника: Print Analyzer Savings Solutions3) Американизм: Post Approval Surveillance System, Procurement Automated Source System, Proof Of Age Standards Scheme5) Военный термин: PACOM ADP Server Site, PACOM IPAC Intelligence Computer System Analyst Support System, Photo Interpretation Analyst Support System, parked aircraft sentry system, passive aircraft surveillance system, patrol advanced surveillance system, penetration aids/strike system, position and surveying system, precision angulation and support system, pressurized air start system, prototype artillery subsystem6) Техника: Personal Alert Safety System, post-accident sampling system, precision auto collimating solar sensor, programmed access/security system7) Юридический термин: Peer Assistance Support Scheme8) Статистика: Power Analysis and Sample Size9) Автомобильный термин: personalized automotive security system10) Грубое выражение: Polite And So Sexy11) Радио: Pressures Applications Solenoids Sensors12) Сокращение: Passive & Active Sensor Subsystem, Postal Application and Scheduling System (2001, employment test system), passage, passenger, Personal Access Satellite System (NASA)13) Университет: Patron Satisfaction Survey, Program And Semester Switch14) Физиология: Post Abortion Stress Syndrome15) Школьное выражение: Princeton Alternative Secondary School16) Экология: Programmable Atmospheric Sampling Control17) Образование: Parents Assuring Student Success, Partners At School Sharing, Partnership For Achieving Student Success, Peer Assisted Study Session, Practice Assessment Strengthen Skills, Preparatory Academic Skills For Students, Preventing Alcohol Sales To Students, Profile Of Achievement And School Success, Program For Academic Skills And Success, Program For Academic Student Success, Project Attendance For Secondary Schools, Pull Aim Squeeze And Sweep18) Должность: Professional Airways System Specialist19) НАСА: Primary Avionics Software System -
73 pats
1) Военный термин: passive angle tracking system, personnel assistance teams, personnel in an awaiting training status, preacademic training student, primary aircraft training system3) Юридический термин: Personal Anti Theft System4) Автомобильный термин: (Passive Anti-Theft System) пассивная противоугонная система5) Сокращение: Portable Acoustic Tracking System, Precision Attack Targeting System (USAFR), Precision Attack Targeting System, Precision Automated Tracking Station, Precision Automatic Tracking System, Prototype Automatic Target Screener6) Транспорт: Passenger Assistant Training Scheme, Passive Anti Theft System, Precision Automated Tracking System7) Деловая лексика: Partly Assisted Trading System8) НАСДАК: International Superconductor -
74 development
разработка; опытно-конструкторские работы; развитие, эволюция; усовершенствование; доводка; отработка; отладка; наполнение купола ( парашюта) ; проявление ( фотоматериалов) ; усовершенствованный образец; вариант; модификация; опытный ( образец) ; экспериментальный; головной серииdevelopment of planetary quarantine — разработка мер [средств] (биологической) защиты планет (исследуемых с помощью КЛА)
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75 Ohain, Hans Joachim Pabst von
SUBJECT AREA: Aerospace[br]b. 14 December 1911 Dessau, Germany[br]German engineer who designed the first jet engine to power an aeroplane successfully.[br]Von Ohain studied engineering at the University of Göttingen, where he carried out research on gas-turbine engines, and centrifugal compressors in particular. In 1935 he patented a design for a jet engine (in Britain, Frank Whittle patented his jet-engine design in 1930). Von Ohain was recruited by the Heinkel company in 1936 to develop an engine for a jet aircraft. Ernst Heinkel was impressed by von Ohain's ideas and gave the project a high priority. The first engine was bench tested in September 1937. A more powerful version was developed and tested in air, suspended beneath a Heinkel dive-bomber, during the spring of 1939. A new airframe was designed to house the revolutionary power plant and designated the Heinkel He 178. A short flight was made on 24 August 1939 and the first recognized flight on 27 August. This important achievement received only a lukewarm response from the German authorities. Von Ohain's turbojet engine had a centrifugal compressor and developed a thrust of 380 kg (837 lb). An improved, more powerful, engine was developed and installed in a new twin-engined fighter design, the He 280. This flew on 2 April 1941 but never progressed beyond the prototype stage. By this time two other German companies, BMW and Junkers, were constructing successful turbojets with axial compressors: luckily for the Allies, Hitler was reluctant to pour his hard-pressed resources into this new breed of jet fighters. After the war, von Ohain emigrated to the United States and worked for the Air Force there.[br]Bibliography1929, "The evolution and future of aeropropulsion system", The Jet Age. 40 Years of Jet Aviation, Washington, DC: National Air \& Space Museum, Smithsonian Institution.Further ReadingVon Ohain's work is described in many books covering the history of aviation, and aero engines in particular, for example: R.Schlaifer and S.D.Heron, 1950, Development of Aircraft Engines and fuels, Boston. G.G.Smith, 1955, Gas Turbines and Jet Propulsion.Grover Heiman, 1963, Jet Pioneers.JDSBiographical history of technology > Ohain, Hans Joachim Pabst von
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76 Séguin, Louis
[br]b. 1869d. 1918[br]French co-designer, with his brother Laurent Séguin (b. 1883 Rhône, France; d. 1944), of the extremely successful Gnome rotary engines.[br]Most early aero-engines were adaptations of automobile engines, but Louis Séguin and his brother Laurent set out to produce a genuine aero-engine. They decided to build a "rotary" engine in which the crankshaft remained stationary and the cylinders rotated: the propeller was attached to the cylinders. The idea was not new, for rotary engines had been proposed by engineers from James Watt to Samuel P. Langley, rival of the Wright brothers. (An engine with stationary cylinders and a rotating crankshaftplus-propeller is classed as a "radial".) Louis Séguin formed the Société des Moteurs Gnome in 1906 to build stationary industrial engines. Laurent joined him to develop a lightweight engine specifically for aeronautical use. They built a fivecylinder air-cooled radial engine in 1908 and then a prototype seven-cylinder rotary engine. Later in the year the Gnome Oméga rotary, developing 50 hp (37 kW), was produced. This was test-flown in a Voisin biplane during June 1909. The Gnome was much lighter than its conventional rivals and surprisingly reliable in view of the technical problems of supplying rotating cylinders with the petrol-air mixture and a spark to ignite it. It was an instant success.Gnomes were mass-produced for use during the First World War. Both sides built and flew rotary engines, which were improved over the years until, by 1917, their size had grown to such an extent that a further increase was not practicable. The gyroscopic effects of a large rotating engine became a serious handicap to manoeuvrability, and the technical problems inherent in a rotary engine were accentuated.[br]Bibliography1912, L'Aérophile 20(4) (Louis Séguin's description of the Gnome).Further ReadingC.F.Taylor, 1971, "Aircraft Propulsion", Smithsonian Annals of Flight 1(4) (an account of the evolution of aircraft piston engines).A.Nahum, 1987, the Rotary Aero-Engine, London.JDS -
77 Short, Hugh Oswald
SUBJECT AREA: Aerospace[br]b. 16 January 1883 Derbyshire, Englandd. 4 December 1969 Haslemere, England[br]English co-founder, with his brothers Horace Short (1872–1917) and Eustace (1875–1932), of the first company to design and build aeroplanes in Britain.[br]Oswald Short trained as an engineer; he was largely self-taught but was assisted by his brothers Eustace and Horace. In 1898 Eustace and the young Oswald set up a balloon business, building their first balloon in 1901. Two years later they sold observation balloons to the Government of India, and further orders followed. Meanwhile, in 1906 Horace designed a high-altitude balloon with a spherical pressurized gondola, an idea later used by Auguste Piccard, in 1931. Horace, a strange genius with a dominating character, joined his younger brothers in 1908 to found Short Brothers. Their first design, based on the Wright Flyer, was a limited success, but No. 2 won a Daily Mail prize of £1,000. In the same year, 1909, the Wright brothers chose Shorts to build six of their new Model A biplanes. Still using the basic Wright layout, Horace designed the world's first twin-engined aeroplane to fly successfully: it had one engine forward of the pilot, and one aft. During the years before the First World War the Shorts turned to tractor biplanes and specialized in floatplanes for the Admiralty.Oswald established a seaplane factory at Rochester, Kent, during 1913–14, and an airship works at Cardington, Bedfordshire, in 1916. Short Brothers went on to build the rigid airship R 32, which was completed in 1919. Unfortunately, Horace died in 1917, which threw a greater responsibility onto Oswald, who became the main innovator. He introduced the use of aluminium alloys combined with a smooth "stressed-skin" construction (unlike Junkers, who used corrugated skins). His sleek biplane the Silver Streak flew in 1920, well ahead of its time, but official support was not forthcoming. Oswald Short struggled on, trying to introduce his all-metal construction, especially for flying boats. He eventually succeeded with the biplane Singapore, of 1926, which had an all-metal hull. The prototype was used by Sir Alan Cobham for his flight round Africa. Several successful all-metal flying boats followed, including the Empire flying boats (1936) and the ubiquitous Sunderland (1937). The Stirling bomber (1939) was derived from the Sunderland. The company was nationalized in 1942 and Oswald Short retired the following year.[br]Principal Honours and DistinctionsHonorary Fellow of the Royal Aeronautical Society. Freeman of the City of London. Oswald Short turned down an MBE in 1919 as he felt it did not reflect the achievements of the Short Brothers.Bibliography1966, "Aircraft with stressed skin metal construction", Journal of the Royal Aeronautical Society (November) (an account of the problems with patents and officialdom).Further ReadingC.H.Barnes, 1967, Shorts Aircraft since 1900, London; reprinted 1989 (a detailed account of the work of the Short brothers).JDS -
78 Tupolev, Andrei Nikolayevich
[br]b. 10 November 1888 Pastomazovo, Russiad. 23 December 1972 Moscow, Russia[br]Russian aircraft designer.[br]In 1909 he entered the Moscow Higher Technical School and became a pupil of Nikolai Zhukovsky, who was known as "the father of Russian aviation". Graduating in 1918, he helped Zhukovsky to set up the Zhukovsky Central Aerohydrodynamic Institute and was made Assistant Director. He was appointed Head of the Institute's Design Department in 1922: his work was concentrated on wind tunnels and gliders, but later included aerodynamic calculations and the construction of all-metal aircraft. His first significant design project was the twin-engined Ant-29 fighter prototype, which appeared in the early 1930s and eventually entered service as the SB-2. However, Tupolev and his wife fell victim to Stalin's purges in 1937: she was sent to a labour camp and he was imprisoned, but in 1943 both were rehabilitated and Tupolev was able to resume his design work. He devoted his attention to long-range strategic bombers, the first of these being the Tu-4, a copy of the US B-29, followed by the Tu-70 bomber. He also designed the Tu-104 airliner, and in 1967 he produced the world's first supersonic airliner, the Tu-144. Tupolev also became interested in fast-attack naval craft and designed a number of torpedo launches, and he rose to the rank of Lieutenant-General in the Soviet air force's Engineering and Technical Service.[br]Principal Honours and DistinctionsHonoured Scientist and Technologist RSFSR 1933. Hero of Socialist Labour 1945. Member of the Supreme Soviet 1950–58. Member of the Soviet Academy of Sciences 1953. Lenin Prize 1957. Stalin Prize.CMBiographical history of technology > Tupolev, Andrei Nikolayevich
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79 EAP
EAP, effective air path————————EAP, emergency action(s) procedure(s)————————EAP, experimental aircraft program————————EAP, experimental aircraft prototypeEnglish-Russian dictionary of planing, cross-planing and slotting machines > EAP
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80 PASS
PASS, parked aircraft sentry system————————PASS, passive aircraft surveillance system————————PASS, patrol advanced surveillance system————————PASS, penetration aids/strike systemсистема средств обеспечения прорыва ПВО [ПРО] и поражения целей————————PASS, position and surveying system————————PASS, precision angulation and support system————————PASS, pressurized air start system————————PASS, prototype artillery subsystemEnglish-Russian dictionary of planing, cross-planing and slotting machines > PASS
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