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  • 101 assembled crankshaft

    <mvhcl.mot> (in 2-stroke bike engines) ■ gebaute Kurbelwelle f

    English-german technical dictionary > assembled crankshaft

  • 102 built-up crankshaft

    <mvhcl.mot> (in 2-stroke bike engines) ■ gebaute Kurbelwelle f

    English-german technical dictionary > built-up crankshaft

  • 103 displacement

    <tech.gen> (physical) ■ Verdrängung f
    <tech.gen> (moving sth. from location A to location B, over any distance) ■ Verlagerung f
    <tech.gen> (smooth shifting of sth., any direction, any distance) ■ Verschiebung f
    <tech.gen> (the distance over which sth. is displaced) ■ Weg m
    < convey> (piston pump) ■ Förderstrom m
    < geo> ■ Verwerfung f ; Lagerungsstörung f ; Sprung m
    < mech> (lateral deflection) ■ Auslenkung f
    form < mot> (of reciprocating piston engines; in cid, liters or cc) ■ Hubraum m ; Hubvolumen n form
    < nav> (ship size) ■ Verdrängung f ; Wasserverdrängung f
    < nav> ■ Verdrängung f
    < plast> (inj. molding mach.; screw cross section area x the injection stroke) ■ Hubvolumen n
    <tech.gen> (e.g. body, ship, boat, competition) ■ Verdrängungs...

    English-german technical dictionary > displacement

  • 104 piston

    ['pɪstən]
    nome pistone m.
    * * *
    ['pistən]
    ((in engines, pumps etc) a round piece usually of metal that fits inside a cylinder and moves up and down or backwards and forwards inside it.) pistone
    * * *
    piston /ˈpɪstən/
    n.
    1 (mecc.) pistone; stantuffo
    2 (mus.) pistone
    ● (mecc.) piston displacement, cilindrata ( di un motore) □ (mecc.) piston drill, perforatrice a pistone □ (mecc.) piston engine, motore a pistoni □ (mecc.) piston pin, perno del pistone; spinotto □ (autom., mecc.) piston ring, anello per stantuffo; fascia elastica del pistone; segmento □ piston rod, biella □ piston stroke, corsa del pistone.
    * * *
    ['pɪstən]
    nome pistone m.

    English-Italian dictionary > piston

  • 105 piston

    ['pɪstən] noun Kolben, der
    * * *
    ['pistən]
    ((in engines, pumps etc) a round piece usually of metal that fits inside a cylinder and moves up and down or backwards and forwards inside it.) der Kolben
    * * *
    pis·ton
    [ˈpɪstən]
    n TECH Kolben m
    * * *
    ['pɪstən]
    n
    Kolben m
    * * *
    piston [ˈpıstən] s
    1. TECH Kolben m
    2. auch piston valve MUS Piston n, (Gleit)Ventil n (bei Blasinstrumenten)
    3. auch piston knob MUS Kombinationsknopf m (der Orgel)
    * * *
    ['pɪstən] noun Kolben, der
    * * *
    n.
    Kolben - m.

    English-german dictionary > piston

  • 106 точка


    point
    - бортовая заправочная — external servicing point
    - верхняя мертвая (вмт, поршня пд) — top dead center (tdc
    положение поршня и соответствующего кривошипа копенвапа в точке, наиболее удаленной от оси коленвапа, т.е. положение поршня в самой верхней точке хода (рис. 64). — the position of а piston and its crankshaft arm when the piston is at its farthest removed position from the center line of the crankshaft, i.e., it is at the top of stroke.
    - весеннего равноденствия весны — vernal equinox
    - выброски, беспосадочного десантирования (парашютистов, грузов) — (para) drop point /area/
    - выхода из района (зоны) — exit fix
    -, десятичная (на пульте управнения и индикации) — decimal point. all decimal points are illuminated.
    - заземления (эл.) — ground connection
    на схеме должны быть указаны внутренние перемычки и точки заземления, — internal jumpers and ground connections be shown in the wiring diagram.
    - замера — measuring point
    - замерзания — freezing point
    - заправки водой (маслом, топливом) — water (oil, fuel) servicing point
    - измерения — measuring point
    -, исходная — origin, initial point
    - касания — contact point
    - касания самолета при посадке (рис. 116) — touchdown point
    - кипения — boiling point (bp)
    - кислородного питания (штуцер) — oxygen outlet
    -, конечная — terminal point
    -, контрольная (контрольный вывод в аппаратуре) (кг) — test point (тр). a number of strategically placed тр provides simple and rapid trouble-shooting.
    - крепления — attachment /attach /point
    - крепления страховочных строп — afety harness attach(ment) point /receptacle/
    -, критическая (точка нулевой скорости в потоке, обтекающам тело) (рис. 142) — stagnation point. a point in а field of flow about а body where the air particles have zero velocity with respect to the body.
    -, критическая (отказа двигателя при взлете) — critical point, critical engine failure point
    точка, в которой при разбеге самолета предполагается отказ критического двигателя с цепью опредепения дистанции прерванного взлета и траектории взлета, — critical point is а selected point at which, for the purpose of determining the accelerate-stop distance and take-off path, failure of the critical power unit is assumed to occur.
    -, мертвая (в системе управпения) — dead spot
    зона нечувствительности у нейтрального положения в системе управления, в котарой незначительные перемещения исполнительного мехацизма не вызывают к-л. срабатывания системы. — in а control system, а region centered about the neutral control position where small movements of the actuator do not produce any response in the system.
    - места местоположения (ла) — position (fix), pos
    - минимальной высоты принятия решения идти на посадку — minimum landing commit point. do not attempt а go-around after the minimum commit point (1000 ft above airport elevation).
    -, наведения (при заходе на посадку) — land point. fix а land point on the runway
    - из впп, не обеспечивающая безопасности выполнения посадки — nо-land point (on runway)
    - на поверхности земли — point on surface of the earth, point on the earth's surface
    - на траектории — point on flight path
    - на траектории, указанная в графике на рис. — point(s) on flight path plotted in fig.
    - начала выброски (тнв, парашютистов, грузов) — drop initiation point (dip)
    - начала выравнивания (при посадке) — flare-out point
    - начала выравнивания (после набора высоты) — leveling-off point
    - начала координат — origin of coordinates
    - начала отсчета — datum point, origin, reference point
    - начала отсчета дистанций (пo продольной оси ла) — station numbering origin
    - начала отсчета (траектории начального взлета) — (takeoff flight path) reference zero
    начало отсчета координат различных точек на траектории начального набора высоты, расположенное в конце взлетной дистанции на уровне 35 фт (10,7 м) ниже траектории взлета. — this is а reference to which the coordinates of the various points in the takeoff flight path are referred. it is defined as the end of the takeoff distance and 35 feet below the flight path at this point.
    - начала разворота — initial point of turn, roll-in point, turn point
    - начала шкалы (прибора) — scale origin point
    -, нейтральная — neutral point
    -, неподвижная — fixed point
    - нечувствительности (в системe управления) — dead spot
    -, нивелировочная — leveling mark /point/
    контрольные точки на определенных местах конструкции самолета, служащие для нивелировки ла. — reference marks for leveling the airplane on the ground.
    -, нижняя мертвая (нмт) — bottom dead center (bdc)
    положение поршня пд при его максимальном удалении от головки цилиндра (рис. 64). — the crankshaft position when the piston of an engine is at the greatest possible distance from the cylinder head.
    -, нулевая (напр., электрического соединения *звездой*) — neutral point
    -, нулевая заземленная — grounded neutral point
    -, нулевая незаземленная — ungrounded neutral point
    - нулевой подъемной силы — zero lift point
    - обслуживания туалетов (заправки водой, химжидкостью, слив) — lavatory servicing point
    -, опорная (отсчета, привязки) — reference point
    - опоры — fulcrum
    точка, относительно которой поворачивается или совершает колебательные движения рычаг. — the pivot point about which а lever oscillates or turns.
    - осени, осеннего равнодействия — autumn equinox
    - отказа двигателя (при взлете — engine failure point
    - отрыва воздушного потока — airflow separation point
    точка, в которой происходит отрыв пограничного слоя потока.
    - отрыва (срыва) возд. потока, точка начала турбулизации — burble point. the point in increasing angle of attack at which burble begins.
    - отрыва при взлете — lift-off point
    - отсчета, нулевая — reference zero, origin
    - пересечения — paint of intersection
    - перехода (рис. 142) — transition point
    - питания кислородом (штуцер) — oxygen outlet
    - повышенного внимания (при осмотре, контроле) — thorough-inspection point /area, zone/, point subject to thorough inspection
    - подъема (такелажная) — lifting /hoist/ point
    - полного торможения (лотока) — stagnation point
    -, посадочная (на впп) — land point fix а land-no land point on the runway.
    - прибытия (прилета) — point of destination
    - приземления — touchdown point
    - приложения вектора — point of vector application
    - приложения нагрузки — point of load application
    - приложения силы — point of force application
    - принятия решения — decision point
    - принятия решения идти на посадку (300 м над уровнем аэродрома) — landing commit point (1000 ft above airport elevation)
    - прицеливания — aim(ing) point
    - прицеливания, наведения (предполагаемого касания впп при посадке) — land point
    - пятиминутного взлета — five minute power point
    точка, достигаемая самалетом через 5 минут после на чала взлета. режим работы двигателей (после достижения этой точки) должен быть уменьшен до макс. продолжительного. — the point at which a time of 5 minutes has elapsed after start of takeoff. the power of the operative engines must then be reduced to maximum continuous.
    - равноденствия (в астронавигации) — equinoctical point, equinox
    -, радионавигационная (рнт) — radio navigation station
    - разворота — turn point
    -, реперная (для нивелировки) — leveling point /mark/
    - росы — dewpoint
    температура, до которой нужно охладить воздух, чтобы содержащийся в нем водяной пар достиг состояния насыщения, — the temperature to which a given parcel of air must be cooled at constant pressure and constant water-vapor content in order for saturation to occur.
    -, световая (отметка на экране катодно-лучевой трубки) — blip. a spot of light on cathoderay tube display.
    -, световая (от осветителя) — spot of light
    - смазки (на карте смазки) — greasing point (on lubrication chart)
    - сообщения о месте (местоположении) ла — reporting point
    - соррикосновения — point of contact
    - срабатывания — actuation point
    -, средняя (трех-фазной сети с четвертым проводом, с возможным заземлением) — neutral point (of three-phase, four-wire system). the neutral point may be grounded.
    - старта (при взлете) — start of takeoff
    - старта (начала полета) — point of departure
    -, створная — align point
    -, такелажная — lifting/hoist/point

    chart showing lifting and jacking points shall be provided.
    -, такелажная (надпись) — hoist point, hoist here
    -, тарируемая — calibrated point
    - технического обслуживания (бортовая, на борту ла) — (external) servicing point
    - траектории полета — flight path point
    - четверти хорды — quarter-chord point
    точка на хорде аэродинамического профиля, отстоящая на 1/4 длины хорды от передней кромки (рис. 8). — quarter-chord point is on the aerofoil section chord at one quarter of the chord length behind the leading edge.
    - шарнирного крепления — hinge point
    элерон крепится (подвешивается) в (з-х) точках, — aileron is hinged at (three) points.
    -, швартовочная (груза в отсеке) — tie-down point
    -, швартовочная (ла) (рис. 150) — mooring/picketing/point
    - шкалы (прибора) — scale point /mark/
    - шкалы (рис. 72) — scale dot
    - шкалы, оцифрованная, числовая — scale point marked with figure, figure-marked scale point
    в вмт (верхней мертвой точке) — at tdc. the piston of cylinder no.1 is at tdc.
    в нмт (нижней мертвой точке) — at bdc
    до вмт — before tdc
    замер в т. "а" — measurement at point "а"
    недоход поршня до верхней мертвой т. на...град. — piston failure to reach tdc by... degrees
    после вмт — after /past/ tdc
    доходить до вмт (о поршне) — reach tdc
    не доходить до вмт — fail to reach tdc
    рассчитывать т. разворота — calculate turn point

    Русско-английский сборник авиационно-технических терминов > точка

  • 107 Cecil, Revd William

    [br]
    b. 1792 England
    d. 1882 England
    [br]
    English inventor of a gas vacuum engine.
    [br]
    Admitted to Magdalene College, Cambridge, in 1810, Cecil was elected a Fellow in 1814. The son of an Anglican priest, he was himself ordained in 1820; he devoted his life to the Church of England, but he also showed a commendable aptitude for technical matters. His paper on a means of motive power, presented to the Cambridge Philosophical Society in 1820, created immense interest. A working model of his engine, using hydrogen as fuel, was demonstrated during the presentation. The operating principle required that a vacuum be produced in a closed cylinder by quenching a burning flame, the pressure difference between the vacuum and atmosphere then being used to produce the working stroke. Cecil's engine was never manufactured in any number, but the working principle was adapted by other pioneers, namely Samuel Brown, in 1824, and, more successfully, Otto- Langen in 1867.
    [br]
    Bibliography
    1820, "On the application of hydrogen gas to produce a moving power in machinery", Transactions of the Cambridge Philosophical Society 1(2):217–39.
    Further Reading
    John Venn, Alumni Cantabrienses Part II (1752–1900): p. 567.
    KAB

    Biographical history of technology > Cecil, Revd William

  • 108 Gurney, Sir Goldsworthy

    [br]
    b. 14 February 1793 Treator, near Padstow, Cornwall, England
    d. 28 February 1875 Reeds, near Bude, Cornwall, England
    [br]
    English pioneer of steam road transport.
    [br]
    Educated at Truro Grammar School, he then studied under Dr Avery at Wadebridge to become a doctor of medicine. He settled as a surgeon in Wadebridge, spending his leisure time in building an organ and in the study of chemistry and mechanical science. He married Elizabeth Symons in 1814, and in 1820 moved with his wife to London. He delivered a course of lectures at the Surrey Institution on the elements of chemical science, attended by, amongst others, the young Michael Faraday. While there, Gurney made his first invention, the oxyhydrogen blowpipe. For this he received the Gold Medal of the Society of Arts. He experimented with lime and magnesia for the production of an illuminant for lighthouses with some success. He invented a musical instrument of glasses played like a piano.
    In 1823 he started experiments related to steam and locomotion which necessitated taking a partner in to his medical practice, from which he resigned shortly after. His objective was to produce a steam-driven vehicle to run on common roads. His invention of the steam-jet of blast greatly improved the performance of the steam engine. In 1827 he took his steam carriage to Cyfarthfa at the request of Mr Crawshaw, and while there applied his steam-jet to the blast furnaces, greatly improving their performance in the manufacture of iron. Much of the success of George Stephenson's steam engine, the Rocket was due to Gurney's steam blast.
    In July 1829 Gurney made a historic trip with his road locomotive. This was from London to Bath and back, which was accomplished at a speed of 18 mph (29 km/h) and was made at the instigation of the Quartermaster-General of the Army. So successful was the carriage that Sir Charles Dance started to run a regular service with it between Gloucester and Cheltenham. This ran for three months without accident, until Parliament introduced prohibitive taxation on all self-propelled vehicles. A House of Commons committee proposed that these should be abolished as inhibiting progress, but this was not done. Sir Goldsworthy petitioned Parliament on the harm being done to him, but nothing was done and the coming of the railways put the matter beyond consideration. He devoted his time to finding other uses for the steam-jet: it was used for extinguishing fires in coal-mines, some of which had been burning for many years; he developed a stove for the production of gas from oil and other fatty substances, intended for lighthouses; he was responsible for the heating and the lighting of both the old and the new Houses of Parliament. His evidence after a colliery explosion resulted in an Act of Parliament requiring all mines to have two shafts. He was knighted in 1863, the same year that he suffered a stroke which incapacitated him. He retired to his house at Reeds, near Bude, where he was looked after by his daughter, Anna.
    [br]
    Principal Honours and Distinctions
    Knighted 1863. Society of Arts Gold Medal.
    IMcN

    Biographical history of technology > Gurney, Sir Goldsworthy

  • 109 Perkins, Jacob

    [br]
    b. 9 July 1766 Newburyport, Massachusetts, USA
    d. 30 July 1849 London, England
    [br]
    American inventor of a nail-making machine and a method of printing banknotes, investigator of the use of steam at very high pressures.
    [br]
    Perkins's occupation was that of a gold-and silversmith; while he does not seem to have followed this after 1800, however, it gave him the skills in working metals which he would continue to employ in his inventions. He had been working in America for four years before he patented his nail-making machine in 1796. At the time there was a great shortage of nails because only hand-forged ones were available. By 1800, other people had followed his example and produced automatic nail-making machines, but in 1811 Perkins' improved machines were introduced to England by J.C. Dyer. Eventually Perkins had twenty-one American patents for a range of inventions in his name.
    In 1799 Perkins invented a system of engraving steel plates for printing banknotes, which became the foundation of modern siderographic work. It discouraged forging and was adopted by many banking houses, including the Federal Government when the Second United States Bank was inaugurated in 1816. This led Perkins to move to Philadelphia. In the intervening years, Perkins had improved his nail-making machine, invented a machine for graining morocco leather in 1809, a fire-engine in 1812, a letter-lock for bank vaults and improved methods of rolling out spoons in 1813, and improved armament and equipment for naval ships from 1812 to 1815.
    It was in Philadelphia that Perkins became interested in the steam engine, when he met Oliver Evans, who had pioneered the use of high-pressure steam. He became a member of the American Philosophical Society and conducted experiments on the compressibility of water before a committee of that society. Perkins claimed to have liquified air during his experiments in 1822 and, if so, was the real discoverer of the liquification of gases. In 1819 he came to England to demonstrate his forgery-proof system of printing banknotes, but the Bank of England was the only one which did not adopt his system.
    While in London, Perkins began to experiment with the highest steam pressures used up to that time and in 1822 took out his first of nineteen British patents. This was followed by another in 1823 for a 10 hp (7.5 kW) engine with only 2 in. (51 mm) bore, 12 in. (305 mm) stroke but a pressure of 500 psi (35 kg/cm2), for which he claimed exceptional economy. After 1826, Perkins abandoned his drum boiler for iron tubes and steam pressures of 1,500 psi (105 kg/cm2), but the materials would not withstand such pressures or temperatures for long. It was in that same year that he patented a form of uniflow cylinder that was later taken up by L.J. Todd. One of his engines ran for five days, continuously pumping water at St Katherine's docks, but Perkins could not raise more finance to continue his experiments.
    In 1823 one his high-pressure hot-water systems was installed to heat the Duke of Wellington's house at Stratfield Saye and it acquired a considerable vogue, being used by Sir John Soane, among others. In 1834 Perkins patented a compression ice-making apparatus, but it did not succeed commercially because ice was imported more cheaply from Norway as ballast for sailing ships. Perkins was often dubbed "the American inventor" because his inquisitive personality allied to his inventive ingenuity enabled him to solve so many mechanical challenges.
    [br]
    Further Reading
    Historical Society of Pennsylvania, 1943, biography which appeared previously as a shortened version in the Transactions of the Newcomen Society 24.
    D.Bathe and G.Bathe, 1943–5, "The contribution of Jacob Perkins to science and engineering", Transactions of the Newcomen Society 24.
    D.S.L.Cardwell, 1971, From Watt to Clausius. The Rise of Thermodynamics in the Early Industrial Age, London: Heinemann (includes comments on the importance of Perkins's steam engine).
    A.F.Dufton, 1940–1, "Early application of engineering to warming of buildings", Transactions of the Newcomen Society 21 (includes a note on Perkins's application of a high-pressure hot-water heating system).
    RLH

    Biographical history of technology > Perkins, Jacob

  • 110 Wankel, Felix

    [br]
    b. 13 August 1902 Lahr, Black Forest, Germany
    d. 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 Reading
    N.Faith, 1975, Wankel: The Curious Story Behind the Revolutionary Rotary Engine, New York: Stein \& Day.
    IMcN

    Biographical history of technology > Wankel, Felix

  • 111 power

    power n
    мощность
    accessory power system
    система энергопитания оборудования
    adjust idle power
    регулировать малый газ
    aft power nacelle
    хвостовая часть гондолы двигателя
    aircraft power reduction
    уменьшение мощности двигателей воздушного судна
    aircraft power supply
    бортовой источник электропитания
    asymmetric engines power
    асимметричная тяга двигателей
    at idle power
    на режиме малого газа
    attain the power
    достигать заданной мощности
    augmented power
    форсированный режим
    augment power
    форсировать мощность
    auxiliary power supply
    вспомогательный источник энергопитания
    auxiliary power unit
    вспомогательная силовая установка
    bearing power
    несущая способность
    best economy power
    оптимальный режим
    bus power failure
    отказ бортовой электрошины
    chop the power
    внезапно изменять режим
    climbing power
    мощность, необходимая для набора высоты
    come to takeoff power
    выходить на взлетный режим
    contingency power
    мощность на чрезвычайном режиме
    cruising power
    крейсерская мощность
    develop power
    развивать мощность
    draw power
    передавать мощность
    dry power
    мощность без впрыска воды
    electrical power source
    источник электропитания
    electric power cart
    электротележка
    emergency power supply
    аварийный источник энергопитания
    emergency power system
    система аварийного энергопитания
    equivalent shaft power
    эквивалентная мощность на валу
    excess power
    избыточная мощность
    external electrical power
    аэродромное электропитание
    external electrical power system
    система аэродромного электропитания
    external power connector
    разъем аэродромного питания
    external power not available
    аэродромное питание отсутствует
    external power receptacle
    разъем аэродромного питания
    external power relay
    реле включения внешнего питания
    flight idle power
    мощность на режиме полетного малого газа
    free power turbine
    свободная турбина
    full power conditions
    максимальный режим
    gain the power
    достигать заданной мощность
    gas turbine power plant
    газотурбинная силовая установка
    ground power unit
    аэродромный пусковой агрегат
    hydraulic power cylinder
    гидравлический силовой цилиндр
    idle power rating
    режим малого газа
    induced drag power
    мощность на преодоление аэродинамического сопротивления
    lifting power
    подъемная сила
    (lift force, lift, ascensional force, buoyancy) maximum continuous power
    номинальный режим
    move under own power
    двигаться за счет собственной тяги
    output power
    выходная мощность
    outside power unit
    внешний источник питания
    pneumatic power cylinder
    пневматический силовой цилиндр
    power augmentation
    форсирование мощности
    power augmentation control
    управление форсажем
    power calibration
    тарировка мощности
    power cylinder
    силовой цилиндр
    power fail relay
    реле сигнализации отказа питания
    power indicator
    указатель мощности
    power margin
    запас мощности
    power off
    убрать режим
    power output
    выходная мощность
    power patrol operation
    патрулирование линий электропередач с воздуха
    power plant
    силовая установка
    power recovery turbine
    турбина с приводом от выхлопных газов
    power reduction operation
    уменьшение мощности
    power reversal ejector
    отражатель в механизме реверса тяги
    power setting
    установка мощности
    (двигателя) power shaft
    вал привода
    power source
    генератор
    power spin
    штопор при работающих двигателях
    power stroke
    рабочий ход
    (поршня) power supply circuit
    цепь подачи питания
    power taking-off
    процесс отбора мощности
    power the bus
    включать шину
    power unit
    силовой агрегат
    profile drag power
    мощность на преодоление профильного сопротивления
    provide power
    выдавать мощность
    rated power
    номинальная мощность
    reheat power
    форсажный режим
    required power
    потребная мощность
    run at idle power
    работать на режиме малого газа
    secondary power supply
    резервный источник энергопитания
    set idle power
    выводить на режим малого газа
    set takeoff power
    устанавливать взлетный режим
    sound power
    звуковая мощность
    specific power
    удельная мощность
    standby power unit
    запасной агрегат
    starting on external power
    запуск от внешнего источника
    takeoff power
    взлетная мощность
    take off power to the shaft
    отбирать мощность на вал
    thrust power
    тяговая мощность
    transmission power input
    мощность, поступающая на вал трансмиссии
    transmit power
    передавать мощность
    with rated power flight
    полет на номинальном расчетном режиме

    English-Russian aviation dictionary > power

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