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1 pressurized area
1) Космонавтика: герметизированная зона, зона повышенного давления, отсек конструкции с повышенным давлением, отсек с повышенным давлением2) Авиационная медицина: гермоотсек -
2 pressurized area
Англо-русский словарь по авиационной медицине > pressurized area
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3 pressurized area
зона повышенного давления; гермоотсекEnglsh-Russian aviation and space dictionary > pressurized area
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4 area
площадь; участок; пространство; область, район, зона; поверхность"gold-plated" area of instrument panel — наиболее легко обозреваемый (лётчиком) участок приборной доски
area of high pressure — метео. область высокого давления, антициклон
area of low pressure — метео. область низкого давления, циклон
assembly and test area — ркт. сборочно-проверочная площадка
booster (engine) disposal area — район сброса [падения] стартовых двигателей [ускорителей]
booster (engine) impact area — район сброса [падения] стартовых двигателей [ускорителей]
disc area of main rotor — верт. площадь диска несущего винта
exhaust jet area — площадь выходного сечения сопла; площадь сечения струи истекающих газов
floor area between the ramps — площадь пола грузовой кабины между (передним и задним) грузовыми трапами
guidance and control area — ркт. площадка управления пуском и наведением
— fin area— VFR area -
5 system
система; установка; устройство; ркт. комплекс"see to land" system — система посадки с визуальным приземлением
A.S.I. system — система указателя воздушной скорости
ablating heat-protection system — аблирующая [абляционная] система тепловой защиты
ablating heat-shield system — аблирующая [абляционная] система тепловой защиты
active attitude control system — ксм. активная система ориентации
aft-end rocket ignition system — система воспламенения заряда с задней части РДТТ [со стороны сопла]
aircraft response sensing system — система измерений параметров, характеризующих поведение ЛА
air-inlet bypass door system — дв. система перепуска воздуха на входе
antiaircraft guided missile system — ракетная система ПВО; зенитный ракетный комплекс
antiaircraft guided weapons system — ракетная система ПВО; зенитный ракетный комплекс
attenuated intercept satellite rendez-vous system — система безударного соединения спутников на орбите
attitude and azimuth reference system — система измерения или индикации углов тангажа, крена и азимута
automatic departure prevention system — система автоматического предотвращения сваливания или вращения после сваливания
automatic drift kick-off system — система автоматического устранения угла упреждения сноса (перед приземлением)
automatic hovering control system — верт. система автостабилизации на висении
automatic indicating feathering system — автоматическая система флюгирования с индикацией отказа (двигателя)
automatic mixture-ratio control system — система автоматического регулирования состава (топливной) смеси
automatic pitch control system — автомат тангажа; автоматическая система продольного управления [управления по каналу тангажа]
B.L.C. high-lift system — система управления пограничным слоем для повышения подъёмной силы (крыла)
backpack life support system — ксм. ранцевая система жизнеобеспечения
beam-rider (control, guidance) system — ркт. система наведения по лучу
biowaste electric propulsion system — электрический двигатель, работающий на биологических отходах
buddy (refueling, tank) system — (подвесная) автономная система дозаправки топливом в полете
closed(-circuit, -cycle) system — замкнутая система, система с замкнутым контуром или циклом; система с обратной связью
Cooper-Harper pilot rating system — система баллов оценки ЛА лётчиком по Куперу — Харперу
deployable aerodynamic deceleration system — развёртываемая (в атмосфере) аэродинамическая тормозная система
depressurize the fuel system — стравливать избыточное давление (воздуха, газа) в топливной системе
driver gas heating system — аэрд. система подогрева толкающего газа
dry sump (lubrication) system — дв. система смазки с сухим картером [отстойником]
electrically powered hydraulic system — электронасосная гидросистема (в отличие от гидросистемы с насосами, приводимыми от двигателя)
exponential control flare system — система выравнивания с экспоненциальным управлением (перед приземлением)
flywheel attitude control system — ксм. инерционная система ориентации
gas-ejection attitude control system — ксм. газоструйная система ориентация
gas-jet attitude control system — ксм. газоструйная система ориентация
ground proximity extraction system — система извлечения грузов из самолёта, пролетающего на уровне земли
hot-air balloon water recovery system — система спасения путем посадки на воду с помощью баллонов, наполняемых горячими газами
hypersonic air data entry system — система для оценки аэродинамики тела, входящего в атмосферу планеты с гиперзвуковой скоростью
igh-temperature fatigue test system — установка для испытаний на выносливость при высоких температурах
interceptor (directing, vectoring) system — система наведения перехватчиков
ion electrical propulsion system — ксм. ионная двигательная установка
isotope-heated catalytic oxidizer system — система каталитического окислителя с нагревом от изотопного источника
jet vane actuation system — ркт. система привода газового руля
laminar flow pumping system — система насосов [компрессоров] для ламинаризации обтекания
launching range safety system — система безопасности ракетного полигона; система обеспечения безопасности космодрома
leading edge slat system — система выдвижных [отклоняемых] предкрылков
low-altitude parachute extraction system — система беспосадочного десантирования грузов с малых высот с использованием вытяжных парашютов
magnetic attitude control system — ксм. магнитная система ориентации
magnetically slaved compass system — курсовая система с магнитной коррекцией, гироиндукционная курсовая система
mass-expulsion attitude control system — система ориентации за счёт истечения массы (газа, жидкости)
mass-motion attitude control system — ксм. система ориентации за счёт перемещения масс
mass-shifting attitude control system — ксм. система ориентации за счёт перемещения масс
monopropellant rocket propulsion system — двигательная установка с ЖРД на унитарном [однокомпонентном] топливе
nucleonic propellant gauging and utilization system — система измерения и регулирования подачи топлива с использованием радиоактивных изотопов
open(-circuit, -cycle) system — открытая [незамкнутая] система, система с незамкнутым контуром или циклом; система без обратной связи
plenum chamber burning system — дв. система сжигания топлива во втором контуре
positioning system for the landing gear — система регулирования высоты шасси (при стоянке самолёта на земле)
radar altimeter low-altitude control system — система управления на малых высотах с использованием радиовысотомера
radar system for unmanned cooperative rendezvous in space — радиолокационная система для обеспечения встречи (на орбите) беспилотных кооперируемых КЛА
range and orbit determination system — система определения дальностей [расстояний] и орбит
real-time telemetry processing system — система обработки радиотелеметрических данных в реальном масштабе времени
recuperative cycle regenerable carbon dioxide removal system — система удаления углекислого газа с регенерацией поглотителя, работающая по рекуперативному циклу
rendezvous beacon and command system — маячно-командная система обеспечения встречи («а орбите)
satellite automatic terminal rendezvous and coupling system — автоматическая система сближения и стыковки спутников на орбите
Schuler tuned inertial navigation system — система инерциальной навигации на принципе маятника Шулера
sodium superoxide carbon dioxide removal system — система удаления углекислого газа с помощью надперекиси натрия
space shuttle separation system — система разделения ступеней челночного воздушно-космического аппарата
stellar-monitored astroinertial navigation guidance system — астроинерциальная система навигации и управления с астрокоррекцией
terminal control landing system — система управления посадкой по траектории, связанной с выбранной точкой приземления
terminal descent control system — ксм. система управления на конечном этапе спуска [снижения]
terminal guidance system for a satellite rendezvous — система управления на конечном участке траектории встречи спутников
test cell flow system — ркт. система питания (двигателя) топливом в огневом боксе
vectored thrust (propulsion) system — силовая установка с подъёмно-маршевым двигателем [двигателями]
water to oxygen system — ксм. система добывания кислорода из воды
wind tunnel data acquisition system — система регистрации (и обработки) данных при испытаниях в аэродинамической трубе
— D system -
6 tank
бак; резервуар; цистерна; бассейн; заправлять бакиcold gas storage tank — газовый аккумулятор; аккумулятор давления
combined oil tank and sump — маслобак, объединённый с отстойником
wing pylon mounted tank — бак, подвешиваемый под крылом на пилоне
— air tank— HTP tank— lox tank— oil tank— tip tank -
7 Piccard, Auguste
SUBJECT AREA: Aerospace[br]b. 28 January 1884 Basel, Switzerlandd. 24 March 1962 Lausanne, Switzerland[br]Swiss physicist who developed balloons to explore the upper atmosphere.[br]Auguste Piccard and his twin brother, Jean-Félix, studied together in Zurich and qualified as a physicist and a chemist, respectively. In 1913 they made a sixteen-hour balloon flight together, and in 1915 they joined the balloon section of the Swiss Army. Auguste moved to Brussels as Professor of Applied Physics in 1922 and he carried out research into cosmic radiation. He realized that he needed to ascend into the rarefied air of the stratosphere in order to study these cosmic rays. His target was 16,000 m (52,500 ft), but no one had ever ventured to this height before.Not surprisingly, Auguste Piccard turned to a balloon for his experiments, and during 1930 he designed a hydrogen balloon with a spherical gondola to house the crew. This gondola was sealed and pressurized with air, just as a modern airliner has a pressurized cabin. With Belgian finance, Piccard was able to build his balloon, and on 27 May 1931 he and his colleague Paul Kipfer reached a height of 15,781 m (51,775 ft). Although this was a world record and created great public interest, Piccard was a scientist rather than a record breaker, and as he needed further information he prepared for another ascent. His new gondola was equipped with radio and improved scientific equipment. On 18 August 1932 it ascended from Zurich and reached a height of 16,201 m (53,152 ft).Jean-Félix was also interested in high-altitude balloon flights and in 1934, together with his wife, he ascended through a clouded sky and reached 17,550m (57,579ft). Jean- Félix also tested a gondola lifted by ninety-eight small balloons, and he developed frost-resistant windows. Other balloonists followed with record-breaking high-altitude flights, but Auguste Piccard, aided by his son Jacques, turned his attention to exploration of the depths of the ocean.[br]Bibliography1950, Between Earth and Sky, London. 1956, In Balloon and Bathyscaph, London.Further ReadingD.H.de Vorkin, 1990, Race to the Stratosphere, Berlin (the first chapters describe the work of the Piccard twins).Pierre de Latil and Jean Rivoire, 1962, Le Professeur Auguste Piccard, France.JDS -
8 fuselage
фюзеляж, корпус (ЛА) -
9 Brayton, George Bailey
SUBJECT AREA: Steam and internal combustion engines[br]b. 1839 Rhode Island, USAd. 1892 Leeds, England[br]American engineer, inventor of gas and oil engines.[br]During the thirty years prior to his death, Brayton devoted considerable effort to the development of internal-combustion engines. He designed the first commercial gas engine of American origin in 1872. An oil-burning engine was produced in 1875. An aptitude for mechanical innovation became apparent whilst he was employed at the Exeter Machine Works, New Hampshire, where he developed a successful steam generator for use in domestic and industrial heating systems. Brayton engines were distinguished by the method of combustion. A pressurized air-fuel mixture from a reservoir was ignited as it entered the working cylinder—a precursor of the constant-pressure cycle. A further feature of these early engines was a rocking beam. There exist accounts of Brayton engines fitted into river craft, and of one in a carriage which operated for a few months in 1872–3. However, the appearance of the four-stroke Otto engine in 1876, together with technical problems associated with backfiring into the fuel reservoir, prevented large-scale acceptance of the Brayton engine. Although Thompson Sterne \& Co. of Glasgow became licensees, the engine failed to gain usage in Britain. A working model of Brayton's gas engine is exhibited in the Museum of History and Technology in Washington, DC.[br]Bibliography1872, US patent no. 125,166 (Brayton gas engine).July 1890, British patent no. 11,062 (oil engine; under patent agent W.R.Lake).Further ReadingD.Clerk, 1895, The Gas and Oil Engine, 6th edn, London, pp. 152–62 (includes a description and report of tests carried out on a Brayton engine).KAB -
10 Holly, Birdsill
SUBJECT AREA: Mechanical, pneumatic and hydraulic engineering[br]b. Auburn, New York, USAd. 27 April 1894 Lockport, New York, USA[br]American inventor of water-pumping machinery and a steam heating system.[br]Holly was educated in mechanics and millwrighting work. He was an indefatigable inventor and took out over 150 patents for his ideas. He became Superintendent and later Proprietor of a millwrighting shop in Uniontown, Pennsylvania. Then at Seneca Falls, New York, he began manufacturing hydraulic machinery with the firm of Silsby, Race \& Holly. He made the Silsby fire-engine famous through his invention in 1852 of a rotary pump which was later developed into a steam fire pump. In 1866 he introduced at Lockport, New York, a pressurized water-supply system using a pump rather than an elevated reservoir or standpipe. While this installation at Lockport was powered by a water-wheel, a second one in Dunkirk, New York, used steam-driven pumps, which had a significant effect on the history of steam pumping engines.[br]Further ReadingObituary, 1894, Engineering Record 29.Obituary, 1894, Iron Age 53.I.McNeil (ed.), 1990, An Encyclopaedia of the History of Technology, London: Routledge (mentions his work on water supply).RLH -
11 Meusnier, Jean Baptiste Marie
SUBJECT AREA: Aerospace[br]b. 1754 Tours, Franced. 1793 Mainz, Germany[br]French designer of the "dirigible balloon" (airship).[br]Just a few days after the first balloon flight by the relatively primitive Montgolfier hot-air balloon, a design for a sophisticated steerable or "dirigible" balloon was proposed by a young French army officer. On 3 December 1783, Lieutenant (later General) Jean Baptiste Marie Meusnier of the Corps of Engineers presented to the Académie des Sciences a paper entitled Mémoire sur l'équilibre des machines aérostatiques. This outlined Meusnier's ideas and so impressed the learned members of the Academy that they commissioned him to make a more complete study. This was published in 1784 and contained sixteen water-colour drawings of the proposed airship, which are preserved by the Musée de l'Air in Paris.Meusnier's "machine aérostatique" was ellipsoidal in shape, in contrast to those of his unsuccessful contemporaries who tried to make spherical balloons steerable, often using oars for propulsion. Meusnier's proposed airship was 79.2 m (260 ft) long with the crew in a slim boat slung below the envelope (in case of a landing on water); it was steered by a large sail-like rudder at the rear end. Between the envelope and the boat were three propellers, which were to be manually driven as there was no suitable engine available; this was the first design for a propeller-driven aircraft. The most important innovation was a ballonnet, a balloon within the main envelope that was pressurized with air supplied by bellows in the boat. Varying the amount of air in the ballonnet would compensate for changes in the volume of hydrogen gas in the main envelope when the airship changed altitude. The ballonnet would also help to maintain the external shape of the main envelope.General Meusnier was killed in action in 1793 and it was almost one hundred years from the date of his publication that his idea of ballonnets was put into practice, by Dupuy de Lome in 1872, and later by Renard and Krebs.[br]Bibliography1784, Mémoire sur l'équilibre des machines aérostatiques, Paris; repub. Paris: Musée de l'Air.Further ReadingL.T.C.Rolt, 1966, The Aeronauts, London (paperback 1985). Basil Clarke, 1961, The History of Airships, London.JDSBiographical history of technology > Meusnier, Jean Baptiste Marie
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12 Priestman, William Dent
SUBJECT AREA: Steam and internal combustion engines[br]b. 23 August 1847 Sutton, Hull, Englandd. 7 September 1936 Hull, England[br]English oil engine pioneer.[br]William was the second son and one of eleven children of Samuel Priestman, who had moved to Hull after retiring as a corn miller in Kirkstall, Leeds, and who in retirement had become a director of the North Eastern Railway Company. The family were strict Quakers, so William was sent to the Quaker School in Bootham, York. He left school at the age of 17 to start an engineering apprenticeship at the Humber Iron Works, but this company failed so the apprenticeship was continued with the North Eastern Railway, Gateshead. In 1869 he joined the hydraulics department of Sir William Armstrong \& Company, Newcastle upon Tyne, but after a year there his father financed him in business at a small, run down works, the Holderness Foundry, Hull. He was soon joined by his brother, Samuel, their main business being the manufacture of dredging equipment (grabs), cranes and winches. In the late 1870s William became interested in internal combustion engines. He took a sublicence to manufacture petrol engines to the patents of Eugène Etève of Paris from the British licensees, Moll and Dando. These engines operated in a similar manner to the non-compression gas engines of Lenoir. Failure to make the two-stroke version of this engine work satisfactorily forced him to pay royalties to Crossley Bros, the British licensees of the Otto four-stroke patents.Fear of the dangers of petrol as a fuel, reflected by the associated very high insurance premiums, led William to experiment with the use of lamp oil as an engine fuel. His first of many patents was for a vaporizer. This was in 1885, well before Ackroyd Stuart. What distinguished the Priestman engine was the provision of an air pump which pressurized the fuel tank, outlets at the top and bottom of which led to a fuel atomizer injecting continuously into a vaporizing chamber heated by the exhaust gases. A spring-loaded inlet valve connected the chamber to the atmosphere, with the inlet valve proper between the chamber and the working cylinder being camoperated. A plug valve in the fuel line and a butterfly valve at the inlet to the chamber were operated, via a linkage, by the speed governor; this is believed to be the first use of this method of control. It was found that vaporization was only partly achieved, the higher fractions of the fuel condensing on the cylinder walls. A virtue was made of this as it provided vital lubrication. A starting system had to be provided, this comprising a lamp for preheating the vaporizing chamber and a hand pump for pressurizing the fuel tank.Engines of 2–10 hp (1.5–7.5 kW) were exhibited to the press in 1886; of these, a vertical engine was installed in a tram car and one of the horizontals in a motor dray. In 1888, engines were shown publicly at the Royal Agricultural Show, while in 1890 two-cylinder vertical marine engines were introduced in sizes from 2 to 10 hp (1.5–7.5 kW), and later double-acting ones up to some 60 hp (45 kW). First, clutch and gearbox reversing was used, but reversing propellers were fitted later (Priestman patent of 1892). In the same year a factory was established in Philadelphia, USA, where engines in the range 5–20 hp (3.7–15 kW) were made. Construction was radically different from that of the previous ones, the bosses of the twin flywheels acting as crank discs with the main bearings on the outside.On independent test in 1892, a Priestman engine achieved a full-load brake thermal efficiency of some 14 per cent, a very creditable figure for a compression ratio limited to under 3:1 by detonation problems. However, efficiency at low loads fell off seriously owing to the throttle governing, and the engines were heavy, complex and expensive compared with the competition.Decline in sales of dredging equipment and bad debts forced the firm into insolvency in 1895 and receivers took over. A new company was formed, the brothers being excluded. However, they were able to attend board meetings, but to exert no influence. Engine activities ceased in about 1904 after over 1,000 engines had been made. It is probable that the Quaker ethics of the brothers were out of place in a business that was becoming increasingly cut-throat. William spent the rest of his long life serving others.[br]Further ReadingC.Lyle Cummins, 1976, Internal Fire, Carnot Press.C.Lyle Cummins and J.D.Priestman, 1985, "William Dent Priestman, oil engine pioneer and inventor: his engine patents 1885–1901", Proceedings of the Institution ofMechanical Engineers 199:133.Anthony Harcombe, 1977, "Priestman's oil engine", Stationary Engine Magazine 42 (August).JBBiographical history of technology > Priestman, William Dent
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13 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
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