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1 aerospace test wing
1) Военный термин: авиакрыло обеспечения воздушно-космических испытаний2) Космонавтика: экспериментальное воздушно-космическое крыло -
2 aerospace test wing
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3 aerospace test wing
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4 wing
авиационное крыло, авиакрыло ( организационная единица) ; фланг; крыло; pl. крылья ( нагрудный знак летного состава) ; отделение ( учебного заведения)— air wing -
5 vehicle
(авто)транспортное средство; летательный аппарат; ракета, см. тж. aircraft, missile, spacecraft; растворитель, связующее веществоlimited power space vehicle — КЛА с силовой установкой ограниченной тяги [ограниченного ресурса работы]
multipurpose manned entry space vehicle — многоцелевой пилотируемый КЛА, рассчитанный на вход в атмосферу
nonspinning reentry space vehicle — КЛА, нестабилизируемый вращением при входе в атмосферу
nuclear(-powered, -propelled) vehicle — ЛА с ядерной силовой [двигательной] установкой
pogo-stick type lunar surface vehicle — аппарат с пружинным шестом для передвижения по лунной поверхности
space shuttle booster vehicle — ускоритель [стартовый двигатель] челночного воздушно-космического аппарата
spinning reentry space vehicle — КЛА, стабилизируемый вращением при входе в атмосферу
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6 Phillips, Horatio Frederick
SUBJECT AREA: Aerospace[br]b. 2 February 1845 London, Englandd. 15 July 1926 Hampshire, England[br]English aerodynamicist whose cambered two-surface wing sections provided the foundations for aerofoil design.[br]At the age of 19, Phillips developed an interest in flight and constructed models with lightweight engines. He spent a large amount of time and money over many years, carrying out practical research into the science of aerodynamics. In the early 1880s he built a wind tunnel with a working section of 15 in. by 10 in. (38 cm by 25 cm). Air was sucked through the working section by an adaptation of the steam injector used in boilers and invented by Henry Giffard, the airship pioneer. Phillips tested aerofoils based on the cross-section of bird's wings, with a greater curvature on the upper surface than the lower. He measured the lift and drag and showed that the major component of lift came from suction on the upper surface, rather than pressure on the lower. He took out patents for his aerofoil sections in 1884 and 1891. In addition to his wind-tunnel test, Phillips tested his wing sections on a whirling arm, as used earlier by Cayley, Wenham and Lilienthal. After a series of tests using an arm of 15 ft (4.57 m) radius, Phillips built a massive whirling arm driven by a steam engine. His test pieces were mounted on the end of the arm, which had a radius of 50 ft (15.24 m), giving them a linear speed of 70 mph (113 km/h). By 1893 Phillips was ready to put his theories to a more practical test, so he built a large model aircraft driven by a steam engine and tethered to run round a circular track. It had a wing span of 19 ft (5.79 m), but it had fifty wings, one above the other. These wings were only 10 in. (25 cm) wide and mounted in a frame, so it looked rather like a Venetian blind. At 40 mph (64 km/h) it lifted off the track. In 1904 Phillips built a full-size multi-wing aeroplane with twenty wings which just lifted off the ground but did not fly. He built another multi-wing machine in 1907, this time with four Venetian blind' frames in tandem, giving it two hundred wings! Phillips made a short flight of almost 500 ft (152 m) which could be claimed to be the first powered aeroplane flight in England by an Englishman. He retired from flying at the age of 62.[br]Bibliography1900, "Mechanical flight and matters relating thereto", Engineering (reprint).1891–3, "On the sustentation of weight by mechanical flight", Aeronautical Society of Great Britain 23rd Report.Further ReadingJ.Laurence Pritchard, 1957, "The dawn of aerodynamics", Journal of the Royal Aeronautical Society (March) (good descriptions of Phillips's early work and his wind tunnel).J.E.Hodgson, 1924, The History of Aeronautics in Great Britain, London.F.W.Brearey, 1891–3, "Remarks on experiments made by Horatio Phillips", Aeronautical Society of Great Britain 23rd Report.JDSBiographical history of technology > Phillips, Horatio Frederick
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7 center
центр; середина; pl. расстояние между центрами [осями]; центрировать; ставить в нейтральное положениеair combat operations center — Бр. центр управления боевыми действиями авиации
air command operations center — Бр. центр управления боевыми действиями авиации
air defense direction center — РЛС [пункт] наведения средств ПВО
air proving ground center — центр испытаний авиационной техники; испытательный центр ВВС
airborne battlefield command and control center — воздушный командный пункт управления боевыми действиями тактической авиации
Arnold Engineering Development center — исследовательский инженерный центр ВВС им. Арнольда
center of the glide slope (beam) — ось [равносигнальная зона] глиссадного луча
control and reporting center — центр управления [наведения] и оповещения
integrated mission control center — объединённый центр управления полётами; координационно-вычислительный центр обеспечения полётов КЛА
missile (fire) control center — центральный ракетный пост (подводной лодки); центральный пост управления пуском ракет
propellant center of gravity — ркт. центр тяжести (заправленного) топлива
Royal Air Force Training center — Бр. учебный центр ВВС
tactical air direction center — центр наведения самолётов тактической авиации; центр наведения авиации поддержки
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8 Dunne, John William
SUBJECT AREA: Aerospace[br]b. 2 December 1875 Co. Kildare, Irelandd. 24 August 1949 Oxfordshire, England[br]Irish inventor who pioneered tailless aircraft designed to be inherently stable.[br]After serving in the British Army during the Boer War. Dunne returned home convinced that aeroplanes would be more suitable than balloons for reconnaissance work. He built models to test his ideas for a tailless design based on the winged seed of a Javanese climbing plant. In 1906 Dunne joined the staff of the Balloon Factory at Farnborough, where the Superintendent, Colonel J.E.Capper, was also interested in manned kites and aeroplanes. Since 1904 the colourful American "Colonel" S.F. Cody had been experimenting at Farnborough with manned kites, and in 1908 his "British Army Dirigible No. 1" made the first powered flight in Britain. Dunne's first swept-wing tailless glider was ready to fly in the spring of 1907, but it was deemed to be a military secret and flying it at Farnborough would be too public. Dunne, Colonel Capper and a team of army engineers took the glider to a remote site at Blair Atholl in Scotland for its test flights. It was not a great success, although it attracted snoopers, with the result that it was camouflaged. Powered versions made short hops in 1908, but then the War Office withdrew its support. Dunne and his associates set up a syndicate to continue the development of a new tailless aeroplane, the D 5; this was built by Short Brothers (see Short, Hugh Oswald) and flew successfully in 1910. It had combined elevators and ailerons on the wing tips (or elevons as they are now called when fitted to modern delta-winged aircraft). In 1913 an improved version of the D 5 was demonstrated in France, where the pilot left his cockpit and walked along the wing in flight. Dunne had proved his point and designed a stable aircraft, but his health was suffering and he retired. During the First World War, however, it was soon learned that military aircraft needed to be manoeuvrable rather than stable.[br]Bibliography1913, "The theory of the Dunne aeroplane", Journal of the Royal Aeronautical Society (April).After he left aviation, Dunne became well known for his writings on the nature of the universe and the interpretation of dreams. His best known-work was An ExperimentWith Time (1927; and reprints).Further ReadingP.B.Walker, 1971, Early Aviation at Farnborough, Vol. I, London; 1974, Vol. II (provides a detailed account of Dunne's early work; Vol. II is the more relevant).P.Lewis, 1962, British Air craft 1809–1914, London (for details of Dunne's aircraft).JDS -
9 pilot
лётчик, пилот; первый лётчик, командир ЛА; система управления; автопилот; пилотировать, вести самолёт; ведущий, головной, начальный; пусковой; контрольный; вспомогательный; пилотский, связанный с лётчикомaerial maneuver demonstration pilot — лётчик — мастер фигурного пилотажа
pilot of superior ability — лётчик высшего класса [высшей квалификации]
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10 Focke, E.H.Heinrich
SUBJECT AREA: Aerospace[br]b. October 1890 Bremen, Germanyd. February 1979 Bremen, Germany[br]German aircraft designer who was responsible for the first practical helicopter, in 1936.[br]Between 1911 and 1914 Heinrich Focke and Georg Wulf built a monoplane and some years later, in 1924, they founded the Focke-Wulf company. They designed and built a variety of civil and military aircraft including the F 19Ente, a tail-first design of 1927. This canard layout was thought to be safer than conventional designs but, unfortunately, it crashed, killing Wulf. Around 1930 Focke became interested in rotary-wing aircraft, and in 1931 he set up a company with Gerd Achgelis to conduct research in this field. The Focke-Wulf company took out a licence to build Cierva autogiros. Focke designed an improved autogiro, the Fw 186, which flew in 1938; it was entered for a military competition, but it was beaten by a fixed-wing aircraft, the Fieseler Storch. In May 1935 Focke resigned from Focke-Wulf to concentrate on helicopter development with the Focke-Achgelis company. His first design was the Fa 61 helicopter, which utilized the fuselage and engine of a conventional aeroplane but instead of wings had two out-riggers, each carrying a rotor. The engine drove these rotors in opposite directions to counteract the adverse torque effect (with a single rotor the fuselage tends to rotate in the opposite direction to the rotor). Following its first flight on 26 June 1936, the Fa 61 went on to break several world records. However, it attracted more public attention when it was flown inside the huge Deutschlandhalle in Berlin by the famous female test pilot Hanna Reitsch in February 1938. Focke continued to develop his helicopter projects for the Focke-Achgelis company and produced the Fa 223 Drache in 1940. This used twin contra-rotating rotors, like the Fa 61, but could carry six people. Its production was hampered by allied bombing of the factory. During the Second World War Focke- Achgelis also produced a rotor kite which could be towed behind a U-boat to provide a flying "crow's nest", as well as designs for an advanced convertiplane (part aeroplane, part helicopter). After the war, Focke worked in France, the Netherlands and Brazil, then in 1954 he became Professor of Aeroplane and Helicopter Design at the University of Stuttgart.[br]Principal Honours and DistinctionsWissenschaftliche, Gesellschaft für Luftfahrt Lilienthal Medal, Prandtl-Ring.Bibliography1965, "German thinking on rotary-wing development", Journal of the Royal Aeronautical Society, (May).Further ReadingW.Gunston and J.Batchelor, 1977, Helicopters 1900–1960, London.J.R.Smith, 1973, Focke-Wulf: An Aircraft Album, London (primarily a picture book). R.N.Liptrot, 1948, Rotating Wing Activities in Germany during the Period 1939–45, London.K.von Gersdorff and K.Knobling, 1982, Hubschrauber und Tragschrauber, Munich (a more recent publication, in German).JDS -
11 Lilienthal, Otto
SUBJECT AREA: Aerospace[br]b. 23 May 1848 Anklam, Prussia (now Germany)d. 10 August 1896 Berlin, Germany[br]German glider pioneer, the first to make a controlled flight using wings.[br]Otto Lilienthal and his brother Gustav developed an interest in flying as boys, when they studied birds in flight, built models and even tried to fit wings to their arms. Gustav went on to become a successful architect while Otto, after a brilliant scholastic career, became a mechanical engineer. Otto was able to devote his spare time to the problems of flight, and Gustav helped when his work allowed. They considered manpowered and mechanically powered projects, but neither looked hopeful so they turned to gliding. Otto published his research work in a book, Bird Flight as a Basis for Aviation. By 1889 Otto Lilienthal was ready to test his first full-size gliders. No. 1 and No. 2 were not successful, but No. 3, built in 1891, showed promise. He gradually improved his designs and his launching sites as he gained experience. To take off he ran downhill carrying his hang-glider until it became airborne, then he controlled it by swinging his body weight in the appropriate direction. He even built an artificial mound near Berlin so that he could take off into the wind whichever way it was blowing.In all, Lilienthal built some eighteen gliders with various wing shapes, including biplanes. By 1895 he was planning movable control surfaces (operated by head movement) and a powered version using a carbonic acid gas motor. Unfortunately, Lilienthal crashed and died of his injuries before these ideas could be tested. In all, he made over two thousand flights covering distances up to 300 m (300 yds. Many of these flights were recorded on photographs and so generated an interest in flying. Lilienthal's achievements also encouraged other pioneers, such as Percy Pilcher in Britain, and Octave Chanute and the Wright brothers in the United States.[br]Bibliography1899, Der Vogelflug als Grundlage der Fliegekunst, Berlin, reprinted c. 1977; repub. in English, 1911, as Bird Flight as a Basis for Aviation.Further ReadingCharles H.Gibbs-Smith, 1985, Aviation, London (provides a detailed account of Lilienthal's gliders).P.H.Lilienthal, 1978, "Die Lilienthal Gebrüder", Aerospace (Royal Aeronautical Society) (January) (for more personal information)."The Lilienthal and Pilcher gliders compared", Flight (1 January 1910 and 8 January 1910) (for details about and plans of a typical Lilienthal glider).JDS -
12 vehicle
средство передвижения; транспортное средство; подвижное средство; боевая машина, БМ; летательный аппарат, ЛА; см. тж. car, truckair cushion landing vehicle, assault — десантно-высадочное средство на воздушной подушке; десантный АВП
armored cavalry (assault) vehicle — бронированная разведывательная машина, БРМ
armoured vehicle, RE — Бр. саперный танк
assault vehicle, RE — Бр. десантно-высадочное средство инженерных войск
AT (guided) missile launch vehicle — БМ для пуска ПТУР; самоходный ПТРК
C2 vehicle — машина управления (войсками); (командно-) штабная машина
double air cushion vehicle, assault — десантный корабль на двойной воздушной подушке
landing vehicle, assault — десантно-высадочное средство; плавающий БТР на воздушной подушке
landing vehicle, hydrofoil — десантный КПК
landing vehicle, tank, engineer — десантный саперный танк
landing vehicle, track, armored — десантный (плавающий) гусеничный БТР
landing vehicle, track, covered — крытый десантный плавающий гусеничный транспортер
landing vehicle, tracked, engineer — десант ная гусеничная инженерная машина
landing vehicle, tracked, heavy — тяжелый десантный плавающий гусеничный транспортер
landing vehicle, tracked, howitzer — десантная гусеничная гаубичная СУ
landing vehicle, tracked, personnel — десантная гусеничная машина для ЛС
landing vehicle, tracked, recovery — десантная гусеничная ремонтно-эвакуационная машина
mine-clearing vehicle, flail-type — танк [танковый тягач] с бойковым тралом
mine-clearing vehicle, plow-pushing — танк [танковый тягач] с передним плужным минным тралом
mine-clearing vehicle, roller — танк [танковый тягач] с Катковым минным тралом
terminally guided (maneuvering) reentry vehicle — ркт. маневрирующая ГЧ с наведением на конечном участке траектории
— administrative use vehicle— bacteriological bomb vehicle— boost-glide reentry vehicle— flamethrower vehicle— ground-supported vehicle— launcher vehicle— logistical air vehicle— logistical vehicle— maintenance assistance vehicle— MarineCorps landing vehicle— oversize load vehicle— ship-to-shore assault vehicle— support armored vehicle— topographic surveying vehicle— troop-carryingair vehicle— wader-swimmer combat vehicle -
13 Flettner, Anton
SUBJECT AREA: Aerospace[br]b. 1 November 1885 Eddersheim-am-Main, Germanyd. 29 December 1961 New York, USA[br]German engineer and inventor who produced a practical helicopter for the German navy in 1940.[br]Anton Flettner was an engineer with a great interest in hydraulics and aerodynamics. At the beginning of the First World War Flettner was recruited by Zeppelin to investigate the possibility of radio-controlled airships as guided missiles. In 1915 he constructed a small radio-controlled tank equipped to cut barbed-wire defences; the military experts rejected it, but he was engaged to investigate radio-controlled pilotless aircraft and he invented a servo-control device to assist their control systems. These servo-controls, or trim tabs, were used on large German bombers towards the end of the war. In 1924 he invented a sailing ship powered by rotating cylinders, but although one of these crossed the Atlantic they were never a commercial success. He also invented a windmill and a marine rudder. In the late 1920s Flettner turned his attention to rotating-wing aircraft, and in 1931 he built a helicopter with small engines mounted on the rotor blades. Progress was slow and it was abandoned after being damaged during testing in 1934. An autogiro followed in 1936, but it caught fire on a test flight and was destroyed. Undeterred, Flettner continued his development work on helicopters and in 1937 produced the Fl 185, which had a single rotor to provide lift and two propellers on outriggers to combat the torque and provide forward thrust. This arrangement was not a great success, so he turned to twin contra-rotating rotors, as used by his rival Focke, but broke new ground by using intermeshing rotors to make a more compact machine. The Fl 265 with its "egg-beater" rotors was ordered by the German navy in 1938 and flew the following year. After exhaustive testing, Flettner improved his design and produced the two-seater Fl 282 Kolibri, which flew in 1940 and became the only helicopter to be used operationally during the Second World War.After the war, Flettner moved to the United States where his intermeshing-rotor idea was developed by the Kaman Aircraft Corporation.[br]Bibliography1926, Mein Weg zum Rotor, Leipzig; also published as The Story of the Rotor, New York (describes his early work with rotors—i.e. cylinders).Further ReadingW.Gunston and J.Batchelor, 1977, Helicopters 1900–1960, London.R.N.Liptrot, 1948, Rotating Wing Activities in Germany during the Period 1939–45, London.K.von Gersdorff and K.Knobling, 1982, Hubschrauber und Tragschrauber, Munich (a more recent publication, in German).JDS -
14 Stringfellow, John
SUBJECT AREA: Aerospace[br]b. 6 December 1799 Sheffield, Englandd. 13 December 1883 Chard, England[br]English inventor and builder of a series of experimental model aeroplanes.[br]After serving an apprenticeship in the lace industry, Stringfellow left Nottingham in about 1820 and moved to Chard in Somerset, where he set up his own business. He had wide interests such as photography, politics, and the use of electricity for medical treatment. Stringfellow met William Samuel Henson, who also lived in Chard and was involved in lacemaking, and became interested in his "aerial steam carriage" of 1842–3. When support for this project foundered, Henson and Stringfellow drew up an agreement "Whereas it is intended to construct a model of an Aerial Machine". They built a large model with a wing span of 20 ft (6 m) and powered by a steam engine, which was probably the work of Stringfellow. The model was tested on a hillside near Chard, often at night to avoid publicity, but despite many attempts it never made a successful flight. At this point Henson emigrated to the United States. From 1848 Stringfellow continued to experiment with models of his own design, starting with one with a wing span of 10 ft (3m). He decided to test it in a disused lace factory, rather than in the open air. Stringfellow fitted a horizontal wire which supported the model as it gained speed prior to free flight. Unfortunately, neither this nor later models made a sustained flight, despite Stringfellow's efficient lightweight steam engine. For many years Stringfellow abandoned his aeronautical experiments, then in 1866 when the (Royal) Aeronautical Society was founded, his interest was revived. He built a steam-powered triplane, which was demonstrated "flying" along a wire at the world's first Aeronautical Exhibition, held at Crystal Palace, London, in 1868. Stringfellow also received a cash prize for one of his engines, which was the lightest practical power unit at the Exhibition. Although Stringfellow's models never achieved a really successful flight, his designs showed the way for others to follow. Several of his models are preserved in the Science Museum in London.[br]Principal Honours and DistinctionsMember of the (Royal) Aeronautical Society 1868.BibliographyMany of Stringfellow's letters and papers are held by the Royal Aeronautical Society, London.Further ReadingHarald Penrose, 1988, An Ancient Air: A Biography of John Stringfellow, Shrewsbury. A.M.Balantyne and J.Laurence Pritchard, 1956, "The lives and work of William Samuel Henson and John Stringfellow", Journal of the Royal Aeronautical Society (June) (an attempt to analyse conflicting evidence).M.J.B.Davy, 1931, Henson and Stringfellow, London (an earlier work with excellent drawings from Henson's patent)."The aeronautical work of John Stringfellow, with some account of W.S.Henson", Aeronau-tical Classics No. 5 (written by John Stringfellow's son and held by the Royal Aeronautical Society in London).JDS -
15 community
(научно-техническое) сообщество; специалисты; кадры специалистовaeronautical communityaerospace communityAEW communityaircraft communityattack communityaviation communitycontrol communityengineering communityfighter communityfixed-wing communityflying qualities communityR&D communityresearch communityscientific communitysimulation communitystructural communitysurvivability communitytechnological communitytest community -
16 capability
способность; возможность; производительность, мощность1-hour «turn-around» capability — возможность осуществления одночасового цикла разгрузки, загрузки и обслуживания самолёта (с момента посадки до взлета)
all-weather weapons delivery capability — способность доставки оружия (к цели) в любых метеорологических условиях
capability of on/off operation — ркт. способность к повторному запуску (двигателя)
hydraulic system rate capability — обеспечиваемая гидросистемой угловая скорость перемещения (напр. руля)
look down — shoot down capability — способность атаковать самолёт сверху с задней полусферы
sustained Mach 2.3 capability — способность совершать установившийся полет с числом М-2,3
zero altitude (escape) capability — возможность покидания (самолёта) с земли [с нулевой высоты]
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17 Maxim, Sir Hiram Stevens
[br]b. 5 February 1840 Brockway's Mills, Maine, USAd. 24 November 1916 Streatham, London, England[br]American (naturalized British) inventor; designer of the first fully automatic machine gun and of an experimental steam-powered aircraft.[br]Maxim was born the son of a pioneer farmer who later became a wood turner. Young Maxim was first apprenticed to a carriage maker and then embarked on a succession of jobs before joining his uncle in his engineering firm in Massachusetts in 1864. As a young man he gained a reputation as a boxer, but it was his uncle who first identified and encouraged Hiram's latent talent for invention.It was not, however, until 1878, when Maxim joined the first electric-light company to be established in the USA, as its Chief Engineer, that he began to make a name for himself. He developed an improved light filament and his electric pressure regulator not only won a prize at the first International Electrical Exhibition, held in Paris in 1881, but also resulted in his being made a Chevalier de la Légion d'honneur. While in Europe he was advised that weapons development was a more lucrative field than electricity; consequently, he moved to England and established a small laboratory at Hatton Garden, London. He began by investigating improvements to the Gatling gun in order to produce a weapon with a faster rate of fire and which was more accurate. In 1883, by adapting a Winchester carbine, he successfully produced a semi-automatic weapon, which used the recoil to cock the gun automatically after firing. The following year he took this concept a stage further and produced a fully automatic belt-fed weapon. The recoil drove barrel and breechblock to the vent. The barrel then halted, while the breechblock, now unlocked from the former, continued rearwards, extracting the spent case and recocking the firing mechanism. The return spring, which it had been compressing, then drove the breechblock forward again, chambering the next round, which had been fed from the belt, as it did so. Keeping the trigger pressed enabled the gun to continue firing until the belt was expended. The Maxim gun, as it became known, was adopted by almost every army within the decade, and was to remain in service for nearly fifty years. Maxim himself joined forces with the large British armaments firm of Vickers, and the Vickers machine gun, which served the British Army during two world wars, was merely a refined version of the Maxim gun.Maxim's interests continued to occupy several fields of technology, including flight. In 1891 he took out a patent for a steam-powered aeroplane fitted with a pendulous gyroscopic stabilizer which would maintain the pitch of the aeroplane at any desired inclination (basically, a simple autopilot). Maxim decided to test the relationship between power, thrust and lift before moving on to stability and control. He designed a lightweight steam-engine which developed 180 hp (135 kW) and drove a propeller measuring 17 ft 10 in. (5.44 m) in diameter. He fitted two of these engines into his huge flying machine testrig, which needed a wing span of 104 ft (31.7 m) to generate enough lift to overcome a total weight of 4 tons. The machine was not designed for free flight, but ran on one set of rails with a second set to prevent it rising more than about 2 ft (61 cm). At Baldwyn's Park in Kent on 31 July 1894 the huge machine, carrying Maxim and his crew, reached a speed of 42 mph (67.6 km/h) and lifted off its rails. Unfortunately, one of the restraining axles broke and the machine was extensively damaged. Although it was subsequently repaired and further trials carried out, these experiments were very expensive. Maxim eventually abandoned the flying machine and did not develop his idea for a stabilizer, turning instead to other projects. At the age of almost 70 he returned to the problems of flight and designed a biplane with a petrol engine: it was built in 1910 but never left the ground.In all, Maxim registered 122 US and 149 British patents on objects ranging from mousetraps to automatic spindles. Included among them was a 1901 patent for a foot-operated suction cleaner. In 1900 he became a British subject and he was knighted the following year. He remained a larger-than-life figure, both physically and in character, until the end of his life.[br]Principal Honours and DistinctionsChevalier de la Légion d'Honneur 1881. Knighted 1901.Bibliography1908, Natural and Artificial Flight, London. 1915, My Life, London: Methuen (autobiography).Further ReadingObituary, 1916, Engineer (1 December).Obituary, 1916, Engineering (1 December).P.F.Mottelay, 1920, The Life and Work of Sir Hiram Maxim, London and New York: John Lane.Dictionary of National Biography, 1912–1921, 1927, Oxford: Oxford University Press.See also: Pilcher, Percy SinclairCM / JDSBiographical history of technology > Maxim, Sir Hiram Stevens
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18 Wright, Wilbur
SUBJECT AREA: Aerospace[br]b. 16 April 1867 Millville, Indiana, USAd. 30 May 1912 Dayton, Ohio, USA[br]American co-inventor, with his brother Orville Wright (b. 19 August 1871 Dayton, Ohio, USA; d. 30 January 1948 Dayton, Ohio, USA), of the first powered aeroplane capable of sustained, controlled flight.[br]Wilbur and Orville designed and built bicycles in Dayton, Ohio. In the 1890s they developed an interest in flying which led them to study the experiments of gliding pioneers such as Otto Lilienthal in Germany, and their fellow American Octave Chanute. The Wrights were very methodical and tackled the many problems stage by stage. First, they developed a method of controlling a glider using movable control surfaces, instead of weight-shifting as used in the early hand-gliders. They built a wind tunnel to test their wing sections and by 1902 they had produced a controllable glider. Next they needed a petrol engine, and when they could not find one to suit their needs they designed and built one themselves.On 17 December 1903 their Flyer was ready and Orville made the first short flight of 12 seconds; Wilbur followed with a 59-second flight covering 853 ft (260 m). An improved design, Flyer II, followed in 1904 and made about eighty flights, including circuits and simple ma-noeuvres. In 1905 Flyer III made several long flights, including one of 38 minutes covering 24½ miles (39 km). Most of the Wrights' flying was carried out in secret to protect their patents, so their achievements received little publicity. For a period of two and a half years they did not fly, but they worked to improve their Flyer and to negotiate terms for the sale of their invention to various governments and commercial syndi-cates.In 1908 the Wright Model A appeared, and when Wilbur demonstrated it in France he astounded the European aviators by making several flights lasting more than one hour and one of 2 hours 20 minutes. Considerable numbers of the Model A were built, but the European designers rapidly caught up and overtook the Wrights. The Wright brothers became involved in several legal battles to protect their patents: one of these, with Glenn Curtiss, went on for many years. Wilbur died of typhoid fever in 1912. Orville sold his interest in the Wright Company in 1915, but retained an interest in aeronautical research and lived on to see an aeroplane fly faster than the speed of sound.[br]Principal Honours and DistinctionsRoyal Aeronautical Society (London) Gold Medal (awarded to both Wilbur and Orville) May 1909. Medals from the Aero Club of America, Congress, Ohio State and the City of Dayton.Bibliography1951, Miracle at Kitty Hawk. The Letters of Wilbur \& Orville Wright, ed. F.C.Kelly, New York.1953, The Papers of Wilbur and Orville Wright, ed. Marvin W.McFarland, 2 vols, New York.Orville Wright, 1953, How We Invented the Aeroplane, ed. F.C.Kelly, New York.Further ReadingA.G.Renstrom, 1968, Wilbur \& Orville Wright. A Bibliography, Washington, DC (with 2,055 entries).C.H.Gibbs-Smith, 1963, The Wright Brothers, London (reprint) (a concise account).J.L.Pritchard, 1953, The Wright Brothers', Journal of the Royal Aeronautical Society (December) (includes much documentary material).F.C.Kelly, 1943, The Wright Brothers, New York (reprint) (authorized by Orville Wright).H.B.Combs with M.Caidin, 1980, Kill Devil Hill, London (contains more technical information).T.D.Crouch, 1989, The Bishop's Boys: A Life of Wilbur \& Orville Wright, New York (perhaps the best of various subsequent biographies).JDS
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