-
1 Brandt Aero Engine Modular Management Aid
Abbreviation: BAEMMA (UK Royal Air Force)Универсальный русско-английский словарь > Brandt Aero Engine Modular Management Aid
-
2 аэродвигатель
-
3 авиационный двигатель
Русско-английский авиационный словарь > авиационный двигатель
-
4 авиационный двигатель
Русско-английский аэрокосмический словарь > авиационный двигатель
-
5 авиационный двигатель
Русско-английский научно-технический словарь Масловского > авиационный двигатель
-
6 авиадвигатель
-
7 авиационный двигатель
Авиация и космонавтика. Русско-английский словарь > авиационный двигатель
-
8 silnik lotniczy
• aero-engine• aeromotor• aircraft engine -
9 авиадвигателестроение
Русско-английский авиационный словарь > авиадвигателестроение
-
10 авиадвигателестроение
Русско-английский аэрокосмический словарь > авиадвигателестроение
-
11 авиадвигателестроение
Авиация и космонавтика. Русско-английский словарь > авиадвигателестроение
-
12 aeromotor
m.1 aero-engine.2 aeromotor, airplane.* * *SM aero-engine* * *masculino aero-engine* * *masculino aero-engine* * *aero-engine -
13 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 -
14 Langley, Samuel Pierpont
SUBJECT AREA: Aerospace[br]b. 22 August 1834 Roxbury, Massachusetts, USAd. 27 February 1906 Aiken, South Carolina, USA[br]American scientist who built an unsuccessful aeroplane in 1903, just before the success of the Wright brothers.[br]Professor Langley was a distinguished mathematician and astronomer who became Secretary of the Smithsonian Institution (US National Museum) in 1887. He was also interested in aviation and embarked on a programme of experiments with a whirling arm to test wings and with a series of free-flying models. In 1896 one of his steam-powered models made a flight of 4,199 ft (1,280 m): this led to a grant from the Government to subsidize the construction of a manned aeroplane. Langley commissioned Stephen M. Balzer, an automobile engine designer, to build a lightweight aero-engine and appointed his assistant, Charles M.Manly, to oversee the project. After many variations, including rotary and radical designs, two versions of the Balzer-Manly engine were produced, one quarter size and one full size. In August 1903 the small engine powered a model which thus became the first petrol-engined aeroplane to fly. Langley designed his full-size aeroplane (which he called an Aerodrome) with tandem wings and a cruciform tail unit. The Balzer-Manly engine drove two pusher propellers. Manly was to be the pilot as Langley was now almost 70 years old. Most early aviators tested their machines by making tentative hops, but Langley decided to launch his Aerodrome by catapult from the roof of a houseboat on the Potomac river. Two attempts were made and on both occasions the Aerodrome crashed into the river: catapult problems and perhaps a structural weakness were to blame. The second crash occurred on 8 December 1903 and it is ironic that the Wright brothers, with limited funds and no Government support, successfully achieved a manned flight just nine days later. Langley was heartbroken. After his death there followed a strange affair in 1914 when Glenn Curtiss took Langley's Aerodrome, modified it, and tried to prove that but for the faulty catapult it would have flown before the Wrights' Flyer. A brief flight was made with floats instead of the catapult, and it flew rather better after more extensive modifications and a new engine.[br]Bibliography1897, Langley Memoir on Mechanical Flight, Part 1, Washington, DC: Smithsonian Institution; 1911, Part 2.Further ReadingJ.Gordon Vaeth, 1966, Langley: Man of Science and Flight, New York (biography).Charles H. Gibbs-Smith, 1985, Aviation, London (includes an analysis of Langley's work).Tom D.Crouch, 1981, A Dream of Wings, New York.Robert B.Meyer Jr (ed.), 1971, Langley's Aero Engine of 1903, Washington, DC: Smithsonian Annals of Flight, No. 6 (provides details about the engine).JDSBiographical history of technology > Langley, Samuel Pierpont
-
15 Ellehammer, Jacob Christian Hansen
SUBJECT AREA: Aerospace[br]b. 14 June 1871 South Zealand, Denmarkd. b. 20 May 1946 Copenhagen, Denmark[br]Danish inventor who took out some four hundred patents for his inventions, including aircraft.[br]Flying kites as a boy aroused Ellehammer's interest in aeronautics, and he developed a kite that could lift him off the ground. After completing an apprenticeship, he started his own manufacturing business, whose products included motor cycles. He experimented with model aircraft as a sideline and used his mo tor-cycle experience to build an aero engine during 1903–4. It had three cylinders radiating from the crankshaft, making it, in all probability, the world's first air-cooled radial engine. Ellehammer built his first full-size aircraft in 1905 and tested it in January 1906. It ran round a circular track, was tethered to a central mast and was unmanned. A more powerful engine was needed, and by September Ellehammer had improved his engine so that it was capable of lifting him for a tethered flight. In 1907 Ellehammer produced a new five-cylinder radial engine and installed it in the first manned tri-plane, which made a number of free-flight hops. Various wing designs were tested and during 1908–9 Ellehammer developed yet another radial engine, which had six cylinders arranged in two rows of three. Ellehammer's engines had a very good power-to-weight ratio, but his aircraft designs lacked an understanding of control; consequently, he never progressed beyond short hops in a straight line. In 1912 he built a helicopter with contra-rotating rotors that was a limited success. Ellehammer turned his attention to his other interests, but if he had concentrated on his excellent engines he might have become a major aero engine manufacturer.[br]Bibliography1931, Jeg fløj [I Flew], Copenhagen (Ellehammer's memoirs).Further ReadingC.H.Gibbs-Smith, 1965, The Invention of the Aeroplane 1799–1909, London (contains concise information on Ellehammer's aircraft and their performance).J.H.Parkin, 1964, Bell and Baldwin, Toronto (provides more detailed descriptions).JDSBiographical history of technology > Ellehammer, Jacob Christian Hansen
-
16 Ricardo, Sir Harry Ralph
[br]b. 26 January 1885 London, Englandd. 18 May 1974 Graffham, Sussex, England[br]English mechanical engineer; researcher, designer and developer of internal combustion engines.[br]Harry Ricardo was the eldest child and only son of Halsey Ricardo (architect) and Catherine Rendel (daughter of Alexander Rendel, senior partner in the firm of consulting civil engineers that later became Rendel, Palmer and Tritton). He was educated at Rugby School and at Cambridge. While still at school, he designed and made a steam engine to drive his bicycle, and by the time he went up to Cambridge in 1903 he was a skilled craftsman. At Cambridge, he made a motor cycle powered by a petrol engine of his own design, and with this he won a fuel-consumption competition by covering almost 40 miles (64 km) on a quart (1.14 1) of petrol. This brought him to the attention of Professor Bertram Hopkinson, who invited him to help with research on turbulence and pre-ignition in internal combustion engines. After leaving Cambridge in 1907, he joined his grandfather's firm and became head of the design department for mechanical equipment used in civil engineering. In 1916 he was asked to help with the problem of loading tanks on to railway trucks. He was then given the task of designing and organizing the manufacture of engines for tanks, and the success of this enterprise encouraged him to set up his own establishment at Shoreham, devoted to research on, and design and development of, internal combustion engines.Leading on from the work with Hopkinson were his discoveries on the suppression of detonation in spark-ignition engines. He noted that the current paraffinic fuels were more prone to detonation than the aromatics, which were being discarded as they did not comply with the existing specifications because of their high specific gravity. He introduced the concepts of "highest useful compression ratio" (HUCR) and "toluene number" for fuel samples burned in a special variable compression-ratio engine. The toluene number was the proportion of toluene in heptane that gave the same HUCR as the fuel sample. Later, toluene was superseded by iso-octane to give the now familiar octane rating. He went on to improve the combustion in side-valve engines by increasing turbulence, shortening the flame path and minimizing the clearance between piston and head by concentrating the combustion space over the valves. By these means, the compression ratio could be increased to that used by overhead-valve engines before detonation intervened. The very hot poppet valve restricted the advancement of all internal combustion engines, so he turned his attention to eliminating it by use of the single sleeve-valve, this being developed with support from the Air Ministry. By the end of the Second World War some 130,000 such aero-engines had been built by Bristol, Napier and Rolls-Royce before the piston aero-engine was superseded by the gas turbine of Whittle. He even contributed to the success of the latter by developing a fuel control system for it.Concurrent with this was work on the diesel engine. He designed and developed the engine that halved the fuel consumption of London buses. He invented and perfected the "Comet" series of combustion chambers for diesel engines, and the Company was consulted by the vast majority of international internal combustion engine manufacturers. He published and lectured widely and fully deserved his many honours; he was elected FRS in 1929, was President of the Institution of Mechanical Engineers in 1944–5 and was knighted in 1948. This shy and modest, though very determined man was highly regarded by all who came into contact with him. It was said that research into internal combustion engines, his family and boats constituted all that he would wish from life.[br]Principal Honours and DistinctionsKnighted 1948. FRS 1929. President, Institution of Mechanical Engineers 1944–5.Bibliography1968, Memo \& Machines. The Pattern of My Life, London: Constable.Further ReadingSir William Hawthorne, 1976, "Harry Ralph Ricardo", Biographical Memoirs of Fellows of the Royal Society 22.JBBiographical history of technology > Ricardo, Sir Harry Ralph
-
17 воздушно-реактивный двигатель
1) General subject: air-breather, jet-engine, jettie, thermojet3) Military: air-breathing engine, air-breathing engine system, airbreathing engine4) Engineering: air breathing engine, air-feed jet engine, air-jet engine, airbreather5) Astronautics: aero-engine, aerojet engine, air engine, air-breathing engine, air-breathing power plant, air-breathing power unit, air-breathing propulsion system, air-burning engine, airstream engine, atmospheric jet, jet engine, jet motor, jet propulsion motor, jet-propulsion engine, propulsion jet engine, thermal jet, thermal jet propulsion, thermal-jet engine, thermojet engine6) Makarov: air-breathing jet engine, ram jetУниверсальный русско-английский словарь > воздушно-реактивный двигатель
-
18 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 -
19 Flugmotorenhersteller
Flug·mo·to·ren·her·stel·lerm aircraft [or aero] engine maker* * *m.aero engine maker n. -
20 Aircraft Derivative
f < turb> (Gasturbinentyp) ■ aircraft derivative; aircraft engine derived gas turbine did ; aero-engine derivative; aero-derived gas turbine; lightweight gas turbine
См. также в других словарях:
aero-engine — n. an engine used to power an aircraft. * * * aˈero engine noun An aircraft engine • • • Main Entry: ↑aero … Useful english dictionary
aero-engine — /ˈɛəroʊ ˌɛndʒən/ (say airroh .enjuhn) noun the source of power in an aircraft …
Component Validator for Environmentally Friendly Aero Engine — Component Validator for Environmentally Friendly Aero Engine, also known as CLEAN, is a EU funded research program within the EEFAE (Efficient and Environmentally Friendly Aircraft Engine) project. All major European engine manufacturers are… … Wikipedia
United States military aero engine designations — was introduced in 1926, originally for piston engines it was expanded in the 1947 to include a separate system for turbine and rocket engines.Piston enginesA piston engine designation has three separate elements, a type prefix, a number… … Wikipedia
Lawrance Aero Engine Corporation — Lawrance L 4S Lawrance L 3 Die Lawrance Aero Engine Corporation … Deutsch Wikipedia
Aero — may refer to:* the Latin prefix relating to flight, * a chiefly British adjective related to flight, as in aero engine Products* Windows Aero, a user interface in Windows Vista * Aero (chocolate) chocolate bar * Mitsubishi Fuso Aero Bus series *… … Wikipedia
Engine Alliance GP7000 — The Engine Alliance GP7000 (known as the GP7200 for a brief time period) is a new turbofan jet engine that will incorporate advanced technologies of proven wide body products, originally from the world s No.1 and No.3 aero engine manufacturers,… … Wikipedia
aero- — [[t]e͟əroʊ [/t]] 1) PREFIX aero is used at the beginning of words, especially nouns, that refer to things or activities connected with air or movement through the air. 2) COMB in N COUNT aero combines with nouns to form nouns relating to… … English dictionary
aero — I. adjective Etymology: aero Date: 1874 of or relating to aircraft or aeronautics < an aero engine > II. abbreviation aerodynamic … New Collegiate Dictionary
Aero Commander — was an aircraft manufacturer, a subsidiary of Rockwell International.HistoryAero was formed in Culver City in 1944 to design and manufacture a light twin engined transport aircraft, the Aero Commander 500. In 1950 it became the Aero Design and… … Wikipedia
Aero Adventure Aviation — (formerly Arnet Pereyra Inc) is an american aircraft manufacturer based in Rockledge, Florida. It produces ultralights, light aircraft, and is currently developing a small turboprop engine.In 1996, the firm acquired the assets and production… … Wikipedia
