- can-annular combustion chamber
- трубчато-кольцевая камера сгорания
Англо-русский словарь по авиации. 2013.
can-annular combustion chamber
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Combustion chamber — A combustion chamber is the part of an engine in which fuel is burned. Contents 1 Internal combustion engine 1.1 Petrol or gasoline engine 1.2 Diesel engine 1.3 Gas … Wikipedia
combustion chamber — i. The section of the gas turbine engine into which fuel is injected and burned. The combustion results in very high temperatures, which expands the air flowing through the combustion chamber and directs it onto the turbine at a uniform speed and … Aviation dictionary
cannular/can-annular chamber combustion chamber — An arrangement in which flame tubes are laid out within the casing, resulting in weight reduction and an ease of construction advantage. The supply of secondary air to the flame tubes is made through a common air casing while primary air for… … Aviation dictionary
can-type combustor — A combustor, or burner section, of a gas turbine engine made up of several individual cans. These cans are long and cylindrical and consist of an outer casing within which there is a perforated stainless steel combustion chamber liner, or inner… … Aviation dictionary
Oil pump (internal combustion engine) — This article is about a part in an internal combustion engine. For other uses, see Oil pump. Oil circulation system … Wikipedia
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Rolls-Royce Avon — The Avon was Rolls Royce s first axial flow jet engine. Introduced in 1950, it went on to become one of their most successful post World War II engine designs. It was used in a wide variety of aircraft, both military and civilian, ending… … Wikipedia
Pratt & Whitney J52 — engine.The J52 employs a split 12 stage axial compressor consisting of a five stage low pressure unit and a seven stage high pressure unit. Behind the compressor is a nine unit can annular combustion chamber and a two stage split turbine … Wikipedia
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Rolls-Royce Olympus — Olympus Preserved Bristol Siddeley Olympus Mk 301 Engine Change Unit (ECU) complete with ancillaries and bulkheads. Type … Wikipedia
Hans von Ohain — Hans Joachim Pabst von Ohain (December 14 1911ndash March 13 1998) was one of the inventors of jet propulsion. The engineers, Frank Whittle in the United Kingdom and Hans von Ohain in Germany, developed the concept independently during the late… … Wikipedia
