bleed-gas turbine

bleed-gas turbine
турбина (ТНА), работающая на газе, отбираемом из камеры сгорания двигателя

English-russian astronautics dictionary. - M.: Military Publishing house. . 1964.

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  • Bleed air — in gas turbine engines is compressed air taken from within the engine, after the compressor stage(s) and before the fuel is injected in the burners. While in theory bleed air could be drawn in any gas turbine engine, its usage is generally… …   Wikipedia

  • bleed air — Compressed air bled from gas turbine engines. It can be used in an aircraft pressurization system, cabin temperature control, and deicing and anti icing systems, as well as for boundary layer control …   Aviation dictionary

  • bleed — i. To allow a quantity of fluid or air to escape from a closed system until excess pressure has fallen to a lower level or is equalized with the surroundings (e.g., high pressure fuel pumps). ii. To remove unwanted fluid contaminating a system… …   Aviation dictionary

  • air bleed — i. A small hole in the fuel passage between the float bowl and the discharge nozzle of a float carburetor. This air bleed provides a more even mixture over a wide range of airflows to improve atomizing the fuel and reduces the size of the fuel… …   Aviation dictionary

  • compressor bleed air — Air taken out of the compressor section of a gas turbine engine to prevent compressor stall and operate cabin pressurization and air conditioning systems. Air may also be bled from the compressor for boundary layer control …   Aviation dictionary

  • газотурбинный двигатель с отбором воздуха [газа] — Газотурбинный двигатель, в котором для внешнего использования предусмотрен отбор сжатого воздуха между ступенями компрессора и/или на выходе из компрессора [горячего газа на входе в турбину и/или между ступенями турбины]. [ГОСТ Р 51852 2001]… …   Справочник технического переводчика

  • Components of jet engines — Diagram of a typical gas turbine jet engine. Air is compressed by the fan blades as it enters the engine, and it is mixed and burned with fuel in the combustion section. The hot exhaust gases provide forward thrust and turn the turbines which… …   Wikipedia

  • Jet engine performance — This article describes how jet engine performance is estimated during the design phase. Similar techniques are used once the engine has been built and is being tested, except the performance of individual components, rather than being assumed, is …   Wikipedia

  • Space Shuttle main engine — SSME redirect here. For the services field, see Service Science, Management and Engineering infobox rocket engine imsize=250 caption=Space Shuttle Main Engine test firing name=Space Shuttle Main Engine country of origin=United States manufacturer …   Wikipedia

  • ГОСТ 23851-79: Двигатели газотурбинные авиационные. Термины и определения — Терминология ГОСТ 23851 79: Двигатели газотурбинные авиационные. Термины и определения оригинал документа: 293. Аварийное выключение ГТД Аварийное выключение Ндп. Аварийное отключение ГТД D. Notausschaltung Е. Emergency shutdown F. Arrêt urgent… …   Словарь-справочник терминов нормативно-технической документации

  • Centrifugal compressor — Centrifugal compressors, sometimes termed radial compressors, are a sub class of dynamic axisymmetric work absorbing turbomachinery.[1] Centrifugal impeller with a highly polished surface likely to improve performance …   Wikipedia


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