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gas-turbine engine
Fonte1
INTERNATIONAL CIVIL AVIATION ORGANIZATION. Committee on aviation environmental protection: eighth meeting: Montreal, 1-12 february 2010: report. Montreal, 2010. (Doc. 9938)
Fonte2
ASSOCIAÇÃO BRASILEIRA DE NORMAS TÉCNICAS. NBR 15971-4: aeronáutica – vocabulário – parte 4: propulsão aeronáutica. Rio de Janeiro, 2011. 44 p.
Contexto
An auxiliary power unit (APU) is a small gas-turbine engine coupled to an electrical generator and is used to provide electrical and pneumatic power to aircraft systems when required.
Subárea1
Engine
Related Term
turbine engine
Português
motor à turbina a gás
Imagem

 A typical axial-flow gas turbine turbojet, the J85, sectioned for display. Flow is left to right, multistage compressor on left, combustion chambers center, two-stage turbine on right.

A typical axial-flow gas turbine turbojet, the J85, sectioned for display. Flow is left to right, multistage compressor on left, combustion chambers center, two-stage turbine on right.

Fonte: http://en.wikipedia.org/wiki/File:J85_ge_17a_turbojet_engine.jpg