지정품명부호 검색

연속 연소형 엔진으로서 "압축기,항공기 가스터빈엔진용(COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE)", "실,연소용,항공기 가스터빈엔진용(CHAMBER, COMBUSTION, AIRCRAFT GAS TURBINE ENGINE)" 및 "터빈조립체,항공기 가스터빈엔진용(TURBINE ASSEMBLY, AIRCRAFT GAS TURBINE ENGINE)"으로 주로 구성되어 있다. "재연소장치,터빈엔진용(AFTERBURNER, TURBINE ENGINE)" 과 송풍기 부분품으로 되어 있다. 공기는 가연연료로 압축되고 가열되며 터빈으로 팽창된다. 회전축,공기력 혹은 추진 마력의 힘을 제공하도록 고안되었으며 공기력은 엔진 압축기로 빼내어얻는다.

A continuous combustion type engine. Consists primarily of a COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE, CHAMBER, COMBUSTION, AIRCRAFT GAS TURBINE ENGINE and a TURBINE ASSEMBLY, AIRCRAFT GAS TURBINE ENGINE. It may have an AFTERBURNER, TURBINE ENGINE and/or a fan section. Air is compressed and heated by a combustible fuel and expanded through the turbine. It is designed to furnish a source of rotary shaft, pneumatic power or thrust power. The pneumatic power is obtained by a bleedoff of the engine compressor. For a complete operating power unit, mounted on a base, see POWER UNIT, GAS TURBINE ENGINE.