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Title:
【発明の名称】ガスタービンエンジン動力装置の運転方法及びガスタービンエンジン動力装置
Document Type and Number:
Japanese Patent JP2002539354
Kind Code:
A
Abstract:
A gas turbine engine that has a turbine (1) mounted downstream of a combustor (5), a compressor turbine (2) mounted downstream of turbine (1) for producing power for driving a compressor (3), a heat exchanger (6) having a first circuit (61) connected to compressor turbine (2) and a second circuit (62) connected between compressor (2) and turbine (1) and a fluid discharge device (7) between compressor (3) and combustor (5). The gas turbine engine has a reactor (8) that has a heating device (9), inlets (F, W) connected to sources of fuel and water and an outlet connected to combustor (5). Heating device (9) is connected the outlet of compressor turbine (2). The engine also has a system for keeping the temperature at the outlet of compressor turbine (2) constant.

Inventors:
ラクマイロフ アナトリ
Application Number:
JP2000604110A
Publication Date:
November 19, 2002
Filing Date:
March 10, 2000
Export Citation:
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Assignee:
エーエルエム ディベロップメント インコーポレイテッド
International Classes:
F01D15/10; F02C3/067; F02C3/10; F02C3/20; F02C3/28; F02C3/34; F02C6/18; F02C7/08; F02C9/00; F02C9/28; (IPC1-7): F02C3/067; F01D15/10; F02C3/10; F02C3/20; F02C3/34; F02C7/08; F02C9/00
Attorney, Agent or Firm:
中村 稔 (外10名)