Title:
【発明の名称】ガスタービンエンジン
Document Type and Number:
Japanese Patent JP2002526710
Kind Code:
A
Abstract:
A gas turbine engine has a turbine mounted downstream of a compressor and a compressor turbine mounted downstream of the turbine for driving the compressor. The compressor turbine has a rotor disk that is mechanically coupled to the compressor and rotates in a direction opposite to the direction of rotation of the turbine rotor disk. A heat exchanger has a first circuit connected to the compressor turbine and a second circuit connected between the compressor and the turbine. An electric load for taking off a fraction of power produced by the compressor turbine includes an electric generator that is mechanically coupled to the compressor turbine. An electric load controller changes the fraction of power produced by the compressor turbine based on readings from the temperature sensor located in the engine.
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Inventors:
Lakmailov Anatoli
Application Number:
JP2000574818A
Publication Date:
August 20, 2002
Filing Date:
September 24, 1999
Export Citation:
Assignee:
ALM Development, Inc.
International Classes:
F01D15/10; F02C3/067; F02C3/10; F02C6/00; F02C7/08; F02C9/00; F04B49/00; F04D15/00; H02K11/00; H02P9/04; F02C9/28; (IPC1-7): F02C9/28; F02C3/067; F02C3/10; F02C6/00; F02C7/08; F02C9/00; F04B49/00; F04D15/00; H02K11/00; H02P9/04
Attorney, Agent or Firm:
Minoru Nakamura (9 outside)