|국가/구분||United States(US) Patent 등록|
|우선권정보||FR-12 00343 (2012-02-06)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 9|
A regulator device (10) for regulating a turbine engine (3). The regulator device (10) includes mechanical power take-off means (100) for taking off power mechanically from a gas generator (4), and an engine computer (20) controlling said engine (3) to comply with at least a first limitation (LimTET, LimT45) of a temperature (TET, T45) of the gas within the engine, and with a second limitation (LimNg) of a speed of rotation (Ng) of the gas generator (4). The engine computer (20) determines whether the speed of rotation (Ng) of the gas generator has reach...
1. A method of regulating an aircraft power plant including at least one turbine engine, the turbine engine including a gas generator, an auxiliary shaft, and a turbine assembly, the turbine assembly including a free turbine and a high-pressure turbine arranged upstream from the free turbine, the gas generator including a compressor connected to the high-pressure turbine, the power plant further including mechanical power take-off means connected to the gas generator via the auxiliary shaft for taking off power mechanically from the gas generator and the...