发明名称 Device for Automatically Regulating Aircraft Power Plant Gas Generator and Free Turbine Speeds as a Function of Heating, Electricity Generation, Noise Emission, and Fuel Consumption
摘要 A regulator device for automatically regulating a power plant of a rotary wing aircraft having a turbine engine includes a computer system. The computer system, while implementation of an idling mode of operation of the turbine engine is requested and the aircraft is standing on ground, implements the idling mode of operation and operates the turbine engine in compliance with idling mode of operation as a function of operational and hierarchically ordered conditions either through a first mode of regulation by regulating a speed of rotation (Ng) of a gas generator of the turbine engine or through a second mode of regulation by regulating a speed of rotation (NTL) of a free turbine of the turbine engine.
申请公布号 US2017009662(A1) 申请公布日期 2017.01.12
申请号 US201615273805 申请日期 2016.09.23
申请人 Airbus Helicopters 发明人 Corpron Alban
分类号 F02C9/00;B64C27/14;B64D27/10;F02C3/04;B64D31/00 主分类号 F02C9/00
代理机构 代理人
主权项 1. A regulator device for automatically regulating a power plant of an aircraft having a rotary wing and a turbine engine, the turbine engine being operable in an idling mode of operation and having a gas generator and a free turbine, the regulator device comprising: a computer system configured to control the turbine engine, the computer system further configured to, while implementation of the idling mode of operation is requested and the aircraft is standing on ground, implement the idling mode of operation and operate the turbine engine in compliance with the idling mode of operation as a function of a plurality of operational and hierarchically ordered conditions either through: a first mode of regulation by regulating a speed of rotation (Ng) of the gas generator; ora second mode of regulation by regulating a speed of rotation (NTL) of the free turbine.
地址 Marignane FR