发明名称 |
TURBINE ENGINE COMPRISING AN ELECTRICALLY ACTIVATED FUEL SUPPLY PUMP, AND TURBINE ENGINE FUEL SUPPLY METHOD |
摘要 |
A turbine engine for an aircraft including a turbine engine shaft and a pumping module, including: a pump shaft, connected to the turbine engine shaft; a pump for supplying fuel to the turbine engine, mounted on the pump shaft, configured to deliver a flow of fuel as a function of a speed of rotation of the turbine engine shaft; and an electrical device mounted on the pump shaft and configured, according to a first mode of operation, to drive the pump shaft in rotation to actuate the supply pump and, according to a second mode of operation, to be driven in rotation by the pump shaft to supply electrical power to equipment of the turbine engine. |
申请公布号 |
EP2785981(A1) |
申请公布日期 |
2014.10.08 |
申请号 |
EP20120806589 |
申请日期 |
2012.11.28 |
申请人 |
TURBOMECA |
发明人 |
LINDEMAN, JEAN;BENEZECH, PHILIPPE, JEAN, RENÉ, MARIE;FREALLE, JEAN-LUC, CHARLES, GILBERT;MOINE, BERTRAND |
分类号 |
F01D15/08;F01D15/10;F02C7/22;F02C7/32 |
主分类号 |
F01D15/08 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|