|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F02C-007/22 F01D-015/08 F01D-015/10 F02C-007/32|
|우선권정보||FR-11 60887 (2011-11-29)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 1 인용 특허 : 1|
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 ...
1. A turbine engine for an aircraft including a shaft of a turbine engine and a pumping module, comprising: a structural housing including a suction flange, to draw off fuel from a tank, and a delivery flange;a pump shaft connected to the shaft of the turbine engine;a supply pump for supplying the fuel to the turbine engine, mounted on the pump shaft and mounted inside the structural housing, configured to deliver a flow of the fuel as a function of a speed of rotation of the shaft of the turbine engine, the supply pump including a first fixed central pa...