Invention Grant
- Patent Title: Method for controlling the generation of electricity applied to an aircraft gas turbine, and device implementing such a method
- Patent Title (中): 控制飞机燃气轮机发电的控制方法以及实施这种方法的装置
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Application No.: US13884822Application Date: 2011-12-12
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Publication No.: US08866318B2Publication Date: 2014-10-21
- Inventor: Stephen Langford , Pierre Harriet
- Applicant: Stephen Langford , Pierre Harriet
- Applicant Address: FR Bordes
- Assignee: Turbomeca
- Current Assignee: Turbomeca
- Current Assignee Address: FR Bordes
- Agency: Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR1060419 20101213
- International Application: PCT/FR2011/052935 WO 20111212
- International Announcement: WO2012/080633 WO 20120621
- Main IPC: F01D15/10
- IPC: F01D15/10 ; F02C7/275 ; B60R16/03 ; F02C3/10 ; F02C7/32 ; F02C7/26

Abstract:
A method improving acceleration efficiency of a gas generator of a gas turbine by reducing take-up of electric power, during transition phases, to conserve a sufficiently large surge margin for an operating line. The method increases acceleration/deceleration power of the gas generator by adjusting voltage of an electric network onboard the aircraft. After a phase of starting the gas turbine, voltage of the onboard network is adjusted by a voltage set value controlled by determining unballasting/ballasting status of a main electricity generation source of the onboard network. The status-determining is executed according to demand for taking power to be supplied for propulsion of the aircraft. The status-determining is followed by selecting a voltage set value from plural levels according to the determining the unballasting/ballasting status, and applying the selected set value to a control loop of the voltage supplied to the onboard network.
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