Invention Application
- Patent Title: TURBINE ENGINE RAPID REACTIVATION METHOD AND SYSTEM
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Application No.: US15129309Application Date: 2015-03-19
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Publication No.: US20180171874A1Publication Date: 2018-06-21
- Inventor: Thomas KLONOWSKI , Jean-Michel BAZET , Vincent POUMAREDE , Pierre HARRIET
- Applicant: SAFRAN HELICOPTER ENGINES
- Applicant Address: FR Bordes
- Assignee: SAFRAN HELICOPTER ENGINES
- Current Assignee: SAFRAN HELICOPTER ENGINES
- Current Assignee Address: FR Bordes
- Priority: FR1452628 20140327
- International Application: PCT/FR2015/050675 WO 20150319
- Main IPC: F02C7/268
- IPC: F02C7/268 ; B64D31/00 ; H02J7/14

Abstract:
The system for rapidly reactivating a turbine engine of an aircraft includes an electrical machine that is DC powered from an on-board electrical power supply network. The system also includes a switch interposed between the on-board network and the electrical machine, an additional set including a plurality N electrical energy storage elements, and a control unit for controlling a device for discharging the storage elements and adapted to enable a series circuit including at least some of the N electrical energy storage elements to be connected in parallel with the on-board network so that when the rapid reactivation system is in operation the electrical machine is powered by a voltage level higher than the voltage level of its nominal characteristics.
Information query
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