Invention Grant
US08213136B2 Engine having power bus fault short circuit control with a disconnection switch
有权
发动机具有断路开关的电源总线故障短路控制
- Patent Title: Engine having power bus fault short circuit control with a disconnection switch
- Patent Title (中): 发动机具有断路开关的电源总线故障短路控制
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Application No.: US11839763Application Date: 2007-08-16
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Publication No.: US08213136B2Publication Date: 2012-07-03
- Inventor: Vijay K. Maddali , Gregory I. Rozman , Kevin Dooley
- Applicant: Vijay K. Maddali , Gregory I. Rozman , Kevin Dooley
- Applicant Address: CA Quebec US CT Windsor Locks
- Assignee: Pratt & Whitney Canada Corp.,Hamilton Sundstrand Corporation
- Current Assignee: Pratt & Whitney Canada Corp.,Hamilton Sundstrand Corporation
- Current Assignee Address: CA Quebec US CT Windsor Locks
- Agency: Carlson, Gaskey & Olds, PC
- Main IPC: H02H7/06
- IPC: H02H7/06 ; H02H3/08 ; B64D41/00

Abstract:
An aircraft electrical system comprises a generator to be driven as part of a gas turbine engine. The generator supplies electrical power to a plurality of accessories associated with the gas turbine engine, and to an aircraft power bus in parallel to the supply to the accessories. A control detects a short circuit on the aircraft power bus. When a short circuit is detected on the aircraft power bus, a switch is driven open to disconnect the aircraft power bus from the generator. In this manner, the power will continue to be delivered to the plurality of accessories. In a separate feature, a control voltage is provided by an auxiliary permanent magnet generator to a voltage regulator for the main generator.
Public/Granted literature
- US20090045292A1 ENGINE HAVING POWER BUS FAULT SHORT CIRCUIT CONTROL WITH A DISCONNECTION SWITCH Public/Granted day:2009-02-19
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