Invention Grant
US08967530B2 Signal strength dependent cover unlocking device for a duct housing a secondary power supply device in an aircraft fuselage
有权
信号强度相关的盖解锁装置,用于容纳飞机机身中的次级电源装置的管道
- Patent Title: Signal strength dependent cover unlocking device for a duct housing a secondary power supply device in an aircraft fuselage
- Patent Title (中): 信号强度相关的盖解锁装置,用于容纳飞机机身中的次级电源装置的管道
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Application No.: US13203055Application Date: 2010-02-24
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Publication No.: US08967530B2Publication Date: 2015-03-03
- Inventor: Sten Gatzke
- Applicant: Sten Gatzke
- Applicant Address: DE Hamburg
- Assignee: Airbus Operations GmbH
- Current Assignee: Airbus Operations GmbH
- Current Assignee Address: DE Hamburg
- Agency: Jenkins, Wilson, Taylor & Hunt, P.A.
- Priority: DE102009010243 20090224
- International Application: PCT/EP2010/001151 WO 20100224
- International Announcement: WO2010/097213 WO 20100902
- Main IPC: B64D41/00
- IPC: B64D41/00 ; F03D9/00

Abstract:
A power generation system for integration into an aircraft system, including a secondary power supply device having a generator turbine arranged in a duct running between a forward opening and a rearward opening on the fuselage of the aircraft. An electromagnetic unlocking device locks and unlocks a covering device on the forward opening, depending on a signal strength supplied to the unlocking device. The system also includes an actuation device that generates an opening or closing signal for an opening and closing device, and an opening function switching device that activates the unlocking device electrically with a signal strength that locks the covering device in an initial state, and on receipt of a power requirement signal from a power generation monitoring device, activates the unlocking device with a second signal strength that unlocks the covering device.
Public/Granted literature
- US20120006938A1 POWER GENERATING SYSTEM FOR INTEGRATION INTO AN AIRCRAFT SYSTEM Public/Granted day:2012-01-12
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