Invention Grant
- Patent Title: Landing load monitor for aircraft landing gear
- Patent Title (中): 飞机起落架着陆载荷监视器
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Application No.: US11989785Application Date: 2006-08-23
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Publication No.: US08055396B2Publication Date: 2011-11-08
- Inventor: Michael Stuart Yates , Philip Gregory Keen
- Applicant: Michael Stuart Yates , Philip Gregory Keen
- Applicant Address: GB Bristol
- Assignee: Airbus Operations Limited
- Current Assignee: Airbus Operations Limited
- Current Assignee Address: GB Bristol
- Agency: Nixon & Vanderhye P.C.
- Priority: GB0517351.3 20050824
- International Application: PCT/GB2006/003154 WO 20060823
- International Announcement: WO2007/023280 WO 20070301
- Main IPC: B64C25/10
- IPC: B64C25/10

Abstract:
A landing gear monitor for aircraft landing gear including a plurality of pairs of wheels on a bogie, in which the main strut oil pressure serves to indicate landing load and is monitored in relation to, respectively, the two-wheel mode and the four-wheel mode, the two-wheel mode being the condition when a first of the plurality of pairs of wheels on the bogie contacts the ground and the four-wheel mode being the condition of a first and a second of the plurality of pairs of wheels on the bogie being in full contact with the ground.
Public/Granted literature
- US20100161174A1 Landing Load Monitor for Aircraft Landing Gear Public/Granted day:2010-06-24
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