Landing load monitor for aircraft landing gear

Details Landing load monitor for aircraft landing gear Landing load monitor for aircraft landing gear

2006-08-23

2011-11-08

Dickson, Paul N (Department: 3616)

Data processing: vehicles, navigation, and relative location

Vehicle control, guidance, operation, or indication

Aeronautical vehicle

C701S003000, C244S202000, C244S203000, C244S10000R, C244S1020SS, C340S960000

Reexamination Certificate

active

08055396

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.

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International Search Report for PCT/GB2006/003154 mailed Nov. 27, 2006.
Great Britain Search Report for GB 0517351.3 dated Oct. 31, 2005.
Written Opinion of the International Searching Authority.

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