Aeronautics and astronautics – Landing gear – Retractable
Reexamination Certificate
2006-06-27
2006-06-27
Poon, Peter M. (Department: 3643)
Aeronautics and astronautics
Landing gear
Retractable
C244S1020SL
Reexamination Certificate
active
07066429
ABSTRACT:
A system and method is provided for directing a separation sequence of structural components, such as, for example, aircraft landing gear components, during an overload condition. This system and method may be used to stop a component in rotation and thereby allow the component to fail in a predictable and controllable manner. This system and method may be used on any type of device that utilizes components that rotate relative to one another and/or that has components that rotate during an overload condition.
REFERENCES:
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patent: 2668030 (1954-02-01), Smith et al.
patent: 4087062 (1978-05-01), Masclet
patent: 4155522 (1979-05-01), Sealey
patent: 4328939 (1982-05-01), Davies et al.
Mellor Mitchell L.
Reitz Christopher A.
Collins T D.
Marshall & Gerstein & Borun LLP
Poon Peter M.
The Boeing Company
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