Aeronautics and astronautics – Aircraft structure – Details
Reexamination Certificate
2007-08-14
2007-08-14
Collins, Timothy D. (Department: 3643)
Aeronautics and astronautics
Aircraft structure
Details
C049S379000, C244S05300R
Reexamination Certificate
active
10919348
ABSTRACT:
A closure panel arrangement is provided in which a closure panel6can only be retained when appropriately aligned with engagement between clasp hooks8and pins9is achieved along with association between latch hooks10and pins11. If there is not appropriate association and alignment then a bias12, 22, 32, 42creates an outward bias force upon the closure panel6whereby the panel6will continue to fall out. In such circumstances, the panel6cannot remain in position due to simply key fit interference/friction association of sufficient strength for non-operational conditions but which will fail during operation due to vibration or stresses.
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Collins Timothy D.
Manelli Denison & Selter PLLC
Rolls-Royce plc
Taltavull W. Warren
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