Aeronautics and astronautics – Aircraft structure – Load accommodation
Reexamination Certificate
2009-08-24
2010-11-16
Lee, Benjamin P (Department: 3641)
Aeronautics and astronautics
Aircraft structure
Load accommodation
C244S129400, C296S037800, C312S248000
Reexamination Certificate
active
07832685
ABSTRACT:
An aircraft stowage bin assembly includes shear fittings configured to route a content load from the bucket of the bin assembly to the airframe in the event of a forward load condition, such as a crash or severe turbulence. When the forward inertial load factor on the stowage bin is greater than about 1 g, the shear fittings create an efficient load path from the bucket to the airframe which bypasses the large metallic or composite endframes required by the designs of many conventional overhead stowage bins. As a result, significant reductions in overall bulk and weight, as well as lower manufacturing costs, can be realized.
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Haynes Michael S.
Manhardt Joseph M.
Schmitz Chad D.
Gumpel Charles S.
Lee Benjamin P
The Boeing Company
Yee & Associates P.C.
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