发明名称 STOWAGE BIN WITH SHEAR FITTINGS
摘要 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 lg, 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.
申请公布号 WO2012067734(A1) 申请公布日期 2012.05.24
申请号 WO2011US55775 申请日期 2011.10.11
申请人 THE BOEING COMPANY;SCHMITZ, CHAD D.;MANHARDT, JOSEPH MATTHIAS 发明人 SCHMITZ, CHAD D.;MANHARDT, JOSEPH MATTHIAS
分类号 B64D11/00 主分类号 B64D11/00
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