发明名称 Thermal expansion compensating joint assembly
摘要 A thermal stress-free joint assembly for joining a low thermal expansion member and a high thermal expansion member uses a fastener and a bushing fitted within a bore in the low thermal expansion member, wherein the fastener and bushing materials are selected to have predetermined coefficients of thermal expansion. The fastener includes a shank which passes through the bore in the low thermal expansion member. The bushing, bore and shank are dimensioned according to a mathematical relationship to maintain a predetermined clearance or preload as the joint undergoes changes in temperature, without damage to either joined member from thermally induced stress.
申请公布号 US4834569(A) 申请公布日期 1989.05.30
申请号 US19870049307 申请日期 1987.05.13
申请人 THE BOEING COMPANY 发明人 FOOTE, EUGENE B.;GILES, DANIEL N.
分类号 F16B1/00;F16B5/02 主分类号 F16B1/00
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