发明名称 Composite structural skin spar joint and method of making
摘要 PCT No. PCT/US81/01319 Sec. 371 Date Sep. 30, 1981 Sec. 102(e) Date Sep. 30, 1981 PCT Filed Sep. 30, 1981 PCT Pub. No. WO83/01238 PCT Pub. Date Apr. 14, 1983.A resin impregnated woven fabric extends the length of a joint with a pair of spaced apart panels intersecting and interwoven with an intermediate laterally extending panel. A reinforcing core extends between the spaced apart panels on one side of the laterally extending panel. Three cores are located on the other side of the laterally extending panel. The intermediate core of the three is located between the two spaced apart panels and is reinforced to provide torsional load resistance. The other two cores are reinforced to provide varying load bearing properties in a spanwise direction.
申请公布号 US4395450(A) 申请公布日期 1983.07.26
申请号 US19810333247 申请日期 1981.09.30
申请人 THE BOEING COMPANY 发明人 WHITENER, PHILIP C.
分类号 B29C53/58;B29C70/08;B29C70/24;B29C70/50;B29D24/00;B29D99/00;B64C1/06;B64C3/18;(IPC1-7):B64C3/18;B32B5/00 主分类号 B29C53/58
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