发明名称 LANDING GEAR LOAD TRANSDUCER
摘要 PCT No. PCT/US87/00936 Sec. 371 Date Apr. 29, 1987 Sec. 102(e) Date Apr. 29, 1987 PCT Filed Apr. 29, 1987 PCT Pub. No. WO88/08391 PCT Pub. Date Mar. 3, 1988.A landing gear load sensor (24) for an aircraft (10) having a skid type landing gear (14) is provided. The sensor (24) includes a shear beam (30) having a loadbearing area (40). Structure (32, 34) is provided for mounting the shear beam (30) to the aircraft (10), such that the loadbearing area (40) is disposed adjacent the landing gear (14). Structure (50) is disposed on the shear beam (30) between the mounting structure (32, 34) and the loadbearing area (40) for sensing shear load on the shear beam (30).
申请公布号 AU8152387(A) 申请公布日期 1988.12.02
申请号 AU19870081523 申请日期 1987.04.29
申请人 BELL HELICOPTER TEXTRON INC. 发明人 BILLY H. DICKSON;PAUL EUGENE DARDEN
分类号 B64C25/32;B64C25/00;B64D45/00;G01G19/07;G01G19/12;G01L 主分类号 B64C25/32
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