发明名称 |
LANDING GEAR LOAD TRANSDUCER |
摘要 |
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 |
WO8808391(A1) |
申请公布日期 |
1988.11.03 |
申请号 |
WO1987US00936 |
申请日期 |
1987.04.29 |
申请人 |
BELL HELICOPTER TEXTRON INC. |
发明人 |
DARDEN, PAUL, EUGENE;DICKSON, BILLY, H. |
分类号 |
B64C25/32;B64C25/00;B64D45/00;G01G19/07;G01G19/12;G01L;(IPC1-7):B64C25/00 |
主分类号 |
B64C25/32 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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