发明名称 SEAT TRACK FITTING
摘要 An improved track fitting for anchoring an aircraft seat to a seat track has a threaded "anti-rattle" fastener for forcing a flanged top portion of a movement restricting shear pin against the top of the seat track to prevent rattle and wear due to aircraft vibrations. A pivoted lever which also functions as a cover for the fitting is mounted on the body of the fitting for lifting the shear pin against the force of a shear pin spring which normally urges the pin into locking engagement with one of the slots in a seat track. To prevent tampering by a passenger, the lever is rendered inoperable when the anti-rattle fastener is actuated. A leaf spring carried by the lever engages the body and prevents the lever from rattling due to vibration. The lever can lock the shear pin in its upper disengaged position as the seat fitting is lowered into the seat track and can then be released so that the shear pin will drop into one of the slots in the seat track automatically as the fitting is moved fore or aft.
申请公布号 DE3169461(D1) 申请公布日期 1985.04.25
申请号 DE19813169461 申请日期 1981.12.04
申请人 PTC AEROSPACE INC. 发明人 LONG, WILLIAM ALLEN;FISCHER, WARD ELLSWORTH;BRUNELLE, RENE JOSEPH
分类号 B60N2/44;B64D11/06;(IPC1-7):B64D11/06 主分类号 B60N2/44
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