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    • 10. 发明授权
    • High sensitivity, load alleviating load sensor for strut application
    • 高灵敏度,负载减轻负载传感器用于支柱应用
    • US09459168B2
    • 2016-10-04
    • US14222061
    • 2014-03-21
    • Moog Inc.
    • Kerry Randall KohuthDerek Pedersen
    • G01L5/22G01N3/08B64C13/00B64C9/16B64C9/20B64C13/34G01L5/00B64D45/00
    • G01L5/22B64C9/16B64C9/20B64C13/00B64C13/34B64D2045/0085G01L5/0028G01N3/08
    • A load-sensing strut has a main body (26) having a longitudinal loading axis (A) along which an applied load is transmitted, and a load sensing member (38) arranged to carry at least a portion of the applied load when the load is within a predetermined range, wherein the load sensing member (38) includes at least one load sensor (46) generating a load signal. The strut also has a load alleviation member (36) arranged to reduce the portion of the applied load carried by the load sensing member (38) when the applied load is outside the predetermined loading range. Consequently, the load sensors exhibit greater sensitivity to incremental changes in the applied load within the predetermined range, yet the strut provides high strength and is capable of reacting to very high loads outside of the predetermined range. The strut may be used in actuating aircraft control surfaces in a high-lift system.
    • 负载感测支柱具有主体(26),所述主体(26)具有纵向加载轴线(A),所施加的负载穿过所述纵向加载轴线(A),以及负载感测构件(38),其布置成在负载时承载所施加的负载的至少一部分 在预定范围内,其中所述负载感测构件(38)包括产生负载信号的至少一个负载传感器(46)。 支柱还具有负载减轻构件(36),其被布置成当施加的负载在预定负载范围之外时减小由负载感测构件(38)承载的施加负载的部分。 因此,负载传感器在预定范围内对所施加的负载的增量变化表现出更大的灵敏度,但是支柱提供高强度并且能够对超出预定范围的非常高的负载作出反应。 支柱可用于在高升力系统中起动飞机控制面。