首页> 外国专利> DETECTION OF THE ABSORPTION OF EFFORT BY A SECONDARY ROAD OF A FLIGHT CONTROL ACTUATOR.

DETECTION OF THE ABSORPTION OF EFFORT BY A SECONDARY ROAD OF A FLIGHT CONTROL ACTUATOR.

机译:飞行控制执行器的第二条路对努力的吸收的检测。

摘要

Device for detecting the absorption of effort by a secondary track of a flight control actuator (1) having a primary track (3, 4, 5) and a secondary track (7, 8, 9, 10) suitable for absorb the stress of the primary track in the event of failure of the latter, the primary path comprising a screw (3), the screw terminating by a coupling piece of the primary track, the secondary track comprising a safety rod (9) of absorption of stress that passes through the screw (3), this rod (9) being terminated by a male form (7) housed - with play when the primary track supports the effort - in a female form (10) of a coupling piece (8) of the secondary track, the male form (7) terminating the rod (9) and the female form (10) of the spherical or revolution coupling piece (8), characterized in that at least one sensing element (11 ) is arranged on the male form (7) that ends the rod, on the hem form bra (10) or between these two forms, this detection element (11) being intended to be worn under the effect of friction between the male form (7) and the female form (10) when the secondary track is loaded and absorbs the stress, this detection element (11) being connected or being suitable to be connected to appropriate treatment means to detect the wear of this detection element (11).
机译:用于检测由飞行控制致动器(1)的次级轨道吸收的力的装置,该飞行控制致动器(1)具有适合于吸收飞行器应力的初级轨道(3、4、5)和次级轨道(7、8、9、10)。如果主轨道发生故障,则主轨道包括一个螺钉(3),该螺钉由主轨道的连接件终止,辅助轨道包括一个安全杆(9),该安全杆吸收通过的应力螺钉(3),该杆(9)由凸形(7)端接,该凸形以次级轨道的连接件(8)的凹形(10)的凹形(10)形式容纳在主轨道支撑力的情况下。 ,凸形(7)终止球形或旋转连接件(8)的杆(9)和凹形(10),其特征在于,至少一个传感元件(11)布置在凸形(7)上),在下摆式文胸(10)上或在这两种形式之间将杆末端固定),该检测元件(11)应当佩戴在当副轨道被加载并吸收应力时,公模(7)和母模(10)之间的摩擦影响,该检测元件(11)被连接或适于被连接至适当的处理装置以检测磨损该检测元件(11)的部分。

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