An aircraft hydraulic mechanical load mechanism
A technology of mechanical load and aircraft hydraulic pressure, which is applied in the direction of aircraft transmission, aircraft power transmission, aircraft power device, etc., can solve the problems of mechanism jamming, affecting the control force, and unstable work, etc., to solve the problem of mechanism jamming and reduce The effect of throttling loss and improving work efficiency
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[0026] The technical solutions of the present invention will be described below in conjunction with the drawings, which is apparent from the accompanying drawings. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art are in the range of the present invention without making creative labor premise.
[0027] Aircraft hydraulic mechanical load mechanism, such as figure 1 and image 3 As shown, the housing 1 is provided with a transmission structure 2 and a spring structure 3, and the housing 1 includes a hydraulic oil, and the driven port 11 and the oil port 12 are provided on the driven device 22, the spring structure 3 and the transmission. Structure 2 fixed connection.
[0028] Such as figure 2 As shown, the main drive device 21 includes a rocker arm structure 211, a cam 212, and a roller structure 213, a rocker arm structure 211 includes a first rocker arm 2111, a second rocker arm 2112, a third rocker arm 2113, and...
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