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[CN 201710817393.9] Aircraft hydraulic mechanical load mechanism
[CN 201710817393.9] Title of an Aircraft Hydraulic Mechanical Load Mechanism: Application Number of an Aircraft Hydraulic Mechanical Load Mechanism: CN 201710817393.9 Applicant: Shaanxi Aircraft Industry (Group) Co., Ltd. Application Date: 2017-9-12 Patent Type: Invention Application The present invention belongs to the field of aircraft mechanical control, especially an aircraft hydraulic mechanical load mechanism. The hydraulic mechanical load mechanism is composed of a housing 1, a limit rocker arm 2, a diaphragm 3, a spring 4, a throttle slide valve 5, a piston 6, an ejector rod 7, a spring 8, a rocker arm 9, a rocker arm 10, and a rocker arm 11, A spring 12, a cam 13, a rocker arm 14, a roller 15, and a housing 17. It overcomes the shortcomings that the traditional hydraulic mechanical load mechanism cannot change the control force with the change of flight speed, and can overcome the shortcomings of high processing accuracy requirements for each component, complex installation and coordination, and easy jamming of the mechanism.
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