A braking method for an electro-hydraulic brake valve of an unmanned aerial vehicle landing gear
A landing gear and unmanned aerial vehicle technology, applied in the field of aircraft design and fluid transmission, to achieve the effects of improved accuracy and efficiency, easy installation and maintenance, and simple structure
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[0030] In order to make the purpose, content, and advantages of the present invention clearer, the specific implementation manners of the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments.
[0031] The present invention provides a braking method for an electro-hydraulic brake valve of a UAV landing gear. The method is realized based on an electro-hydraulic brake valve, such as figure 2 As shown, the electro-hydraulic brake valve includes an oil storage cup 1, a housing 3, a bushing 5, a gland 6, an end cap 8, a piston rod 9, a voice coil motor 10, a screw 11, a limit support 13, a limit Rod 14, sleeve 15, limit spring 16, cone valve assembly 19, nozzle 21, pressure sensor 22, retaining ring 24, O-rings of different specifications, gaskets, etc.
[0032]Wherein, the oil storage cup 1 is installed on the housing 3 through threaded connection, and is sealed by the gasket 2; The ring 4 is sealed, and the tai...
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