A debuggable and dismantling self-locking structure for an aviation heat exchanger bypass valve
A technology of self-locking structure and heat exchanger, which is applied in the direction of valve housing structure, functional valve type, mechanical equipment, etc., can solve the problems of unqualified variation of valve opening pressure difference, valve cannot be repaired, and valve scrap rate is high, so as to achieve reliable Self-locking function, improved maintainability, and reduced maintenance cost
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[0019] The specific implementation manner of the present invention will be described in detail below according to the accompanying drawings.
[0020] A self-locking structure that can be adjusted and disassembled for the bypass valve of an aviation heat exchanger. The bypass valve includes a valve shell 1, a lock nut 7 and a lock rod gasket 8 that are sequentially arranged in the inner hole of the valve shell 1 from top to bottom. , spring seat 3, spring 5, valve sealing valve 6; lock nut 7 upper outer peripheral surface has a rotating rib structure, the lower part is threaded with the inner hole of the valve housing 1; the spring seat 3 is threaded with the inner hole of the valve housing 1, and the valve The bottom of the sealing valve 6 is limited by the flange of the valve housing 1 inner hole.
[0021] An adjusting washer 4 is arranged between the end surface of the spring 5 and the spring seat 3, and the working pressure of the valve is adjusted by increasing or decreasi...
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