Single-actuating type magneto-rheological shock absorber used for aircraft landing gear
A magneto-rheological shock absorber and aircraft landing gear technology, which is applied in the direction of shock absorbers, springs/shock absorbers, shock absorbers, etc., can solve the problem of increasing the mass of landing gear, reducing the shock-absorbing performance and shock-absorbing effect, etc. problems, to achieve the effect of reducing settlement and silting, reducing viscous force, and compact piston structure
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[0036] The present invention will be further described in detail below in conjunction with the accompanying drawings and through specific embodiments.
[0037] A single-acting magneto-rheological shock absorber for aircraft landing gear, such as Figure 1 to Figure 3 As shown, it includes an outer cylinder 3, an inner cylinder 7, a piston rod 6, a piston assembly, and a wheel shaft base 5. The top of the outer cylinder is a flange structure, and the top of the outer cylinder is sealed with an end cover 10. The outer cylinder The inner cylinder is coaxially slidably installed in the lower end, and the lower end of the inner cylinder is threaded to install the wheel axle base, and the piston rod is coaxially installed in the inner and outer cylinders, and the upper end of the piston rod is coaxially fixed on the Below the end cover, a piston assembly is installed on the lower end of the piston rod, and the outer edge of the piston assembly is in frictional contact with the inner...
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