Air inflation device for high-pressure chamber and low-pressure chamber of buffering strut of aircraft landing gear
A technology for aircraft landing gear and buffer struts, which is applied to mechanical equipment, springs, shock absorbers, etc., can solve the problem of poor air tightness between the high and low pressure cavities between the inflatable equipment and the landing gear buffer strut, inaccurate control of the inflation volume, and the inflating process. Complex problems, to achieve the effect of good airtight performance, simple structure, precise control of air volume
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Publication Date
- 2015-04-01
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Abstract
Description
technical field
[0001] The invention relates to an inflatable device, in particular to an inflatable device for high and low pressure chambers of buffer struts of an aircraft landing gear, and belongs to the technical field of aircraft inflatable devices. Background technique
[0002] The main device for an aircraft to take off and land is the landing gear, which is a device used to support the weight of the aircraft and bear the corresponding load when the aircraft is parked, taxied, taken off, and landed on the ground. It dissipates and absorbs the impact energy of the aircraft during landing and taxiing.
[0003] When the aircraft is landing and rolling, the aerodynamic lift it receives is less than the gravity of the aircraft, the landing gear will be supported by the ground and the friction between the ground and the wheels. The force on the wheel and the moment relative to the center of gravity of the aircraft are an important part of the resultant force and moment on...
Examples
Embodiment Construction
[0012] Preferred embodiments of the present invention will be described in detail below with reference to the accompanying drawings.
[0013] As shown in the figure, the high and low pressure chamber inflation equipment for the cushioning strut of the landing gear of the aircraft according to the present invention includes a first straight-through 1, an inflation ball valve 2, an inflation switch 3, a main valve body 4, a second straight-through 5, a deflation ball valve 6, and a discharge valve. Air switch 7, fine-tuning switch 8 and pressure gauge 9; said main valve body 4 is provided with a valve cavity 10 horizontally inside, the left end of the valve cavity is blocked by a plug 11, the right end of the valve cavity 10 is connected with the second straight-through 5, the second Straight through 1 is connected with inflatable ball valve 2, and described inflatable ball valve 2 and deflated ball valve 6 are arranged side by side, and inflated ball valve 2 and deflated ball va...