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TEST STAND FOR CONDUCTING ENDURANCE TESTS OF FLYING VEHICLE LANDING GEAR

机译:进行飞行器起落架耐久性试验的试验台

摘要

FIELD: tests stands for conducting tests of full-scale undercarriages of flying vehicles. SUBSTANCE: proposed test stand includes drive with flywheel and several loading passages; each passage has pipe line with force-forming hydraulic cylinder whose one end is articulated on immovable base and other end is articulated with fixed undercarriage. Each loading passage is provided with crank and power hydraulic cylinder whose cavity is connected with cavity of force-forming hydraulic cylinder by means of pipe line; piston of power hydraulic cylinder is connected with crank which is linked with drive common for several loading passages. Drive is provided with flywheel. Each passage may be provided with additional hydraulic cylinder whose cavity is communicated with cavities of power and force forming cylinders through cocks; piston of additional hydraulic cylinder is connected with one end of flexible member of varying rigidity; its other end is secured immovably. EFFECT: reduced labor consumption and time for conducting tests. 5 cl, 4 dwg
机译:领域:测试代表对飞行器的全尺寸起落架进行测试。实质:建议的试验台包括带飞轮的驱动器和多个装载通道;每条通道的管路上都带有形成力的液压缸,液压缸的一端铰接在不动的基座上,另一端铰接在固定的底盘上。每个加载通道上设有曲柄动力液压缸,其腔体通过管路与成力液压缸腔体相连。动力液压缸的活塞与曲柄连接,曲柄与多个装载通道的公共驱动装置相连。驱动器配有飞轮。每个通道可设有附加的液压缸,其液压腔通过旋塞与动力和力形成缸的腔连通。附加液压缸的活塞与刚性不同的柔性件的一端相连。另一端固定不动。效果:减少了劳动消耗并减少了进行测试的时间。 5厘升,4载重吨

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