A landing gear aerodynamic load test device and its design method
A technology of aerodynamic load and test equipment, which is applied in the directions of ground equipment, transportation and packaging, and aircraft component testing, etc., can solve problems such as not being able to meet the test requirements, and achieve the effects of convenient implementation, novel structure, and cost saving
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[0031] The present invention will be described in detail below with reference to the accompanying drawings and examples. It should be noted that, in the case of no conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other. For the convenience of description, if the words "up", "down", "left" and "right" appear in the following, it only means that the directions of up, down, left and right are consistent with the drawings themselves, and do not limit the structure.
[0032] Such as Figure 1~3 As shown, a landing gear aerodynamic load test device provided in this embodiment includes a mounting frame 1 , a loading device 2 , a loading wire rope 3 , an angle sensor 4 and a mounting support 5 .
[0033] The mounting frame 1 is used to fix the landing gear 10 . The main shaft of the undercarriage 10 is fixed to the upper end of the mounting frame 1 by bolts. The dummy wheel assembly 11 is provided on the mounting frame...
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