Air vehicle with buffering structure and working method
A buffer structure and working method technology, applied in the field of aircraft, can solve the problems of damage to the service life of the aircraft, the inability to adjust the gradient, and insufficient buffer effect, etc., to achieve the effects of extending the service life, improving the buffer effect, and improving the buffer effect
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[0034] The first embodiment:
[0035] Such as Figure 1 to Figure 3 As shown, the aircraft with a buffer structure of this embodiment includes a frame 10, a buffer assembly 20, and a first pushing assembly 30.
[0036] The rack 10 has a receiving groove 11. The buffer assembly 20 is arranged in the receiving groove 11, the first pushing assembly 30 is arranged on the frame 10, the first end of the first pushing assembly 30 is connected to the frame 10, and the second end of the first pushing assembly 30 is connected to the buffer assembly 20. Connected, the first pushing assembly 30 has a telescopic structure, and the telescopic structure is used to drive the buffer assembly 20 to move.
[0037] Specifically, the first pushing assembly 30 includes a hydraulic assembly 31 and a telescopic structure 32 connected in sequence, and the telescopic structure 32 is connected to the buffer assembly 20. The buffer assembly 20 includes a first connecting block 21, an elastic member 22, a sec...
Example
[0047] The second embodiment:
[0048] The aircraft of this embodiment is basically the same as the above-mentioned first embodiment, and only the differences will be described in detail below.
[0049] Such as Figure 4 As shown, the first pushing assembly 30 of this embodiment includes a first motor 41, a driving gear 42, a first driven gear 44, a first connecting rod 45, a second driven gear 46, and a first screw rod 47, which are sequentially connected. , The first screw rod 47 is connected to the buffer assembly 20 (refer to the first embodiment for the structure). When the second driven gear 46 rotates, the first screw rod 47 moves along the axis of the second driven gear 46. The first pushing assembly 30 also includes a third driven gear 51, a second connecting rod 52, a fourth driven gear 53, and a second screw rod 54 that are sequentially connected, the second screw rod 54 and another buffer assembly 20 (structure reference The first embodiment) is connected, when the fou...
Example
[0053] The third embodiment:
[0054] The aircraft of this embodiment is basically the same as the above-mentioned first embodiment, and only the differences will be described in detail below.
[0055] The aircraft also includes a wing and a power mechanism. The power mechanism is connected to the wing, and the control unit is connected to the power mechanism; the control unit has a comparison module, which is used to compare whether the ratio of the pressure detection value of the pressure sensor to the set pressure value exceeds the set pressure value. When the ratio of the pressure detection value to the set pressure value exceeds the set range, the control unit increases the power of the power mechanism.
[0056] The working method of this embodiment also includes the following steps:
[0057] T1: When the comparison module compares the ratio of the pressure detection value of the pressure sensor to the set pressure value exceeds the set range, the control unit increases the power...
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