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Loading support for aircraft, aircraft and shock absorption method for aircraft

A technology for loading brackets and aircraft, applied in the aviation field, can solve the problems of insignificant anti-vibration effect, limited performance of shock absorbers, etc., and achieve the effects of improving anti-vibration performance, good stability, and increasing inertia

Active Publication Date: 2014-04-23
SZ DJI OSMO TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, this anti-vibration solution will be limited by the performance of the shock-absorbing device, and the anti-vibration effect is not obvious

Method used

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  • Loading support for aircraft, aircraft and shock absorption method for aircraft
  • Loading support for aircraft, aircraft and shock absorption method for aircraft
  • Loading support for aircraft, aircraft and shock absorption method for aircraft

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Embodiment Construction

[0024] Please refer to figure 1 with figure 2 , figure 1 is a top view of the aircraft of the embodiment of the present invention, figure 2 yes figure 1 A cross-sectional view of the aircraft along dashed line A-A' is shown.

[0025] Such as figure 1 with figure 2 As shown, the aircraft 10 of the present invention includes a frame assembly 11 , a loading bracket 12 and a shock absorbing assembly 13 . Wherein, the loading bracket 12 includes a loading platform assembly 121 on which a photographing device 123 is installed and a component mounting position 122, and the components set on the component mounting position 122 are fixedly connected with the loading platform assembly 121 as a whole. The loading bracket 12 is connected with the frame assembly 11 of the aircraft 10 through the shock absorbing assembly 13 .

[0026] It should be noted that the loading bracket 12 of this embodiment can be connected to the shock absorbing assembly 13 by screwing or riveting, and f...

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PUM

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Abstract

The invention discloses a loading support for an aircraft, the aircraft and a shock absorption method for the aircraft. The loading support for the aircraft is used for being connected with the rack assembly of the aircraft by a shock absorption assembly; the loading support comprises a carrying platform assembly provided with a shooting device and a component installation position, wherein a component arranged on the component installation position is fixedly and integrally connected with the carrying platform assembly. By virtue of the mode abovementioned, according to the loading support, the aircraft and the shock absorption method disclosed by the invention, the shock resistance performance of the loading support can be improved, thus improving the aerial photography effect of the aircraft.

Description

technical field [0001] The invention relates to the field of aviation technology, in particular to a loading bracket of an aircraft, an aircraft and a shock absorbing method thereof. Background technique [0002] With the development of science and technology, it is more and more common to use the aircraft carrying the camera for aerial photography. During the flight, the aircraft will vibrate due to the rotation of the rotor, which will affect the shooting effect of the camera, and anti-vibration design is required. The anti-shock solution in the prior art is to install a shock-absorbing device between the pan-tilt carrying the camera and the frame. However, this anti-vibration solution is limited by the performance of the shock-absorbing device, and the anti-vibration effect is not obvious. Contents of the invention [0003] The technical problem mainly solved by the embodiments of the present invention is to provide a loading bracket for an aircraft, an aircraft and a...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D47/08
Inventor 肖文龙张宝燕陶冶
Owner SZ DJI OSMO TECH CO LTD
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