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Damping device and aircraft employing same

A shock absorbing device and a technology for an aircraft, applied in the field of aircraft, can solve problems such as the inability of aircraft to meet, and achieve the effect of suppressing or eliminating shock vibration

Active Publication Date: 2015-02-25
SZ DJI TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In this way, the vibration generated by the power unit on the fuselage will be directly transmitted to the load, causing the load to vibrate with the fuselage, so that the aircraft cannot meet the needs of practical applications.

Method used

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  • Damping device and aircraft employing same
  • Damping device and aircraft employing same
  • Damping device and aircraft employing same

Examples

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Embodiment Construction

[0027] Such as Figure 1 to Figure 4 As shown, a shock absorbing device 10 provided by an embodiment of the present invention reduces unnecessary vibrations for a load (not shown) mounted thereon, which includes a base 1, a mounting base 2 separated from the base 1 by a certain distance, At least one shock absorber 3 connected to both the base 1 and the mounting base 2 .

[0028] The base 1 includes a bottom plate 11 , a plurality of bottom arms 12 extending from the bottom plate 11 , and a first receiving groove 13 penetrating through the bottom arms 12 .

[0029] The at least one shock absorber 3 is spaced between the mounting seat 2 and the base 1 . The mounting base 2 includes a mounting plate 21 , a plurality of mounting arms 22 extending from the mounting plate 21 , and a second receiving groove (not labeled) passing through the mounting arms 22 .

[0030] In this embodiment, there are four bottom arms 12 and four mounting arms 22 each in a cross shape. Therefore, the...

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PUM

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Abstract

The invention discloses a damping device and an aircraft employing the same. The damping device comprises a base and an installing seat, there is a certain distance between the base and the installing seat, the damping device also comprises at least a damping piece clamped between the base and the installing seat and anti-falling pieces respectively connected with the base and the installing seat, one ends of the damping pieces are connected with the base, the other ends of the damping pieces are connected with the installing seat, and at least parts of the anti-falling pieces penetrate through the damping pieces. According to the damping device, the damping pieces are additionally arranged between the base and the installing seat so that a damping function is provided.

Description

【Technical field】 [0001] The invention belongs to the technical field of aircraft, and in particular relates to a damping device and an aircraft using the damping device. 【Background technique】 [0002] The aircraft in the related art usually carries a load to realize a specific function, for example, when the load is a camera or video camera, it can be carried on the aircraft to realize aerial photography. The aircraft includes a fuselage and a power device connected to the fuselage to provide flight power for the aircraft. The payload is connected to the fuselage. [0003] However, in the aircraft of the related art, the load and the fuselage adopt a hard connection method of direct connection. In this way, the vibration generated by the power unit on the fuselage will be directly transmitted to the load, causing the load to vibrate along with the fuselage, so that the aircraft cannot meet the requirements of practical applications. [0004] Therefore, it is necessary t...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F16F7/108F16F15/08B64D47/08
CPCB64D47/08F16F7/108F16F15/08
Inventor 林源赵涛
Owner SZ DJI TECH CO LTD
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