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Damping platform and unmanned aerial vehicle

A platform and installation platform technology, applied in the field of aircraft accessories, can solve the problems of easy aging and short life, and achieve the effect of improving stability

Pending Publication Date: 2021-12-24
SICHUAN AEE AVIATION TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The main purpose of the present invention is to provide a shock-absorbing platform, which aims to solve the problems of short life, easy aging and consistent material properties of traditional silicon capsules

Method used

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  • Damping platform and unmanned aerial vehicle
  • Damping platform and unmanned aerial vehicle
  • Damping platform and unmanned aerial vehicle

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Embodiment Construction

[0029] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0030] It should be noted that all directional indications (such as up, down, left, right, front, back...) in the embodiments of the present invention are only used to explain the relationship between the components in a certain posture (as shown in the accompanying drawings). Relative positional relationship, movement conditions, etc., if the specific posture changes, the directional indication will also change accordingly.

[0031] In the present in...

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Abstract

The invention discloses a damping platform and an unmanned aerial vehicle. According to the damping platform disclosed by the invention, a damping assembly is mounted between a first mounting platform and a second mounting platform, so that the damping effect is achieved; the damping assembly of the damping platform comprises first valve bodies and second valve bodies, the first mounting platform is connected with the first valve bodies, the second mounting platform is connected with the second valve bodies, and the second valve bodies are hollow; and the first valve bodies are movably mounted to the second valve bodies, the first valve bodies and the second valve bodies are sealed internally to form cavities, and the first mounting platform and the second mounting platform are connected through the first valve bodies and the second valve bodies. The cavities are vacuumized, the resistance of air in the cavities generates the damping effect, and the air resistance forms a pressure opposite to the acting force transferred from the second mounting platform in direction, so that the first mounting platform is prevented from swinging and vibrating, and the stability of the first mounting platform is improved, thereby taking the damping effect on a flight control main body part mounted on the first mounting platform.

Description

technical field [0001] The invention relates to the technical field of aircraft accessories, in particular to a shock-absorbing platform and an unmanned aerial vehicle. Background technique [0002] During the flight of the drone in the air, there are often engine and blade movements or the impact of the airflow, which will continue to shake and vibrate, and it is easy to be applied to the electronic equipment such as the flight controller and sensors in the drone. It produces strong shock and vibration, which makes it difficult to ensure the normal operation of electronic equipment when the drone is flying. Therefore, it is necessary to provide reliable shock-absorbing protection for the electronic equipment on the drone or install the electronic equipment on a shock-absorbing platform to prevent the electronic equipment from being damaged by vibration when the drone encounters airflow or takes off and lands, ensuring that the drone The normal operation of flight control a...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F16F15/02F16F15/023F16F15/04B64C39/02B64D47/00
CPCF16F15/022F16F15/0232F16F15/046B64D47/00B64C39/02
Inventor 张显志杨光学
Owner SICHUAN AEE AVIATION TECH CO LTD
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