Shock-absorbing device and unmanned aerial vehicle
A shock absorbing device and aircraft technology, applied in the field of aircraft, to achieve miniaturization, small size, and improved stability
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment 1
[0051] see figure 2 as shown, figure 2 It is an exploded schematic diagram of a shock absorbing device provided in Embodiment 1. The shock absorbing device 100 provided in this embodiment includes a first connecting piece 10, two second connecting pieces 20 and four shock absorbing pieces 30, each The second connecting piece 20 is connected to the first connecting piece 10 through two shock absorbing pieces 30;
[0052] see image 3 as shown, image 3 It is a schematic cross-sectional structure diagram of a single shock absorber 30 provided in Embodiment 1, each shock absorber 30 includes: a shock absorber body 31, and the shock absorber body 31 includes a flexible cavity 310 with an opening; a throttle valve 32 , the throttle valve 32 is correspondingly arranged at the opening of the flexible cavity 310 ; each throttle valve 32 has at least one throttle hole 321 connecting the interior of the flexible cavity 310 with the external environment.
[0053] In specific implem...
Embodiment 2
[0084] Based on the same inventive concept, this embodiment provides an unmanned aerial vehicle, see Figure 5 as shown, Figure 5 It is a schematic diagram of the exploded structure of the unmanned aerial vehicle provided in the second embodiment. The unmanned aerial vehicle provided in this embodiment includes the aircraft body 200 and the camera device 300, and also includes a shock absorbing device 100 as provided in the first embodiment above. The camera device 300 passes through A shock absorbing device 100 is mounted on the aircraft body 200 .
[0085] In specific implementation, there is at least one camera, and a plurality of camera devices can be set on an aircraft body according to actual use requirements; The camera device is installed on the aircraft body through a plurality of damping devices, which further improves the shock absorption effect of the camera device.
[0086] In the unmanned aerial vehicle provided in this embodiment, the aircraft body and the im...
PUM
Abstract
Description
Claims
Application Information
- R&D Engineer
- R&D Manager
- IP Professional
- Industry Leading Data Capabilities
- Powerful AI technology
- Patent DNA Extraction
Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.
© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com