Flight control shock absorption device and unmanned aerial vehicle
A shock-absorbing device and flight control technology, applied in shock absorbers, aircraft parts, springs/shock absorbers, etc., can solve problems such as drone execution deviation, flight control system impact, crashes, etc., to absorb impact kinetic energy , Safe and reliable operation, good shock absorption effect
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
no. 1 example
[0035] figure 1 For the overall structure diagram of the flight control damping device 100 provided in the first embodiment of the present invention, please refer to figure 1 .
[0036] The flight control shock absorbing device 100 provided in this embodiment is used for buffering, shock absorbing and fixing the flight control box 101 . The flight control damping device 100 includes a shock absorbing plate 110 , a first support 120 , a second support 130 and a non-Newtonian fluid buffer layer 140 . The first support 120 and the second support 130 are respectively arranged on two sides of the flight control box 101 . One end of the first support 120 is connected to the damping plate 110 , and the other end of the first support 120 is connected to the flight control box 101 . One end of the second support 130 is connected to the flight control box 101 , and the other end of the second support 130 is connected to the non-Newtonian fluid buffer layer 140 .
[0037] Both the fir...
no. 2 example
[0045] image 3 For the structural schematic diagram of the non-Newtonian fluid column 125 of the flight control damping device 100 provided in the second embodiment of the present invention, please refer to image 3 .
[0046] In this embodiment, both the first pillar 120 and the second pillar 130 use the non-Newtonian fluid column 125 , and the second pillar 130 is also immersed in the non-Newtonian fluid buffer layer 140 . Preferably, the non-Newtonian fluid column 125 includes a locking splint 147, a buffer strip 145, a waterproof splint 143, an elastic pad 149 and a non-Newtonian fluid layer 141, and the two ends of the non-Newtonian fluid layer 141 are respectively connected to the waterproof splint 143, and the waterproof splint 143 is away from the non-Newtonian fluid layer 143. One side of the Newtonian fluid layer 141 is connected to the buffer strip 145 , and the side of the buffer strip 145 away from the waterproof splint 143 (that is, the buffer strip 145 is away...
no. 3 example
[0059] Figure 6 Another schematic diagram of the overall structure of the flight control damping device 100 provided in the third embodiment of the present invention, please refer to Figure 6 .
[0060]The flight control shock absorbing device 100 provided in this embodiment is used for the flight control box 101, and includes a first shock absorber 111, a second shock absorber 113, a first strut 120 and a second strut 130, the first strut 120 and the second strut 130. The second support 130 adopts the non-Newtonian fluid column 125, of course, it can also include the non-Newtonian fluid column 125 and the spring at the same time. The first shock absorber 111 and the second shock absorber 113 are arranged oppositely, the flight control box 101 is arranged between the first shock absorber 111 and the second shock absorber 113, the first shock absorber 111 and the second shock absorber 113 plays a role of fixing and damping the flight control box 101 . Both ends of the firs...
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