An aircraft outer wing positioning and clamping device
A technology of positioning clamping and outer wings, which is applied in aircraft assembly, workpiece clamping devices, manufacturing tools, etc., to achieve the effects of internal stress balance, increased reliability, and less stress concentration
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment Construction
[0043] The present invention will be further described in detail below with reference to the accompanying drawings and embodiments. It should be noted that the following embodiments are intended to facilitate the understanding of the present invention, but do not limit it in any way.
[0044] The whole set of aircraft outer wing positioning and clamping mechanism is as follows: figure 1 As shown, the device is installed from left to right at the wingtip, wing center and wing tail.
[0045] Such as Figure 2-5 As shown, an aircraft outer wing positioning and clamping device can be used for both fixed wing clamping and positioning and folding wing clamping and positioning. The fixed base 6 is provided with a plurality of mounting holes, and according to the position of the outer wing of the clamped aircraft, the positions and quantities of different components can be adjusted as required.
[0046] The position of clamping the wingtip of the aircraft needs to be in accordance w...
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