Morphing aircraft with variable swept wings and head deflection
A variant aircraft and aircraft technology, applied in the field of variant aircraft, can solve the problems of uneven streamline of the fuselage and complex configuration of the variant aircraft, and achieve smooth streamline, increase lift, and increase force area. Effect
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment Construction
[0034] In order to make the purpose, technical solution and advantages of the present application clearer, the implementation manners of the present application will be further described in detail below in conjunction with the accompanying drawings.
[0035] First combine the following figure 1 A possible system architecture applicable to the embodiments of the present application is introduced.
[0036] Please refer to figure 1 , which exemplarily shows a schematic structural diagram of a low-sonic time-axis view of a variant aircraft with variable-sweep wings and head deflection applicable to the embodiment of the present application.
[0037] Such as figure 2 As shown, it is a schematic diagram of the front view structure of a variant aircraft with variable sweep and head deflection provided by the embodiment of the present application at low supersonic speed.
[0038] The variant aircraft with variable swept wing and head deflection provided by the present application ...
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