Multidimensional dynamic active variant flapping wing aircraft
A flapping aircraft and variant technology, applied in the field of multi-dimensional dynamic active variant flapping aircraft, can solve the problems of low aerodynamic efficiency and large energy consumption of flapping mechanism, and achieve the effects of reducing energy consumption and flexible maneuvering flight capability.
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment Construction
[0023] Please refer to figure 1 and figure 2 As shown, the overall structure of the multi-dimensional dynamic active variant flapping wing aircraft of the present invention is composed of a fuselage 1, a flapping wing 2, an empennage 3, a control system 4 and an actuation system (not marked); wherein the flapping wing consists of a wing skin 5 and a flapping wing The wing leading edge skeleton is composed of the wing skin 5 made of elastic organic film material; the control system 4 is installed in the fuselage, and is connected with various mechanisms of the actuating system by a circuit.
[0024] Please refer to figure 1 and figure 2 As shown, the shape of the flapping wing 2 of the multi-dimensional dynamic variant flapping wing aircraft of the present invention is as follows: figure 2 As shown, the shape of the flapping wing 2 when flapping and shrinking is as follows: figure 1 shown. Since the area of the flapping wing increases when it is deployed downwards, an...
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