Multi-flapping-wing aircraft and flying control method thereof
A flapping wing aircraft and wing technology, applied in the field of aircraft, can solve the problems of complex flapping wing mechanism, small lift, difficulty in increasing wing swing frequency, etc., and achieve the effects of low manufacturing cost, large torque, and less magnetic flux leakage
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment Construction
[0032] The present invention will be further described below in conjunction with accompanying drawing.
[0033]Overall structure of the present invention is as figure 1 As shown, the long dashed line is the first hinge axis of the left front flapping wing mechanism, and the short dashed line is the shortest line segment between the first hinge axis of the left front flapping wing mechanism and the vertical axis of the flapping wing aircraft. The specific structure includes frame 1 (such as Figure 8 As shown), there is a landing gear below the frame 1, and when the flapping-wing aircraft is parked on a horizontal plane, the bottom surface of the frame 1 is parallel to the horizontal plane. figure 2 It is a plan view that the left front and right rear wings of the present invention swing clockwise to the maximum angle around the second hinge and the left rear and right front wings swing counterclockwise to the maximum angle around the second hinge. image 3 It is a plan view ...
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