A multi-axis fixed-wing aircraft
An aircraft and fixed-wing technology, applied in the field of aircraft, can solve the problems of short sailing time, slow flying speed, unable to hover at a fixed point, etc., and achieve the effects of long sailing time, stable flight process and high safety factor
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment 1
[0021] Embodiment one: a multi-axis fixed-wing aircraft, comprising a fuselage 1, a left wing 2, a right wing 3, an empennage 4, a thrust device 5, a joystick 6, a rotating shaft 7, and a flight control device 9; the left wing 2 and the right wing 3 have certain Angle of attack, the left wing 2 and the right wing 3 are symmetrically arranged on the left and right sides of the fuselage 1; the empennage 4 is arranged at the rear end of the fuselage 1; Lively connected with right wing 3 and horizontally arranged on the center of lift of left wing 2 and right wing 3. Both the left wing 2 and the right wing 3 are provided with ailerons 25 and flaps 26; the thrust device 5 provides thrust in the form that the motor 51 drives the propeller 52 to rotate, and the motor 51 is connected with the rotating shaft 7 through the support frame 8 and installed on the support frame A plurality of motors 51 on the 8 are evenly arranged on the leading edge, the trailing edge and the tip of the win...
Embodiment 2
[0034]Embodiment two: a multi-axis fixed-wing aircraft, comprising a fuselage 1, a left wing 2, a right wing 3, an empennage 4, a thrust device 5, a joystick 6, a rotating shaft 7, and a flight control device 9; the left wing 2 and the right wing 3 have certain Angle of attack, the left wing 2 and the right wing 3 are symmetrically arranged on the left and right sides of the fuselage 1; the empennage 4 is arranged at the rear end of the fuselage 1; Lively connected with right wing 3 and horizontally arranged on the center of lift of left wing 2 and right wing 3. Both the left wing 2 and the right wing 3 are provided with ailerons 25 and flaps 26; the thrust device 5 provides thrust in the form that the motor 51 drives the propeller 52 to rotate, and the motor 51 is connected with the rotating shaft 7 through the support frame 8 and installed on the support frame A plurality of motors 51 on the 8 are evenly arranged on the leading edge, the trailing edge and the tip of the wing...
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