Annular honeycomb excitation vector-propelled double-rotor aircraft

An umbrella-shaped, soil-based technology, applied to aircraft, rotorcraft, power plant types, etc., can solve problems such as inability to realize aircraft flight, difficulty in aircraft performance, and long engine development cycle

Inactive Publication Date: 2018-11-06
燕胜
View PDF6 Cites 1 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] At present, most aircraft adopt a single-rotor design. The improvement of flight speed and efficiency mainly depends on improving the engine design, and the development cycle of the engine is very long. It is difficult to improv

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Annular honeycomb excitation vector-propelled double-rotor aircraft
  • Annular honeycomb excitation vector-propelled double-rotor aircraft
  • Annular honeycomb excitation vector-propelled double-rotor aircraft

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0021] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0022] see Figure 1-10 , including two rotor bodies and a connecting bridge connecting the two rotor bodies,

[0023] The rotor body includes an excitation pole housing 1, which is annular, and the excitation pole housing 1 is a ring-shaped housing spliced ​​by a plurality of triangular uniformly distributed iron sheets 15.

[0024] A support frame 3 is installed on the upper part of the excitation pole housing 1, a ball hinge shaft 5 is installed at the cen...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

PUM

No PUM Login to view more

Abstract

The invention discloses an annular honeycomb excitation vector-propelled double-rotor aircraft. The annular honeycomb excitation vector-propelled double-rotor aircraft comprises two rotor bodies and aconnecting bridge for connecting the two rotor bodies, wherein each rotor body comprises an excitation pole shell; the excitation pole shell is annular; an excitation wall is arranged on the inner wall of the excitation pole shell; a supporting frame is mounted on the upper part of the excitation pole shell; a ball hinge shaft is mounted at the center of the supporting frame; a propeller is mounted on the end part of the ball hinge shaft, so that the propeller rotates around the ball hinge shaft; a propeller ball hinge hole is formed in the center of the propeller, and is matched with the ball hinge shaft to form movable connection; the propeller has four blades; permanent magnets are arranged on the end parts of the blades; the permanent magnets are hollow; hollow cavities are formed inthe middle parts of the permanent magnets; springs are fixed to the inner walls of the cavities.

Description

technical field [0001] The invention relates to an annular honeycomb excitation vector propulsion double-rotor aircraft. Background technique [0002] At present, most aircraft adopt a single-rotor design. The improvement of flight speed and efficiency mainly depends on improving the engine design, and the development cycle of the engine is very long. It is difficult to improve the performance of the aircraft by increasing the thrust of the engine in a short period of time. The existing dual-rotor aircraft relies on ordinary propellers. The motor and control system cannot realize the flight of the aircraft. Contents of the invention [0003] In view of the above existing problems, the present invention provides a circular honeycomb excitation vector propulsion birotor aircraft, and the normal control of the biplane aircraft can be realized by vector propulsion of the screw motor. [0004] In order to achieve the above object, the technical solution provided by the present...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

Application Information

Patent Timeline
no application Login to view more
IPC IPC(8): B64C27/08B64C27/12B64D27/24
CPCB64C27/08B64C27/12B64D27/24
Inventor 燕胜鲁晨熊宇
Owner 燕胜
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap