Unlock instant, AI-driven research and patent intelligence for your innovation.

Wind-ball roller-wing aircraft

A technology of roller wings and wind balls, which is applied in the field of aviation aircraft, can solve the problems of difficult short-distance take-off and landing, poor flexibility of aircraft, and a small range of adjustable lift, so as to achieve the effect of flying maneuverability

Active Publication Date: 2015-07-22
保定国奥新能源工程材料科技有限责任公司
View PDF6 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Traditional aircraft wings are fixed, and the lift force can be adjusted in a small range, making it difficult to achieve short-distance take-off and landing, and the flexibility of the aircraft is poor

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
  • Wind-ball roller-wing aircraft

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0010] now attached figure 1 The present invention is described in detail: a kind of wind bulb roller wing aircraft, comprises fuselage 1, power unit, left wing 3, right wing 4, empennage and landing gear 7. Fuselage 1 is equipped with control system and airborne equipment. Landing gear 7 adopts rear three-point type wheeled landing gear. The power device includes an energy supply system and a puller 2 . The tension device 2 is installed on the front end of the fuselage 1, and the tension device 2 adopts the mode of a piston engine and a propeller, and provides energy with fuel oil. The left wing 3 and the right wing 4 have the same structure and size and are symmetrically arranged on the left and right sides of the longitudinal symmetry plane of the fuselage 1 . The left wing 3 includes a left motor 31 , a left clutch 32 , a left wing shaft 33 , a left roller wing 34 and a left wind ball 35 . The right wing 4 includes a right motor 41 , a right clutch 42 , a right wing sh...

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 relates to a wind-ball roller-wing aircraft, belonging to the technical field of aviation aircrafts. The wind-ball roller-wing aircraft comprises a fuselage, a power device, a left wing, a right wing, an empennage and an undercarriage. The power device comprises an energy supply system and a propeller or towing force device. The left wing and the right wing are the same in structure and size and are symmetrically arranged at the left and right sides of a longitudinal symmetric plane of the fuselage. The left wing comprises a left electromotor, a left clutch, a left wing shaft, a left roller wing and a left wind ball. The right wing comprises a right electromotor, a right clutch, a right wing shaft, a right roller wing and a right wind ball. Under the action of forwards-coming flow, the left wind ball and the right wind ball can rotate, and looking right from the left side of the fuselage, the left roller wing is driven to do clockwise rotation by the left wind ball; the right roller wing is driven to also do clockwise rotation by the right wind ball. Under the combined action of the forwards-coming flow and circulatory flow of the rotating left and right roller wings, an upward lifting force is generated by the left and right roller wings, so that the aircraft can fly in the air. The aircraft disclosed by the invention can achieve STOL (Short Take Off and Landing) and is maneuverable and flexible in flight.

Description

technical field [0001] The utility model relates to a wind balloon roller-wing aircraft, which belongs to the technical field of aviation aircraft, and in particular relates to a roller-wing aircraft. Background technique [0002] Traditional aircraft wings are fixed, and the lift force can be adjusted in a small range, so it is difficult to realize short-distance take-off and landing, and the flexibility of the aircraft is relatively poor. Contents of the invention [0003] The purpose of the invention is to overcome the above-mentioned shortcomings of traditional fixed-wing aircraft, and to invent a wind bulb roller-wing aircraft capable of short-distance take-off and landing and flexible flight. [0004] A wind balloon roller wing aircraft comprises a fuselage, a power plant, a left wing, a right wing, an empennage and a landing gear. The fuselage is equipped with a control system and airborne equipment. The landing gear adopts rear three-point wheeled landing gear. ...

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): B64C39/00
Inventor 王志成
Owner 保定国奥新能源工程材料科技有限责任公司