CN2923518Y

CN2923518Y - Circular jet-air aircraft

Info

Publication number: CN2923518Y
Application number: CN 200620083552
Authority: CN
Inventors: 李贤明
Original assignee: LI XAINMING
Current assignee: LI XAINMING
Priority date: 2006-04-28
Filing date: 2006-04-28
Publication date: 2007-07-18
Anticipated expiration: 2016-04-28

Abstract

The utility model relates to an aircraft in particular to a round jet aircraft, a real-meaning flying saucer with practicality value. The utility model includes an engine, a fuselage and an aircraft body. The utility model is characterized in that the aircraft body is a round shape, and the engine and fuselage is disposed in the inner aircraft body. The utility model has a small volume and small occupancy when parking; The utility model has a landing gear without wheels to save the efficient space; The utility model can vertically take off and land as well as hovering on the air without building planning runway. The engine is a plus force type fanjet aero-engine with 90 DEG of body rotation on the air and the air-intake opening at front and air-outlet opening at back. The flying direction and gesture control thereof is achieved by a rudder at the back of a horizontal fin and vertical fin. The engine takes advantages of high efficiency, low oil consumption, far flying head range, large driving force, stable flying and high horizontal cruising speeding to achieve a supersonic flight with long time and far distance. The utility model is installed as additions with navigation system, radar, weapon system and photographing equipment to ensure the functions of the superscout, rescue, transportation, surveying and mapping and combat on the air.

Description

Circular air injection aerial vehicle

(1) technical field

The utility model relates to a kind of aircraft, the jet capable device of especially a kind of circle.

(2) background technology

Existing in the world air injection aerial vehicle mainly comprises various erose jet airplane and disposable guided missile and carrier rocket, the jet capable device of legendary circle is not also really succeeded in developing, and scientists thinks that the performance-oriented truly flying saucer with practical value is impracticable on principle.

Aircraft such as the difform jet airplane of existing various uses have that volume is big, and flying speed is slow, and turn radius is big, the shortcoming of the landing and sliding distance that takes off.Remove minority jet fighter (as the sparrow hawk formula fighter plane of Britain), most of jet airplane does not possess vertical takeoff and landing and hovering function.

(3) summary of the invention

The utility model provides a kind of circular air injection aerial vehicle in order to remedy the deficiencies in the prior art, a kind of flying saucer truly with practical value.

The utility model is achieved through the following technical solutions:

Circular its special character of air injection aerial vehicle of the utility model is: airframe structure is circular, and the position of driving engine forms just as the single engine jet fighter of a driving engine below ventral is bowed downward to an annulus with the wing two ends at the center of fuselage.

The wing that the body of the circular air injection aerial vehicle of the utility model itself also is crooked.Connecting panel between driving engine and the body is made up of 4 wale pieces, 4 perpendicular faggings and 4 tilt props respectively.4 wale pieces horizontal tail just wherein, 4 perpendicular faggings are equivalent to normal limb.4 just oblique wings of tilt prop.

The circular air injection aerial vehicle of the utility model has alighting gear, no wheel; Adopt the vertical takeoff and landing mode; Driving engine adopts afterburning formula turbine fan jet aerial engine; Lift-off back body revolves and turn 90 degrees, engine inlet port forward, air nozzle high speed level cruise backwards, the control of heading and attitude are to finish by the yaw rudder of horizontal tail and normal limb back.

The circular air injection aerial vehicle of the utility model has two kinds of drone version and manned versions, the turbine fan jet drone version is because the space availability ratio height, need not consider the tolerance of aviator to supersonic flight, just as a driving engine oneself flies on high, can realize long-time, remote supersonic flight.The miniature self-service driving-type can adopt battery and fans drive, or is power with small-sized spark ignition engine.

The beneficial effects of the utility model are, volume is little, and it is little to take up room when parking; There is alighting gear not have wheel, alleviates own wt, save available space; Can vertical takeoff and landing, can aloft hover, need not build plane track, level cruise speed height, voyage are far away.

(4) description of drawings

Fig. 1 and Fig. 2 are that the structure of the circular air injection aerial vehicle of the utility model is vertically analysed and observe and front elevational schematic;

Fig. 3 and Fig. 4 are horizontal tail and normal limb structural front view and vertical cross-sectional schematic of the circular air injection aerial vehicle of the utility model;

Wherein: 1, body, 2, driving engine, 3, yaw rudder, 4, horizontal tail, 5, the oblique wing, 6, normal limb.

(5) specific embodiment

Accompanying drawing is a kind of specific embodiment of the present utility model.The circular air injection aerial vehicle of the utility model comprises body 1, driving engine 2, yaw rudder 3, horizontal tail 4, the oblique wing 5, normal limb 6.

Adopt the turbofan technology of aviation field maturation, particularly the engine efficiency height, oil consumption is low, voyage is far away, thrust is big, flying speed is high, the successful Application of the afterburning formula turbine fan jet aerial engine of having a smooth flight, and makes circular the succeeding in developing of aircraft of the utility model become possibility.

This aircraft lift-off back body revolves and turn 90 degrees, engine inlet port forward, air nozzle high speed level cruise backwards, the control of heading and attitude is to finish by the yaw rudder of horizontal tail and normal limb back, can vertical takeoff and landing, can aloft hover, need not build plane track.

Owing to have level cruise speed height, can realize the characteristics of long-time, remote supersonic flight, add that its volume is little, own wt is light, advantages such as saving available space can effectively improve it and use alerting ability, by installing navigationsystem, radar, armament systems additional and taking the photograph photographing device mutually, can possess aerial reconnaissance, rescue, transportation, mapping and fight function.

Claims

1. circular air injection aerial vehicle, comprise body (1), wing (4), (5), (6) and driving engine (2), it is characterized in that: body (1) is circular, and driving engine (2) connects by wing (4), (5), (6) between driving engine (2) and the body (1) at the center of body (1).

2. circular air injection aerial vehicle according to claim 1 is characterized in that: have alighting gear not have wheel.

3. circular air injection aerial vehicle according to claim 1 is characterized in that: driving engine is afterburning formula turbine fan jet aerial engine.