CN1433930A

CN1433930A - Disk shape aerobat

Info

Publication number: CN1433930A
Application number: CN 03114854
Authority: CN
Inventors: 于明华
Original assignee: Individual
Current assignee: Individual
Priority date: 2003-01-13
Filing date: 2003-01-13
Publication date: 2003-08-06

Abstract

The present invention relates to a disk shape aerobat. It possesses the double functions of helicopter and general aircraft, not only can be flown quickly, far and highly, can be vertically lifted and landed, and can be stopped in the sky, but also can be flown slowly and can implement minimum altitute flying like helicopter. Besides, it has good balance ability, and can safety pass through violent typhoon and tornado.

Description

The disc-shaped aircraft

Affiliated technical field

The present invention relates to a kind of aircraft.

Background technology

At present, known aircraft has two big classes: a class is various types of conventional airplanes, and another kind of is autogyro.The flying speed of conventional airplane also can fly very highly than very fast, but its shortcoming is can not vertical lift and aloft certain a bit keeps static; Autogyro can vertical lift and aloft certain a bit keeps static, but that its shortcoming is a flying speed is slow, and can not fly De Taigao.

Summary of the invention

The invention provides a kind of aircraft, this aircraft has two outstanding features: the one, and the external form of disc; The 2nd, the whole rotation of the shell of the aircraft storehouse, top and Lower Hold of parallel motion driving engine (installed except), the effect of rotation has two: the one, provide lift to aircraft; The 2nd, make aircraft keep balance.

The technical solution adopted for the present invention to solve the technical problems is: 1. the exterior design of aircraft becomes disc.2. aircraft is made up of the two large divisions, it is respectively the non-high speed revolution part of high speed revolution partial sum, wherein high speed revolution partly is the shell of aircraft, all the other all are non-high speed revolution part (comprise storehouse, top, Lower Hold), this two large divisions couples together by an axle, wherein high speed revolution part flexibly connects (that is: this part can around the axle high speed revolution) with axle, and non-high speed revolution part is captiveed joint with axle.Storehouse, top and Lower Hold are cockpit and manned storehouse, shell is a high speed revolution part of keeping the aircraft balance, and the bottom surface of shell is provided with wing plate, and the inside of shell is the loading storehouse of aircraft, but, therefore article must be fixed in the storehouse because shell is among the high speed revolution always.3. provide power at a pair of driving engine of aircraft skin edge designs for the rotation of shell, the high speed revolution one of shell is a balance of keeping aircraft, the 2nd, provide lift by the wing plate that is arranged on the shell bottom surface to aircraft.4. respectively design a driving engine at the storehouse, top of aircraft and Lower Hold and provide power for the parallel motion of aircraft.5. provide power at put-put of the storehouse, top of aircraft edge designs for aircraft turning in the horizontal direction, storehouse, top, Lower Hold, axle and parallel motion driving engine can rotate freely under this level turns to the promotion of driving engine.6. the principle of work of aircraft.Lift-off: start the shell rotary engine---is opened the wing plate on the shell---when the shell rotation reaches certain rotating speed aircraft lift-off; Flight: start the parallel motion driving engine when aircraft rises to certain altitude---aircraft is flat to fly, along with the quickening gradually of level speed can be turned the wing plate angle slowly down and reduce shell rotary engine rotating speed, can close wing plate fully when flying to reach certain speed and the rotative speed of shell also can be reduced to minimum (can keep the aircraft balance get final product) when flat, air acted on resistance that the shell bottom surface the produced component at vertical direction when the lift of aircraft came from aircraft and advances at this moment.The flat Cheng Zhongru that flies over thinks that the lifting aircraft then can be by regulating parallel motion driving engine or shell rotary engine rotating speed or adjusting the wing plate angle and realize.In the time of need on horizontal surface, changing working direction, can turn to driving engine to realize by level; Land: close the parallel motion driving engine---aircraft speed of advance slow down gradually (restarting after when needs reduce speed of advance fast, can making contrarotation of parallel motion driving engine or Rotate 180 degree), flying height reduces gradually simultaneously---when dropping to certain altitude, opens by aircraft wing plate, adjust wing plate angle and shell rotary engine rotating speed and slowly land landing front opening foot rest or hook by aircraft.

The invention has the beneficial effects as follows: 1. the disc-shaped aircraft has autogyro and conventional airplane dual-use function concurrently, it not only can be swift-winged, fly far, fly high but also can vertical takeoff and landing and transfixion aloft, can also resemble to fly very slowly the autogyro and in hedgehopping; 2. the shell (only pushing up except storehouse and the Lower Hold) owing to the disc-shaped aircraft all is in the high speed revolution state always in flight course, therefore the disc-shaped aircraft has very strong balanced capacity, less object strikes will be difficult to make its lack of equilibrium, especially the external force of Chi Xuing is had no effect to its balance, therefore this aircraft can pass through blast air, even pass through 12 grades of typhoons and wind spout can lack of equilibrium, so this aircraft can aloft or at sea be executed the task under worst weather condition; 3. the disc-shaped aircraft can be as the loop wheel machine of autogyro as the handling object, and it is more laborsaving than autogyro, this is because the arm of force of the active force of disc-shaped aircraft is greater than by the arm of force of power, and the arm of force of the active force of autogyro is less than by the arm of force of power; 4. therefore it is readily embodied in vertical takeoff and landing waterborne and uses as the Drifting device disc-shaped aircraft owing to its special external form, it can also be dived beneath the water if necessary.

Description of drawings

The present invention is further described below in conjunction with accompanying drawing and example.

Fig. 1 is a disc-shaped aircraft front elevation.

Fig. 2 is a disc-shaped aircraft birds-eye view.

Fig. 3 is the scheme drawing of disc-shaped aircraft wing plate when opening.

Fig. 4 is a disc-shaped aircraft lands scheme drawing.

Fig. 5 is the disc-shaped aircraft scheme drawing that is provided with manned interior storehouse.

Fig. 6, Fig. 7 are the disc-shaped aircraft scheme drawings of other two kinds of forms.

Among the figure: 1. shell rotary engine, 2. parallel motion driving engine, 3. level turns to driving engine, 4. shell, 5. storehouse, top, 6. Lower Hold, 7. spool, and 8. wing plate, 9. supporting leg (three), 10. hook, in 11. storehouses, 12. air chambers (or vacuum chamber).

The specific embodiment

1. the structure of disc-shaped aircraft (see for details Fig. 1 ~ shown in Figure 4)

This aircraft is made up of the two large divisions, is respectively the non-high speed revolution part of high speed revolution partial sum, and wherein high speed revolution partly is the shell of aircraft, and all the other all are non-high speed revolution part (comprise storehouse, top, Lower Hold).The top is provided with a parallel motion driving engine (2) in the storehouse and a level turns to a driving engine (3) and a hook (10); Be provided with two shell rotary engines (1) and wing plate (8) in the shell; Be provided with a parallel motion driving engine (2) and three supporting legs (9) in the Lower Hold.Three parts couple together by axle (7), wherein push up storehouse partial sum Lower Hold part and captive joint with axle (7), and housing parts can rotate freely around axle (7).Supporting leg (9) is hidden in the Lower Hold, stretches out during aircraft lands again and opens; Hook (10) is hidden in the storehouse, top, stretches out during aircraft lands again and opens.The storehouse, top of aircraft and Lower Hold both can be used as cockpit and also can be used as manned storehouse, but because the little manned amount in storehouse is very limited.Part between aircraft skin and the interior storehouse is the loading storehouse, but because the shell of aircraft is in the high speed revolution state always therefore article and shell must be fixed together.

2. the effect of each parts of disc-shaped aircraft (see for details Fig. 1 ~ shown in Figure 4)

The effect of shell rotary engine (1) is to drive shell (4) rotation.The effect of shell (4) rotation has two: the one, keep the balance of aircraft, and the 2nd, cooperating to aircraft with wing plate (8) provides lift.When aircraft was in lift-off or landing period, the lift of aircraft mainly or was all provided by wing plate, and its power resources are shell rotary engine (1).When aircraft moving velocity in the horizontal direction acquires a certain degree, air acted on the resistance that the shell bottom surface produced when the lift of aircraft can all be advanced by aircraft provides at the component of vertical direction, its power resources are parallel motion driving engine (2), can close wing plate this moment fully, and the main task of shell rotary engine (1) this moment is that the rotating speed of shell is maintained the minimum standard that can keep the aircraft balance, sometimes even can temporary close shell rotary engine.Therefore owing to closed wing plate, shell (4) almost is to rotate under the situation that does not have what resistance to aircraft when normal flight, and the consumption of fuel of shell rotary engine this moment (1) is very low; The effect of parallel motion driving engine (2) also has two: the one, and moving in the horizontal direction to aircraft provides power, and the 2nd, provide lift by the shell bottom surface to aircraft; It is to provide power to aircraft turning in the horizontal direction that level turns to the effect of driving engine (3).

3. the principle of work of disc-shaped aircraft (see for details Fig. 1 ~ shown in Figure 4)

Start shell rotary engine (1), (1) drive shell (4) rotation---open wing plate (8), adjust the wing plate angle, the aircraft lift-off---is regained supporting leg (9) or hook (10)---and is started parallel motion driving engine (2), flying before the aircraft---the startup level turns to driving engine (3), then can make aircraft in horizontal surface, change working direction---after aircraft arrives at the destination, close parallel motion driving engine (2).As want emergency braking then can make (2) contrarotation (or restarting behind the Rotate 180 degree) that resistance is provided.After aircraft drops to certain altitude, open wing plate, can aircraft slowly be landed by adjusting wing plate angle and shell rotary engine rotating speed.Stretch out supporting leg or hook before the landing, the effect of hook is that aircraft is hung on the special-purpose support (as shown in Figure 4), and this is another landing mode.The approach such as rotating speed that need to prove the angle of rotating speed that aircraft can be by adjusting shell rotary engine (1) in flight course or wing plate (8) or parallel motion driving engine (2) in addition make that aircraft is flat to fly, climb, descends or static aloft.

4. as shown in Figure 5, when the disc-shaped aircraft need be used in a large number when manned, an interior storehouse can be set in its shell, (interior storehouse also can flexibly connect as shown in Figure 6 with axle) captiveed joint in interior storehouse with axle (7).Gap between interior storehouse and the shell can be that an air chamber also can make a vacuum chamber to reduce air resistance.

5. as shown in Figure 6, also the upper surface of disc-shaped aircraft can be designed to cambered surface and lower surface is designed to the plane.When this disc-shaped aircraft in horizontal surface during low-speed operations its lift be mainly derived from the wing plate that is located on the aircraft bottom surface, when this disc-shaped aircraft in horizontal surface during high-speed flight its lift then be mainly derived from the difference of pressure that air produces at aircraft upper surface and lower surface, this difference of pressure is different generation of speed when passing through the aircraft upper surface with lower surface owing to air, and this principle is identical with the wing of conventional airplane.

6. as shown in Figure 7, also the upper surface of disc-shaped aircraft all can be designed to identical cambered surface with lower surface.When its lift all derives from the wing plate that is located on the aircraft bottom surface to this disc-shaped aircraft.

Claims

1. aerodynamic type aircraft is characterized in that: have the external form of disc, its housing parts in the flight course storehouse, top and Lower Hold of parallel motion driving engine (installed except) is in the high speed revolution state always.

2. aircraft according to claim 1, it is characterized in that: this aircraft is made up of the two large divisions, it is respectively the non-high speed revolution part of high speed revolution partial sum, wherein high speed revolution partly is the shell of aircraft, all the other all are non-high speed revolution parts, these two parts couple together by an axle, and wherein high speed revolution part flexibly connects (that is: this part can around the axle high speed revolution) with axle, and non-high speed revolution part is captiveed joint with axle.

3. aircraft according to claim 1 is characterized in that: provide power at a pair of driving engine of aircraft skin edge designs for the rotation of aircraft skin.

4. aircraft according to claim 1 is characterized in that: respectively design a driving engine the upper end of axle (7) (promptly pushing up the storehouse) and lower end (being Lower Hold) and provide power for the parallel motion of aircraft.

5. aircraft according to claim 1 is characterized in that: provide power at put-put of the storehouse, top of aircraft edge designs for aircraft turning in the horizontal direction.

6. aircraft according to claim 1 is characterized in that: the high speed revolution of this aircraft partly is the shell (4) of aircraft, and the effect of shell high speed revolution mainly contains two: the one, keep the balance of aircraft; The 2nd, because be provided with wing plate in the aircraft skin bottom surface, wing plate can open or close and can adjust the angle between wing plate and shell bottom surface, and shell can provide lift to aircraft by wing plate when high speed revolution.

7. aircraft according to claim 1 is characterized in that: the inside of this aircraft skin can establish one manned in the storehouse, separate by an air chamber or a vacuum chamber between storehouse and the shell in manned.

8. aircraft according to claim 1, it is characterized in that: the non-high speed revolution of this aircraft partly is storehouse, top (5) and Lower Hold (6) and the axle (7) that the parallel motion driving engine has been installed, also have manned interior storehouse (11), the effect of these parts mainly is to promote aircraft parallel motion, driving or manned.