CN102490560A

CN102490560A - Automotive airplane capable of taking off and landing vertically

Info

Publication number: CN102490560A
Application number: CN2011104103037A
Authority: CN
Inventors: 林志兴
Original assignee: Individual
Current assignee: Individual
Priority date: 2011-12-10
Filing date: 2011-12-10
Publication date: 2012-06-13

Abstract

The invention discloses an automotive airplane capable of taking off and landing vertically. The automotive airplane comprises a plane body, wheels, an engine, a horizontal rudder and a steering rudder, and is characterized in that: the engine is arranged on a handpiece; the rotating shaft of the engine is connected with a fan blade of a high-pressure fan; the plane body is provided with a high-pressure annular air pipe; a shell of the fan blade of the fan is connected with the high-pressure annular air pipe; large-air exhaust pushing pipes of which the openings are downwards, outwards and backwards on the tail part respectively are arranged on the front and rear sides of two sides of the high-pressure annular air pipe; and small-air exhaust pushing pipes of which the openings are downwards are arranged on the front and rear sides of two sides and in the middle of the high-pressure annular air pipe. The automotive airplane has the advantages of simple structure, easiness in manufacturing, low cost and convenience for operation.

Description

A kind of ability VTOL carplane

Technical field

The present invention relates to a kind of carplane technical field, particularly a kind of design and manufacturing of ability VTOL carplane.

Background technology

Along with the development of national economy fast speed, people's living standard improves day by day, and the People more and more of purchasing automobile is many, and arteries of communication is very obstructed, seriously influences people's live and work.The development carplane is opened up a road in the air, can alleviate the pressure of surface road traffic, and real society is significant.Number of patent application is: 99119836.0, a kind of " Helitruck aircraft " disclosed, and it is provided with front wing, roof limb and three aerofoils of tailplane.Mechanical accident appears in this patent application power machine transmission more complicated easily.The present invention develops that a kind of mechanical drive is simple, mechanical accident is few, easy to operate a kind of can the VTOL carplane, will obtain people's welcome.

Summary of the invention

The purpose of this invention is to provide a kind of ability VTOL carplane, to overcome the deficiency that present carplane exists.

In order to realize above-mentioned purpose; A kind of ability VTOL carplane provided by the invention; Comprise fuselage 1, wheel 2, driving engine 3, diving rudder 8 and turn to rudder 9, tool present technique scheme: described driving engine 3 is located on the head, and the rotating shaft of driving engine links to each other with the high pressure positive blower fan blade 4 of setting; Described fuselage 1 is provided with high pressure air loop duct 5; The shell of described impeller of blower 4 contains mutually with high pressure air loop duct 5 and connects; Be respectively equipped with in the front and back on these high pressure air loop duct 5 both sides that Open Side Down, opening outwards and the big air draft backward of afterbody opening promote pipe 6; Front and back and middle part on these high pressure air loop duct 5 both sides also are respectively arranged with the float wind promotion pipe 7 that Open Side Down; The described big air draft that Open Side Down promotes pipe 6 can control swing forward or backward with float wind promotion pipe 7, regulates the direction that wind-force promotes.

Adopt the present invention of above-mentioned measure to have simple in structure, easy manufacturing, with low cost and easy to operate advantage.

Description of drawings

Fig. 1 is that master of the present invention looks scheme drawing;

Fig. 2 is an elevational schematic view of the present invention;

Fig. 3 is that scheme drawing is looked on a left side of the present invention.

Below in conjunction with accompanying drawing to the present invention's further detailed explanation again.

The specific embodiment

With reference to figure 1, Fig. 2; Fig. 1 is that master of the present invention looks scheme drawing; Fig. 2 is an elevational schematic view of the present invention, from Fig. 1 and Fig. 2, knows structure of the present invention, comprises fuselage 1, wheel 2, driving engine 3, diving rudder 8 and turns to rudder 9; The specific embodiment: this driving engine 3 is located on the head, and the rotating shaft of driving engine links to each other with the high pressure positive blower fan blade 4 of setting; This fuselage 1 is provided with high pressure air loop duct 5; The shell of this impeller of blower 4 contains mutually with high pressure air loop duct 5 and connects; Be respectively equipped with in the front and back on these high pressure air loop duct 5 both sides that Open Side Down, opening outwards and the big air draft backward of afterbody opening promote pipe 6; Front and back and middle part on these high pressure air loop duct 5 both sides also are respectively arranged with the float wind promotion pipe 7 that Open Side Down; Big air draft that should Open Side Down promotes pipe 6 and promotes pipe 7 with float wind and can control swing forward or backward, regulates the direction that wind-force promotes.

With reference to figure 3, Fig. 3 is that scheme drawing is looked on a left side of the present invention, from Fig. 3, can find out the structure that a left side of the present invention is looked, and is high pressure positive blower fan blade 4 in the middle of the front, and the high pressure air loop duct 5 that this fuselage 1 is provided with is the both sides at fuselage 1.Be respectively equipped with the outside big air draft of opening in the head both sides and promote pipe 6.

Principle of work of the present invention:

One. when ground run, earlier the big air draft promotion of drive end unit pipe 6 is opened, other big air draft promotion pipe 6 is controlled with float wind promotion pipe 7 and is closed or semi-closed state.Fire an engine 3 then, force high-pressure blast to pass through the big air draft of high pressure air loop duct 5 to afterbody and promote pipe 6, produce propelling thrust carplane is gone.The preceding wheel 2 of this right and left is similar with the front-wheel of automobile, is straight-line travelling during general run of thins, when steering wheel rotation or head receive external force, also can turn.If when needing turnon left, the big air draft of opening the head right side promotes pipe 6, if when needing right-hand corner, the big air draft of opening the head left surface promotes to turn about pipe 6 or service orientation dish carry out.

Two. when taking off vertically, earlier the big air draft of afterbody is promoted pipe 6 and close, the big air draft in front and back, both sides of opening high pressure air loop duct 5 promotes pipe 6; Fire an engine 3 then; Big air draft promotes pipe 6 to Open Side Down to force high-pressure blast to pass through high pressure air loop duct 5, produces upwards propelling thrust, and aircraft is taken off vertically.

Three. during horizontal flight, when aircraft rises to certain altitude, open the big air draft of afterbody immediately and promote pipe 6, and then big air draft that will be downward promotes slowly swing backward of pipe 6, make the aircraft state of flight that is up to the standard, and the flight that is up to the standard of the diving rudder 8 of adjusting tail.If during aircraft the right and left overbalance, utilize the float wind on both sides to promote pipe 7 and regulate and get final product.When the left side tilted, the float wind that can open the left side promoted pipe 7 or regulates diving rudder 8 to reach balance flight such as aircraft.When turning about horizontal flight, turn about can promoting pipe 6 or turn to rudder 9 to realize through the outwards big air draft of high pressure air loop duct 5 both sides openings.

Four. during aircraft landing, the big air draft of closing airplane tail group earlier promotes pipe 6, and before and after starting throttle slowly to turn down in aircraft then or controlling, the big air draft in both sides promotes the exhaust air rate of pipe 6, makes the weight of the propelling thrust of wind less than aircraft, aircraft just slowly lowers.

The present invention is a kind of carplane, and fuselage (vehicle body) length can be 3.5-4.5 rice, and width can be 1.8-2.4 rice.Fuselage adopts aluminum alloy or lightweight material to make.It is 120-300 horsepower that driving engine adopts power, and disposes the fan blade of corresponding high pressure positive blower.

Claims

1. an ability VTOL carplane comprises fuselage (1), wheel (2), driving engine (3), diving rudder (8) and turns to rudder (9), and it is characterized in that: described driving engine (3) is located on the head, and the rotating shaft of driving engine links to each other with the high pressure positive blower fan blade (4) of setting; Described fuselage (1) is provided with high pressure air loop duct (5); The shell of described impeller of blower (4) contains mutually with high pressure air loop duct (5) and connects; Be respectively equipped with in the front and back on these high pressure air loop duct (5) both sides that Open Side Down, opening outwards and the big air draft backward of afterbody opening promote pipe (6); Front and back and middle part on these high pressure air loop duct (5) both sides also are respectively arranged with the float wind promotion pipe (7) that Open Side Down.

2. ability VTOL carplane is characterized in that: the described big air draft that Open Side Down promotes pipe (6) and promotes pipe (7) with float wind and all can control swing forward or backward, the direction of regulating the wind-force promotion.