CN101575005A - Disc-shaped aircraft - Google Patents

Disc-shaped aircraft Download PDF

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Publication number
CN101575005A
CN101575005A CNA2009100207928A CN200910020792A CN101575005A CN 101575005 A CN101575005 A CN 101575005A CN A2009100207928 A CNA2009100207928 A CN A2009100207928A CN 200910020792 A CN200910020792 A CN 200910020792A CN 101575005 A CN101575005 A CN 101575005A
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CN
China
Prior art keywords
disc
shaped housing
shaped
surfboard
cockpit
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CNA2009100207928A
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Chinese (zh)
Inventor
王杨建
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Individual
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Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CNA2009100207928A priority Critical patent/CN101575005A/en
Publication of CN101575005A publication Critical patent/CN101575005A/en
Pending legal-status Critical Current

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Abstract

The invention relates to a disc-shaped aircraft, which comprises a cockpit, a fixed base, a landing pad, airplane wheels, an engine and a control device, wherein an annular groove is formed at a connectioin positon of the cockpit and the fixed base; the inner ring of a disk-shaped housing is sleeved in the groove; the disc-shaped housing is provided with two aerovanes symmetrically; and the aerovanes are connected with an aerovane on-off control device; the engine is connected with a transfer case through a clutch; the first output shaft of the transfer case is connected with a disc-shaped housing drive shaft through a bevel gear group; a drive gear arranged on the upper end of the disc-shaped drive shaft is engaged with an internal gear arranged on the internal ring of the disc-shaped housing; the second output shaft of the transfer case is connected with a propeller shaft through three constant velocity cardan joints; the propeller shaft is connected with a propeller fixedly; the inwall of the fixed base is provided with a rotatable disc; a bearing seat connected with disc fringe fixedly is sleeved on the propeller shaft; and a disc is connected with a disc operating rod in the cockpit through a connecting rod. The disc-shaped aircraft of the invention has convenient operation and combined functions of an automobile, a watercraft and an airplane, and running in a triphibious way.

Description

Disc-shaped flying craft
Technical field:
The present invention relates to a kind of aircraft, especially a kind of disc-shaped flying craft.
Background technology:
The existing vehicle are varied, but they generally only have independent a kind of function, can only travel on land as automobile, then can't advance when running into darker water; Boats and ships can only navigate by water in water, can not be used for land, also can't fly; Aircraft also can only aloft fly, and can't be used as automobile or boats and ships and use in land or water, and conventional airplane can't can only slide landing as the autogyro vertical takeoff and landing.
Summary of the invention:
The invention provides a kind of disc-shaped flying craft, it is simple in structure, and is easy to operate, can integrate three kinds of functions of automobile, boats and ships, aircraft, and realization three is dwelt and advanced, and has solved problems of the prior art.
The present invention solves the problems of the technologies described above the technical scheme that is adopted to be: it comprises cockpit, firm banking, landing pad, wheel, driving engine and control setup, form an annular groove in the junction of cockpit and firm banking, the inner ring sleeve of dish housing is gone in the groove, be arranged with two rotatable rotors on dish-shaped housing, rotor links to each other with the rotor switch controlling device that dish-shaped lower housing portion is connected; Firm banking in-to-in driving engine links to each other with part-time case by power-transfer clutch, first output shaft of part-time case links to each other with vertical disc-shaped housing axle drive shaft by the conical insert wheels, internal gearing in the driven wheel of disc-shaped housing axle drive shaft upper end and the dish-shaped housing on the ring, second output shaft of part-time case links to each other with propshaft by three joint constant-velocity universal joints, and propshaft stretches out the firm banking outside and is connected with propeller; Be provided with the disk of movable rotation on the firm banking inwall above the propshaft, the bearing sleeve that disk border is connected is contained on the propshaft, and disk links to each other with disk control lever in the cockpit by connecting rod.
The further technical scheme of the present invention is, described wheel top one side and landing pad lower end flexibly connect, and is provided with a wheel control setup in the outside, bottom of landing pad, and the wheel control setup links to each other with wheel; In the internal cavities of landing pad, be provided with water-slipping equipment, described water-slipping equipment comprises a surfboard, the surfboard retractor device that is connected on surfboard and the landing pad inwall flexibly connects, and also is provided with the surfboard angular adjustment apparatus on the expansion link of surfboard retractor device lower end.
The invention has the beneficial effects as follows that simple in structure, easy to operate, maneuverability is easily made, cost is lower, can be implemented under land, aerial, the various conditions of the water surface to walk; Driving engine drives dish-shaped housing by power-transfer clutch, part-time case and rotates, when the rotor on the dish-shaped housing of control is opened, rotor upwards forms the elevation angle, make dish-shaped housing produce lift upwards, make aircraft vertical uplift of the present invention, when closing rotor, dish-shaped housing loses raising force, aircraft of the present invention lands gradually, realizes the vertical lift of this aircraft; Control disk control lever can make propshaft drive propeller and rotate, to realize the turning of aircraft of the present invention in advancing; The inner water-slipping equipment that is provided with of landing pad can make aircraft of the present invention be implemented on the water surface and walk.
Description of drawings:
Fig. 1 is a structural representation of the present invention.
Fig. 2 is the A bilge construction enlarged drawing among Fig. 1.
Fig. 3 is the B bilge construction enlarged drawing among Fig. 1.
Among the figure, 1, cockpit; 2, firm banking; 3, landing pad; 4, wheel; 5, driving engine; 6, control setup; 7, groove; 8, dish-shaped housing; 9, rotor; 10, rotor switch controlling device; 11, power-transfer clutch; 12, part-time case; 13, first output shaft; 14, conical insert wheels; 15, disc-shaped housing axle drive shaft; 16, second output shaft; 17, constant-velocity universal joint; 18, propshaft; 19, propeller; 20, disk; 21, disk control lever; 22, wheel control setup; 23, surfboard; 24, surfboard retractor device; 25, surfboard angular adjustment apparatus.
The specific embodiment:
For clearly demonstrating the technical characterstic of this programme, below by the specific embodiment, and in conjunction with its accompanying drawing, the present invention will be described in detail.
As shown in FIG., the present invention includes cockpit 1, firm banking 2, landing pad 3, wheel 4, driving engine 5 and control setup 6, junction at cockpit 1 and firm banking 2 forms an annular groove 7, the inner ring sleeve of dish housing 8 is gone in the groove 7, be arranged with two rotatable rotors 9 on dish-shaped housing 8, rotor 9 links to each other with the rotor switch controlling device 10 that dish-shaped housing 8 bottoms are connected; Firm banking 2 in-to-in driving engines 5 link to each other with part-time case 12 by power-transfer clutch 11, first output shaft 13 of part-time case 12 links to each other with vertical disc-shaped housing axle drive shaft 15 by conical insert wheels 14, internal gearing in the driven wheel of disc-shaped housing axle drive shaft 15 upper ends and the dish-shaped housing 8 on the ring, second output shaft 16 of part-time case 12 links to each other with propshaft 18 by three joint constant-velocity universal joints 17, propshaft 18 stretches out firm banking 2 outsides and propeller 19 is connected, and described three joint constant-velocity universal joints 17 can use ball-joint universal-joint, ball cage universal-joint or three pin universal-joints; Be provided with the disk 20 of movable rotation on 2 inwalls of the firm banking above the propshaft 18, the bearing sleeve that disk 20 edges are connected is contained on the propshaft 18, and disk 20 links to each other by the disk control lever 21 in connecting rod and the cockpit 1.
The further technical scheme of the present invention is, described wheel 4 tops, one side and landing pad 3 lower ends flexibly connect, the outside, bottom at landing pad 3 is provided with a wheel control setup 22, and wheel control setup 22 links to each other with wheel 4, and described wheel control setup 22 is a telescopic hydraulic cylinder; In the internal cavities of landing pad 3, be provided with water-slipping equipment, described water-slipping equipment comprises a surfboard 23, the surfboard retractor device 24 that is connected on surfboard 23 and landing pad 3 inwalls flexibly connects, also be provided with surfboard angular adjustment apparatus 25 on the expansion link of surfboard retractor device 24 lower ends, described surfboard retractor device 24 and surfboard angular adjustment apparatus 25 are telescopic hydraulic cylinder.
When walking on land, by control setup 6 control clutchs 11 and the part-time case 12 in the cockpit 1, make 5 in driving engine drive propeller 19 rotations, by the direction of disk control lever 21 adjustable screws slurry 19, so that this aircraft is realized advancing, about turn, handle very flexible.
When needs when the water surface uses, by control setup 6 control clutchs 11 and the part-time case 12 in the cockpit 1, make dish-shaped housing 8 rotations, open upwards to rise by rotor switch controlling device 10 control rotors 9 again and form certain angle of attack, the air that rotor 9 runs into is forced to turn to dish-shaped housing 8 belows through rotor 9, dish-shaped housing 8 below air pressure are raise, dish housing 8 top air pressure reduce, make dish-shaped housing 8 produce lift upwards, the drive aircraft rises, by control setup 6 control wheel control setups 22 wheel 4 is packed up then, by control surfboard retractor device 24 and surfboard angular adjustment apparatus 25 surfboard 23 is stretched out expansion from landing pad 3 again, and then make propeller 19 rotation produce thrusts by power-transfer clutch 11 and part-time case 12, this aircraft is advanced on the water surface.When advancing, can according to circumstances control the rotor 9 of closing on the dish-shaped housing 8 by rotor switch controlling device 10, stop dish-shaped housing 8 rotations by power-transfer clutch 11 and part-time case 12, only keep the thrust that propeller 19 rotations produce, the lift that utilizes surfboard 23 water skiing to be produced just can normally be advanced, and can reduce consumption of fuel like this.
When needs fly, at first by control setup 6 control clutchs 11 and part-time case 12 in the cockpit 1, make dish-shaped housing 8 rotations, open upwards to rise by rotor switch controlling device 10 control rotors 9 again and form certain angle of attack, make dish-shaped housing 8 produce lift upwards, make this aircraft built on stilts, drive screw propeller 19 rotations by part-time case 12 before liftoff, advance the moment of reaction that is produced with balance rotor 9 again by the equidirectional of disk control lever 21 control propeller 19 towards the hand of rotation of dish-shaped housing 8.When this aircraft reach a certain height, control disk control lever 21 drove propeller 19 and rotates, and advanced towards required direction flight to control this aircraft.
The above-mentioned specific embodiment can not be as limiting the scope of the invention, and for those skilled in the art, any alternate modification or conversion that embodiment of the present invention is made all drop in protection scope of the present invention.
The present invention does not describe part in detail, is those skilled in the art of the present technique's known technology.

Claims (2)

1, a kind of disc-shaped flying craft, comprise cockpit, firm banking, landing pad, wheel, driving engine and control setup, it is characterized in that: form an annular groove in the junction of cockpit and firm banking, the inner ring sleeve of dish housing is gone in the groove, be arranged with two rotatable rotors on dish-shaped housing, rotor links to each other with the rotor switch controlling device that dish-shaped lower housing portion is connected; Firm banking in-to-in driving engine links to each other with part-time case by power-transfer clutch, first output shaft of part-time case links to each other with vertical disc-shaped housing axle drive shaft by the conical insert wheels, internal gearing in the driven wheel of disc-shaped housing axle drive shaft upper end and the dish-shaped housing on the ring, second output shaft of part-time case links to each other with propshaft by three joint constant-velocity universal joints, and propshaft stretches out the firm banking outside and is connected with propeller; Be provided with the disk of movable rotation on the firm banking inwall above the propshaft, the bearing sleeve that disk border is connected is contained on the propshaft, and disk links to each other with disk control lever in the cockpit by connecting rod.
2, disc-shaped flying craft according to claim 1 is characterized in that: described wheel top one side and landing pad lower end flexibly connect, and are provided with a wheel control setup in the outside, bottom of landing pad, and the wheel control setup links to each other with wheel; In the internal cavities of landing pad, be provided with water-slipping equipment, described water-slipping equipment comprises a surfboard, the surfboard retractor device that is connected on surfboard and the landing pad inwall flexibly connects, and also is provided with the surfboard angular adjustment apparatus on the expansion link of surfboard retractor device lower end.
CNA2009100207928A 2009-05-05 2009-05-05 Disc-shaped aircraft Pending CN101575005A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNA2009100207928A CN101575005A (en) 2009-05-05 2009-05-05 Disc-shaped aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNA2009100207928A CN101575005A (en) 2009-05-05 2009-05-05 Disc-shaped aircraft

Publications (1)

Publication Number Publication Date
CN101575005A true CN101575005A (en) 2009-11-11

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Family Applications (1)

Application Number Title Priority Date Filing Date
CNA2009100207928A Pending CN101575005A (en) 2009-05-05 2009-05-05 Disc-shaped aircraft

Country Status (1)

Country Link
CN (1) CN101575005A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101927826A (en) * 2010-05-10 2010-12-29 李文奇 Rotor wing disk-shaped aviation aircraft
CN104626904A (en) * 2015-02-24 2015-05-20 丁乃祥 Multifunctional flying saucer
CN110979666A (en) * 2019-12-27 2020-04-10 浙江大学 Water-air robot

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101927826A (en) * 2010-05-10 2010-12-29 李文奇 Rotor wing disk-shaped aviation aircraft
CN104626904A (en) * 2015-02-24 2015-05-20 丁乃祥 Multifunctional flying saucer
CN110979666A (en) * 2019-12-27 2020-04-10 浙江大学 Water-air robot
CN110979666B (en) * 2019-12-27 2021-09-21 浙江大学 Water-air robot

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C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C02 Deemed withdrawal of patent application after publication (patent law 2001)
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Open date: 20091111