CN102020020A - Aerospace flying saucer aircraft - Google Patents

Aerospace flying saucer aircraft Download PDF

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Publication number
CN102020020A
CN102020020A CN2010105915916A CN201010591591A CN102020020A CN 102020020 A CN102020020 A CN 102020020A CN 2010105915916 A CN2010105915916 A CN 2010105915916A CN 201010591591 A CN201010591591 A CN 201010591591A CN 102020020 A CN102020020 A CN 102020020A
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CN
China
Prior art keywords
aircraft
aerospace
flying saucer
shaft
flying disc
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
CN2010105915916A
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Chinese (zh)
Inventor
张奎
张慧
张慧宇
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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 CN2010105915916A priority Critical patent/CN102020020A/en
Publication of CN102020020A publication Critical patent/CN102020020A/en
Pending legal-status Critical Current

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Abstract

The invention discloses an aerospace flying saucer aircraft, and belongs to the cutting-edge technology in the field of aerospace. The aerospace flying saucer aircraft is provided with a direct dual-shaft counter-rotating turbo-shaft engine and a rocket engine; when the aerospace flying saucer aircraft flies in the atmosphere of the earth, the direct dual-shaft counter-rotating turbo-shaft engine is utilized to provide power; when the aerospace flying saucer aircraft flies in outer space, the rocket engine is utilized to provide power; and when the aerospace flying saucer aircraft flies in the atmosphere of the earth, the two engines can be started simultaneously, and the aerospace flying saucer aircraft does not need a runway, can vertically take off and land, and can freely fly at a high speed or a low speed through control. The aerospace flying saucer aircraft radically solves the technical problems of a disc-shaped aircraft and a circular aircraft; unique innovative concepts and scientific and reasonable designs are shown in the aspects of the integral structure, the power device, the control of flying balance, the control of flying direction and the like; and at present, the aerospace flying saucer aircraft developed and manufactured has important significance for development of the airspace strategy of China, airspace security and airspace battles.

Description

Empty day flying disc
One, technical field
An empty day flying disc belongs to the high hard-core technology of aerospace field, can be widely used in national defence, military affairs, Aeronautics and Astronautics cause and commerce.
Two, background technology
Flying saucer (UFO) always in people's the imagination and illusion, does not have shadow, and going does not have track, and majority think that flying saucer is a day exotic, it is had that much to be difficult to the mystery explained very mysterious in this world; Present circular aircraft or disc-shaped flying craft mostly exist knotty problems such as dynamical problem, equilibrium problem, rotation and counter-rotating, are restricting the development and utilization of this type of aircraft; For this reason, it is modern that (CN201010216019.1 is designed by people such as Zhang Kui, Zhang Hui, Zhang Huiyu according to the direct-type double-shaft counter-rotating turbine engine, now open) or turboaxle motor through the combination and the utilization of technology such as coaxial transmission, solved great knotty problem therebetween, our innovative design goes out-empty day flying disc.
Three, summary of the invention
Empty day flying disc be disc, with the circle structure; Its main structural components (see figure 1) has: last clamshell 1, wheel rotating disk 2, (three) are compositions such as support and connection axle 3, last rotor turbine fan 4, following rotor turbine fan 5, double-shaft counter-rotating turbine shaft generator 6, rocket engine 7, control desk 8, annular fuel case 9, fuselage 10, parachute 11 up and down.
The present invention is as major impetus with direct-type double-shaft counter-rotating turbine shaft generator 6 (or turboaxle motor is through coaxial transmission), with this engine installation in the fuselage centre, can make the whole center of gravity of aircraft keep balance, in characteristic according to direct-type double-shaft counter-rotating turbine shaft generator, during operation, make that going up rotor turbine fan 4 is just changeing 5 counter-rotatings of following rotor turbine fan, torsion is offset each other, thereby has solved the rotation problem of aircraft.
Upper clamshell 1 periphery of the present invention is circular arc type, is umbilicate type in the middle of the top, is beneficial to like this suction of upper air stream and reduces resistance, and inboard inner ring with wheel rotating disk 2 is connected and fixed in the middle of the upper clamshell; The wheel rotating disk 2 the outer ring with three about support and connection axle 3 be connected and fixed, go up like this clamshell 1 and can arbitrarily rotate; Three support and connection axle 3 belows are fixed on the fuselage, until fuselage bottom forms firm overall structure.
Three support and connection axle 3 scalable helical rotation, when rotating one of them, it is the parallel angle of deflectable wheel rotating disk 2, thereby clamshell 1 offset collimated angle on the interlock, then change the air flow rate of going up the clamshell inside circumference, to outside fuselage 10, form bias current, thus change of flight device single-piece balance and control heading.
The present invention be because jacket 1 can arbitrarily rotate, and it is in when flight, and when colliding with other aircraft or other object, jacket 1 rotations of will taking advantage of a situation, and can wiping mutually moment staggered mutually, thereby guaranteed the flight safety of empty sky flying disc.
Thrust and arrow power that the present invention mainly uses direct-type double-shaft counter-rotating turbine axle to start; When engine moved, the air stream (seeing Fig. 2) that upper and lower rotor turbine fan sucks was so that produce a negative pressuren zone in the over top of aircraft, and at zone of positive pressure of the inner formation of upper clamshell, and by on the uniform air-flow of clamshell periphery ejection, produce arrow power and lift, and at engine bottom, just produce thrust under the fuselage, make day flying disc of having leisure not need runway, but VTOL, and by control, speed at random circles in the air freely.
Four, description of drawings
Fig. 1 is the section-drawing of empty day flying disc;
Fig. 2 is the side view of empty day dish aircraft;
Fig. 3 is the exploded drawings of empty day flying disc;
Five, the specific embodiment
On the empty day flying disc direct-type double-shaft counter-rotating turbine shaft generator and rocket engine are installed, when it flies in earth atmosphere, utilize direct-type double-shaft counter-rotating turbine shaft generator to do power; When in space, flying, just utilize rocket engine to do power; And when in earth atmosphere, flying, also can start simultaneously direct-type double-shaft counter-rotating turbine shaft generator and rocket engine, so manned, fortune thing amount is big, also will greatly improve its flying speed.
The present invention can design its single-piece size according to the size of power configuration, and according to the practical application needs manned or fortune thing, thereby arrange the inner space; In order to ensure the safety of flight, on empty day flying disc, in the clamshell 11 parachutes are installed, and are fixed on three support and connection axles 3; When aircraft broke down or be unexpected, parachute 11 was dished out and will be opened automatically, whole aircraft security can be landed reposefully.
The present invention has solved the technological difficulties of dish-shaped class aircraft and circle class aircraft at all, and the control of its overall structure, power set, flight balance and the control of heading etc. all have unique innovative idea and scientific and reasonable design; At present, we develop and make empty day flying disc, to the development of China's air and space strategy with on air and space security, air and space operation, will play a significant role.

Claims (6)

1. empty day flying disc is characterized in that: include clamshell (1), wheel rotating disk (2), three up and down support and connection axle (3), go up rotor turbine fan (4), rotor turbine fan (5), direct-type double-shaft counter-rotating turbine shaft generator (6), rocket engine (7), control desk (8), annular fuel case (9), fuselage (10), parachute (11) main structural components composition down.
2. empty day flying disc according to claim 1, it is characterized in that: described direct-type double-shaft counter-rotating turbine shaft generator (6) vertically is mounted on fuselage (10) centre, last rotor turbine fan (4) is installed on the driving engine in the upright rotating shaft, then descend rotor turbine fan (5) to be installed on the reversing shaft, control desk places around the driving engine, and rocket engine (7) is installed on fuselage (10) bottom
3. empty day according to claim 1 flying disc, it is characterized in that: described upper clamshell (1) periphery is circular arc type, be umbilicate type in the middle of the top, inboard inner ring with wheel rotating disk (2) is connected and fixed in the middle of the upper clamshell (1), and upper clamshell (1) can arbitrarily rotate.
4. empty day flying disc according to claim 1, it is characterized in that: described outer ring of taking turns rotating disk (2) and three support and connection axle (3) up and down are connected and fixed, the scalable helical rotation of three support and connection axles (3) also is fixed on the fuselage, until fuselage (10) bottom, form crash-resistant integral structure.
5. empty day according to claim 1 flying disc, it is characterized in that: described the present invention can design the size of its integral body according to the size of power configuration, and according to the practical application needs, manned or fortune thing, thus the inner space arranged.
6. empty day according to claim 1 flying disc is characterized in that: described parachute (11) is installed in last clamshell (1), and is fixed on three support and connection axles; When aircraft broke down or be unexpected, parachute was opened, and whole aircraft security can be fallen reposefully.
CN2010105915916A 2010-12-08 2010-12-08 Aerospace flying saucer aircraft Pending CN102020020A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2010105915916A CN102020020A (en) 2010-12-08 2010-12-08 Aerospace flying saucer aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2010105915916A CN102020020A (en) 2010-12-08 2010-12-08 Aerospace flying saucer aircraft

Publications (1)

Publication Number Publication Date
CN102020020A true CN102020020A (en) 2011-04-20

Family

ID=43861891

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2010105915916A Pending CN102020020A (en) 2010-12-08 2010-12-08 Aerospace flying saucer aircraft

Country Status (1)

Country Link
CN (1) CN102020020A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102211661A (en) * 2011-05-03 2011-10-12 陈洪国 Helistat
CN105083552A (en) * 2014-05-23 2015-11-25 漯河市宇祥余热利用科技有限公司 Saucer-shaped aircraft
CN106143907A (en) * 2016-06-30 2016-11-23 宁波市成大机械研究所 A kind of jet flying saucer
US10239615B2 (en) 2014-01-07 2019-03-26 4525612 Canada Inc. Personal flight vehicle
CN112319799A (en) * 2020-11-03 2021-02-05 谭成刚 Wingless aircraft

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102211661A (en) * 2011-05-03 2011-10-12 陈洪国 Helistat
US10239615B2 (en) 2014-01-07 2019-03-26 4525612 Canada Inc. Personal flight vehicle
US10464671B2 (en) 2014-01-07 2019-11-05 4525612 Canada Inc. Personal flight vehicle
US10710718B2 (en) 2014-01-07 2020-07-14 4525612 Canada Inc. Personal flight vehicle
CN105083552A (en) * 2014-05-23 2015-11-25 漯河市宇祥余热利用科技有限公司 Saucer-shaped aircraft
CN106143907A (en) * 2016-06-30 2016-11-23 宁波市成大机械研究所 A kind of jet flying saucer
CN112319799A (en) * 2020-11-03 2021-02-05 谭成刚 Wingless aircraft

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C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20110420