CN101428687A - General dynamic flying disk - Google Patents
General dynamic flying disk Download PDFInfo
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- CN101428687A CN101428687A CNA2008101831435A CN200810183143A CN101428687A CN 101428687 A CN101428687 A CN 101428687A CN A2008101831435 A CNA2008101831435 A CN A2008101831435A CN 200810183143 A CN200810183143 A CN 200810183143A CN 101428687 A CN101428687 A CN 101428687A
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Abstract
A general power flying saucer relates to an aircraft, in particular to an aircraft of a flying saucer. The aircraft is characterized in that a cockpit (1) is arranged above a saucer body (3); the cockpit (1) and the saucer body (3) are connected together through a plurality of connecting bridge beams (2); an upper-ring rood (4), a mid-ring rood (5), a lower-ring rood (6), an upper-lifting force fan (7), a lower-lifting force fan (8), an engine (9), a spare space (10), a plurality of supporting feet (11), an universal ring (12), a plurality of universal joints (13), a transfer gear (14), an end connecting ring (15) and a center fixed shaft (16) are arranged inside the saucer body (3). Because double-lifting force fan systems do a concentric circle circumference motion in the same plane, Gyroscopic Effect is utilized to achieve a stable effect naturally, so that worldwide problems like stabilization difficulty and the like are solved. The invention has the advantages of competitive price, attractive appearance, economical efficiency, applicability, convenient popularization, generalization and application, and low application cost.
Description
Technical field:
The present invention relates to a kind of aircraft, be specifically related to a kind of flying disc.
Background technology:
At present, military affairs both at home and abroad, scientific research, company, individual develop a lot of of artificial flying saucer.But real success also does not have! Though some has carried out product testing, also obtained certain achievement.But still exist: power, lift deficiency, effect is than low; Poor stability; Fatal shortcoming such as be difficult to control, finally all end in failure!
Present aircraft mainly is that aircraft, dirigible, hot gas are ball, general aloft can be flexible be aircraft, aircraft is divided into conventional airplane and autogyro again, and general helicopter is owing to be subjected to the bottleneck restriction of fragile screw propeller, axle system, per hour during 150 kms, propeller speed generally is no more than 210 rpms to normal flight.Though but the manoevreability of these aircrafts has obtained on the very big improvement aggregate level, maneuvering performance is still very poor.Dirigible, the ball aircraft flight speed of hot gas are slow, manoevreability is poorer.
Present aircraft, autogyro generally adopt noble metals such as aluminum alloy, titanium alloy to make, and the price of these metals own is more valuable, causes the rising of manufacturing cost.
Summary of the invention:
The purpose of this invention is to provide a kind of general dynamic flying disk, it is good and cheap, and is economic and practical, is convenient to popularize, promotes, uses, and has controlled direction, the attitude of flight easily, has solved the global problem of the flicon difficulty that runs in this field development.In order to solve the existing problem of background technology, the present invention is by the following technical solutions: it by passenger cabin 1, several connect bridges 2, dish body 3, on encircle cross bar 4, middle ring cross bar 5, down encircle cross bar 6, raising force fan 7, lift fan 8, driving engine 9, spare space 10, several feets 11, cardo ring 12, several universal-joints 13, transfer gear 14, end coupling link 15, central fixed shaft 16 are formed down; Passenger cabin 1 is arranged on the top of dish body 3, and several connect bridge 2 passenger cabin 1 and dish body 3 are linked together; Be provided with ring cross bar 4, middle ring cross bar 5 in the inside of dish body 3, encircle cross bar 6, raising force fan 7, lift fan 8, driving engine 9, spare space 10, several feets 11, cardo ring 12, several universal-joints 13, transfer gear 14, end coupling link 15, central fixed shaft 16 down down; Cardo ring 12 is arranged on the inboard of dish body 3, several universal-joints 13 are separately positioned on the inboard of cardo ring 12,16 last times of central fixed shaft are provided with ring cross bar 4, middle ring cross bar 5, under encircle cross bar 6, between last ring cross bar 4 and middle ring cross bar 5, be provided with raising force fan 7, be provided with down lift fan between middle ring cross bar 5 and the following ring cross bar 6, last ring cross bar 4 is connected with end coupling link 15 respectively with four ends that encircle cross bar 6 down, the centre of middle ring cross bar 5 is provided with driving engine 9, spare space 10, in the ring cross bar 5 a side be provided with transfer gear 14, the two ends up and down of transfer gear 14 respectively with raising force fan 7, following lift fan 8 is connected; The lower surface of encircling cross bar 6 down is provided with several feets 11.
The present invention uses general dynamic, by transfer gear 14 power is evenly distributed to upper and lower lift fan 7,8, thereby obtains enough power, motor-driven, the flight of lift.
Driving engine, transfer gear, upper and lower lift fan are fixed by three groups of ring cross structures among the present invention.Fixedly the while does not hinder the rotation of lift fan.Have strong, solid, firm characteristics.So just be that this dish lift fan rotating speed changes greater than per minute 1000, the designing requirement of flying speed 600-800 kilometer per hour provides assurance and technical support.And general helicopter is owing to be subjected to the bottleneck restriction of fragile screw propeller, axle system, and normal flight is per hour during 150 kms, only 210 rpms of propeller speed.
The present invention is by a word layout, and the cross layout can be arranged monomotor, and is twin-engined, even multiple-motor; Diameter can expand ten meters to by three, four meters, even bigger; The member can be single, double, even many people.Has huge development room for promotion.Power has increased, and the lift fan diameter has increased, and fan blade area has increased, and lift is inevitable to be improved greatly.
Two universal-joints connected cardo rings about power, the lift system that the present invention has reinforced passed through, and cardo ring is connected with the dish body by former and later two universal-joints.By joystick, the lift fan rotary cutting surface is tilted to the power operated direction of any needs.Thereby better controlled direction, the attitude of flying by power steering, solved the global problem of the flicon difficulty that runs in existing this field development.
Because two ascending fan systems are to make the concentric circles circular movement in same plane, thereby have utilized " gyro effect " to reach stablizing effect naturally.Global problems such as stable difficulty have been solved.
The present invention is good and cheap, and is economic and practical, is convenient to popularize, promotes, uses, and application cost is low.
Description of drawings:
Fig. 1 is a structural representation of the present invention, Fig. 2 is the birds-eye view of Fig. 1, Fig. 3 is an inner structure scheme drawing of the present invention, Fig. 4 is a structural representation of going up ring cross bar 4, Fig. 5 is the structural representation of middle ring cross bar 5, Fig. 6 is the structural representation of following ring cross bar 6, and Fig. 7 is the structural representation of raising force fan 7, and Fig. 8 is the structural representation of following lift fan 8.
The specific embodiment:
Referring to Fig. 1-8, this specific embodiment by the following technical solutions: it by passenger cabin 1, several connect bridges 2, dish body 3, on encircle cross bar 4, middle ring cross bar 5, down encircle cross bar 6, raising force fan 7, lift fan 8, driving engine 9, spare space 10, several feets 11, cardo ring 12, several universal-joints 13, transfer gear 14, end coupling link 15, central fixed shaft 16 are formed down; Passenger cabin 1 is arranged on the top of dish body 3, and several connect bridge 2 passenger cabin 1 and dish body 3 are linked together; Be provided with ring cross bar 4, middle ring cross bar 5 in the inside of dish body 3, encircle cross bar 6, raising force fan 7, lift fan 8, driving engine 9, spare space 10, several feets 11, cardo ring 12, several universal-joints 13, transfer gear 14, end coupling link 15, central fixed shaft 16 down down; Cardo ring 12 is arranged on the inboard of dish body 3, several universal-joints 13 are separately positioned on the inboard of cardo ring 12,16 last times of central fixed shaft are provided with ring cross bar 4, middle ring cross bar 5, under encircle cross bar 6, between last ring cross bar 4 and middle ring cross bar 5, be provided with raising force fan 7, be provided with down lift fan between middle ring cross bar 5 and the following ring cross bar 6, last ring cross bar 4 is connected with end coupling link 15 respectively with four ends that encircle cross bar 6 down, the centre of middle ring cross bar 5 is provided with driving engine 9, spare space 10, in the ring cross bar 5 a side be provided with transfer gear 14, the two ends up and down of transfer gear 14 respectively with raising force fan 7, following lift fan 8 is connected; The lower surface of encircling cross bar 6 down is provided with several feets 11.
Described go up ring cross bar 4 be provided with set collar 4-4, a plurality of steady wheel 4-1, two cardo ring 4-2, two gimbal point 4-3, on encircle cross bar stabilizer rod 4-5, on be passenger cabin 1 in the middle of encircling cross bar 4.
The described cross bar 6 of ring down is provided with a plurality of steady wheel 6-1, set collar 6-2, middle ring cross bar stabilizer rod 6-3, the total point of connection 6-4 in several outer ends, is passenger cabin 1 in the middle of the middle ring cross bar 5.
Steady wheel 4-1 is meshed on the interior ring of the upper end of described raising force fan 7 and last ring cross bar 4, and the lower end of raising force fan 7 is meshed with transfer gear 14, and the frame of raising force fan 7 is connected with steady wheel 5-1 with steady wheel 4-1.
The lower end of described lift fan 8 down is meshed with steady wheel 6-1 on the interior ring that encircles cross bar 6 down, and the upper end of following lift fan 8 is meshed with transfer gear 14, and the frame of following lift fan 8 is connected with steady wheel 6-1 with steady wheel 5-1.
This specific embodiment is used general dynamic, by transfer gear 14 power is evenly distributed to upper and lower lift fan 7,8, thereby obtains enough power, motor-driven, the flight of lift.
Driving engine, transfer gear, upper and lower lift fan are fixed by three groups of ring cross structures in this specific embodiment.Fixedly the while does not hinder the rotation of lift fan.Have strong, solid, firm characteristics.So just be that this dish lift fan rotating speed changes greater than per minute 1000, the designing requirement of flying speed 600-800 kilometer per hour provides assurance and technical support.And general helicopter is owing to be subjected to the bottleneck restriction of fragile screw propeller, axle system, and normal flight is per hour during 150 kms, only 210 rpms of propeller speed.
This specific embodiment is by a word layout, and the cross layout can be arranged monomotor, and is twin-engined, even multiple-motor; Diameter can expand ten meters to by three, four meters, even bigger; The member can be single, double, even many people.Has huge development room for promotion.Power has increased, and the lift fan diameter has increased, and fan blade area has increased, and lift is inevitable to be improved greatly.
Two universal-joints connected cardo rings about power, the lift system that this specific embodiment has been reinforced passed through, and cardo ring is connected with the dish body by former and later two universal-joints.By joystick, the lift fan rotary cutting surface is tilted to the power operated direction of any needs.Thereby better controlled direction, the attitude of flying by power steering, solved the global problem of the flicon difficulty that runs in existing this field development.Because two ascending fan systems are to make the concentric circles circular movement in same plane, thereby have utilized " gyro effect " to reach stablizing effect naturally.Global problems such as stable difficulty have been solved.
Claims (6)
1, a kind of general dynamic flying disk, it is characterized in that it by passenger cabin (1), several connect bridges (2), dish body (3), on encircle cross bar (4), middle ring cross bar (5), down encircle cross bar (6), raising force fan (7), lift fan (8), driving engine (9), spare space (10), several feets (11), cardo ring (12), several universal-joints (13), transfer gear (14), end coupling link (15), central fixed shaft (16) are formed down; Passenger cabin (1) is arranged on the top of dish body (3), and several connect bridge (2) passenger cabin (1) and dish body (3) are linked together; Be provided with ring cross bar (4), middle ring cross bar (5) in the inside of dish body (3), encircle cross bar (6), raising force fan (7), lift fan (8), driving engine (9), spare space (10), several feets (11), cardo ring (12), several universal-joints (13), transfer gear (14), end coupling link (15), central fixed shaft (16) down down; Cardo ring (12) is arranged on the inboard of dish body (3), several universal-joints (13) are separately positioned on cardo ring (12 inboard, central fixed shaft (16) last time is provided with ring cross bar (4), middle ring cross bar (5), under encircle cross bar (6), between last ring cross bar (4) and middle ring cross bar (5), be provided with raising force fan (7), be provided with down lift fan between middle ring cross bar (5) and the following ring cross bar (6), last ring cross bar (4) is connected with end coupling link (15) respectively with four ends that encircle cross bar (6) down, the centre of middle ring cross bar (5) is provided with driving engine (9), spare space (10), in the ring cross bar (5) a side be provided with transfer gear (14), the two ends up and down of transfer gear (14) respectively with raising force fan (7), following lift fan (8) is connected; The lower surface of encircling cross bar (6) down is provided with several feets (11).
2, a kind of general dynamic flying disk according to claim 1, it is characterized in that described go up ring cross bar (4) be provided with set collar (4-4), a plurality of steady wheel (4-1), two cardo rings (4-2), two gimbal points (4-3), on encircle cross bar stabilizer rod (4-5), on be passenger cabin (1) in the middle of encircling cross bar (4).
3, a kind of general dynamic flying disk according to claim 1, it is characterized in that described middle ring cross bar (5) is provided with a plurality of steady wheels (5-1), transfer gear (14), set collar (5-2), middle ring cross bar stabilizer rod (5-3), several gimbal points (5-4), is passenger cabin (1) in the middle of the middle ring cross bar (5).
4, a kind of general dynamic flying disk according to claim 1, it is characterized in that described ring cross bar (6) down is provided with a plurality of steady wheels (6-1), set collar (6-2), middle ring cross bar stabilizer rod (6-3), the total point of connection in several outer ends (6-4), is passenger cabin (1) in the middle of the middle ring cross bar (5).
5, a kind of general dynamic flying disk according to claim 1, the upper end that it is characterized in that described raising force fan (7) is meshed with steady wheel (4-1) on the interior ring of last ring cross bar (4), the lower end of raising force fan (7) is meshed with transfer gear (14), and the frame of raising force fan (7) is connected with steady wheel (5-1) with steady wheel (4-1).
6, a kind of general dynamic flying disk according to claim 1, it is characterized in that the lower end of described lift fan (8) down is meshed with steady wheel (6-1) on the interior ring that encircles cross bar (6) down, the upper end of following lift fan (8) is meshed with transfer gear (14), and the frame of following lift fan (8) is connected with steady wheel (6-1) with steady wheel (5-1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNA2008101831435A CN101428687A (en) | 2008-12-12 | 2008-12-12 | General dynamic flying disk |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNA2008101831435A CN101428687A (en) | 2008-12-12 | 2008-12-12 | General dynamic flying disk |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN101428687A true CN101428687A (en) | 2009-05-13 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNA2008101831435A Pending CN101428687A (en) | 2008-12-12 | 2008-12-12 | General dynamic flying disk |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN101428687A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102328745A (en) * | 2011-07-08 | 2012-01-25 | 吉风旺 | Disc-shaped manned aircraft |
| CN104071331A (en) * | 2014-06-24 | 2014-10-01 | 谭燕斌 | Jet-propelled type airship stabilized by spinning tops |
| WO2016154976A1 (en) * | 2015-04-01 | 2016-10-06 | 尚平 | Aircraft |
| WO2018209458A1 (en) * | 2017-05-19 | 2018-11-22 | 李海波 | Tai chi flying saucer |
-
2008
- 2008-12-12 CN CNA2008101831435A patent/CN101428687A/en active Pending
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102328745A (en) * | 2011-07-08 | 2012-01-25 | 吉风旺 | Disc-shaped manned aircraft |
| CN104071331A (en) * | 2014-06-24 | 2014-10-01 | 谭燕斌 | Jet-propelled type airship stabilized by spinning tops |
| CN104071331B (en) * | 2014-06-24 | 2016-04-13 | 谭燕斌 | The gyro-stabilized jet airship of a kind of employing |
| WO2016154976A1 (en) * | 2015-04-01 | 2016-10-06 | 尚平 | Aircraft |
| WO2018209458A1 (en) * | 2017-05-19 | 2018-11-22 | 李海波 | Tai chi flying saucer |
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| C06 | Publication | ||
| PB01 | Publication | ||
| 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) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Open date: 20090513 |