CN2734621Y - Dish type flight device - Google Patents
Dish type flight device Download PDFInfo
- Publication number
- CN2734621Y CN2734621Y CN 200420050062 CN200420050062U CN2734621Y CN 2734621 Y CN2734621 Y CN 2734621Y CN 200420050062 CN200420050062 CN 200420050062 CN 200420050062 U CN200420050062 U CN 200420050062U CN 2734621 Y CN2734621 Y CN 2734621Y
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- CN
- China
- Prior art keywords
- dish
- disc
- machine body
- cockpit
- rotation
- 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.)
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Abstract
The utility model discloses a dish type flight device which can fly at low altitude. A driving room and a machine body are connected in a machine body, and the machine body is a fixing dish core. The driving room is arranged in the machine body, and a rotary dish is arranged outside the machine body. A twin engine and a double-jet device are arranged between the driving room and the rotary dish, the open position of the middle portion of the rotary dish is respectively connected with the fixing dish core and a pedestal, the inner portion of the rotary dish is concave and hollow and is provided with a concave tooth ring which is connected with a gear disc, and the outer portion of the rotary dish is a solid body. An engine, the gear disc and the concave tooth ring are connected to make the rotary dish rotate at high speed, and make the pressure on the dish and the pressure below the dish contrast, and make the downward jet air of the double-jet device form reaction force. The flight direction is controlled by changing the direction of the air jet port, and the purpose that the dish type flight device upward flies is obtained.
Description
Technical field
The utility model relates to a kind of low-latitude flying device, especially can be at the disc aircraft of hedgehopping closely.
Background technology
At present, the autogyro of known low-latitude flying, its structure mainly is that screw propeller, body, empennage are formed by connecting, by the flight of screw propeller rotary lifting, and by the control of the small propeller on empennage heading.But because of its body is big, the rotation wing is longer, landing and flight all are subjected to certain place, course line restriction, and in addition, complex structure own is difficult for popularizing.
Summary of the invention
Existing autogyro body is big in order to solve, the rotation wing is longer, landing and flight all are subjected to the problem of place, course line restriction, the utility model provides a kind of aircraft, this aircraft can not only be as the flight of autogyro vertical takeoff and landing, and can be with rising with falling, not limited by place, course line, small and exquisite convenient.
The technical scheme in the invention for solving the technical problem is: in body, cockpit, fuselage connect, and cockpit is arranged in the fuselage, and fuselage is rotation disc, no empennage outward.Fuselage is a fixedly dish heart of being made up of inside and outside two cylinders that are nested, and each cylinder is supported by 4 steel pipes, all is connected with base.Inner cylinder is a cockpit, places 2 driving engine and 2 air jet systems with power in the outer Cylinder and on the base, and the bearing tube is set on the support tube of front and back; The rotation disc is the disc shape, under the dish mind-set, the upper and lower opening in saturating vacancy, center respectively with fixing dish in the heart end be connected with bottom and base, the rotation disc partly is a hollow by the fixing dish heart, inwall is by 4 vertical fixed supports and the some crosswise fixed bands spill that is formed by connecting, a recessed gear ring is established at the position, center, and disc outer part is a solid; Cockpit is that single dish car is sailed, and yaw rudder, throttle are connected with driving engine, air jet system; Twin-enginedly be placed on supporting steel pipe places before and after the exterior circular column, be connected with bearing swinging head on the support tube; Two air jet systems are upside down in the support tube place, the left and right sides of exterior circular column, and air nozzle down.Drive disc around fixing dish heart high speed revolution when twin-engined by toothed disc, recessed gear ring, can be considered motionless and the principle pressure contrast according to the dish heart of high speed revolution, the air cushion that produces under disc makes disc form the pressure contrast up and down, with whole disc picking-up; Two air jet systems are the air-flow of ejection downwards, produces antagonistic force upwards, about the control spout, the direction of front and back, can reach the purpose that disc aircraft flies.
The beneficial effects of the utility model are that landing and flight are not limited by place, course line, with rising with falling, are low latitude small vehicles easily, and is simple in structure, easy to operate.
Description of drawings
Below in conjunction with drawings and Examples the utility model is further specified.
Fig. 1 is the utility model side-looking constructional drawing.The disc aircraft external form is made of cockpit storehouse cover (1), lid (2), rotation disc (3).
Fig. 2 is first embodiment elevation profile constructional drawing of disc aircraft.
Fig. 3 is second penetrating constructional drawing of embodiment of disc aircraft.
Fig. 4 is the fixedly penetrating constructional drawing of the dish heart of the 3rd embodiment of disc aircraft
Fig. 5 is the air jet system position view.On the exterior circular column and base (38) of two air jet systems (7) outside the fixing dish heart (4) inner cylinder.
Fig. 6 is the 4th penetrating constructional drawing of embodiment cockpit of disc aircraft.
Fig. 7 is a cockpit yaw rudder scheme drawing.Motor switch (22), air jet system switch (23), engine throttle (24), air jet system throttle (25), semi-disc (26) line are connected with the control loop of air nozzle, the controlling aircraft left and right directions.
Fig. 8 is a cockpit height handle scheme drawing.Height handle (27) below yaw rudder is connected with the air nozzle control loop, control front and back and height heading.
Fig. 9 is fixing air nozzle control plane scheme drawing on the dish heart and the base.Fixedly the dish heart (4), cockpit (14), air nozzle (21), control loop (28).Semi-disc (26) line control air nozzle left and right directions, height handle (27) line control air nozzle front and back and height direction.
Figure 10 is the air nozzle organigram of air jet system.Gimbal suspension rotating shaft (29), knuckle guard (30).
Figure 11 is Figure 10 knuckle guard organigram.
Figure 12 is Figure 10 joint rotating shaft organigram.
Figure 13 is an air nozzle control loop scheme drawing.
Figure 14 is travel(l)ing rest structure (contraction) scheme drawing.Disc aircraft takes off, and up lifts semicircle switch (10), pulls out removable pin (33), and travel(l)ing rest (13), the whippletree that contacts to earth (36) shrink.Removable pin, the built-in spring of travel(l)ing rest.
Figure 15 is Figure 14 travel(l)ing rest organigram.
Figure 16 is travel(l)ing rest structure (strutting) scheme drawing.With shown in Figure 14 opposite, aircraft descends, down depresses semicircle switch (10), pressure frame (35) pressure moving casing (32) exposes movable lock-joint (34), and movable bayonet lock (33) blocks travel(l)ing rest (13), supports aircraft by the whippletree that contacts to earth (36).
Figure 17 is Figure 16 travel(l)ing rest organigram.
Figure 18 is the rotation disc belfry figure of disc aircraft.4 vertical fixed supports (19) connect into concave body with some crosswise fixed bands (20).
Figure 19 is a bearing swinging head organigram.Bearing swinging head (15) goes up to toothed disc (5), be fixed gear wheel (16) down.
Figure 20 is Figure 19 bearing swinging head bearing scheme drawing.
Figure 21 is the suitable for reading and fixing dish heart connection diagram of rotation disc.Rotation disc (11) suitable for reading is connected with the fixing dish heart (2), and interface is the bearing slip.
Figure 22 is Figure 21,23 interface bearing construction scheme drawings.
Figure 23 is rotation disc end opening and base connection diagram.Rotation disc end opening (12) is connected with base (38), and interface is that bearing slides.
Figure 24 is the air jet system organigram.Driving engine (37) connects as one with air-jet cover, and air nozzle (21) down.
1. storehouses cover among the figure, 2. lid, 3. rotation disc, the 4. fixing dish heart, 5. toothed disc, 6. driving engine, 7. air jet system, 8. recessed gear ring, 9. yaw rudder, 10. half garden switch, 11. discs are suitable for reading, 12. the disc end opening, 13. travel(l)ing rests, 14. cockpits, 15. the bearing swinging head, 16. fixed gear wheels, 17. fuel tanks, 18. support tube, 19. vertical fixed supports, 20. crosswise fixed bands, 21. air nozzle, 22. motor switchs, 23. air jet system switches, 24. engine throttle, 25. air jet system throttles, 26. semi-discs, 27. the height handle, 28. air nozzle direction control loops, 29. gimbal suspension rotating shafts, 30. knuckle guard, 31. extension rods, 32. moving casings, 33. removable pin, 34. movable lock-joints, 35. pressure frames, the whippletree 36. contact to earth, 37. jet engines, 38. bases.
The specific embodiment
In enforcement shown in Figure 2, fixedly overlap cockpit (14) in the dish heart (4), go up and be storehouse cover (1), lid (2), bearing swinging head (15), toothed disc (5) fixedly are set respectively on the symmetrical steel pipe of the dish heart (4) outside cylinder and are connected with rotation disc (3), rotation disc (3) (11) suitable for reading is connected with the fixing dish heart (4), end opening (12) is connected with base (38), and the junction is the bearing rotation.
In second embodiment shown in Figure 3, the disc aircraft center is the fixing dish heart (4), is made up of two cylinders that size is nested, and each cylinder is supported by 4 steel pipes (18), inner cylinder is that cockpit (14) is a little more than locating cylinder, all around sealing, in yaw rudder (9), semicircle switch (10) are set, upward cover (1) for the storehouse, the storehouse cover is opened from the place ahead, the rear is connected by hinge, is connected with base (38) down, and cockpit is a single dish seat (limited space); Exterior circular column is empty thoroughly, and front and back are provided with each driving engine (6) respectively, about each air jet system (7) is set respectively, go up to lid (2), lid are fuel tank (17) down, be connected with base (38) down; Contact to earth whippletree (36) in base (38) below.Rotation disc (3) partly is a hollow by the fixing dish heart, in have 4 vertically to connect into spill because of fixed rack (19) and some crosswise fixed bands (20), its center is located to establish recessed gear ring (8) and be connected with the toothed disc (5) of bearing swinging head (15).Rotation disc (11) suitable for reading is held in the heart with fixing dish and is connected, and end opening (12) is connected with base (38).
In the 3rd embodiment shown in Figure 4, before and after fixedly in the dish heart (4) exterior circular column (being as the criterion) with the chaufeur direction respectively be provided with a driving engine (6), about an air jet system (7) respectively is set, driving engine is connected with bearing swinging head (15) and fixed gear wheel (16) on the steel pipe of front and back respectively, and the toothed disc on the bearing swinging head (5) is connected with recessed gear ring (8) in the rotation dish; Left and right sides air jet system air nozzle (21) has control loop (28) to be connected with cockpit (14) and yaw rudder (9) down on the air nozzle.
In the 4th embodiment shown in Figure 6, yaw rudder (9), motor switch (22), engine throttle (24) connection driving engine are set in the cockpit (14); Air jet system switch (23), air jet system throttle (25) connect air jet system; Yaw rudder (9), semi-disc (26), height handle (27) connect air nozzle direction control loop (28), control flight all around direction; Semicircle switch (10), extension rod (31), pressure frame (35), removable pin (33), moving casing (32) connect travel(l)ing rest (13), removable pin, the built-in spring of moving casing.Semicircle switch (10) is walked around the chaufeur head and is up lifted, and pulls out removable pin (33), travel(l)ing rest (13) contraction, and aircraft becomes state of flight; The semicircle switch is depressed the interior travel(l)ing rest of moving casing (33) toward pressing down by pressure frame (35) during landing, and removable pin blocks travel(l)ing rest, supports the aircraft of landing.
Claims (4)
1, a kind of disc aircraft.In body, cockpit, fuselage connect, and it is characterized in that: fixedly the dish heart is a fuselage, and cockpit is arranged on internal layer, are driving engine and air jet system between skin and the rotation disc, and fuselage is the rotation disc outward.
2, disc aircraft according to claim 1, it is characterized in that: saturating vacancy, rotation disc middle part is suitable for reading to be connected with the fixing dish heart, and end opening is connected with base, and disc is interior to be spill hollow by fixing dish heart place, if recessed gear ring is connected with double gear panel, disc is outward a solid.
3, disc aircraft according to claim 1 is characterized in that: twin-enginedly be connected with the duplex bearing swinging head respectively, the toothed disc on the bearing swinging head is connected with recessed gear ring in the rotation dish.
4, disc aircraft according to claim 1 is characterized in that: fixedly about dish heart bottom and base each air jet system, air nozzle control loop is set with the cockpit yaw rudder, just handle is connected on the air nozzle down.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200420050062 CN2734621Y (en) | 2004-04-18 | 2004-04-18 | Dish type flight device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200420050062 CN2734621Y (en) | 2004-04-18 | 2004-04-18 | Dish type flight device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2734621Y true CN2734621Y (en) | 2005-10-19 |
Family
ID=35264503
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200420050062 Expired - Fee Related CN2734621Y (en) | 2004-04-18 | 2004-04-18 | Dish type flight device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2734621Y (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102211661A (en) * | 2011-05-03 | 2011-10-12 | 陈洪国 | Helistat |
| CN102862680A (en) * | 2011-07-04 | 2013-01-09 | 刘刚 | Spherically dished aircraft |
-
2004
- 2004-04-18 CN CN 200420050062 patent/CN2734621Y/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102211661A (en) * | 2011-05-03 | 2011-10-12 | 陈洪国 | Helistat |
| CN102862680A (en) * | 2011-07-04 | 2013-01-09 | 刘刚 | Spherically dished aircraft |
| WO2013004070A1 (en) * | 2011-07-04 | 2013-01-10 | Liu Gang | Spherical saucer-shaped aviation aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |