CN204506375U - Multi-functional flying saucer - Google Patents
Multi-functional flying saucer Download PDFInfo
- Publication number
- CN204506375U CN204506375U CN201520114781.7U CN201520114781U CN204506375U CN 204506375 U CN204506375 U CN 204506375U CN 201520114781 U CN201520114781 U CN 201520114781U CN 204506375 U CN204506375 U CN 204506375U
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- China
- Prior art keywords
- mounting rod
- fuselage
- screw propeller
- oil cylinder
- flying saucer
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Abstract
The utility model relates to a kind of multi-functional flying saucer, belong to aircraft field, comprise circular fuselage, the smooth upper lobes of underbelly is wing shape, and uniform four mounting rods of fuselage edge, establish drive link in mounting rod, drive link is all connected with the driving engine of fuselage interior by power-transfer clutch, land, water and air can be realized all can run, economical and practical, be beneficial to and promote the use of and carry out salvage work.
Description
Technical field
The utility model relates to a kind of multi-functional flying saucer, belongs to aircraft field.
Background technology
In field of vehicles, be divided into the vehicle of land, water and air three types, the general water, land and air vehicle just can only run in its corresponding field.Present amphibious automobiles etc. are also greatly developed, but cannot use as aircraft, and running velocity is slow on the water, can delay as implemented the salvage works such as search and rescue the opportunity of recovering; Although existing hydroairplane can realize lifting waterborne, it takes off and landing by sliding realization on the water, and required stroke is comparatively large, and cannot realize vertical lift, pinpoint landing is more difficult; That is is researching and developing the aircraft of land locomotion can be similar to aerodone, has the wing that the span is larger, promotes difficulty high.
Utility model content
According to above deficiency of the prior art, the technical problems to be solved in the utility model is: provide a kind of multi-functional flying saucer realizing land, water and air and all can run, overcome the deficiency in above-mentioned background technology, economical and practical, be beneficial to and promote the use of and carry out salvage work.
Multi-functional flying saucer described in the utility model, comprises circular fuselage, and the smooth upper lobes of underbelly is wing shape, uniform four mounting rods of fuselage edge, and establish drive link in mounting rod, drive link is all connected with the driving engine of fuselage interior by power-transfer clutch;
Hinged two sections of mounting rods continuously on the mounting rod in front, all drive link is established in mounting rod, mounting rod head and the tail are hinged, adjacent drive bar is connected by differential drive, adjacent mounting rod passes through hydraulic oil cylinder driving, cylinder pedestal and piston rod are hinged on adjacent mounting rod respectively, the mounting rod of caudal end establishes screw propeller, screw propeller is fixedly connected with drive link, the flexible mounting rod that drives of oil cylinder rotates, screw propeller can realize four direction all around and rotate, and it is overlapping with fuselage or contact that screw propeller streaks region;
Hinged a bit of mounting rod on the mounting rod of both sides, all drive link is established in mounting rod, two drive links are connected by differential drive, mounting rod is by hydraulic oil cylinder driving, and cylinder pedestal and piston rod are hinged on adjacent mounting rod respectively, and the mounting rod of caudal end fixes screw propeller, screw propeller is connected with drive link, the flexible mounting rod that drives of oil cylinder rotates, and screw propeller can realize former and later two directions and rotate, and it is overlapping with fuselage or contact that screw propeller streaks region;
The mounting rod at rear upwards bends L-shaped, the a bit of mounting rod of its upper end thereof, establish drive link in mounting rod is equal, two drive links are connected by differential drive, and adjacent mounting rod passes through hydraulic oil cylinder driving, cylinder pedestal and piston rod are hinged on adjacent mounting rod respectively, the mounting rod of caudal end fixes screw propeller, and screw propeller is fixedly connected with drive link, and the flexible mounting rod that drives of oil cylinder rotates, screw propeller can realize four direction all around and rotate, and it is overlapping with fuselage or contact that screw propeller streaks region;
Fuselage circumference establishes four air bags, and air bag is by air-pump inflating and bleed;
Hinged four the retractable support pin of underbelly, feet stroke is controlled by oil cylinder, all establishes infrared distance sensor bottom feet, and infrared distance sensor is all connected with control system.
The screw propeller of fuselage both sides is replaceable is jet engines,
Underbelly convexes to form sump, and upper lobes is wing shape.
Fuselage is oval, conveniently travels in water.
Back is lid shape, and bottom is bowl-type.
The oil pipe of oil cylinder is fixed on the outer wall bottom of mounting rod.
Principle of work and process:
During work, four screw propellers are made all upward by controlling oil cylinder, start the engine, driving engine drives drive rod rotation by power-transfer clutch, drive link is rotated by differential drive carrying screws, the lift that screw propeller is formed drives fuselage to take off up, when need accelerate to rise, forward, such forebody upward for after screw, then by four screw propellers toward the front, promote flying saucer ascending velocity, when reaching desired height, then by after screw upward, flying saucer level is flown forward, then by after screw forward.Four screw propellers are controlled toward the front by oil cylinder, flying saucer and flight forward, because fuselage is wing shape, the lift of air is inherently subject to when flying, because front screw propeller can rotate by left and right four direction forwards, backwards, by regulate front screw propeller towards the direction, place controlling flying saucer and advance, after screw plays the effect of balance fuselage, by the boosting of four screw propellers, flying saucer is brought to destination.
Flying saucer is when landing, and control four screw propellers slightly backwards by oil cylinder, propeller shape becomes windage that flying saucer is slowed down and stops moving ahead, and now screw propeller returns just upward and reduces rotating speed gradually, and flying saucer starts to decline, if accelerate to decline, by front propeller forward, flying saucer front portion down, rotating speed or stall is reduced by the screw propeller of clutch control rear and both sides, to certain distance again by front propeller upward, before treating that flying saucer fuselage will be up to the standard, start other screw propellers, the orientation needing landing is now regulated by front and back screw propeller, four expansion links are made to stretch out by controlling oil cylinder, infrared distance sensor bottom expansion link detects the height of the level point immediately below it from expansion link, and be transferred to control system, control system is minimum by calculating which expansion link ground clearance, then other expansion links extend or shrink until identical with this root expansion link ground clearance, even if now also can land at accidental relief four strut bars that land simultaneously, stability is very strong.For the flying saucer of underbelly level, if drop to waterborne when carrying out the work such as rescue, when being reduced to dried up certain altitude, by air pump, airbag-releasing can be increased the buoyancy of flying saucer in advance when landing, for the flying saucer of bottom with sump, if exceed the displacement of flying saucer, then need to open the buoyancy that air bag increases flying saucer, when needs flying saucer hidden in water time, start water pump by the sump of water suction fuselage bottom, fuselage slowly submerges in water, when needs flying saucer surfaces, opened by water pump and discharged by the water in sump, fuselage emerges.
The beneficial effect that the utility model is compared with prior art had is:
Multi-functional flying saucer described in the utility model, because fuselage is wing shape, the lift of air is inherently subject to when flying, because front screw propeller can rotate by left and right four direction forwards, backwards, direction by adjustment front screw propeller controls the direction that flying saucer is advanced, can fly at complex-terrain, four strut bars can land simultaneously, and stability is very strong.Can drop to waterborne by air bag, purposes is wide, is easy to promote, and can be widely used in national defence exploration and search-and-rescue work.
Accompanying drawing explanation
Fig. 1 is the utility model embodiment 1 schematic diagram;
Fig. 2 is the utility model embodiment 2 schematic diagram;
Fig. 3 is the birds-eye view of embodiment 1 and 2.
In figure: 1, screw propeller; 2, diff; 3, drive link; 4, mounting rod; 5, chimney; 6, oil cylinder; 7, fuselage; 8, air bag; 9, vent window; 10, feet; 11, sump; 12, intake-outlet; 13, hatch door.
Detailed description of the invention
Below in conjunction with accompanying drawing, embodiment of the present utility model is described further:
Embodiment 1
As shown in figures 1 and 3, multi-functional flying saucer described in the utility model, comprises circular fuselage 7, the smooth upper lobes in fuselage 7 bottom is wing shape, uniform four mounting rods 4 in fuselage 7 edge, establish drive link 3 in mounting rod 4, drive link 3 is all connected by the driving engine of power-transfer clutch with fuselage 7 inside;
Hinged two sections of mounting rods 4 continuously on the mounting rod 4 in front, drive link 3 is all established in mounting rod 4, mounting rod 4 head and the tail are hinged, adjacent drive bar 3 is in transmission connection by diff 2, adjacent mounting rod 4 is driven by oil cylinder 6, oil cylinder 6 base and piston rod are hinged on adjacent mounting rod 4 respectively, the mounting rod 4 of caudal end establishes screw propeller 1, screw propeller 1 is fixedly connected with drive link 3, the flexible mounting rod 4 that drives of oil cylinder 6 rotates, screw propeller 1 can realize four direction all around and rotate, and single leaf length of screw propeller 1 is not overlapping with fuselage 7 or contact;
Hinged a bit of mounting rod 4 on the mounting rod 4 of both sides, drive link 3 is all established in mounting rod 4, two drive links 3 are in transmission connection by diff 2, mounting rod 4 is driven by oil cylinder 6, and oil cylinder 6 base and piston rod are hinged on adjacent mounting rod 4 respectively, and the mounting rod 4 of caudal end establishes screw propeller 1, screw propeller 1 is fixedly connected with drive link 3, the flexible mounting rod 4 that drives of oil cylinder 6 rotates, and screw propeller 1 can realize former and later two directions and rotate, and single leaf length of screw propeller 1 is not overlapping with fuselage 7 or contact;
The mounting rod 4 at rear upwards bends L-shaped, the a bit of mounting rod 4 of its upper end thereof, drive link 3 is established in mounting rod 4 is equal, two drive links 3 are in transmission connection by diff 2, adjacent mounting rod 4 is driven by oil cylinder 6, oil cylinder 6 base and piston rod are hinged on adjacent mounting rod 4 respectively, the mounting rod 4 of caudal end establishes screw propeller 1, screw propeller 1 is fixedly connected with drive link 3, the flexible mounting rod 4 that drives of oil cylinder 6 rotates, screw propeller 1 can realize four direction all around and rotate, and single leaf length of screw propeller 1 is not overlapping with fuselage 7 or contact;
Fuselage 7 periphery establishes four air bags 8, and air bag 8 is by air-pump inflating and bleed;
Four retractable support pin 10 are established in fuselage 7 bottom, and feet 10 stroke is controlled by oil cylinder 6, and all establish infrared distance sensor bottom feet 10, infrared distance sensor is all connected with control system.
The screw propeller 1 of fuselage 7 both sides is replaceable is jet engines,
Fuselage 7 lower lobes forms sump 11, and upper lobes is wing shape.
The oil pipe of oil cylinder 6 is fixed on the outer wall bottom of mounting rod 4.
Fuselage 7 is oval, can reduce the resistance of water when travelling in water, improves gait of march.
Principle of work and process:
During work, four screw propellers 1 are made all upward by controlling oil cylinder 6, start the engine, driving engine drives drive link 3 to rotate by power-transfer clutch, drive link 3 is rotated by diff 2 transmission carrying screws 1, the lift that screw propeller 1 is formed drives fuselage 7 to take off up, when need accelerate to rise, after screw 1 forward, such fuselage 7 front portion upward, then by four screw propellers 1 toward the front, promote flying saucer ascending velocity, again by after screw 1 upward, flying saucer level is flown forward, then by after screw 1 forward.Four screw propellers 1 are controlled toward the front by oil cylinder 6, flying saucer and flight forward, because fuselage 7 is in wing shape, the lift of air is inherently subject to when flying, because front screw propeller 1 can rotate by left and right four direction forwards, backwards, by regulate front screw propeller 1 towards the direction, place controlling flying saucer and advance, after screw 1 plays the effect of balance fuselage 7.Flying saucer is when landing, screw propeller 1 is controlled slightly backwards by oil cylinder 6, screw propeller 1 forms windage and flying saucer is slowed down and stops moving ahead, now screw propeller 1 time just upward and reduce rotating speed gradually, if accelerate to decline, by front propeller 1 forward, flying saucer front portion down, rotating speed or stall is reduced by the screw propeller 1 of clutch control rear and both sides, to certain distance again by front propeller 1 upward, treat that flying saucer fuselage 7 will before level, start other screw propellers 1, the orientation needing landing is now regulated by front and back screw propeller 1, stretch out four expansion links, infrared distance sensor bottom expansion link detects the height of the level point immediately below it from expansion link, and be transferred to control system, control system is minimum by calculating which expansion link ground clearance, then other expansion links extend or shrink until identical with this root expansion link ground clearance, four strut bars that now land can land simultaneously, stability is very strong.If drop to waterborne when carrying out the work such as rescue, air bag 8 can be opened by air pump the buoyancy increasing flying saucer when landing, when needs flying saucer hidden in water time, start water pump by the sump 11 bottom water suction fuselage 7, fuselage 7 slowly submerges in water, when needs flying saucer surfaces, opened by water pump and discharged by the water in sump 11, fuselage 7 emerges.
Embodiment 2
As shown in Figures 2 and 3, fuselage is bottom surface is plane, and fuselage is wing shape, and other structures are identical with embodiment 1, and so aloft during high-speed flight, the draught head of fuselage upper and lower surface, to the certain lift of fuselage, is beneficial to flight.
Embodiment 3
Fuselage is oval, is beneficial to and travels in water.
Embodiment 4
Back is lid shape, and bottom is bowl-type.
Claims (7)
1. a multi-functional flying saucer, comprise circular fuselage (7), it is characterized in that: the smooth upper lobes in bottom is wing shape, uniform four mounting rods (4) in fuselage (7) edge, establish drive link (3) in mounting rod (4), drive link (3) is all connected by the driving engine that power-transfer clutch is inner with fuselage (7);
Hinged two sections of mounting rods (4) continuously on the mounting rod (4) in front, drive link (3) is all established in mounting rod (4), mounting rod (4) head and the tail are hinged, adjacent drive bar (3) is in transmission connection by diff (2), adjacent mounting rod (4) is driven by oil cylinder (6), oil cylinder (6) base and piston rod are hinged on adjacent mounting rod (4) respectively, the mounting rod (4) of caudal end establishes screw propeller (1), screw propeller (1) is fixedly connected with drive link (3), the flexible mounting rod (4) that drives of oil cylinder (6) rotates, screw propeller (1) can realize four direction all around and rotate, single leaf length of screw propeller (1) is not overlapping with fuselage (7) or contact,
The upper hinged a bit of mounting rod (4) of mounting rod (4) of both sides, drive link (3) is all established in mounting rod (4), two drive links (3) are in transmission connection by diff (2), mounting rod (4) is driven by oil cylinder (6), oil cylinder (6) base and piston rod are hinged on adjacent mounting rod (4) respectively, the mounting rod (4) of caudal end establishes screw propeller (1), screw propeller (1) is fixedly connected with drive link (3), the flexible mounting rod (4) that drives of oil cylinder (6) rotates, screw propeller (1) can realize former and later two directions and rotate, single leaf length of screw propeller (1) is not overlapping with fuselage (7) or contact,
The mounting rod (4) at rear upwards bends L-shaped, the a bit of mounting rod of its upper end thereof (4), drive link (3) is all established in mounting rod (4), two drive links (3) are in transmission connection by diff (2), adjacent mounting rod (4) is driven by oil cylinder (6), oil cylinder (6) base and piston rod are hinged on adjacent mounting rod (4) respectively, the mounting rod (4) of caudal end establishes screw propeller (1), screw propeller (1) is fixedly connected with drive link (3), the flexible mounting rod (4) that drives of oil cylinder (6) rotates, screw propeller (1) can realize four direction all around and rotate, single leaf length of screw propeller (1) is not overlapping with fuselage (7) or contact.
2. multi-functional flying saucer according to claim 1, is characterized in that: fuselage (7) periphery establishes four air bags (8), and air bag (8) is by air-pump inflating and bleed.
3. multi-functional flying saucer according to claim 2, it is characterized in that: four retractable support pin (10) are established in fuselage (7) bottom, feet (10) stroke is controlled by oil cylinder (6), infrared distance sensor is all established in feet (10) bottom, and infrared distance sensor is all connected with control system.
4. multi-functional flying saucer according to claim 1, is characterized in that: the screw propeller (1) of fuselage (7) both sides is replaceable is jet engines.
5. multi-functional flying saucer according to claim 1, is characterized in that: fuselage (7) lower lobes forms sump (11), and upper lobes is wing shape.
6. multi-functional flying saucer according to claim 3, is characterized in that: the oil pipe of oil cylinder (6) is fixed on the outer wall bottom of mounting rod (4).
7. multi-functional flying saucer according to claim 1, is characterized in that: fuselage (7) is for oval.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520114781.7U CN204506375U (en) | 2015-02-24 | 2015-02-24 | Multi-functional flying saucer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520114781.7U CN204506375U (en) | 2015-02-24 | 2015-02-24 | Multi-functional flying saucer |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204506375U true CN204506375U (en) | 2015-07-29 |
Family
ID=53704375
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520114781.7U Expired - Fee Related CN204506375U (en) | 2015-02-24 | 2015-02-24 | Multi-functional flying saucer |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204506375U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104626904A (en) * | 2015-02-24 | 2015-05-20 | 丁乃祥 | Multifunctional flying saucer |
| CN109334365A (en) * | 2018-08-21 | 2019-02-15 | 哈工大机器人义乌人工智能研究院 | A kind of land, water and air three are dwelt rotor robot and its working method |
-
2015
- 2015-02-24 CN CN201520114781.7U patent/CN204506375U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104626904A (en) * | 2015-02-24 | 2015-05-20 | 丁乃祥 | Multifunctional flying saucer |
| CN109334365A (en) * | 2018-08-21 | 2019-02-15 | 哈工大机器人义乌人工智能研究院 | A kind of land, water and air three are dwelt rotor robot and its working method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150729 Termination date: 20160224 |