CN101941365A - Personal triphibious transport tool - Google Patents
Personal triphibious transport tool Download PDFInfo
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- CN101941365A CN101941365A CN 201010502705 CN201010502705A CN101941365A CN 101941365 A CN101941365 A CN 101941365A CN 201010502705 CN201010502705 CN 201010502705 CN 201010502705 A CN201010502705 A CN 201010502705A CN 101941365 A CN101941365 A CN 101941365A
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- ducted fan
- lamellar
- airframe
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Abstract
The invention relates to a personal triphibious transport tool comprising an airframe, a cabin and lamellar bodies, wherein the bottom of the front end of each lamellar body is provided with a front undercarriage and a front undercarriage controlling device; the rear end of the airframe is provided with a rear undercarriage and a rear undercarriage controlling device; the front end of the bottom of the airframe is provided with a front ducted fan perpendicular to the airframe, wherein the front end of the bottom of the airframe is positioned between the two lamellar bodies; the top surface of the rear end of the airframe is provided with a rear ducted fan perpendicular to the airframe; the front ducted fan and the rear ducted fan are respectively provided with a guide plate, a diffuser grid, a guide plate deflection control mechanism and a diffuser grid deflection control mechanism; both sides of the rear end of the airframe or both sides of the rear ducted fan are articulated with rear airfoils; the rear end of the airframe is articulated with a U-shaped hydrofoil. The invention adopts a peculiar overturned airframe type and thrust deflection type mixed configuration structure and meets the requirements of outing of people through the overall transition of water, land and air.
Description
Technical field
The present invention relates to a kind of personal small vehicles, specifically a kind of individual three-purpose vehicle.
Background technology
Practical application has some two amphibious or land and air double-used purpose vehicles at present, and these two purpose vehicles have been expanded the application of ordinary traffic instrument, for use provides certain convenience.But the structure of these two purpose vehicles is generally all comparatively complicated, and floor area is big, has " deadweight " many and not high problem of safety.The design plan of existing three-purpose vehicle, all unreasonable because of its structure, so can not drop into practical application, can not solve the traffic problems that water, land and air three is dwelt effectively simultaneously, also all can not realize vertical/short take-off and landing (STOL).
Summary of the invention
Purpose of the present invention just provides a kind of individual three-purpose vehicle, to overcome the use limitation that existing Personal Transporter exists, solve that compound type vehicle configurations complexity, volume are big, " deadweight " is many, safety is low with can not vertical/problems such as short take-off and landing (STOL).
The present invention is achieved in that a kind of individual three-purpose vehicle, comprise body, passenger cabin in the body upper setting, and the lamellar body that is provided with in the bottom surface of body bilateral symmetry, described lamellar body be hypotenuse under right-angled triangle, front bottom end at described lamellar body is provided with nose-gear and nose-gear draw off gear, is provided with back alighting gear and back undercarriage control device in the rear end of described body; The bottom front of the described body between described two lamellar bodies is provided with perpendicular to described body and the windward side preceding ducted fan towards the front upper place, is provided with perpendicular to described body and the windward side back ducted fan towards the front upper place at the rear end of described body end face; Before described, be respectively equipped with deflecting plate, airflow fence and deflecting plate deflection control mechanism and airflow fence deflection control mechanism in ducted fan and the described back ducted fan; Be hinged with the back wing in the both sides, rear end of described body or the both sides of described back ducted fan, be hinged with in the rear end of described body and can do the U-shaped hydrofoil that rotates up and down.
Described lamellar body is fixedly connected on the bottom of described body, is connected to preceding hydrofoil between the front bottom end of two described lamellar bodies, is hinged with preceding wing in the front end both sides of described body.
The two ends of hydrofoil are fixed on the medial surface of two described lamellar bodies before described.
Be provided with switching mechanism in described lamellar body inside, the two ends of described preceding hydrofoil join with described switching mechanism respectively.
Described lamellar body is hinged on the bottom surface of described body, is provided with the hydraulic control that the described lamellar body of control turns up in described body.
Ducted fan is fixed on the bottom of described body or the bottom of hinged described body before described.
The duct rear port of ducted fan and/or described back ducted fan is the inclined-plane port that the top extends back before described.
The vehicle of the present invention are by body, in the passenger cabin of body upper setting and a kind of structure of being done on the basis of the catamaran that the lamellar body of the bottom surface of body bilateral symmetry setting is formed, function and the invention of characteristics brand new.The vehicle of the present invention are set up the forward and backward ducted fan of windward side towards the front upper place respectively by front lower place and back upper place at body, on forward and backward ducted fan, cooperate airflow fence that air flow line is carried out downwards or the adjustment and the control of backward directions, be aided with the lifting force of wings effect again, can realize the vertical takeoff and landing and the skyborne stabilized flight of these vehicle.When these vehicle during at surface navigation, be with catamaran form, provide navigating power by the back ducted fan, so just exempted the setting of the actuating device under water of the original structure more complicated of catamaran.In addition, in the process of vertical takeoff and landing or horizontal flight, all ducted fans on these vehicle are all in running order.The existence of these characteristics has reduced " the flight deadweight " of these vehicle, " deadweight " the big problem that overcomes to greatest extent.And the setting of the forward and backward alighting gear in the vehicle of the present invention both can realize these vehicle powered travel function on land, also can be used as the vertical/short take-off and landing (STOL) device of flight tool.The sheet body structure of the right-angled triangle of organism bottom, the low situation in high back before these vehicle are presented under the dead state of ground, make the angle of inclination of the windward side maintenance of the forward and backward ducted fan on the body towards the front upper place, so just can utilize the airflow fence in the forward and backward ducted fan air-flow that is produced by the screw propeller high speed revolution to be carried out vertically downward or level air-flow guiding backward, realize the vertical takeoff and landing and the horizontal flight function of these vehicle thus.Wing can form folding wing behind the pivotally attached, thereby reduces the space hold of these vehicle in the driving process of land effectively.And the setting of the U-shaped hydrofoil of After-Body has improved the lift of the surface navigation of these vehicle on the one hand, and passes through the raising of navigation lift, can correspondingly raise body, reduces the wetted area of body, reduces running resistance; On the other hand, can remedy lamellar body again effectively and make the deficiency that the navigation degree of stability that exists behind the triangle reduces into, make these vehicle when surface navigation, can keep higher smoothness and route speed faster; Simultaneously, cooperate the lamellar body setting of both sides again, will gather a certain amount of delay gas, form cushioning effect, thereby more help the surface navigation of these vehicle at the underpart of raising.The rotary type of U-shaped hydrofoil connects, the different needs in the time of can adapting to these vehicle at land locomotion with at surface navigation.
The vehicle of the present invention both can be used as the manned vehicle, also can be used as the unmanned vehicle, also can be used as large-scale water, land and air three-purpose vehicle.
Vehicle configurations of the present invention is simple, uses economic and reliable, be a kind of can either be at land locomotion, can aloft fly again, can also satisfy people's trip needs with comprehensive transition of water, land and air three of the surface navigation Personal Transporter of dwelling.The vehicle of the present invention adopt the distinctive body formula of verting to mix the configuration structure that uses with the thrust gauche form, overcome the use limitation that existing two purpose vehicles exist effectively, solved existing amphibious or three-purpose vehicle complex structure, deadweight is many and safety low problem.The present invention is rational in infrastructure, and is easy and simple to handle, the reliability height.
Description of drawings
Fig. 1 is a structural representation of the present invention.
Fig. 2 is that the A of Fig. 1 is to view.
Fig. 3 is that the B of Fig. 1 is to view.
Fig. 4 is an external structure scheme drawing of the present invention.
Fig. 5 is the structural representation that adopts three ducted fan embodiment.
Fig. 6 is the structural representation that adopts collapsible lamellar body embodiment.
Fig. 7 is the birds-eye view of Fig. 6.
Fig. 8 is the conversion specification figure of three kinds of operation scheme of the present invention.
The specific embodiment
Embodiment 1:
As shown in Figure 1 and Figure 2, the present invention individual three-purpose vehicle comprise one have upper and lower surface, shape is according to aerodynamic principle design-calculated body 1, passenger cabin is arranged on the top of body 1, be provided with two sagging lamellar bodies 13 in the bottom surface of body 1 bilateral symmetry, rectangular triangle in the side of lamellar body 13 and hypotenuse are following.Two lamellar bodies 13 and body 1 are for captiveing joint.Hydrofoil 9 before between the front bottom end of two lamellar bodies 13, being connected to.The two ends of preceding hydrofoil 9 both can be the medial surfaces that is connected two lamellar bodies 13 by fixed form; One cover switching mechanism also can be set respectively in the inside of two lamellar bodies 13, the two ends of preceding hydrofoil 9 are joined with this two switching mechanism respectively, form a kind of convertible top and bottom interchangeable before hydrofoil, to adapt to land and different needs under water.Front bottom end at lamellar body 13 also is provided with nose-gear 10 and nose-gear draw off gear 12, and wheel 11 before be equipped with the bottom of nose-gear 10.Be provided with back alighting gear 15 and back undercarriage control device 17 in the rear end of body 1, back wheel 16 be housed in the bottom of back alighting gear 15.
As shown in Figure 1 and Figure 2, between the bottom front of body 1, two lamellar bodies 13, be arranged side by side two preceding ducted fans 4 perpendicular to body 1, because the low gesture in high back before body 1 is, so two preceding ducted fans 4 that are loaded on body 1 front end just form the situation of windward side towards the front upper place naturally.Preceding ducted fan 4 can be to adopt fixed form to be connected with body 1, also can connect by the pivotally attached mode, with the collapsible connection structure of ducted fan before forming 4 with body 1.Be provided with this folding before ducted fan, when these vehicle during at land locomotion or at surface navigation, with regard to collapsible bottom, to reduce corresponding resistance at body 1.Being provided with two windward sides perpendicular to ducted fan 22 behind 22, two of the back ducted fans of body 1 side by side at the rear end of body 1 end face also is towards the front upper place.The duct setting of this tilting is convenient to produce along with the angular adjustment of airflow fence vertically downward thrust and level thrust backward.The turning cylinder of screw propeller in preceding ducted fan 4 and back ducted fan 22 respectively by pillar 8 support and connection, the blade 5 of screw propeller is loaded on the front end of turning cylinder; Fairing 6 and pitch-changing mechanism etc. also can be installed in the usual way in front portion at screw propeller; Driving engine 7 or the transmission gearbox 20 that drives the screw propeller rotation is housed at the rear portion of screw propeller.Transmission gearbox 20 is applicable to the structure that is provided with of a plurality of ducted fans side by side, and the quantity that is provided with corresponding minimizing driving engine alleviates complete machine weight.Among Fig. 1, in preceding ducted fan 4 and back ducted fan 22, also be respectively arranged with deflecting plate 21 and airflow fence 19, and deflecting plate deflection control mechanism and airflow fence deflection control mechanism, the pull bar 18 among Fig. 1 is exactly a kind of deflection control mechanism of airflow fence.
Before above-mentioned, back ducted fan has adopted the structure of existing ducted fan substantially, and for the ducted fan of this heeling condition among the present invention, the present invention improves the duct of ducted fan especially, the duct rear port of ducted fan 4 and/or back ducted fan 22 is designed to the inclined-plane port that the top extends back before being about to, the angle of inclination that can increase the duct rear port like this and be loaded on the airflow fence at duct rear port place, make the waste of power of air-flow in vertical and horizontal direction switching process littler, be more convenient for keeping carrying out the conversion adjustment of normal thrust and horizontal thrust under the body attitude unmodified situation.
As Fig. 2, Fig. 3 and shown in Figure 4, wing 2 before the left and right sides of body 1 front end also is hinged with respectively is to form folding preceding wing 2.Specifically can adopt wing-folding device 24 that preceding wing 2 is linked together with body 1.Be hinged with back wing 23 in the both sides of back ducted fan 22, form folding back wing 23, promptly back wing 23 also is to link together by the outer hull of wing-folding device with back ducted fan 22.Both sides, rear end at body 1 are hinged with U-shaped hydrofoil 14, and U-shaped hydrofoil 14 can realize being positioned at the top and the upper and lower conversion that is positioned at the body rear end bottom of back ducted fan by electronic or hydraulic control device.Certainly, carry out at U-shaped hydrofoil 14 before the operation of upper and lower conversion, by the wing-folding device back wing 23 to be packed up earlier, make it to be posted by the duct outer wall of back ducted fan 22, just can carry out the transposition of U-shaped hydrofoil afterwards.Wing-folding device 24 can adopt conventional manual or electric control mechanism.
Among Fig. 1, the parachute 25 that receipts gather into folds also can be set at the top of body 1.In case the vehicle of the present invention aloft fly when unexpected dangerous situation occurring, press control button, parachute 25 is ejected, and open automatically, thereby guarantee the vehicle of the present invention and aircrew's safe landing.
Embodiment 2:
As shown in Figure 5, the agent structure of present embodiment is substantially with embodiment 1, and front bottom end, the preceding ducted fan between two lamellar bodies 13 4 that only is arranged on body 1 is side by side three, and what back ducted fan 22 also was provided with is three side by side.Wing 2 is arranged on the front end of body 1 before folding, and folding back wing 23 is arranged on after three in the ducted fan 22 after two of both sides on the hull outside face of ducted fan.Certainly, the quantity of back ducted fan 22 can be not be consistent with the quantity of preceding ducted fan 4 yet, but the quantity of ducted fan 4 before will being less than, and the U type hydrofoil that is loaded on body 1 rear end is turned on smooth.
Present embodiment is because the quantity of forward and backward ducted fan increases, and tractive power strengthens, and therefore, passenger capacity and load carrying ability all can increase to some extent.
Embodiment 3:
As Fig. 6, shown in Figure 7, the agent structure of present embodiment is substantially with embodiment 1, its key distinction point, and the one, preceding ducted fan 4 and back ducted fan 22 all only are provided with one, thereby constitute the individual three-purpose vehicle that weight is the lightest, structure is the simplest; The 2nd, cancelled the setting of preceding wing; The 3rd, back wing 23 has been retrofitted to the both sides, rear portion of body 1 from the duct housing of back ducted fan 22; The 4th, lamellar body 13 changes the bottom surface that is hinged on body 1 into by captive joint, is provided with the external hydraulic control that turns over of control strip in body 1, forms the three-purpose vehicle that a kind of lamellar body can flip to the outside thus.
Because but the lamellar body 13 in the present embodiment is flexible connection forms that a kind of side direction is turned up, and the lamellar body that turns up itself just can be used as a kind of wing use, play the effect that improves lift, therefore, on the one hand the surface texture shape of lamellar body 13 should be made according to aerodynamic principle, hydrofoil before also just can not fixedly mounting between two lamellar bodies 13 on the other hand.Under the effect of the lamellar body 13 open and flat backs of turning up formed a kind of like this " big wing ", the vehicle of the present invention just can successfully be implemented in the hedgehopping on the water surface, just " imitate flight " makes these vehicle form a kind of " ground effect ship " thus.The outstanding effect of this realization the " imitate flight " is the characteristics that the existing vehicle do not possess, can not compare.
Fig. 8 has provided three of the vehicle of the present invention conversion operation mode of dwelling.In conjunction with shown in Figure 8, mode of operation of the present invention is:
1, airflight pattern
Under ground-surface state of nature, the low state in high back before the body 1 of these vehicle is, preceding ducted fan 4 all is towards the front upper place with the windward side of back ducted fan 22.
1.1 at these vehicle when take off in ground, wing 2 and back wing 23 before opening, driving engine 7(or transmission gearbox 20 before utilizing in ducted fan 4 and the back ducted fan 22) driving screw propeller high speed revolution, simultaneously, drive airflow fence 19 deflections in the forward and backward ducted fan respectively by airflow fence deflection control mechanism, so that the high velocity air that is produced in the forward and backward ducted fan is led---when air-flow is directed to straight down direction, can produce thrust straight down, make these vehicle vertically rise (or landing); When air-flow is directed to backward direction of level, can produce level thrust backward, promote these vehicle and fly forward.When aloft flying, also may command body 1 verts, be the level of state, and remain under this state and advance, the windward side of the forward and backward ducted fan of this moment is just all towards horizontal direction, the airflow fence of adjusting again in the forward and backward ducted fan 19 also all is in horizontality, and then the horizontal thrust of these vehicle can reach maximum at this moment, and the speed of a ship or plane is the fastest.
In the process of these vehicle horizontal flight, by adjusting the deflecting direction of the deflecting plate 21 in the forward and backward ducted fan, i.e. may command flight course.In flight course, U-shaped hydrofoil 14 can be put in the bottom position of body 1 rear end down, in order to producing flight lift.
These vehicle also can utilize forward and backward alighting gear, carry out Horizontal Take-off and Landing by the sliding mode of running of short distance.
1.2 when the water surface takes off, need earlier to be turned to upperly from the next U-shaped hydrofoil 14 at these vehicle, promptly forward the upper end of back ducted fan 22 to, other operating process is basic identical with the process of taking off from ground then.
2, surface navigation pattern
Before the navigation, pack up forward and backward alighting gear earlier, pack up the preceding ducted fan (fixed then motionless) of forward and backward wing and radial type again, U-shaped hydrofoil 14 is rotated backward from the top put down, and the stage casing of U-shaped hydrofoil 14 is paralleled with the preceding hydrofoil 9 of body 1 front portion or be in same level.After this get final product start the engine 7, drive the screw propeller high speed revolution in the ducted fan 22 of back, utilize the air-flow thrust of back ducted fan 22, drive these vehicle as catamaran at surface navigation, and can be by the 21 control direct of travels of the deflecting plate in the ducted fan 22 of back.
Because the lifting effect of preceding hydrofoil 9 and U type hydrofoil 14, and the existence of the lamellar body 13 of both sides, body 1 bottom, make front portion lifting to some extent in traveling process of body 1, like this, will gather a certain amount of delay gas in the bottom of body 1, thereby the formation cushioning effect, this moment these vehicle surface navigation just to be analogous to air cushion vehicle equally light, quick.
3, ground run pattern
When these vehicle are parked in ground and prepare to travel, need pack up the preceding ducted fan (fixed motionless) of forward and backward wing and pivotally attached earlier, put down forward and backward alighting gear and adjust the angle of landing of back alighting gears 15 by back undercarriage control device 17, so that body 1 trends towards level as best one can, these sample vehicle just can be analogous to a land vehicle.And the preceding hydrofoil 9 of body 1 front portion can play the effect of deciding the wind wing after 180 ° of axial upsets; In like manner, the U-shaped hydrofoil 14 at body 1 rear portion be turned to upper after, also can play the effect of spoiler.Afterwards, by starter motor, the back wheel 16 that can drive on the alighting gear 15 of back rotates, and these vehicle are advanced at ground run; Preceding wheel 11 on the nose-gear 10 then can be used as the track adjusting wheel that control turns to, and controls the direct of travel of these vehicle.
Claims (7)
1. individual three-purpose vehicle, comprise body (1), the passenger cabin that is provided with on body (1) top, and the lamellar body (13) that is provided with in the bottom surface of body (1) bilateral symmetry, it is characterized in that, described lamellar body (13) be hypotenuse under right-angled triangle, be provided with nose-gear (10) and nose-gear draw off gear (12) in the front bottom end of described lamellar body (13), be provided with back alighting gear (15) and back undercarriage control device (17) in the rear end of described body (1); The bottom front of the described body (1) between described two lamellar bodies (13) is provided with perpendicular to described body and the windward side preceding ducted fan (4) towards the front upper place, is provided with perpendicular to described body and the windward side back ducted fan (22) towards the front upper place at the rear end end face of described body (1); Be respectively equipped with deflecting plate (21), airflow fence (19) and deflecting plate deflection control mechanism and airflow fence deflection control mechanism in ducted fan before described (4) and the described back ducted fan (22); Be hinged with back wing (23) in the both sides, rear end of described body (1) or the both sides of described back ducted fan (22), be hinged with in the rear end of described body (1) and can do the U-shaped hydrofoil (14) that rotates up and down.
2. individual three-purpose vehicle according to claim 1, it is characterized in that, described lamellar body (13) is fixedly connected on the bottom of described body (1), between the front bottom end of two described lamellar bodies (13), be connected to preceding hydrofoil (9), be hinged with preceding wing (2) in the front end both sides of described body (1).
3. individual three-purpose vehicle according to claim 2 is characterized in that, the two ends of described preceding hydrofoil (9) are fixed on the medial surface of two described lamellar bodies (13).
4. individual three-purpose vehicle according to claim 2 is characterized in that, is provided with switching mechanism in described lamellar body (13) inside, and the two ends of described preceding hydrofoil (9) join with described switching mechanism respectively.
5. individual three-purpose vehicle according to claim 1 is characterized in that, described lamellar body (13) is hinged on the bottom surface of described body (1), is provided with the hydraulic control that the described lamellar body of control turns up in described body (1).
6. according to claim 1,2,3,4 or 5 described individual three-purpose vehicles, it is characterized in that described preceding ducted fan (4) is fixed on the bottom of described body (1) or the bottom of hinged described body (1).
7. individual three-purpose vehicle according to claim 6 is characterized in that, the duct rear port of described preceding ducted fan (4) and/or described back ducted fan (22) is the inclined-plane port that the top extends back.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010105027055A CN101941365B (en) | 2010-10-11 | 2010-10-11 | Personal triphibious transport tool |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010105027055A CN101941365B (en) | 2010-10-11 | 2010-10-11 | Personal triphibious transport tool |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN101941365A true CN101941365A (en) | 2011-01-12 |
| CN101941365B CN101941365B (en) | 2011-11-16 |
Family
ID=43433642
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010105027055A Expired - Fee Related CN101941365B (en) | 2010-10-11 | 2010-10-11 | Personal triphibious transport tool |
Country Status (1)
| Country | Link |
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| CN (1) | CN101941365B (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102795070A (en) * | 2012-09-03 | 2012-11-28 | 张廷林 | Aeroamphibious triphibian aircraft with machine body capable of fully balancing stress |
| CN102910080A (en) * | 2011-08-02 | 2013-02-06 | 张家成 | Solar vehicle |
| CN103057700A (en) * | 2011-10-19 | 2013-04-24 | 孙龙骧 | Impeller wing aircraft |
| CN103419924A (en) * | 2013-08-28 | 2013-12-04 | 哈尔滨市奇正水稻种植专业合作社 | All-round sea, land and air wing type airflow orientation aircraft |
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| DE2845260A1 (en) * | 1978-10-18 | 1980-05-14 | Sach Lothar | Air cushion vehicle with retracting wheels - has fore and aft lifting fans and centrally mounted engines |
| RU2016781C1 (en) * | 1991-03-15 | 1994-07-30 | Захаров Николай Владимирович | Vehicle transformable into flying vehicle |
| US5417386A (en) * | 1993-01-25 | 1995-05-23 | Wernicke; Kenneth G. | Flying and road vehicle |
| CN2695270Y (en) * | 2004-05-11 | 2005-04-27 | 陈星� | Triphibian aircraft with vehicle, ship and plane function |
| CN1887609A (en) * | 2006-07-18 | 2007-01-03 | 吴冠豪 | Carplane |
| CN201525255U (en) * | 2009-11-10 | 2010-07-14 | 周彬彬 | Gyroplane landing ship capable of driving on land and water |
| CN201824818U (en) * | 2010-10-11 | 2011-05-11 | 杨朝习 | Personal triphibian vehicle |
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2010
- 2010-10-11 CN CN2010105027055A patent/CN101941365B/en not_active Expired - Fee Related
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2845260A1 (en) * | 1978-10-18 | 1980-05-14 | Sach Lothar | Air cushion vehicle with retracting wheels - has fore and aft lifting fans and centrally mounted engines |
| RU2016781C1 (en) * | 1991-03-15 | 1994-07-30 | Захаров Николай Владимирович | Vehicle transformable into flying vehicle |
| US5417386A (en) * | 1993-01-25 | 1995-05-23 | Wernicke; Kenneth G. | Flying and road vehicle |
| CN2695270Y (en) * | 2004-05-11 | 2005-04-27 | 陈星� | Triphibian aircraft with vehicle, ship and plane function |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102910080A (en) * | 2011-08-02 | 2013-02-06 | 张家成 | Solar vehicle |
| CN103057700A (en) * | 2011-10-19 | 2013-04-24 | 孙龙骧 | Impeller wing aircraft |
| CN102795070A (en) * | 2012-09-03 | 2012-11-28 | 张廷林 | Aeroamphibious triphibian aircraft with machine body capable of fully balancing stress |
| CN103419924A (en) * | 2013-08-28 | 2013-12-04 | 哈尔滨市奇正水稻种植专业合作社 | All-round sea, land and air wing type airflow orientation aircraft |
| CN103419924B (en) * | 2013-08-28 | 2016-02-24 | 哈尔滨市奇正水稻种植专业合作社 | The all-round wing-type air-flow directional aircraft of aeroamphibious |
Also Published As
| Publication number | Publication date |
|---|---|
| CN101941365B (en) | 2011-11-16 |
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