CN205554582U - Land, water and air three way rotor airborne vehicle - Google Patents
Land, water and air three way rotor airborne vehicle Download PDFInfo
- Publication number
- CN205554582U CN205554582U CN201620162601.7U CN201620162601U CN205554582U CN 205554582 U CN205554582 U CN 205554582U CN 201620162601 U CN201620162601 U CN 201620162601U CN 205554582 U CN205554582 U CN 205554582U
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- floating drum
- land
- air
- airborne vehicle
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Abstract
The utility model relates to a land, water and air three way rotor airborne vehicle, which comprises a bod, engine room cover, the flotation pontoon, the wheel, the bracing piece, screw and motor, engine room cover sets up on the organism, and form the cabin between engine room cover and the organism, the flotation pontoon sets up the both sides at the organism, the wheel sets up in the flotation pontoon below, and it is collapsible to the flotation pontoon in, the screw is equipped with 4 groups altogether, set up both ends around the both sides of organism through four spinal branch vaulting poles respectively, the rotation of four group's screws of motor individual drive, the bracing piece is collapsible pole, the screw is in different location State when the bracing piece is folding. Compared with the prior art, the utility model discloses the airborne vehicle has realized that the airborne vehicle has the application in the three kinds of fields in land, water and air, has the multifunctionality, and the utility model discloses the airborne vehicle structure sets up simply, easily control, and it has had great reduction in other airborne vehicles to compare on the cost to operating stability is high with the security.
Description
Technical field
This utility model relates to a kind of airborne vehicle, especially relates to a kind of land, water and air three and uses rotary wing aircraft.
Background technology
Present airborne vehicle mainly has helicopter, fixed wing airplane, gyroplane etc., and these airborne vehicles all realize work in a certain specific field, the most in the air, in water, it is not possible to meet the state that can work under the conditions of three kinds, land, water and air.
Chinese patent CN 102774493 A discloses a kind of variable wing type land, sea and air triphibian aircraft, including fuselage, wing, electromotor, propeller, wheel, fuselage both sides dress Variable Geometry Wing, Variable Geometry Wing is made up of the fin more than two panels arranged in parallel superposition that interlocks, the front end of fin is fixed, fin rear end is movable end, fin is the most all connected with drive control lever by connecting rod, movable flap is set on Variable Geometry Wing outer end plate, engine output shaft is connected with propeller, propeller is installed on inside fan duct, fuselage afterbody is provided with two symmetrical tail booms, equipped with vertical tail and tailplane on tail boom.The variable wing type land, sea and air triphibian aircraft of this utility model has wheel, hull, can on ground, the water surface parks and landing；Launching or close to control flight by controlling Variable Geometry Wing, security performance is high, and propeller is contained in duct, makes the air-flow flowing through propeller more straight, improves the pneumatic efficiency of propeller and overall thrust, and is not easy injure ground staff or get to ground object.But the aircraft of this patent disclosure on the one hand on the water surface to slide effect poor, stability and unbalance stress, accident easily occurs, on the other hand this patent uses variable wing type structure, and structure arranges complexity, it is easy to damage, and maintenance cost is high.
Utility model content
Defect that the purpose of this utility model is contemplated to overcome above-mentioned prior art to exist and provide a kind of there is multiple duty, rotary wing aircraft is used in powerful land, water and air three.
The purpose of this utility model can be achieved through the following technical solutions:
A kind of land, water and air three rotary wing aircraft, including body, cabin cover, floating drum, wheel, support bar, propeller and motor, described cabin cover arranges on body, and between described cabin cover and body, form cabin, described floating drum is arranged on the both sides of body, described wheel is arranged on below floating drum, and be collapsible in floating drum, described propeller is provided with 4 groups altogether, the rear and front end, both sides of body it is arranged on respectively by four support bars, described motor is operated alone the rotation of four groups of propellers, described support bar is collapsible rod, described propeller is in different location status when support bar folds.
Controller, steering wheel and electron speed regulator it is provided with in described cabin, the folded state of described support bar is controlled by the controller, described steering wheel is connected with wheel by steering gear, when land pattern, the use steering gear that turns to of wheel is realized controlling by engine room inside steering wheel, described electron speed regulator is connected with motor, and described airborne vehicle, when offline mode, is controlled the rotating speed of motor by electron speed regulator and then realizes turning of airborne vehicle.
Described support bar is protruding by the body above floating drum.
Often group propeller includes the propeller blade of two coaxial reverse rotations altogether, two propeller blades are driven by two single motors respectively, each motor can be by independent cell powers, other power supply modes can also be used to provide power supply, described motor is arranged on the end of support bar, and described propeller blade is connected with the outfan of motor.
The bottom of described body is ships and light boats formula fuselages, it is achieved that in the function of water surface work.
Described floating drum is divided into front floating drum and rear floating drum, described front floating drum is positioned at the front end of the body left and right sides, described rear floating drum is positioned at the rear end of the body left and right sides, front floating drum and rear floating drum are used for providing airborne vehicle lift in water and balancing the power produced that tilts, described wheel has four groups, it is correspondingly arranged at front floating drum or the lower section of rear floating drum respectively, is scalable in front floating drum or rear floating drum.
Described airborne vehicle is when offline mode: described support bar is elongation state, do not fold or turn up, the center of rotation of four groups of propellers is on same circle, and the center of rotation of four groups of propellers is equal relative to the distance of aircraft centre of gravity, the center of rotation of four groups of propellers is vertical direction, vertical with airborne vehicle direction of advance；Described wheel stretches in floating drum, reduces the resistance of air.
Described airborne vehicle is when land pattern: four groups of propellers of airborne vehicle all will change state, and the support bar being connected with two groups of propellers of front end, body both sides folds, and the two groups of propellers being positioned at front end, body both sides are in collapsed state, and do not rotate；The support bar bending being connected with two groups of propellers of rear end, body both sides, the two groups of propellers being positioned at rear end, body both sides are in the state of turning up, the axis of the two groups of propellers being positioned at rear end, body both sides is parallel with the direction that airborne vehicle advances, being horizontal direction, airborne vehicle onward impulse is rotated by the two groups of propellers being positioned at rear end, body both sides and realizes driving；Four wheels stretch out from floating drum, and airborne vehicle lands with four wheels, and the use steering gear that turns to of wheel is realized controlling by engine room inside steering wheel.
Described airborne vehicle is when water surface pattern: described wheel stretches in floating drum, reduces the resistance of air；The support bar being connected with two groups of propellers of front end, body both sides folds, and the two groups of propellers being positioned at front end, body both sides are in collapsed state, and do not rotate；The support bar bending being connected with two groups of propellers of rear end, body both sides, the two groups of propellers being positioned at rear end, body both sides are in the state of turning up, and the axis of the two groups of propellers being positioned at rear end, body both sides is parallel with the direction that airborne vehicle advances, and is horizontal direction；Airborne vehicle onward impulse is rotated by the two groups of propellers being positioned at rear end, body both sides and realizes driving, the differential speed rotation of the two groups of propellers being positioned at rear end, body both sides realize the turning function at the water surface.
Manned seat it is provided with, it is achieved manned function in described cabin.
Compared with prior art, this utility model is by transforming four rotary wing aircraft, it is achieved that manned function；By to body and the transformation of propeller connecting rod (i.e. support bar), it is achieved that the diverse location state of propeller, and then achieve the function of land work；By using ships and light boats formula fuselage, it is achieved that in the function of water surface work；Relative to other airborne vehicle, this airborne vehicle achieves the multifunctionality of airborne vehicle.And this utility model airframe arranges simply, it is easy to control, on cost, there is bigger reduction compared to other airborne vehicles, and operation stability is high with safety.
Accompanying drawing explanation
Fig. 1 is the perspective view of this utility model airborne vehicle；
Fig. 2 is the main TV structure schematic diagram of this utility model airborne vehicle；
Fig. 3 is the side-looking structural representation of this utility model airborne vehicle；
Fig. 4 is the plan structure schematic diagram of this utility model airborne vehicle；
The perspective view of airborne vehicle when Fig. 5 is propeller folding；
The main TV structure schematic diagram of airborne vehicle when Fig. 6 is propeller folding；
The side-looking structural representation of airborne vehicle when Fig. 7 is propeller folding；
The plan structure schematic diagram of airborne vehicle when Fig. 8 is propeller folding.
Label in figure: 1-cabin cover；2-propeller；Floating drum before 3-；Floating drum after 4-；5-wheel；6-body；7-support bar；8-motor.
Detailed description of the invention
With specific embodiment, this utility model is described in detail below in conjunction with the accompanying drawings.
Embodiment
As shown in Fig. 1～8, a kind of land, water and air three rotary wing aircraft, including body 6, cabin cover 1, floating drum, wheel 5, support bar 7, propeller 2 and motor 8, cabin cover 1 arranges on body 6, and between cabin cover 1 and body 6, form cabin, floating drum is arranged on the both sides of body 6, wheel 5 is arranged on below floating drum, and be collapsible in floating drum, support bar 7 is protruding by the body 6 above floating drum, propeller 2 is provided with 4 groups altogether, the rear and front end, both sides of body 6 it is arranged on respectively by four support bars 7, motor 8 is operated alone the rotation of four groups of propellers 2, support bar 7 is collapsible rod, propeller 2 is in different location status when support bar 7 folds.
Floating drum is divided into front floating drum 3 and rear floating drum 4, front floating drum 3 is positioned at the front end of body 6 left and right sides, rear floating drum 4 is positioned at the rear end of body 6 left and right sides, front floating drum 3 is used for providing airborne vehicle lift in water and balancing the power produced that tilts with rear floating drum 4, wheel 5 has four groups, it is correspondingly arranged at front floating drum 3 or the lower section of rear floating drum 4 respectively, is scalable in front floating drum 3 or rear floating drum 4.Often group propeller 2 includes the propeller blade of two coaxial reverse rotations altogether, two propeller blades are driven by two single motors 8 respectively, each motor can be by independent cell powers, other power supply modes can also be used to provide power supply, motor 8 is arranged on the end of support bar 7, and propeller blade is connected with the outfan of motor 8.The bottom of body 6 is ships and light boats formula fuselages, it is achieved that in the function of water surface work.Controller, steering wheel and electron speed regulator it is provided with in cabin, the folded state of support bar 7 is controlled by the controller, steering wheel is connected with wheel 5 by steering gear, when land pattern, the use steering gear that turns to of wheel 5 is realized controlling by engine room inside steering wheel, electron speed regulator is connected with motor 8, and airborne vehicle, when offline mode, is controlled the rotating speed of motor 8 by electron speed regulator and then realizes turning of airborne vehicle.Manned seat it is provided with, it is achieved manned function in cabin.
Airborne vehicle is when offline mode: support bar 7 is elongation state, do not fold or turn up, the center of rotation of four groups of propellers 2 is on same circle, and the center of rotation of four groups of propellers 2 is equal relative to the distance of aircraft centre of gravity, the center of rotation of four groups of propellers 2 is vertical direction, vertical with airborne vehicle direction of advance；Wheel 5 stretches in floating drum, reduces the resistance of air.
Airborne vehicle four groups of propellers 2 of reference Fig. 5-Fig. 8: airborne vehicle when land pattern all will change state, the support bar 7 being connected with two groups of propellers 2 of front end, body 6 both sides folds, the two groups of propellers 2 being positioned at front end, body 6 both sides are in collapsed state, and do not rotate；The support bar 7 being connected with two groups of propellers 2 of rear end, body 6 both sides bends, the two groups of propellers 2 being positioned at rear end, body 6 both sides are in the state of turning up, the axis of the two groups of propellers 2 being positioned at rear end, body 6 both sides is parallel with the direction that airborne vehicle advances, being horizontal direction, airborne vehicle onward impulse is rotated realization by the two groups of propellers 2 being positioned at rear end, body 6 both sides and drives；Four wheels 5 stretch out from floating drum, and airborne vehicle lands with four wheels 5, and the use steering gear that turns to of wheel 5 is realized controlling by engine room inside steering wheel.
Airborne vehicle is when water surface pattern: wheel 5 stretches in floating drum, reduces the resistance of air；The support bar 7 being connected with two groups of propellers 2 of front end, body 6 both sides folds, and the two groups of propellers 2 being positioned at front end, body 6 both sides are in collapsed state, and do not rotate；The support bar 7 being connected with two groups of propellers 2 of rear end, body 6 both sides bends, the two groups of propellers 2 being positioned at rear end, body 6 both sides are in the state of turning up, the axis of the two groups of propellers 2 being positioned at rear end, body 6 both sides is parallel with the direction that airborne vehicle advances, and is horizontal direction；Airborne vehicle onward impulse is rotated realization by the two groups of propellers 2 being positioned at rear end, body 6 both sides and drives, the differential speed rotation of the two groups of propellers 2 being positioned at rear end, body 6 both sides realize the turning function at the water surface.
The above-mentioned description to embodiment is to be understood that for ease of those skilled in the art and use utility model.These embodiments obviously easily can be made various amendment by person skilled in the art, and General Principle described herein is applied in other embodiments without through performing creative labour.Therefore, this utility model is not limited to above-described embodiment, and those skilled in the art should be within protection domain of the present utility model according to announcement of the present utility model, the improvement made without departing from this utility model category and amendment.
Claims (7)
- null1. rotary wing aircraft is used in land, water and air three，It is characterized in that，Including body (6)、Cabin cover (1)、Floating drum、Wheel (5)、Support bar (7)、Propeller (2) and motor (8)，Described cabin cover (1) is arranged on body (6)，And between described cabin cover (1) and body (6), form cabin，Described floating drum is arranged on the both sides of body (6)，Described wheel (5) is arranged on below floating drum，And be collapsible in floating drum，Described propeller (2) is provided with 4 groups altogether，The rear and front end, both sides of body (6) it is arranged on respectively by four support bars (7)，Described motor (8) is operated alone the rotation of four groups of propellers (2)，Described support bar (7) is collapsible rod，Described propeller (2) is in different location status when support bar (7) folds.
- A kind of land, water and air three the most according to claim 1 rotary wing aircraft, it is characterized in that, it is provided with controller in described cabin, steering wheel and electron speed regulator, the folded state of described support bar (7) is controlled by the controller, described steering wheel is connected with wheel (5) by steering gear, when land pattern, the use steering gear that turns to of wheel (5) is realized controlling by engine room inside steering wheel, described electron speed regulator is connected with motor (8), described airborne vehicle is when offline mode, controlled the rotating speed of motor (8) by electron speed regulator and then realize turning of airborne vehicle.
- A kind of land, water and air three the most according to claim 1 rotary wing aircraft, it is characterised in that described support bar (7) is protruding by the body (6) above floating drum.
- A kind of land, water and air three the most according to claim 1 rotary wing aircraft, it is characterized in that, often organize propeller (2) and include the propeller blade of two coaxial reverse rotations altogether, two propeller blades are driven by two single motors (8) respectively, described motor (8) is arranged on the end of support bar (7), and described propeller blade is connected with the outfan of motor (8).
- A kind of land, water and air three the most according to claim 1 rotary wing aircraft, it is characterised in that the bottom of described body (6) is ships and light boats formula fuselages.
- A kind of land, water and air three the most according to claim 1 rotary wing aircraft, it is characterized in that, described floating drum is divided into front floating drum (3) and rear floating drum (4), described front floating drum (3) is positioned at the front end of body (6) left and right sides, described rear floating drum (4) is positioned at the rear end of body (6) left and right sides, described wheel (5) has four groups, it is correspondingly arranged at front floating drum (3) or the lower section of rear floating drum (4) respectively, is scalable in front floating drum (3) or rear floating drum (4).
- A kind of land, water and air three the most according to claim 1 rotary wing aircraft, it is characterised in that be provided with manned seat in described cabin.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620162601.7U CN205554582U (en) | 2016-03-03 | 2016-03-03 | Land, water and air three way rotor airborne vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620162601.7U CN205554582U (en) | 2016-03-03 | 2016-03-03 | Land, water and air three way rotor airborne vehicle |
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| Publication Number | Publication Date |
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| CN205554582U true CN205554582U (en) | 2016-09-07 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201620162601.7U Expired - Fee Related CN205554582U (en) | 2016-03-03 | 2016-03-03 | Land, water and air three way rotor airborne vehicle |
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN107010197A (en) * | 2016-11-22 | 2017-08-04 | 中国人民解放军空军工程大学 | A kind of stationary spiral oar specific direction generation and fixed mechanism |
| CN107128443A (en) * | 2017-05-09 | 2017-09-05 | 南京航空航天大学 | It is a kind of can VTOL the amphibious airship of air-sea |
| CN107150801A (en) * | 2016-03-03 | 2017-09-12 | 上海奥科赛飞机有限公司 | Use rotary wing aircraft in a kind of land, water and air three |
| CN107650603A (en) * | 2017-10-09 | 2018-02-02 | 南京航空航天大学 | A kind of multi-rotor unmanned aerial vehicle of dwelling more |
| CN107719652A (en) * | 2017-10-09 | 2018-02-23 | 黄文佳 | A kind of express delivery box |
| FR3056555A1 (en) * | 2016-09-29 | 2018-03-30 | Safran Helicopter Engines | HYBRID PROPULSIVE SYSTEM FOR MULTIROTOR ROTARY FLYWELL AIRCRAFT COMPRISING IMPROVED DC / AC CONVERSION MEANS |
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2016
- 2016-03-03 CN CN201620162601.7U patent/CN205554582U/en not_active Expired - Fee Related
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107150801A (en) * | 2016-03-03 | 2017-09-12 | 上海奥科赛飞机有限公司 | Use rotary wing aircraft in a kind of land, water and air three |
| FR3056555A1 (en) * | 2016-09-29 | 2018-03-30 | Safran Helicopter Engines | HYBRID PROPULSIVE SYSTEM FOR MULTIROTOR ROTARY FLYWELL AIRCRAFT COMPRISING IMPROVED DC / AC CONVERSION MEANS |
| WO2018060591A1 (en) * | 2016-09-29 | 2018-04-05 | Safran Helicopter Engines | Hybrid propulsion system for multi-rotor rotary-wing aircraft, comprising improved dc/ac conversion means |
| RU2745465C2 (en) * | 2016-09-29 | 2021-03-25 | Сафран Хеликоптер Энджинз | Hybrid power plant for multipropeller rotary-wing aircraft containing improved dc/ac converter |
| US11608184B2 (en) | 2016-09-29 | 2023-03-21 | Safran Helicopter Engines | Hybrid propulsion system for multi-rotor rotary wing aircraft, comprising improved DC/AC conversion means |
| CN107010197A (en) * | 2016-11-22 | 2017-08-04 | 中国人民解放军空军工程大学 | A kind of stationary spiral oar specific direction generation and fixed mechanism |
| CN107010197B (en) * | 2016-11-22 | 2023-09-12 | 中国人民解放军空军工程大学 | Static propeller specific direction generation and fixing mechanism |
| CN107128443A (en) * | 2017-05-09 | 2017-09-05 | 南京航空航天大学 | It is a kind of can VTOL the amphibious airship of air-sea |
| CN107650603A (en) * | 2017-10-09 | 2018-02-02 | 南京航空航天大学 | A kind of multi-rotor unmanned aerial vehicle of dwelling more |
| CN107719652A (en) * | 2017-10-09 | 2018-02-23 | 黄文佳 | A kind of express delivery box |
| CN107719652B (en) * | 2017-10-09 | 2018-07-24 | 黄文佳 | A kind of express delivery box |
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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: 20160907 Termination date: 20200303 |