CN110588262A - Novel three-rotor amphibious manned aircraft - Google Patents
Novel three-rotor amphibious manned aircraft Download PDFInfo
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- CN110588262A CN110588262A CN201910855238.5A CN201910855238A CN110588262A CN 110588262 A CN110588262 A CN 110588262A CN 201910855238 A CN201910855238 A CN 201910855238A CN 110588262 A CN110588262 A CN 110588262A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
- B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
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- Aviation & Aerospace Engineering (AREA)
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Abstract
The invention discloses a novel three-rotor amphibious manned vehicle, which relates to the field of manned vehicles and is an amphibious vehicle capable of controlling deformation of a wheel wing and taking off and landing vertically. The invention has two control modes, namely a control rod and a holding handle, the control mode similar to the control mode of the control rod of the unmanned aerial vehicle is adopted in the flight mode, and the originally vertical holding handle is changed into a transverse holding handle by rotating 90 degrees outwards along a steering wheel in the riding mode. The purpose of form conversion between flying and riding can be achieved through combined work of a hydraulic pump, a motor, a bevel gear and the like.
Description
Technical Field
The invention relates to the field of manned aircrafts, in particular to a novel three-rotor amphibious manned aircraft.
Background
In the era of rapid technological development nowadays, most people can buy their own vehicles, the quality of living standard is continuously improved, the vehicles are gradually increased along with the increase of population, but the road resources are limited, and all the cities in the world are in traffic jam situations every day. It is believed that everyone has dredged to drive a car to fly through a congested sea of cars.
Currently, flying motorcycles have been developed in China, but various technical reasons cause the high price of products, the number of rotor wings is also four or more, the size is large, the power consumption is high, many technologies are not mature, most technologies are only used in military, the operation mode is complicated, some of the technologies need to be driven by holding a pilot driving license, and various factors hinder the production, popularization and popularization of the products together, so that people in ordinary people want to drive own vehicles to fly to the world.
Disclosure of Invention
The invention aims to solve the technical problem of providing a novel three-rotor amphibious manned vehicle, which can achieve the purpose of form conversion between flying and riding through the combined work of a hydraulic pump, a motor, a bevel gear and the like.
In order to achieve the above purpose, the present invention provides the following technical solutions:
the novel three-rotor amphibious manned vehicle is mainly divided into a driving part, a steering control part and a deformation control part; the driving part comprises three speed reducing motors and three high-speed motors, the high-speed motors respectively control the rotation of three rotors through the transmission of a gear pair and a transmission shaft, the speed reducing motors control the rotation angle of the whole rotating arm, a rechargeable storage battery is arranged at the bottom of the machine body and provides power energy for the motors and a control system, the deformation control part is mainly controlled by a hydraulic system and the speed reducing motors, and the left rotating arm, the right rotating arm and the rear rotating arm are provided with three rotating arms in total, and each rotating arm comprises a high-speed motor, a motor base, a motor box body, a large gear, a small gear, a transmission shaft, a supporting shaft and a protective shaft sleeve, a rotor upper cover, a rotor; two speed reducing motors of the left and right rotating arms are arranged on the slidable base and are in fit connection with the rotating arms through conical gears, when deformation is needed, the hydraulic pump works, the hydraulic rod pushes the speed reducing motors to move forwards, the conical gears connected with the rotating arms are meshed with the conical gears connected with the speed reducing motors, the rotation angles of the whole rotating arms are controlled by the working of the motors, and the hydraulic rod pulls the motors back after the deformation of the wheel wings is finished; the rear rotor wheel only controls the tilting angle and deformation by a speed reducing motor, the steering control part comprises steering control in a flight mode and steering control in a riding mode, the steering in the flight mode is controlled by the rotating speed of the left rotor and the rotating speed of the right rotor and the tilting angle of the rear rotor, the left rotor and the rear rotor rotate clockwise, the right rotor rotates anticlockwise, a gyroscope is arranged below the seat, and the gyroscope and a servo system control the balance of the body; the steering under the riding mode is connected with a steering cam disc by a steering wheel universal shaft, the steering cam disc is connected with a left connecting rod and a right connecting rod, the connecting rods are connected with a shaft behind a rotating arm, the steering wheel rotates left and right by passing through an arc-shaped triangular slidable support, the connecting rods push and pull left and right, the rotating arm and the arc-shaped triangular slidable support swing left and right under the action of the connecting rods so as to achieve direction control, and other structures are all arranged inside a machine body shell except the steering wheel, wheel wings and part of a protective shaft sleeve exposed out of the machine body shell; the front end of the machine body is provided with two headlamps, a ventilation grating is arranged between the headlamps, the grating is designed to drain rainwater outwards, and the rainwater cannot enter the interior of the machine body; the front end of the machine head is provided with an openable buckle cover, and a charging interface of a storage battery is arranged in the buckle cover. Two rear lamps and two rear fog lamps are arranged at the rear part of the machine body, and the steering indicator lamps are arranged on the upper cover and the lower cover of the rotor wing; the shock absorption rubber cushion is arranged at the joint of the protective shaft sleeve and the shell of the machine body, so that the shock generated by the contact friction between the wheel wings and the ground can be reduced in a riding mode; the steering wheel has two kinds of control modes, and control rod (flight), hold formula handle (ride), the control rod is controlled by stirring about the thumb to the sensor response is controlled the direction, and the signal of telecommunication that obtains sends the controller, and the rotation speed size of controller control motor and the angle of verting of back rotor hold the formula handle the same with the control mode of electric motor car, and the wrench movement right-hand grip can accelerate.
Preferably, the fuselage shell is plastic to reduce fuselage weight.
Preferably, the swinging boom comprises high-speed motor, motor base, motor box, gear wheel, pinion, transmission shaft, back shaft, protection axle sleeve, rotor upper cover, rotor lower cover, rotor wheel hub, conical gear, gear shaft, toothed disc, electromagnetic braking ware, and high-speed motor, motor base, gear wheel, pinion are inside the motor box, and the box divide into two parts from the middle, and the centre is fastened with bolt and nut and gasket.
Preferably, transmission shaft, back shaft pass the motor box and link to each other with motor, motor base, and transmission shaft, back shaft are in the protection axle sleeve, and the screw is connected with the motor box for the protection axle sleeve, and the other end is connected with rotor upper cover, rotor lower cover, and gear shaft, conical gear, toothed disc and electromagnetic braking ware are in rotor upper cover, rotor lower cover and rotor wheel rim.
Preferably, the toothed disc and rotor wheel rim are connected and fastened in inside, and the swinging boom rear reaches for the motor box rear bolt fastening connecting piece to be connected with the connecting rod, the connecting piece connects the integral key shaft, the integral key shaft passes arc triangle sliding support, arc triangle sliding support installs in the arc track of track base.
Preferably, the left and right speed reducing motors are installed on a slidable motor base, the slidable motor base is installed on the track base, the rear portion of the slidable motor base is connected with the hydraulic rod, when deformation is not needed, the hydraulic rod pulls the motors back, and when deformation is needed, the hydraulic rod pushes the motors to move forwards, so that the conical gears on the speed reducing motors are meshed with the conical gears penetrating through the spline shaft on the arc-shaped triangular sliding support.
Preferably, hydraulic system is by hydraulic pressure case, hydraulic pressure main pump and two hydraulic transmission pumps, with the hydraulic hose connection between the two, the hydraulic pressure main pump is connected with the controller, the work of controller control main pump, control two transmission pump work about by main pump control hydraulic pressure size, back rotor wheel is only controlled the angle and the deformation of verting of rotor wheel by a gear motor, but rechargeable battery is in the battery box, the battery box is detained by the metal buckle closure, the buckle closure is opened the hot hole of fan, battery box the place ahead is for charging the interface, the rear has a plurality of output interface, provide the power energy for motor and control system.
Preferably, the front end of the steering cam disc is provided with a round-corner rectangular steel groove, a left connecting rod and a right connecting rod are connected to the steel groove, the cam disc drives the steel groove and the connecting rods to move left and right when rotating, a steering shaft of the steering wheel is vertically transmitted with a universal shaft connected with the cam disc, the transmission is engaged by two conical gears, the two conical gears are arranged in an L-shaped gear box, and a bearing is arranged at the opening of the gear box.
Preferably, the steering wheel has control rod and holds formula handle two kinds of manipulation modes, and under the flight mode, the inside locking mechanism of steering wheel will hold formula handle locking, and the handle all can not rotate together with the steering wheel, leans on the control rod to control the aircraft flight, and under the mode of riding, locking mechanism opens, and the vertical formula handle of holding originally is rotatory 90 to fuselage the place ahead and becomes horizontal, is the slide rheostat in the handle, connects master controller and hall motor, and the handle of wrench movement right can control the speed of a motor vehicle size.
Preferably, there are a plurality of buttons on steering wheel and the handle, control rotor wheel deformation respectively, light, loudspeaker, indicator light and signal lamp are installed in rotor upper and lower cover, and the wire of lamp passes protection axle sleeve in-connection and connects the inside master controller of fuselage.
The beneficial effect of adopting above technical scheme is: when this novel three-rotor amphibious manned vehicle used, if traffic jam suddenly on the way of going on a journey, pressed the button on the steering wheel this moment, fuselage below undercarriage roll-off starts the flight mode, and the rotor wheel begins to warp, and the steering wheel warp thereupon for control rod control direction, flies to continue to move ahead from ground. After the vehicle arrives at the destination, if no garage or parking lot exists, the vehicle can stay on a flat roof or any broad floor which can be driven to enter, so that the theft event is prevented better, the vehicle can stay indoors to avoid long-time exposure to the sun and rain, and the charging is also more convenient.
In the forbidden zone or the area unsuitable for flying, the driving way is longer, the power-saving riding mode can be adopted, and the safe driving is realized. The design of three rotor wheels not only saves space but also can better keep the balance of the airplane body. The light design is arranged at the front and the back of the machine body and at the two sides of the rotor wheel, so that the illumination and the steering indication in two modes are met. The two modes employ different modes of manipulation. Before or after the two modes are switched, the locking mechanism in the steering wheel locks the faucet, so that the two operation modes are prevented from conflicting with each other, the two operation modes can be better distinguished, and the operation is simpler and easier to operate. Long-time traffic jam causes the energy loss of automobile consumption to be serious, the emission of carbon dioxide is increased, the noisy and jammed environment is easy to make people in a distracted and disorderly manner, the time is long when the head and the tail are touched, and the noise is loud and the stand is also a frequent matter. The invention solves the problem of traffic jam in many cities, and the aircraft adopts the rechargeable storage battery to provide power supply, thereby reducing the emission of carbon dioxide and belonging to clean energy. The two modes can be used for driving on a limited road and flying in a wide sky, so that mutual friction among people is reduced, and the dream that people drive own vehicles to fly to the sky is realized.
Drawings
The following describes embodiments of the present invention in further detail with reference to the accompanying drawings.
FIG. 1 is a front view of the internal structure of the novel three-rotor amphibious manned vehicle;
FIG. 2 is a top view of the internal structure of the novel three-rotor amphibious manned vehicle;
FIG. 3 is a cross-sectional view A-A of FIG. 2 according to the present invention;
FIG. 4 is a rear view of the novel three-rotor amphibious manned vehicle of the present invention;
FIG. 5 is a front view and a partial cross-sectional view of the novel three-rotor amphibious manned vehicle of the present invention;
FIG. 6 is a left side view of the novel three-rotor amphibious manned vehicle of the present invention;
FIG. 7 is a top view of the novel three-rotor amphibious manned vehicle of the present invention;
FIG. 8 is a schematic view of the internal structure of the novel three-rotor amphibious manned vehicle;
FIG. 9 is a schematic structural view of the novel three-rotor amphibious manned vehicle of the present invention;
wherein, 1-wheel hub rim, 2-protective cover, 3-connecting pin, 4-steering wheel handle and button, 5-instrument panel, 6-control lever, 7-cross universal joint, 8-universal shaft 01, 9-gear pair, 10-bevel gear 01, 11-transmission hydraulic pump, 12-piston push rod, 13-steering wheel connecting support, 14-accumulator box, 15-accumulator, 16-metal buckle cover, 17-steering guide base, 18-bevel gear, 19-bevel gear 02, 20-brushless motor 01, 21-slidable base, 22-protective shaft sleeve, 23-M10 bolt, 24-nut, 25-gasket, 26-rotary connecting rod, 27-high pressure main pump, 28-hydraulic pipe joint, 29-hydraulic output hose, 30-power output interface, 31-hydraulic input hose, 32-M8 bolt, 33-snap ring, 34-movable connecting rod, 35-bending connecting rod, 36-driving box rear cover, 37-driving box front cover, 38-rotor spoke, 39-flat head connecting rod, 40-hydraulic water tank, 41-water tank screw cap, 42-steering wheel disc, 43-fillet rectangular groove, 44-M6 bolt, 45-arc support, 46-spline groove, 47-motor base, 48-brushless motor 02, 49-rigid coupling, 50-helical gear 01, 51-supporting round steel tube, 52-shaft sleeve, 53-electromagnetic brake, 54-M6 screw, 55-M12 screw, 56-helical gear 02, 57-M10 screw, 58-rolling bearing, 59-cardan shaft, 60-conical gear with shaft, 61-rolling bearing, 62-bearing cover and bearing washer, 63-gear shaft, 64-spur gear, 65-gear tray, 66-tray buckle cover, 67-fuselage shell, 68-rear fog lamp, 69-rear view lamp, 70-landing gear, 71-ventilation grille, 72-head lamp, 73-shock absorption rubber pad, 74-charging interface, 75-rear indicator lamp, 76-steering lamp, 77-seat, 78-rotating arm.
Detailed Description
The following describes in detail a preferred embodiment of the novel three-rotor amphibious manned vehicle according to the invention with reference to the accompanying drawings.
Fig. 1 to 9 show a specific embodiment of the novel three-rotor amphibious manned vehicle of the invention:
with reference to fig. 1 to 9, the novel three-rotor amphibious manned vehicle is mainly divided into a driving part, a steering control part and a deformation control part; the driving part comprises three speed reducing motors and three high-speed motors, the high-speed motors respectively control the rotation of three rotors through the transmission of a gear pair 9 and a transmission shaft, the speed reducing motors control the rotation angle of the whole rotating arm 78, a rechargeable storage battery 15 is arranged at the bottom of the machine body and provides power energy for the motors and a control system, the deformation control part is mainly controlled by a hydraulic system and the speed reducing motors, the left side, the right side and the back side are provided with three rotating arms 78, and each rotating arm 78 comprises a high-speed motor, a motor base, a motor box body, a large gear, a small gear, a transmission shaft, a supporting shaft and a protective shaft sleeve 22, a rotor upper cover, a rotor lower cover, a rotor hub, a conical; two speed reducing motors of the left and right rotating arms are arranged on the slidable base 21 and are in fit connection with the rotating arms 78 through the conical gears 19, when deformation is needed, the hydraulic pump works, the hydraulic rod pushes the speed reducing motors to move forwards in a translation mode, the conical gears 19 connected with the rotating arms 78 are meshed with the conical gears 18 connected with the speed reducing motors, the motors work to control the rotating angles of the whole rotating arms 78, and after wheel wings are deformed, the hydraulic rod pulls the motors back; the rear rotor wheel only controls the tilting angle and deformation by a speed reducing motor, the steering control part comprises steering control in a flight mode and steering control in a riding mode, the steering in the flight mode is controlled by the rotating speed of the left rotor and the rotating speed of the right rotor and the tilting angle of the rear rotor, the left rotor and the rear rotor rotate clockwise, the right rotor rotates anticlockwise, a gyroscope is arranged below the seat 77, and the gyroscope and a servo system control the balance of the body; the steering under the riding mode leans on the steering wheel cardan shaft 59 to connect with steering cam disc, the steering cam disc connects with left and right tie rod, the tie rod couples to axle behind swivel arm 78, pass the sliding support of the arc triangle, the steering wheel rotates left and right, the tie rod is pushed and pulled left and right, swivel arm 78 and sliding support of the arc triangle swing left and right under the effort of the tie rod, in order to reach the directional control, except steering wheel, wheel wing and some protective shaft sleeves are exposed outside the outer casing 67 of fuselage, other structures are inside the outer casing 67 of fuselage; two headlamps 72 are arranged at the front end of the machine body, a ventilation grille 71 is arranged between the headlamps 72, the grille is designed to drain rainwater outwards, and rainwater cannot enter the interior of the machine body; the front end of the machine head is provided with an openable buckle cover, and a charging interface 74 of the storage battery 15 is arranged in the buckle cover. Two rear-view lamps 69 and two rear fog lamps 68 are respectively arranged at the rear part of the fuselage, and the steering indicator lamps are arranged on the upper cover and the lower cover of the rotor wing; a shock absorption rubber pad 73 is arranged at the joint of the protective shaft sleeve and the shell of the machine body, so that the shock generated by the contact friction between the wheel wings and the ground can be reduced in a riding mode; the steering wheel has two kinds of control modes, and control rod 6 (flight), hold formula handle (ride), and control rod 6 is controlled by stirring from top to bottom about the thumb to the sensor response is controlled the direction, and the signal of telecommunication that obtains sends the controller, and the rotation speed size of controller control motor and the angle of verting of back rotor hold the formula handle the same with the control mode of electric motor car, and the wrench movement right-hand grip can accelerate.
The fuselage shell 67 is plastic to reduce fuselage weight.
The rotating arm 78 is composed of a high-speed motor, a motor base 47, a motor box body, a large gear, a small gear, a transmission shaft, a supporting shaft, a protective shaft sleeve 22, a rotor upper cover, a rotor lower cover, a rotor hub, a bevel gear 18, a gear shaft 63, a gear disc and an electromagnetic brake 53.
The high-speed motor, the motor base 47, the big gear and the small gear are arranged in the motor box body, the box body is divided into two parts from the middle, and the middle is fastened by the bolt 23, the nut 24 and the gasket 25.
The transmission shaft and the support shaft pass through the motor box body to be connected with the motor and the motor base 47, the transmission shaft and the support shaft are arranged in the protection shaft sleeve 22, the protection shaft sleeve 22 is connected with the motor box body through a screw 55, and the other end of the protection shaft sleeve is connected with the upper rotor cover and the lower rotor cover.
Gear shaft 63, bevel gear 19, gear plate and electromagnetic brake 53 are in the rotor upper cover, rotor lower cover and rotor rim.
The gear disc and the rotor rim are connected and fastened inside.
The connecting piece is fastened by the bolt 32 at the rear of the rotating arm 78 and the rear of the motor box body and is connected with the connecting rod, the connecting piece is connected with a spline shaft, the spline shaft penetrates through an arc-shaped triangular sliding support, and the arc-shaped triangular sliding support is installed in an arc-shaped track of the track base.
The left and right speed reducing motors are installed on the slidable motor bases, the slidable motor bases are installed on the rail base, the rear portions of the slidable motor bases are connected with the hydraulic rods, when deformation is not needed, the hydraulic rods pull the motors back, and when deformation is needed, the hydraulic rods push the motors to move forwards, so that the conical gears on the speed reducing motors are meshed with the conical gears penetrating through the spline shafts on the arc-shaped triangular sliding supports.
The hydraulic system is composed of a hydraulic tank, a hydraulic main pump and two hydraulic transmission pumps, the hydraulic main pump and the controller are connected through hydraulic hoses 29 and 31, the controller controls the main pump to work, and the main pump controls the hydraulic pressure to control the left transmission pump and the right transmission pump to work.
The rear rotor wheel only uses one speed reducing motor to control the tilting angle and deformation of the rotor wheel.
The rechargeable battery 15 is arranged in the battery box 14, the battery box 14 is buckled by the metal buckle cover 16, the metal buckle cover 16 is provided with a heat dissipation hole, the front part of the battery box 14 is provided with a charging interface 74, and the rear part of the battery box 14 is provided with a plurality of output interfaces for providing power energy for the motor and the control system.
The front end of the steering cam disc is provided with a round-angle rectangular steel groove, the left connecting rod and the right connecting rod are connected on the steel groove, and the cam disc drives the steel groove and the connecting rods to move left and right when rotating.
The steering shaft of the steering wheel and a universal shaft connected with the cam disc are in vertical transmission, the transmission is meshed by two conical gears 18/19, the two conical gears 18/19 are arranged in an L-shaped gearbox, and a bearing is arranged at the port of the gearbox respectively.
The steering wheel has two control modes of a control lever 6 and a holding type handle, under the flying mode, a locking mechanism in the steering wheel locks the holding type handle, the handle and the steering wheel cannot rotate, and the control lever 6 is used for controlling the flying of the aircraft. Under the mode of riding, locking mechanism opens, and the vertical formula handle of holding originally becomes horizontal to fuselage the place ahead rotation 90, is the slide rheostat in the handle, connects master controller and hall motor, twists the handle on the right and can control the speed of a motor vehicle size.
The steering wheel and the handle are provided with a plurality of buttons which respectively control the deformation of the rotor wheel, the light and the loudspeaker.
The steering lamp 76 and the signal lamp are arranged in the upper cover and the lower cover of the rotor wing, and the lead of the lamp passes through the inside of the protective shaft sleeve 2 to be connected to a main controller in the fuselage.
The above is only a preferred embodiment of the present invention, and it should be noted that, for those skilled in the art, many variations and modifications can be made without departing from the inventive concept of the present invention, which falls into the protection scope of the present invention.
Claims (10)
1. A novel three-rotor amphibious manned aircraft is characterized in that: the novel three-rotor amphibious manned vehicle is mainly divided into a driving part, a steering control part and a deformation control part; the driving part comprises three speed reducing motors and three high-speed motors, the high-speed motors respectively control the rotation of three rotors through the transmission of a gear pair and a transmission shaft, the speed reducing motors control the rotation angle of the whole rotating arm, a rechargeable storage battery is arranged at the bottom of the machine body and provides power energy for the motors and a control system, the deformation control part is mainly controlled by a hydraulic system and the speed reducing motors, and the left rotating arm, the right rotating arm and the rear rotating arm are provided with three rotating arms in total, and each rotating arm comprises a high-speed motor, a motor base, a motor box body, a large gear, a small gear, a transmission shaft, a supporting shaft and a protective shaft sleeve, a rotor upper cover, a rotor; two speed reducing motors of the left and right rotating arms are arranged on the slidable base and are in fit connection with the rotating arms through conical gears, when deformation is needed, the hydraulic pump works, the hydraulic rod pushes the speed reducing motors to move forwards, the conical gears connected with the rotating arms are meshed with the conical gears connected with the speed reducing motors, the rotation angles of the whole rotating arms are controlled by the working of the motors, and the hydraulic rod pulls the motors back after the deformation of the wheel wings is finished; the rear rotor wheel only controls the tilting angle and deformation by a speed reducing motor, the steering control part comprises steering control in a flight mode and steering control in a riding mode, the steering in the flight mode is controlled by the rotating speed of the left rotor and the rotating speed of the right rotor and the tilting angle of the rear rotor, the left rotor and the rear rotor rotate clockwise, the right rotor rotates anticlockwise, a gyroscope is arranged below the seat, and the gyroscope and a servo system control the balance of the body; the steering under the riding mode is connected with a steering cam disc by a steering wheel universal shaft, the steering cam disc is connected with a left connecting rod and a right connecting rod, the connecting rods are connected with a shaft behind a rotating arm, the steering wheel rotates left and right by passing through an arc-shaped triangular slidable support, the connecting rods push and pull left and right, the rotating arm and the arc-shaped triangular slidable support swing left and right under the action of the connecting rods so as to achieve direction control, and other structures are all arranged inside a machine body shell except the steering wheel, wheel wings and part of a protective shaft sleeve exposed out of the machine body shell; the front end of the machine body is provided with two headlamps, a ventilation grating is arranged between the headlamps, the grating is designed to drain rainwater outwards, and the rainwater cannot enter the interior of the machine body; the front end of the machine head is provided with an openable buckle cover, a charging interface of a storage battery is arranged in the buckle cover, two rear lamps and two rear fog lamps are respectively arranged at the rear part of the machine body, and the steering indicator lamps are arranged on the upper cover and the lower cover of the rotor wing; the shock absorption rubber cushion is arranged at the joint of the protective shaft sleeve and the shell of the machine body, so that the shock generated by the contact friction between the wheel wings and the ground can be reduced in a riding mode; the steering wheel has two kinds of control modes, and control rod (flight), hold formula handle (ride), the control rod is controlled by stirring about the thumb to the sensor response is controlled the direction, and the signal of telecommunication that obtains sends the controller, and the rotation speed size of controller control motor and the angle of verting of back rotor hold the formula handle the same with the control mode of electric motor car, and the wrench movement right-hand grip can accelerate.
2. A novel three-rotor amphibious manned vehicle according to claim 1, wherein: the fuselage shell is plastic to reduce fuselage weight.
3. A novel three-rotor amphibious manned vehicle according to claim 1, wherein: the swinging boom comprises high-speed motor, motor base, motor box, gear wheel, pinion, transmission shaft, back shaft, protection axle sleeve, rotor upper cover, rotor lower cover, rotor wheel hub, conical gear, gear shaft, toothed disc, electromagnetic braking ware, and high-speed motor, motor base, gear wheel, pinion are inside the motor box, and the box divide into two parts from the middle, and the centre is fastened with bolt and nut gasket.
4. A novel three-rotor amphibious manned vehicle according to claim 1, wherein: the transmission shaft and the support shaft penetrate through the motor box body to be connected with the motor and the motor base, the transmission shaft and the support shaft are arranged in the protection shaft sleeve, the protection shaft sleeve is connected with the motor box body through screws, the other end of the protection shaft sleeve is connected with the rotor upper cover and the rotor lower cover, and the gear shaft, the bevel gear, the gear disc and the electromagnetic brake are arranged in the rotor upper cover, the rotor lower cover and the rotor wheel rim.
5. A novel three-rotor amphibious manned vehicle according to claim 1, wherein: the gear plate and the rotor wheel rim are connected and fastened inside, the rear part of the rotating arm and the rear part of the motor box body are fastened by bolts and connected with the connecting rod, the connecting rod is connected with a spline shaft, the spline shaft penetrates through the arc-shaped triangular sliding support, and the arc-shaped triangular sliding support is installed in an arc-shaped track of the track base.
6. A novel three-rotor amphibious manned vehicle according to claim 1, wherein: the left and right speed reducing motors are installed on the slidable motor bases, the slidable motor bases are installed on the rail base, the rear portions of the slidable motor bases are connected with the hydraulic rods, when deformation is not needed, the hydraulic rods pull the motors back, and when deformation is needed, the hydraulic rods push the motors to move forwards, so that the conical gears on the speed reducing motors are meshed with the conical gears which penetrate through the spline shafts on the arc-shaped triangular sliding supports.
7. A novel three-rotor amphibious manned vehicle according to claim 1, wherein: the hydraulic system is by the hydraulic pressure case, hydraulic pressure main pump and two hydraulic transmission pumps, connect with the hydraulic pressure hose between, the hydraulic pressure main pump is connected with the controller, the work of controller control main pump, control two transmission pump work about the hydraulic pressure size is controlled by the main pump, back rotor wheel is only by a gear motor control rotor wheel the angle and the deformation of verting, chargeable battery is in the battery box, the battery box is detained by the metal buckle closure, the buckle closure is opened the hot hole of fan, battery box the place ahead is for the interface that charges, the rear has a plurality of output interface, provide the power energy for motor and control system.
8. A novel three-rotor amphibious manned vehicle according to claim 1, wherein: the front end of the steering cam disc is provided with a round-corner rectangular steel groove, a left connecting rod and a right connecting rod are connected to the steel groove, the steel groove and the connecting rods are driven to move left and right when the cam disc rotates, a steering shaft of a steering wheel and a universal shaft connected with the cam disc are mutually vertically transmitted, the transmission is engaged by two conical gears, the two conical gears are arranged in an L-shaped gear box, and a bearing is respectively arranged at the opening of the gear box.
9. A novel three-rotor amphibious manned vehicle according to claim 1, wherein: the steering wheel has control rod and holds formula handle two kinds of control modes, and under the flight mode, the inside locking mechanism of steering wheel will hold formula handle locking, and the handle all can not rotate together with the steering wheel, leans on the control rod to control the aircraft flight, and under the mode of riding, locking mechanism opens, and the vertical formula handle of holding originally is rotatory 90 to fuselage the place ahead and becomes horizontal, is the slide rheostat in the handle, connects master controller and hall motor, and the handle of wrench movement right can control the speed of a motor vehicle size.
10. A novel three-rotor amphibious manned vehicle according to claim 1, wherein: the steering wheel and the handle are provided with a plurality of buttons which respectively control the deformation of the rotor wheel, the light, the horn, the steering lamp and the signal lamp to be arranged in the upper cover and the lower cover of the rotor, and the lead of the lamp passes through the protective shaft sleeve to be connected to the main controller inside the body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910855238.5A CN110588262A (en) | 2019-09-06 | 2019-09-06 | Novel three-rotor amphibious manned aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910855238.5A CN110588262A (en) | 2019-09-06 | 2019-09-06 | Novel three-rotor amphibious manned aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110588262A true CN110588262A (en) | 2019-12-20 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910855238.5A Pending CN110588262A (en) | 2019-09-06 | 2019-09-06 | Novel three-rotor amphibious manned aircraft |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113879055A (en) * | 2021-11-17 | 2022-01-04 | 广东汇天航空航天科技有限公司 | Multifunctional aircraft and operation method and system thereof |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113879055A (en) * | 2021-11-17 | 2022-01-04 | 广东汇天航空航天科技有限公司 | Multifunctional aircraft and operation method and system thereof |
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Application publication date: 20191220 |