CN112026460A - Triphibian manned tool of land, water and air and parking system thereof - Google Patents

Abstract

The invention discloses a triphibian manned tool used in water, land and air, comprising: a cabin body providing a manned space; the movable wings are arranged on two sides of the cabin body, have elasticity and are of a segmented structure, and comprise wing root sections in rotary connection with the cabin body and wing tip sections in rotary connection with the wing root sections in the length direction of the wings; the outer covering shell is movably connected with the cabin body and moves along the periphery of the cabin body to drive the movable wing to change the extending postures, the extending postures comprise full extending, half extending and full accommodating postures, the wing root section and the wing tip section in the full extending postures are fully extended, the wing root section in the half extending postures is bent and/or folded around the cabin body, the wing tip section is fully extended, and the wing root section and the wing tip section in the full accommodating postures are bent and/or folded around the cabin body; the airplane wheels are arranged on the front side and the rear side of the cabin. Simple structure, convenient to use can realize the triphibian manned of land, water and air, do not need specific environment transition when switching the different driving state that corresponds different environment, and land driving occupation space is little, is convenient for drop into practical application.

Description

Triphibian manned tool of land, water and air and parking system thereof

Technical Field

The invention relates to the field of transportation, in particular to a triphibian manned tool used in water, land and air and a parking system thereof.

Background

Common vehicles can only drive under a single environmental condition and cannot drive under multiple environments; for example, automobiles generally can only run on land, but cannot run in air or underwater environments; similarly, ships and airplanes can only run in water and in the air respectively. Therefore, in the prior art, a multi-purpose manned tool is researched, wherein the multi-purpose manned tool comprises an amphibious manned tool and an air-road amphibious manned tool and the like, so that the effect of one machine with multiple purposes is achieved, but the multi-purpose manned tool in the prior art has more defects, for example, when the existing amphibious manned tool is switched to run in different environments, a shoal is often required to be arranged between land and the water surface for transition, and the running switching of the land and the water is limited by conditions; the existing air-ground amphibious manned tool needs to spread wider wings on the ground, occupies a large space, and therefore cannot be used in actual life, particularly in urban areas with more vehicles. The multi-purpose manned tool in the prior art is still limited in use environment, can only realize an amphibious function at most, and cannot realize a water, land and air triphibious function with stronger practicability. The triphibian vehicle for water, land and air can not only facilitate traveling and is suitable for traveling in various environments, but also overcome many defects of the existing amphibious vehicle based on the air traveling function of the triphibian vehicle for water, air and air, and can transit land traveling and underwater navigation without constructing a special road, so that a water network and a road network are connected, and the problem of road blockage of urban bridges and the like is solved. Therefore, a vehicle capable of triphibian between water and air is urgently needed in modern trips so as to improve the restriction brought by the existing vehicle. Therefore, the prior art also provides a design scheme of the triphibian vehicle, but the structure of the triphibian vehicle is not reasonable, the defects of the amphibious manned tool still exist, the amphibious manned tool is difficult to put into practical application, and an effective amphibious triphibian vehicle cannot be provided.

In addition, existing vehicles also have problems with parking the vehicle, in addition to problems with the vehicle. In the prior art, both an automobile and an amphibious manned tool need to occupy a larger area for parking, and the parking position and the parking space are limited, so that the problems of difficult parking, excessive occupation of public space and the like are easily caused, and the problems are more prominent in developed cities. However, it is difficult to provide effective solutions based on the existing vehicles, and a parking system based on a new vehicle is urgently needed to overcome the parking defects of the vehicles in modern life.

Disclosure of Invention

The invention aims to overcome at least one defect of the prior art, and provides a triphibian manned tool for water, land and air, which has the advantages of simple structure and convenient use, can realize triphibian manned for water, land and air, does not need specific environment transition when switching different driving states corresponding to different environments, occupies small land driving space and is convenient to put into practical application.

Another object of the present invention is to provide a parking system, which is capable of achieving vertical parking based on amphibious vehicle, reducing the occupied parking space of the vehicle, breaking through the limitation of limited space on the parking position, improving the parking convenience, and reducing the parking load of the urban vehicle.

The invention adopts the technical scheme that a triphibian manned tool for water, land and air comprises:

a cabin body providing a manned space; the cabin body is internally provided with a space for a user to take, which is beneficial to realizing manned driving; an operation platform for operating the driving of the triphibian manned tool in water, land and air is arranged in the cabin body, which is beneficial for a user to manually control the driving of the manned tool while riding, so that the manned tool has stronger operability; the manned space is convenient to take and is also beneficial to an independent user in the whole manned tool, so that the driving safety of the manned tool is improved;

the movable wings are arranged on two sides of the cabin body, have elasticity and are of a segmented structure, and comprise wing root sections in rotary connection with the cabin body and wing tip sections in rotary connection with the wing root sections in the length direction of the wings; the movable wing can be bent under the action of external force, and the movable wing with the segmented structure is beneficial to realizing the flapping effect of the bionic batwing wing based on the elasticity of the movable wing and providing advancing power for a manned tool based on the movable wing; more preferably, the wing root section and the cabin body, and the wing tip section and the wing root section are connected through a rotating shaft driven by a motor; the rotary connection between the wing root section and the cabin body and between the wing tip section and the wing root section can be realized through the rotary shaft, and the rotary connection is also facilitated to control whether the rotary connection is carried out so as to maintain the positions of the wing root section and the wing tip section under different stretching postures; besides the rotating shaft, the connecting device can also be connected by arranging a rotating bearing with a specific rotating range; more preferably, the movable wing is made of shape memory alloy and/or beryllium alloy and/or spring steel, and a skin is arranged on the movable wing;

the outer covering shell is movably connected with the cabin body and moves along the periphery of the cabin body to drive the movable wing to change an extending posture, the extending posture comprises a fully extending posture, a half extending posture and a fully accommodating posture, the fully extending posture is that the wing root section and the wing tip section are fully extended, the half extending posture is that the wing root section is bent and/or folded around the cabin body, the wing tip section is fully extended, and the fully accommodating posture is that the wing root section and the wing tip section are bent and/or folded around the cabin body; the outer covering shell moves along the periphery of the cabin body, and preferably moves along the periphery of the cabin body on a plane in the extending direction of the movable wing; the extending posture of the movable wing is changed by moving the propping movable wing; when the movable wings are completely stored around the cabin body, the movable wings are positioned between the cabin body and the outer covering shell, and the outer covering shell covers the movable wings to realize complete storage; because the movable wing has certain elasticity and can be attached to the periphery of the cabin body for storage, when the cabin body is of a cuboid structure and the like with edges and corners, the wing root section and the wing tip section of the movable wing can be attached to the periphery of the cabin body in a completely storage state, so that the wing root section and the wing tip section are folded around the cabin body; when the cabin body has an edge structure and a curved surface structure and the movable wing upwards winds around the cabin body, the wing root section and the wing tip section of the movable wing bend and/or fold around the cabin body; when the periphery of the cabin body is a curved surface and the movable wing winds the curved surface of the cabin body, the wing root section and the wing tip section of the movable wing are both in a bending state; for different cabin body shapes, the states of the wing root sections and the wing tip sections around the cabin body are also different;

the outer covering shell moves to act on the movable wing, so that the movable wing changes the stretching posture, when the outer covering shell is at the initial position, the movable wing is in the complete stretching posture, the function of air driving can be realized based on the movable wing in the complete stretching posture, the movable wings arranged at two sides of the cabin body realize the effect of simulating the flapping of the batwing wing through the wing root section and the wing tip section, and the lift force of the manned tool is maintained; when the movable wing in the fully extended posture is not flapped, the movable wing can be inclined relative to the plane so as to generate lift force by utilizing ascending airflow;

when the outer covering shell moves from the initial position and acts on the wing root section of the movable wing, the wing root section swings upwards to gradually attach to the cabin body, and when the outer covering shell moves to abut against the wing tip section, the wing root section bends or folds around the cabin body and is positioned between the outer covering shell and the cabin body, and the movable wing is in a half-extending posture at the moment, so that the manned tool is facilitated to swing upwards and downwards by utilizing the wing tip section when running underwater, and water lift power is generated; more preferably, the cabin body is also provided with a propeller to further provide power for underwater diving;

after the movable wings are in the half-extension posture, the outer covering shell continuously moves and acts on the wing tip section, the wing tip section is stressed to swing upwards and starts to be attached to the periphery of the cabin body after reaching the position vertical to the plane, and finally the movable wings on the two sides are attached to the periphery of the cabin body, so that complete storage is realized; the completely-contained posture can overcome the defect that the air-ground amphibious vehicle in the prior art needs a larger space to prevent wings when running on the land, thereby facilitating the running of the manned vehicle on the land; and when the outer covering shell moves and returns, the movable wing can be unfolded to be changed into a half-stretching or full-stretching posture. When the outer covering shell moves to return to the original position, the movable wing restores to the fully extended posture.

The airplane wheels are arranged on the front side and the rear side of the cabin. The airplane wheels are arranged on the front side and the rear side, so that the manned tool can provide stable supporting points when running on the land; the wheels are used for helping the manned tool to run on a plane and providing a power foundation for generating lift when the manned tool needs to be switched into an air running state.

The manned tool further comprises a power device, and the power device provides pushing force and/or pulling force and/or lifting force for the triphibian manned tool. The power device comprises a turbine engine in the prior art, the turbine engine is arranged on a wing root section and/or a wing tip section and/or a cabin body, an operation table is arranged in the cabin body, and a user controls a plurality of component operation parameters including the rotation range of the wing root section and the wing tip section in the movable wing, the movement of an outer covering shell, the retraction and release of a wheel and the opening and closing of the turbine engine through the operation table.

The bionic wing has elasticity and is in a joint shape, so that the bionic wing can be realized in a fully-extended posture, and an empty foundation is provided for air driving; the movable wing is changed into a half-stretching posture through the outer covering shell, on one hand, the wing tip section can swing to provide water lifting power, on the other hand, the wing tip section is located at the top of the cabin body in the half-stretching posture and swings on two sides of the top of the cabin body to obtain power, the swing is facilitated to obtain the water lifting power, meanwhile, the stability is kept, and the underwater walking of the manned tool is facilitated. Under the complete storage posture, the movable wing is in a state of being attached to the cabin body, and the defect that the wing unfolded in the prior art can not be put into practical use due to the occupied space is overcome when the movable wing runs on the land. The amphibious manned tool has multiple functions, can be used for manned driving in various environments, is beneficial to developing a traffic network, and solves the problems of common traffic jam and the like. The defects of amphibious vehicles and triphibian vehicles in the prior art are overcome, transition is not needed in specific environment when the driving states are switched, and the wings which are unfolded do not occupy large space when the vehicles are driven on the land, so that the vehicles are beneficial to being put into practical use, including field use in urban areas and other vehicles with limited size.

More preferably, the cabin body is provided with a track, and the outer casing is connected with the cabin body through the track; the movement of the outer cover shell is conveniently controlled through the rail connection, so that the position of the outer cover shell is controlled, and the extending posture of the movable wing is changed. And when the periphery of the cabin body is provided with the groove, the rail extends to the edge of the groove, and the outer covering shell is matched with the groove, the outer covering shell is driven to move to the groove along the rail and is matched with the groove, so that the manned tool can be further beautified. And when the groove is positioned at the top of the cabin body and the movable wing is attached in the groove in the complete storage posture, the outer covering shell moves to the groove and is matched with the groove, the functions of outer covering and beautifying can be realized simultaneously, and the movable wing is hidden.

Preferably, the outer cover comprises an elastic buffer part and a top holding part for supporting the buffer part, and the buffer part is abutted against the lower surface of the movable wing at least when the movable wing is in a fully-extended posture and a half-extended posture. The outer covering shell is provided with an elastic buffer part which can buffer the swing of the movable wing when the outer covering shell is pressed against the lower surface of the movable wing and can also provide power for the swing of the movable wing. When the movable wing swings upwards to a specific angle and then is put down downwards, the movable wing can be forced to swing upwards again when touching the elastic buffer part, and power is added to the swing of the movable wing on the basis of other power; namely, the buffer part is made of flexible elastic material, can be twisted to a certain degree, and can make the wing swing up and down when acting on the wing. The supporting part of the supporting buffer part is helpful for maintaining the stability of the outer covering shell, is convenient for preventing the movable wing from being excessively put down, and is helpful for maintaining the swing range of the movable wing.

Preferably, the cabin is a spindle-shaped cabin, the outer casing includes arc-shaped plates correspondingly disposed below the movable wings on the two sides and bent around the cabin, one side of the arc-shaped plates close to the movable wings forms a buffer part, the opposite side forms a supporting part, and the arc-shaped plates move along the circumferential direction of the spindle-shaped cabin to drive the movable wings on the corresponding sides to change the stretching posture. When the cabin body is a fusiform cabin body, the fusiform cabin body has a streamline shape, which is beneficial to reducing resistance in driving states of three environments of water, land and air and is beneficial to rapid driving of manned tools. And the streamline shape is favorable for running in the air and underwater to reduce the corresponding air and water resistance, thereby being convenient for reducing the requirement on the required power, being favorable for matching with simpler power devices and other auxiliary structures, being convenient for realizing triphibian effect in water, land and air, also being favorable for reducing the cost of manned tools, and being convenient for putting into practical production and use. In addition to the streamline appearance advantages, the fusiform cabin body is in a conical structure at the front end and the rear end, so that the front impact between people carriers in traffic accidents can be avoided, and the safety of the people carriers is improved. The outer covering shell comprises two side arc plates which are bent around the cabin body, and the two side arc plates are beneficial to moving along the circumferential direction of the cabin body, so that the wings can be conveniently pushed to bend around the outer wall of the cabin. And when the arc has buffering portion and top portion of holding, set up in the arc of cabin body both sides, an arc can combine another arc to form the sealing washer when taking in the gesture completely, plays sealed function, more preferably, forms the sealing washer through buffering portion.

Preferably, the total length of the arc-shaped plates on the two sides in the circumferential direction of the cabin is greater than 1/2 of the corresponding circumferential length of the cabin, and the total length of the jacking parts of the arc-shaped plates on the two sides in the circumferential direction of the cabin is less than 1/2 of the corresponding circumferential length of the cabin. More preferably, the arc plates on the two sides are symmetrically arranged, the circumferential length of the arc plate on the single side is greater than 1/4 of the corresponding circumferential length of the cabin, and the length of the jacking part of the arc plate on the single side in the circumferential direction of the cabin is less than 1/4 of the corresponding circumferential length of the cabin. When the circumferential length of the outer covering shell formed by combining the arc plates on the two sides is less than 1/2 of the circumferential length of the cabin, the wing root section or the wing tip section may be separated from the uncovered part of the outer covering shell due to elasticity when the movable wing is in the fully retracted posture, and the fully retracted posture cannot be stably maintained. When the total length of the top supporting parts of the outer covering shell, i.e. the total length of the top supporting parts of the arc-shaped plates at the two sides is greater than 1/2 of the corresponding circumferential length of the cabin, the arrangement and the arrangement of the outer covering shell are not facilitated. In addition, the buffer part of the outer cover is twisted to abut against the lower surface of the movable wing in the fully-extended posture and the half-extended posture of the movable wing, and 1/2, the total length of the propping part of the outer cover in the circumferential direction of the outer cover is smaller than the corresponding circumferential length of the cabin body, so that sufficient setting space is provided for the length of the buffer part, and the buffer and elastic effects of the buffer part on the wing are improved. In addition, when the length of the single-side movable wing is greater than the circumferential length of the single-side arc-shaped plate, the outer surface of the cabin body is also provided with an adsorption device to assist the tip of the wing to be stored. Preferably, the cabin body includes the inner deck, wraps up the outer cabin of anterior segment of inner deck front side, wraps up the outer cabin of back end of inner deck rear side, covers the shell including setting up between anterior segment outer cabin and the outer cabin of back end, the outer both sides of inner deck arc around inner deck circumference crooked. The movable wing is connected with the inner cabin and bent around the inner cabin or connected with the front-section outer cabin and the rear-section outer cabin, namely the movable wing is connected with the front-section outer cabin and the rear-section outer cabin respectively through two sides in the width direction to realize connection. And a track is arranged between the front section outer cabin and the rear section outer cabin and/or a track is arranged on the outer surface of the inner cabin, and the outer covering shell moves through the track. The inner cabin is a totally-enclosed inner cabin. The main structure of the fusiform cabin body can be realized through the front section outer cabin and the rear section outer cabin, the distance exists between the front section outer cabin and the rear section outer cabin, the outer covering shell is arranged between the front section outer cabin and the rear section outer cabin, the connection between the front section outer cabin and the rear section outer cabin is facilitated, and the cabin body is enabled to be smooth in cabin surface. More importantly, the movable wings bent around the inner cabin are covered by the outer covering shell arranged between the front cabin body and the rear cabin body, so that the movable wings can be completely stored, and the movable wings can be completely hidden when being stored.

More preferably, the outer cabin of anterior segment includes toper aircraft nose, front deck, and the outer cabin of back segment includes toper tail, backseat, the toper aircraft nose is connected in the front deck front end, the inner cabin front side is wrapped up to the front deck, toper tail is connected in the backseat rear end, the inner cabin rear side is wrapped up to the backseat. The movable wing is connected to the inner cabin or between the front cabin and the rear cabin; the outer cover shell is movably connected with the inner cabin or movably connected between the front cabin and the rear cabin. The cone nose, which is independent from the forward cabin, rotates outward to protrude the inner cabin wall, thereby facilitating the cone nose to act as a cavitator to contain the manned tool body within the cavity during underwater navigation, which helps to increase the speed of navigation. More preferably, the tapered machine tail end is provided with helical blades to assist in providing thrust to the people mover when thrust is required.

Preferably, the height of the inner chamber is more than or equal to 1.2 times of the sitting height of a user; more preferably, the height of the inner cabin is more than or equal to 1.8m, and the inner cabin is suitable for most people.

Preferably, the upper parts of the front side and the rear side of the cabin body are provided with glass portholes. Through the glass porthole, the passengers of the triphibian manned tool have a large visual field to observe the external environment, the driving state of the triphibian manned tool can be operated in real time by combining the visual observation of the passengers, and the driving safety of the triphibian manned tool can be improved. More preferably, the cabin is the spindle-shaped cabin, and the glass portholes are arranged on the outer cabin and the inner cabin.

Preferably, the cabin body is internally provided with a seat and an all-directional rotating base, and the seat is fixed on the all-directional rotating base. The all-round rotation base rotates around the geometric center of the cabin body, helps adjusting the orientation of the seat according to the position change of the triphibian manned tool, and enables a rider to conveniently carry out the running operation of the triphibian manned tool or to conveniently go out of the cabin. More preferably, the cabin is internally provided with a manipulator, the inner wall of the cabin is provided with a track, one end of the manipulator moves along the track, the other end of the manipulator is connected with the omnibearing rotary base, and the rotation of the omnibearing rotary base around the geometric center of the cabin is realized through the overturning and the rotation of the manipulator and the movement of the manipulator. More preferably, the seat comprises a backrest part and a bearing part which are connected, wherein the backrest part and/or the bearing part is/are provided with a rotating mechanism, and the rotating mechanism is driven to enable the seat to rotate relative to the omnibearing rotating base. Namely, the seat has higher degree of freedom on the basis of the omnibearing rotating base, and is helpful for the passengers to further adjust the position and the orientation of the seat relative to the cabin. More preferably, when the cabin is the spindle-shaped cabin, the seat, the omni-directional rotating base, the manipulator and the track are all disposed in the inner cabin. More preferably, the distance between the top end of the omnibearing rotary base and the top end of the interior of the cabin body is more than or equal to 0.75 time of the height of a user; more preferably, the distance between the top end of the omnibearing rotary base and the top end of the interior of the cabin is more than or equal to 1.5 m.

Preferably, the front end of the cabin body is connected with a cavitator. When the triphibian manned tool of this application was gone at high speed under water, helped forming the cavitation bubble of parcel triphibian manned tool through the cavitation ware, can provide lift and attitude control for the triphibian manned tool who goes under water based on the cavitation ware, help triphibian manned tool to go forward smoothly under water. More preferably, the cabin body is a fusiform cabin body, the cabin body comprises a conical machine head, a conical machine tail, an inner cabin and a barrel-shaped outer cabin, the inner cabin is arranged in the outer cabin, the machine head is arranged at the front end of the outer cabin, the machine tail is arranged at the rear end of the outer cabin, and the cavitator is assembled and arranged on the machine head, so that the fusiform cabin body is combined to further improve the underwater traveling capacity of the triphibian manned tool, and the underwater traveling control accuracy is improved conveniently.

Preferably, the cabin body is provided with a wheel retraction device, and the wheels are connected with the cabin body through the wheel retraction device. The wheel retraction device can change the position of the wheel, and is beneficial to the triphibian manned tool to adjust the position of the wheel so as to reduce the resistance influence of the wheel when the triphibian manned tool runs in an underwater environment or an air environment. More preferably, the cabin body is a spindle-shaped cabin body, and when the aircraft runs in the air or runs underwater, the wheel retraction device retracts the wheel on the front side of the cabin body into a corresponding accommodating groove on the machine head side or in the machine head, or into a corresponding accommodating groove on the outer cabin or in a corresponding accommodating groove on the inner cabin, and raises the wheel on the rear side of the cabin body and retracts the wheel on the tail side; when the airplane wheel is switched to land for driving, the front and rear side airplane wheels are all lowered to be lower than the cabin body by the airplane wheel retraction device. More preferentially, wheel winding and unwinding devices includes connecting rod, slewing mechanism, the one end fixed wheel of connecting rod, the other end with slewing mechanism connects, slewing mechanism fixed connection is on the cabin body, slewing mechanism receives the motor drive to drive the connecting rod and rotates to raise or reduce the wheel, realize receiving and unwinding of wheel. More preferably, the front side is provided with one wheel, and the rear side is provided with more than two wheels, which helps to reduce the space occupied by the front side wheels, and simultaneously maintains the stability of land driving.

Preferably, the rear end of the cabin and/or the rear side engine wheels are provided with tail rudders to provide steering moment stabilizing directions for the engine body. The tail rudder is beneficial to providing stability for the air running of the triphibian manned tool, keeping balance and facilitating the air flying operation of the triphibian manned tool. Also, the underwater diving stability can be improved. More preferably, the nacelle body is a spindle-shaped nacelle body as described above, and the tail rudder is arranged on the tail and/or the rear side wheel. More preferably, an aileron is also provided on the rear side of the nacelle or on the movable wing.

A parking system comprising the triphibian manned tool and a charging pile according to any one of claims 1-9, wherein the triphibian manned tool is vertically parked on the charging pile matched with the triphibian manned tool. In the prior art, the use is limited by the environment, and vehicles with multiple single functions can only be parked by being horizontally placed on the ground. The amphibious multi-purpose vehicle can only horizontally lay because the unfolded wings and the driving transition space occupy larger space. And the wing can be accomodate in this application, and combine to this application and have the triphibian function of land and water, can switch at the state of traveling between air and land, so this application helps realizing standing upright of manned instrument to save parking space. The problem of limited parking space in modern cities is helped to be solved. In addition, the drive mode of the green energy helps saving natural resources, realizes green trip, so this application triphibian manned tool is provided with electric drive device, through the operation of other parts of electric drive. Corresponding, the setting is with the electric pile that fills of air-water triphibian manned instrument matching, then helps when solving prior art vehicle and parks the problem, makes things convenient for manned instrument to charge, is convenient for actually to put into use. Fill electric pile and cabin body front side and match, after manned instrument is upright, cabin body front side is fixed to filling electric pile inside and is accepted to charge. And the combination of the omnibearing rotary base and the manipulator is helpful for adjusting the position of a user after the manned tool is parked, so that the user can conveniently open and exit the cabin door arranged on the inner cabin. More preferably, under the upright charging mode, the front side of the cabin is partially arranged in the charging pile, and in the process of gradually changing from the horizontal navigation state to the upright state, the all-directional rotating base changes the position along with the horizontal navigation state, so that the head of the human body is kept upward. After the cabin is static, the all-directional rotating base is rotated horizontally, so that a human body faces to the cabin door originally positioned at the bottom, the bottom end of the cabin door is consistent with the height of the charging pile platform surface, and a driver can easily walk out of the cabin. Through this application system of parking helps in order to reduce the area of occupation when idle state, makes the driver who lives in high-rise can park the cabin on top layer or balcony. For the drivers with smaller floor space requirements, the cabin door can also be arranged at the rear side of the cabin body.

Compared with the prior art, the invention has the beneficial effects that: the bionic effect of the batwing wing can be realized by utilizing the movable wing with the sectional structure and the elasticity, the triphibian manned tool can be suitable for various environments including water, land and air by changing the movable wing in different extending postures, and the driving effect under the corresponding form environment can be improved by the different extending postures. More importantly, the vehicle can run in various environments based on the application, and is beneficial to expanding the traffic network of modern life, so that the problem of traffic jam in cities and other areas is solved. The outer covering shell is used for driving the movable wing to change the extending posture, so that sufficient extending posture changing driving force can be provided conveniently based on the outer covering shell, and the complexity of the wing structure is obviously reduced compared with the folding and bending through the self control of the movable wing. If the change of the extending posture is controlled by the movable wing, the bending effect of clinging to the cabin body can not be realized, and the local or whole accommodation of the movable wing is not facilitated. For example, the rotating shaft at the joint of the wing root section and the cabin body is controlled to drive the wing root section to swing upwards, but the rotating shaft cannot control the bending of one side of the wing root section close to the wing tip section, so that at most, only the change of the inclination angle of the wing root section can be realized, and the effect of bending or folding around the cabin body cannot be realized. Therefore, the outer covering shell not only can drive the movable wing to change the stretching posture, but also can simplify the structure of the manned tool. Meanwhile, the movable wings can be completely stored by matching the outer covering shell and the cabin body, so that the use limitation of the wings on land driving of the multi-purpose vehicle in the prior art is overcome. The utility model provides a swing of wing can be realized to the buffer portion that movable wing combines outer cover to be convenient for the instant switching at different environment travel states such as land and water. When the lift force generated by the movable wing is enough, the driving state can be switched without transition space. This application still sets up manned instrument whole expression and be olive type, spindle body type structure to make manned instrument all only have less resistance under multiple environment, be convenient for reduce the requirement to power, help putting into practical use. In addition, this application is based on triphibian manned instrument, except solving the problem of traffic jam, can also combine to fill electric pile and solve vehicle parking problem in modern city, only need a small amount of spaces can realize parking, and help combining triphibian manned instrument to realize the effect of energy-conservation, environmental protection.

Drawings

Fig. 1 is a schematic perspective view (i) of the present invention.

Fig. 2 is a side view of the present invention.

Fig. 3 is a schematic side view of the present invention (ii).

Fig. 4 is a schematic perspective view (ii) of the present invention.

Fig. 5 is a schematic view of the fully extended position of the present invention.

Fig. 6 is a schematic view of the semi-extended position of the present invention.

Fig. 7 is a schematic view of the fully retracted position of the present invention.

Figure 8 is a schematic view of the ride configuration of the present invention.

Fig. 9 is a schematic view of the wheel retraction structure of the present invention.

FIG. 10 is a schematic view of the parking system of the present invention.

Detailed Description

The drawings are only for purposes of illustration and are not to be construed as limiting the invention. For a better understanding of the following embodiments, certain features of the drawings may be omitted, enlarged or reduced, and do not represent the size of an actual product; it will be understood by those skilled in the art that certain well-known structures in the drawings and descriptions thereof may be omitted.

Example 1

As shown in fig. 1, the present embodiment discloses a triphibian manned tool, comprising:

a cabin body 1 for providing a manned space;

the movable wings 2 are arranged on two sides of the cabin body 1, have elasticity and are of a segmented structure, and comprise wing root sections 21 and wing tip sections 22 in the length direction of the wings, wherein the wing root sections are rotatably connected with the cabin body;

the outer covering shell 3 is movably connected with the cabin body 1, moves along the periphery of the cabin body 1 to drive the movable wing 2 to change an extending posture, wherein the extending posture comprises a fully extending posture, a half extending posture and a fully accommodating posture, the fully extending posture is that the wing root section 21 and the wing tip section 22 are fully extended, the half extending posture is that the wing root section 21 bends and/or folds around the cabin body 1, the wing tip section 22 is fully extended, and the fully accommodating posture is that the wing root section 21 and the wing tip section 22 bend and/or folds around the cabin body 1; wherein the fully extended position is shown in fig. 5, the half extended position is shown in fig. 6, and the fully stowed position is shown in fig. 7. Wherein fig. 5, 6, 7 show the hidden partial structure for convenience and the outer cover as a dashed line.

The airplane wheels 4 are arranged on the front side and the rear side of the cabin body 1;

the power plant 5 (not shown) for providing thrust and/or tension and/or lift to the people mover comprises a prior art turbine engine (not shown) arranged on the wing root section 21 and/or the wing tip section 22 and/or the nacelle 1. More specifically, the power plant 5 and the movable wing 2 are driven electrically.

As shown in fig. 2, in the present embodiment, the cabin 1 is a spindle-shaped cabin 1, and includes an inner cabin 11, a front-section outer cabin 12 wrapping the front side of the inner cabin 11, and a rear-section outer cabin 13 wrapping the rear side of the inner cabin 11, where a distance exists between the front-section outer cabin 12 and the rear-section outer cabin 13; the movable wings 2 are elastic and sectional wings and are respectively arranged between the front-section outer cabin 12 and the rear-section outer cabin 13 and on two sides of the inner cabin 11; as shown in fig. 1, 3 and 4, the outer casing 3 includes two arc plates which are arranged between the front section outer cabin 12 and the rear section outer cabin 13 and outside the inner cabin 11 and are bent around the circumferential direction of the inner cabin, and the two arc plates are respectively arranged below the movable wings 2 on both sides of the inner cabin 11. As shown in fig. 4, the front-section outer chamber 12 includes a conical nose 121 and a front chamber 122, the rear-section outer chamber 13 includes a conical tail 131 and a rear chamber 132, the conical nose 121 is connected to the front end of the front chamber 122, the front chamber 122 wraps the front side of the inner chamber 11, the conical tail 131 is connected to the rear end of the rear chamber 132, and the rear chamber 132 wraps the rear side of the inner chamber 11. An outer enclosure formed by two curved plates is disposed between the front 122 and rear 132 compartments. The upper sides of the inner cabin 11, the front section outer cabin 12 and the rear section outer cabin 13 of the cabin body are all provided with glass portholes.

In this embodiment, the movable wings 2 are disposed on two sides of the inner cabin 11, and the outer covering shell 3 is located below the movable wings 2. In the embodiment, the movable wing 2 is of a sectional structure and is made of shape memory alloy and/or beryllium alloy and/or spring steel, and a skin is arranged on the movable wing 2; the movable wing 2 can be driven to bend and deform by pushing the outer cover shell 3 upwards, so that the movable wing is suitable for forms under different environments. The wing root section 21 and the cabin body 1, and the wing tip section 22 and the wing root section 21 are connected by a rotating shaft 23 driven by a motor, as shown in fig. 5; the rotating shaft 23 can not only realize the rotating connection between the wing root section 21 and the cabin body 1 and between the wing tip section 22 and the wing root section 21, but also control whether to rotate so as to maintain the positions of the wing root section 21 and the wing tip section 22 under different stretching postures; in addition to the rotating shaft 23, connection can be made by providing a rotary bearing having a specific rotation range. And in this embodiment, an aileron (not shown) is also provided on the movable wing.

The front cabin 122, the rear cabin 132 and the surface of the inner cabin 11 form a groove-shaped structure, the outer covering shell 3 comprises two arc-shaped plates attached to the outer surface of the inner cabin 11, the arc-shaped plates move in the groove along the circumferential direction of the inner cabin, the extending postures of the corresponding side movable wings 2 are changed by pushing the corresponding side movable wings 2 upwards, namely, the movable wings 2 are pushed to be partially or wholly bent, and therefore the extending postures are changed. And when the outer covering shell 3 is pushed to the movable wing 2 to be completely stored, the outer covering shell 3 can be matched with the groove, so that the manned tool can be further beautified on the premise that the movable wing is completely stored. In the present embodiment, the outer casing 3 disposed below the movable wing 2 includes a supporting portion 32 having an elastic buffer portion 31 and a supporting buffer portion 31, when the outer casing 3 is disposed below the movable wing 2, the top portion is the buffer portion 31, and the supporting portion 32 is disposed below the buffer portion 31. The buffer portion 31 abuts against the lower surface of the movable wing 2 at least when the movable wing 2 is in the fully extended posture and the half-extended posture. The elastic buffer part 31 of the outer cover shell 3 can provide buffer for the swing of the movable wing 2 when the outer cover shell is pressed against the lower surface of the movable wing 2, and can also provide power for the swing of the movable wing 2. When the movable wing 2 swings upwards to a specific angle and then is put down downwards, the movable wing 2 can swing upwards again under stress when touching the elastic buffer part 31, and power is added to the swing of the movable wing 2 on the basis of other power; that is, the buffer part 31 is made of flexible elastic material, and can be twisted to a certain degree, and when acting on the wing 2, the wing 2 can be swung up and down. The supporting portion 32 of the supporting buffer portion 31 helps to maintain the stability of the outer skin 3, is also convenient for placing the movable wing 2 over-laid, and helps to maintain the swing range of the movable wing 2. More specifically, when the movable wing 2 is in the fully extended posture, the buffer portion 31 is partially attached to the lower surface of the wing root section 21 and/or the wing tip section 22, and the supporting portion 32 is located below the buffer portion 31 for supporting, and when the movable wing 2 is in the semi-extended posture, the buffer portion 31 is partially attached to the lower surface of the wing tip section 22, and the supporting portion 32 is located below the buffer portion 31 for supporting.

In this embodiment, a rail (not shown) is disposed at one side edge of the front compartment 122 and the rear compartment 132, which are close to each other, and a power structure is connected to the outer casing 3 and is driven by the power structure to move along the rail. In addition, in the present embodiment, the length of the outer covering 3 in the circumferential direction of the inner compartment 11 is slightly greater than 1/2 of the corresponding circumferential length of the inner compartment 11, wherein the length of the top supporting portion 32 is slightly less than 1/2 of the corresponding circumferential length of the compartment.

As shown in fig. 8 and 9, the wheel 4 in this embodiment includes a front-side wheel 41 and a rear-side wheel 42, the front-side wheel 41 is a single wheel disposed below the head 121, the rear-side wheel 42 is two wheels symmetrically disposed below the tail 131, both the front-side wheel and the rear-side wheel are connected to the cabin 1 through a wheel retraction device, in this embodiment, the front-side wheel 41 is connected to the inner cabin 11, and the rear-side wheel 42 is connected to the tapered tail 131; when the airplane wheel retraction device runs in the air or runs underwater, the front side airplane wheel 41 of the cabin body 1 is accommodated in the corresponding accommodating groove of the inner cabin 11, and the rear side airplane wheel 42 of the cabin body 1 is lifted and accommodated below the tail 131; when the vehicle is switched to land driving, the wheel retraction device lowers both the front and rear side wheels 41 and 42 to be lower than the cabin 1. The airplane wheel retraction device comprises a connecting rod and a rotating mechanism, one end of the connecting rod is fixed with an airplane wheel, the other end of the connecting rod is connected with the rotating mechanism, the rotating mechanism is fixedly connected to the cabin body 1, the rotating mechanism is driven by a motor to drive the connecting rod to rotate, so that the airplane wheel is raised or lowered, retraction of the airplane wheel is achieved, and more specifically, the airplane wheel is placed on the connecting rod perpendicular to the ground when the airplane runs on the land, as shown in fig. 3.

In the embodiment, in order to facilitate steering control and improve stability, a tail rudder (not shown in the figure) is further arranged on the rear side wheel 42 to provide a stable steering moment direction for the airplane body.

In addition, in the present embodiment, the inner compartment 11 between the front compartment 122 and the rear compartment 132 is provided with a compartment door for a user to enter the inner compartment 11; an operation table (not shown in the figure), an omnidirectional rotating base 111, a manipulator (not shown in the figure) connected with the omnidirectional rotating base, an internal track (not shown in the figure) for moving the manipulator, and a seat 112 fixed on the omnidirectional rotating base are arranged in the inner cabin 11, and a user sits on the seat 112 and controls a plurality of component operation parameters including the rotation range of the wing root section 21 and the wing tip section 22 in the movable wing 2, the movement of the outer covering shell 3, the retraction and release of the wheel 4, and the opening and closing of the turbine engine 5 through the operation table. One end of the manipulator moves along the track, the other end of the manipulator is connected with the omnibearing rotary base 111, and the omnibearing rotary base 111 rotates around the geometric center of the cabin body 1 through overturning and rotating of the manipulator and moving of the manipulator, so that the orientation and riding direction of a user can be adjusted conveniently. And the seat 112 comprises a backrest part and a bearing part which are connected, wherein the backrest part and/or the bearing part is/are provided with a rotating mechanism which is driven to rotate the seat relative to the omnibearing rotating base.

More specifically, interior cabin 11 is highly more than or equal to 1.8m, and the distance between the inside top of all-round rotating base 111 top and interior cabin 11 is more than or equal to 1.5m, designs for 2m with human height in this embodiment, is applicable to most crowds, and interior cabin height is 1.2 times of human seat height. The multifunctional manned vehicle is suitable for most people and is convenient to reduce the internal space occupation, so that the whole volume of the manned vehicle is reduced, and the use in land transportation is convenient to realize.

The implementation principle is as follows: the outer covering shell 3 moves to act on the movable wing 2, so that the movable wing 2 changes the extending posture, when the outer covering shell 3 is at the initial position, the movable wing 2 is in the fully extending posture, as shown in fig. 5, the movable wing 2 based on the fully extending posture can realize the function of traveling in the air, and the movable wings 2 arranged at two sides of the inner cabin 11 realize the effect of imitating bat wing flapping through the wing root section 21 and the wing tip section 22, so that the lift force of the manned tool is maintained; or in combination with other power means 5 to provide total lift; when the movable wing 2 in the fully extended posture does not swing, the movable wing 2 can be inclined relative to the plane so as to generate lift force by utilizing ascending airflow;

when the arc plates on the two sides of the outer covering shell 3 start to move upwards from the bottom of the initial position and act on the wing root section 21 of the movable wing 2, the wing root section 21 swings upwards to gradually attach to the cabin body 1, and when the arc plates on the two sides of the outer covering shell 3 move to abut against the wing tip section 22, the wing root section 21 is bent around the cabin body 1 and is positioned between the outer covering shell 3 and the cabin body 1, at the moment, the movable wing 2 is in a half-stretching posture, as shown in figure 5 before transformation, and as shown in figure 6 after transformation into half-stretching, the posture can be driven underwater, and when a manned tool is driven underwater, the wing tip section 22 swings upwards and downwards to generate water lifting power; more specifically, the tail 131 is further provided with a propeller to further provide power for underwater diving; the conical nose 121 independent from the front cabin 122 rotates outwards to protrude the inner cabin wall, and the conical nose 121 serves as a cavitator to enable the manned tool body to be contained in the cavity during underwater navigation, so that the navigation speed is improved;

after the arc plates on the two sides of the outer covering shell 3 enable the movable wings 2 to be in the half-extension posture, the arc plates continue to move and act on the wing tip sections 22, the wing tip sections 22 are stressed to swing upwards and begin to be attached to the periphery of the inner cabin 11 after reaching the position vertical to the plane, and finally the movable wings 2 on the two sides are attached to the periphery of the cabin body 1, so that complete storage is realized, as shown in fig. 7; the process of changing the movement of the outer cover 3 is the process of changing from fig. 6 to fig. 7; the manned tool puts down the front side airplane wheel 41 and the rear side airplane wheel 42 through the airplane wheel retraction device so as to drive on the land; the completely-contained posture can overcome the defect that the air-ground amphibious vehicle in the prior art needs a larger space for placing the wings when running on the land; when the outer covering shell 3 moves to return, the movable wing 2 can be unfolded to be changed into a half-stretching or full-stretching posture, and when the outer covering shell 3 moves to return to the original position, the movable wing 2 returns to the full-stretching posture. Namely, the movable wing 2 is driven by the movement of the outer cover shell 3 to be changed into an extending posture corresponding to the driving environment, thereby realizing the triphibian function of water, land and air. Besides the storage mode shown in fig. 5, 6 and 7, when the wing 2 is too long, the wing 2 can be stored by using the arc plates on both sides of the outer casing 3 which move in a staggered manner.

Example 2

As shown in fig. 10, the present embodiment discloses a parking system, which includes the amphibious triphibian manned tool described in embodiment 1 and a charging pile 6, the amphibious triphibian manned tool is vertically parked on the charging pile 6 matched with the amphibious triphibian manned tool in an extended posture in which the movable wing 2 is completely stowed, and the charging pile 6 corresponds to the front-section outer cabin 12 of the cabin body. In the parking process gradually changed from the horizontal navigation state to the upright state, as the adjustment process shown in fig. 9 to 10, the manipulator, the omnibearing rotary base 111 and the seat 112 are combined to enable the head of the human body to be upward, after the human body is static, the rotary base 111 rotates horizontally, the human body faces to the cabin door originally positioned at the bottom, the bottom end of the cabin door is consistent with the height of the charging pile platform surface, and a driver can walk out of the cabin.

It should be understood that the above-mentioned embodiments of the present invention are only examples for clearly illustrating the technical solutions of the present invention, and are not intended to limit the specific embodiments of the present invention. Any modification, equivalent replacement, and improvement made within the spirit and principle of the present invention claims should be included in the protection scope of the present invention claims.

Claims (10)

1. A triphibian manned tool of land, water and air, characterized by that includes:

a cabin body providing a manned space;

the movable wings are arranged on two sides of the cabin body, have elasticity and are of a segmented structure, and comprise wing root sections in rotary connection with the cabin body and wing tip sections in rotary connection with the wing root sections in the length direction of the wings;

the outer covering shell is movably connected with the cabin body and moves along the periphery of the cabin body to drive the movable wing to change an extending posture, the extending posture comprises a fully extending posture, a half extending posture and a fully accommodating posture, the fully extending posture is that the wing root section and the wing tip section are fully extended, the half extending posture is that the wing root section is bent and/or folded around the cabin body, the wing tip section is fully extended, and the fully accommodating posture is that the wing root section and the wing tip section are bent and/or folded around the cabin body;

the airplane wheels are arranged on the front side and the rear side of the cabin.

2. The amphibious vehicle as claimed in claim 1, wherein the outer hull comprises an elastic buffer part and a supporting part for supporting the buffer part, and the buffer part is supported against the lower surface of the movable wing at least when the movable wing is in the fully extended position and the semi-extended position.

3. The amphibious passenger carrying tool as claimed in claim 2, wherein the cabin is a fusiform cabin, the outer covering comprises two arc plates correspondingly disposed below the movable wings on the two sides and bent around the cabin, one side of each arc plate close to the movable wing forms a buffer part, the other side forms a supporting part, and the arc plates move circumferentially along the fusiform cabin to drive the movable wings on the corresponding sides to change the extending posture.

4. The water, land and air triphibian manned tool of claim 3, wherein the total length of the arc plates on both sides in the circumferential direction of the cabin is greater than 1/2 of the corresponding circumferential length of the cabin, and the total length of the top holding parts of the arc plates on both sides in the circumferential direction of the cabin is less than 1/2 of the corresponding circumferential length of the cabin.

5. The amphibious manned vehicle of claim 3, wherein the cabin comprises an inner cabin, a front section outer cabin wrapping the front side of the inner cabin and a rear section outer cabin wrapping the rear side of the inner cabin, and the outer casing comprises arc plates which are arranged between the front section outer cabin and the rear section outer cabin and are bent around the circumference of the inner cabin on two sides outside the inner cabin.

6. The triphibian manned tool of any one of claims 1 to 5, wherein the cabin is provided with glass portholes at the upper parts of the front and rear sides.

7. The triphibian manned tool of any one of claims 1 to 5, wherein a seat and an omni-directional rotating base are arranged in the cabin, and the seat is fixed on the omni-directional rotating base.

8. The amphibious triphibian manned tool according to any one of claims 1 to 5, wherein a cavitation device is provided at the front end of the cabin.

9. The amphibious manned tool of any one of claims 1 to 5, wherein a wheel retraction device is arranged on the cabin body, and the wheel is connected with the cabin body through the wheel retraction device.

10. A parking system, characterized by comprising the land, water and air triphibian manned tool and a charging pile, wherein the land, water and air triphibian manned tool is vertically parked on the charging pile matched with the land, water and air triphibian manned tool.

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