CN210653156U - Unmanned aerial vehicle's carrier - Google Patents

Abstract

The application relates to the technical field of unmanned aerial vehicle transport, provides an unmanned aerial vehicle's carrier, and unmanned aerial vehicle includes: unmanned aerial vehicle body and rotor arm, the carrier includes: a locating part for carrying on the frame of rotor arm and locating on the frame, the one end of frame has the exit that can supply the accessible business turn over of unmanned aerial vehicle body, and the other end of frame is equipped with the handle, and the one end of keeping away from the handle on the frame is equipped with running gear, and based on same reference surface, the height that highly is less than the rotor arm of frame, the locating part is used for when the frame slope with the rotor arm restriction on the frame so that unmanned aerial vehicle hangs on the frame. This physical stamina card of unmanned aerial vehicle is gone into to the access port in, and running gear can pass from rotor arm below to make rotor arm overlap joint on the frame, and carry out the position through the locating part and prescribe a limit to, carry out the frame and enable unmanned aerial vehicle liftoff after lifting, this process just can be accomplished through alone, and need not to lift unmanned aerial vehicle and just can place it on the carrier, makes this carrier have labour saving and time saving and economizes artifical advantage.

Description

Unmanned aerial vehicle's carrier

Technical Field

The utility model belongs to the technical field of the unmanned aerial vehicle transport technique and specifically relates to a carrier of unmanned aerial vehicle is related to.

Background

Unmanned aerial vehicle's outdoor function generally is in more remote or remote mountain area, and traffic is inconvenient, leads to unmanned aerial vehicle can't carry through normal transport vechicle, and because of unmanned aerial vehicle (especially many rotor unmanned aerial vehicle) weight itself and the battery and the goods etc. that load so that unmanned aerial vehicle is whole heavier moreover, needs many people to cooperate to carry, and wastes time and energy through artifical transport unmanned aerial vehicle.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an unmanned aerial vehicle's carrier aims at solving among the prior art unmanned aerial vehicle and wastes time and energy through artifical transport technical problem.

In order to achieve the above object, the utility model adopts the following technical scheme: a cart for a drone, the drone comprising: unmanned aerial vehicle body and rotor arm include: be used for carrying the frame of rotor arm with locate locating part on the frame, the one end of frame has and supplies the exit of accessible business turn over of unmanned aerial vehicle body, the other end of frame is equipped with the handle, keep away from on the frame the one end of handle is equipped with running gear, based on same reference surface, the height that highly is less than the rotor arm of treating transport unmanned aerial vehicle of frame, the locating part is used for will during the frame slope the rotor arm restriction is in so that unmanned aerial vehicle hangs on the frame.

Preferably: the frame includes: the two inner pipes are arranged at intervals and are positioned between the two outer pipes, and the two inner pipes and the two outer pipes are connected through the plurality of cross rods, so that the inlet and the outlet are formed between the two inner pipes.

Preferably: the two inner tubes are parallel, the two outer tubes are parallel, the inner tubes are parallel to the outer tubes, and the inner tubes and the outer tubes are perpendicular to the cross rod.

Preferably: the cross bar is welded with the inner pipe and/or the outer pipe; or the cross bar is movably connected with the inner pipe and/or the outer pipe, so that the fixed positions of the cross bar and the inner pipe and/or the outer pipe can be adjusted, and the width of the inlet and the outlet can be adjusted.

Preferably: the inner pipes are arranged at intervals with the adjacent outer pipes, and the two walking mechanisms are respectively arranged between the adjacent inner pipes and the adjacent outer pipes.

Preferably: the frame is also provided with a plurality of bearing parts capable of supporting the rotor arms, and the bearing parts are connected with the limiting parts.

Preferably: the locating part is for stopping the pipe, the one end that stops the pipe is located on the frame, hold carrier one end and locate on the frame, the other end locate stop on the pipe and with stop and form the step that is used for supporting between the pipe the rotor arm.

Preferably: the carrier includes: first riser and the second riser that is parallel to each other to and first diaphragm and the second diaphragm that is parallel to each other, the one end of first riser is connected on the frame, the other end of first riser with the one end of first diaphragm is connected, the other end of first diaphragm with the one end of second riser is connected, the other end of second riser with the one end of second diaphragm is connected, keep away from the pipe the one end of frame is passed first diaphragm and butt are in on the second diaphragm.

Preferably: the handle and the inner tube are integrally formed, and a strap is arranged on the handle.

Preferably: the running mechanism is a pneumatic wheel or a rubber wheel.

Preferably: the frame, the locating part and the bearing part are all made of steel materials.

Preferably: the limiting part and the bearing part are welded with the frame.

Preferably: the locating part is arranged on the frame in a sliding mode and is fixed in position through a fastener, the bearing part is arranged on the locating part in a sliding mode and is fixed in position through the fastener, or the bearing part is in threaded connection with the locating part.

The utility model has the advantages that:

the utility model provides a pair of unmanned aerial vehicle's carrier, this physical stamina of unmanned aerial vehicle accessible gets into to the business turn over in the mouth, make things convenient for running gear to pass from rotor arm below, so that rotor arm overlap joint is on the frame, and carry out the position through the locating part and prescribe a limit to, then use running gear as the fulcrum, carry out the lifting so that unmanned aerial vehicle is liftoff with the frame through the handle, thereby realize unmanned aerial vehicle's transport, this process just can accomplish unmanned aerial vehicle's transport through alone, and need not to lift up unmanned aerial vehicle and just can place it on the carrier, make this carrier have labour saving and time saving and economize artificial advantage.

Drawings

In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings required for the embodiments or the prior art descriptions will be briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings without inventive labor.

Fig. 1 is a schematic structural diagram of a carrier of an unmanned aerial vehicle according to an embodiment of the present invention;

FIG. 2 is an enlarged view taken at A in FIG. 1;

fig. 3 is a schematic view of a state in which a carrier of an unmanned aerial vehicle carries a multi-rotor unmanned aerial vehicle according to an embodiment of the present invention;

fig. 4 is a schematic plan view illustrating a sliding assembly of the limiting member and the inner tube, and the bearing member and the limiting member according to an embodiment of the present invention;

fig. 5 is a schematic plan view of the bearing member and the limiting member in threaded connection according to an embodiment of the present invention.

Reference numerals: 1. a frame; 11. an inner tube; 12. an outer tube; 13. a cross bar; 14. an inlet and an outlet; 2. a limiting member; 21. a first cross tube; 22. a first vertical tube; 3. a traveling wheel; 4. a handle; 5. a carrier; 51. a first vertical plate; 52. a second vertical plate; 53. a first transverse plate; 54. a second transverse plate; 55. a second cross tube; 56. a second standpipe; 57. a support block; 58. a baffle plate; 59. a placement groove; 6. a harness; 7. an unmanned aerial vehicle; 71. an unmanned aerial vehicle body; 72. a rotor arm; 73. a rotor; 8. a fastener.

Detailed Description

Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are exemplary and intended to be used for explaining the present invention, and should not be construed as limiting the present invention.

In the description of the present invention, it is to be understood that the terms "length", "width", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on those shown in the drawings, and are merely for convenience of description and simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention.

Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless specifically limited otherwise.

In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," and "fixed" are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.

As shown in fig. 1 to fig. 3, a carrier for an unmanned aerial vehicle according to an embodiment of the present invention is now described. In this embodiment, the drone 7 comprises: unmanned aerial vehicle body 71, many rotor arms 72 on locating unmanned aerial vehicle body 71 to and rotate and locate rotor 73 on rotor arm 72, the bottom of unmanned aerial vehicle body 71 is equipped with the foot rest, and the foot rest makes unmanned aerial vehicle body 71 break away from ground, so that has certain interval between rotor arm 72 and the ground, this unmanned aerial vehicle 7 is conventional unmanned aerial vehicle, and its concrete structure does not state here.

In this embodiment, this unmanned aerial vehicle's carrier includes: the bicycle frame comprises a bicycle frame 1 and a limiting part 2 arranged on the bicycle frame 1. Wherein, the one end of frame 1 has exit 14, and the other end of frame 1 is equipped with handle 4, and the one end of keeping away from handle 4 on frame 1 is equipped with running gear, and running gear is walking wheel 3 in this embodiment, and walking wheel 3 is provided with two at least, and two walking wheels 3 rotate to be located on frame 1. Wherein, exit 14 is used for supplying unmanned aerial vehicle body 71 accessible business turn over of unmanned aerial vehicle 7, so that rotor arm 72 takes in frame 1, when walking wheel 3 of the foot rest of unmanned aerial vehicle 7 and carrier is in same bearing plane, when both are based on same reference surface promptly, the height of walking wheel 3 and frame 1 all is less than the height of rotor arm 72, so that unmanned aerial vehicle body 71 of unmanned aerial vehicle 7 can have the card of interference to go into exit 14 and make its rotor arm 72 overlap joint on frame 1, when lifting handle 4, can promote unmanned aerial vehicle 7, make its foot rest liftoff, carry. The limiting member 2 is used for limiting the rotor arm 72 on the vehicle frame 1 so that the unmanned aerial vehicle 7 is hung on the vehicle frame 1.

Specifically, in this embodiment, use unmanned aerial vehicle 7 to explain for eight rotor unmanned aerial vehicle, unmanned aerial vehicle body 71 is the rectangle, and each side all has two rotor arms 72, and the both ends of this side are located respectively to the rotor arm 72 of same side, and like this, every bight correspondence of unmanned aerial vehicle body 71 is equipped with two rotor arms 72, and these two rotor arms 72 are close to with unmanned aerial vehicle body 71's connecting portion. Generally, the two rotor arms 72 for each corner are perpendicular to each other. The limiting members 2 are four in number, the positions of the limiting members 2 on the frame 1 are matched with the connection positions of the rotor arms 72 and the unmanned aerial vehicle body 71, and each limiting member 2 is used for limiting the positions of the rotor arms 72 close to the limiting member 2.

The embodiment of the utility model provides a pair of unmanned aerial vehicle's carrier, when needing transport unmanned aerial vehicle 7, promote the carrier to unmanned aerial vehicle 7 in front, then advance the carrier from rotor arm 72 below with walking wheel 3 in the front, unmanned aerial vehicle body 71 just can block to import and export 14 in, when advancing rotor arm 72 overlap joint on frame 1, and carry out the position through locating part 2 and prescribe a limit to, then use walking wheel 3 as the fulcrum, carry out the lifting so that unmanned aerial vehicle 7's foot rest liftoff with frame 1 through handle 4, thereby realize unmanned aerial vehicle 7's transport. Above-mentioned unmanned aerial vehicle 7's handling only needs alone just can accomplish unmanned aerial vehicle 7's transport, and need not to lift unmanned aerial vehicle 7 and just can place it on the carrier for this carrier has labour saving and time saving and economizes artifical advantage.

Specifically, as shown in fig. 1, in the present embodiment, the vehicle frame 1 includes: two inner tubes 11, two outer tubes 12 and a plurality of cross bars 13. In this embodiment, two inner tubes 11 are arranged in parallel, two outer tubes 12 are arranged in parallel, outer tubes 12 and inner tubes 11 are arranged in parallel, two inner tubes 11 are arranged at intervals and are located between two outer tubes 12, an inner tube 11 and an outer tube 12 on one side of an inlet and outlet 14 are close to each other, an inner tube 11 and an outer tube 12 on the other side of the inlet and outlet 14 are close to each other, cross bars 13 are perpendicular to the outer tubes 12 and the inner tubes 11, a plurality of cross bars 13 are arranged at intervals, and the cross bars 13 are used for connecting the two inner tubes 11 and the two outer tubes 12 together, so that an inlet and outlet 14 is formed.

Each inner tube 11 sets up rather than adjacent outer tube 12 clearance, and the clearance between the inner tube 11 of 14 one side of importing and exporting and outer tube 12 is the same or the same basically with the clearance between the inner tube 11 of 14 opposite sides of importing and exporting and outer tube 12, two walking wheels 3 are located respectively between corresponding inner tube 11 and rather than adjacent outer tube 12, two walking wheels 3 rotate the setting between inner tube 11 and outer tube 12 through the pivot alone like this, thereby guaranteed that the business turn over side of importing and exporting 14 between two inner tubes 11 can supply unmanned aerial vehicle body 71 to freely pass through. In this embodiment, the outer tube 13, the inner tube 11 and the cross bar 13 may be circular tubes or square tubes; can be a solid tube or a hollow tube.

The frame 1 in the embodiment is composed of the outer tube 12, the inner tube 11 and the cross rod 13, so that the frame has the advantages of simple structure, simplicity in manufacturing, low cost and convenience in installation of the walking wheels 3. In this embodiment, the outer tube 12, the inner tube 11 and the cross bar 13 are all steel tubes, which ensures the structural strength and the load-bearing capacity of the frame 1, so that the frame 1 can carry heavy objects. In this embodiment, the number of the cross bars 13 is two, the two cross bars 13 are arranged at intervals, and two ends of the two cross bars 13 are respectively welded with the outer pipe 12 and the inner pipe 11, so that the horizontal pipe, the outer pipe 12 and the inner pipe 11 form a stable quadrilateral structure, and the stability of the size of the inlet and outlet 14 between the two inner pipes 11 is ensured. In other embodiments, the cross bar 13 is welded to the inner tube 11, the cross bar 13 and the outer tube 12 are adjustably positioned by knob screws, or the cross bar 13 and the outer tube 12 are welded, and the cross bar 13 and the inner tube 11 are adjustably positioned by knob screws, so that the size of the inlet and outlet 14 can be adjusted and the walking wheels 3 with different sizes can be adapted.

In other embodiments, the both ends of horizontal pole 13 are equipped with the screw thread section respectively, perhaps horizontal pole 13 is the threaded rod, and the screw thread section is worn to establish with outer tube 12, the activity of inner tube 11, is equipped with locknut on the screw thread section of the both sides of outer tube 12 and inner tube 11 respectively, makes exit 14 size adjustable between two inner tubes 11 like this to can be applicable to the unmanned aerial vehicle 7 of transport variation in size, improve the practicality of this carrier. Of course, the fixing manner between the cross bar 13 and the outer tube 12 and the inner tube 11 can also be adjusted by a knob screw.

In other embodiments, the frame 1 may also be formed by two long plates arranged at intervals and a connecting plate connecting one ends of the two long plates, the two long plates and the connecting plate are U-shaped to form the inlet and outlet 14, and the road wheels 3 are fixed at the bottom of one end of the long plate far away from the connecting plate through bolts.

Specifically, as shown in fig. 1 and fig. 2, a plurality of carriers 5 capable of supporting the rotor arm 72 are further provided on the frame 1, and the carriers 5 are connected to the limiting member 2. The carrier 5 is used to raise the height of the rotor arm 72 on the frame 1 so that it can be adapted to unmanned aerial vehicles 7 carrying foot rests of different heights. When the height of the carriage 1 is insufficient to suspend the drone 7, the rotor arm 72 of the drone 7 may be piggybacked onto the carrier 5.

In this embodiment, the limiting member 2 is a blocking pipe, preferably a steel pipe, for preventing the unmanned aerial vehicle from separating from the frame 1 when the frame 1 is in an inclined transportation state. Preferably, one end of the blocking tube is vertically arranged on the frame 1, and particularly, one end of the blocking tube is vertically welded on the inner tube 11. In the present embodiment, the cross bar 13, the outer tube 12, the inner tube 11 and the blocking tube may be hollow tubes, or may be solid tubes, preferably hollow tubes, which can effectively reduce the weight and cost of the truck. Of course, in order to ensure the load-bearing capacity of the frame 1, the inner tube 11 may preferably be a solid tube.

In the present embodiment, the carrier 5 is provided on the frame 1 at one end and on the blocking tube at the other end with a step formed therebetween for supporting the rotor arm 72. Specifically, hold carrier 5 and block that the step that forms between the pipe is higher than the upper surface of frame 1, can reduce the height that frame 1 need be raised like this, also can be when raising the height and receive the time limit, support the higher unmanned aerial vehicle 7 of height, use walking wheel 3 as the fulcrum promptly, when raising frame 1, need not to make frame 1 lift too high just can make unmanned aerial vehicle 7's foot rest break away from ground, sparingly strength to unmanned aerial vehicle 7's transport.

Specifically, as shown in fig. 2, the carrier 5 includes: a first riser 51 and a second riser 52 parallel to each other, and a first cross plate 53 and a second cross plate 54 parallel to each other. Wherein, one end of the first vertical plate 51 is connected on the frame 1, the other end of the first vertical plate 51 is vertically connected with one end of the first transverse plate 53, the other end of the first transverse plate 53 is vertically connected with one end of the second vertical plate 52, the other end of the second vertical plate 52 is vertically connected with one end of the second transverse plate 54, and the first transverse plate 53, the second vertical plate 52 and the second transverse plate 54 form a U-shaped plate. Wherein, the end of the blocking tube far away from the frame 1 passes through the first cross plate 53 and abuts on the second cross plate 54, so that the supporting member 5 and the blocking tube are stably fixed.

In the present embodiment, the carrier 5 is integrally formed, preferably made of sheet metal, such as by stamping, for example, stainless steel, carbon steel or aluminum alloy. The bearing part 5 is firstly sleeved on the blocking pipe through the first transverse plate 53, the upper end face of the blocking pipe abuts against the inner side of the second transverse plate 54, and then one end of the first vertical plate 51 is welded with the inner pipe 11, so that the bearing part 5 is installed, and the bearing part has the advantages of convenience in installation and firmness. In other embodiments, the carrier 5 may also be a supporting steel tube, one end of which is welded perpendicularly to the barrier tube. Or, the carrier 5 may also be made of wood or plastic material, and specifically may support the weight of the drone 7.

In this embodiment, frame 1, locating part 2 and carrier 5 all adopt the steel material to make, and material source is single like this, acquires convenience and simple manufacture, adopts the steel material to have the advantage that structural strength is high moreover, can effectively bear unmanned aerial vehicle 7's weight.

In this embodiment, locating part 2 and carrier 5 all weld with frame 1, through the welded mode, have guaranteed that locating part 2 and carrier 5 install the fastness on frame 1, have effectively prevented at transport unmanned aerial vehicle 7 in-process, appear not hard up or the risk that drops, protect unmanned aerial vehicle 7 not receive the damage.

In other embodiments, as shown in fig. 4, the limiting member 2 is slidably disposed on the frame 1, and is fixed in position by fastening 8 members, such as a knob screw, specifically, the limiting member 2 is a T-shaped steel tube, and includes a first horizontal tube 21 sleeved on the inner tube 11 and a first vertical tube 22 disposed on the first horizontal tube 21, the knob screw is in threaded connection with the first horizontal tube 21 and abuts against the inner tube 11, so as to limit the movement of the first horizontal tube 21, so as to adjust the distance between the limiting member 2 and the road wheel 3, when the limiting member 2 is far from the road wheel 3, the transportation vehicle can transport the unmanned aerial vehicle 7 with the rotor arm 72 far from the ground, and when the limiting member 2 is far from the road wheel 3, the transportation vehicle can transport the unmanned aerial vehicle 7 with the closer rotor arm 72 far from the ground.

In other embodiments, the bearing member 5 is slidably disposed on the limiting member 2 and fixed in position by a fastening member 8 such as a knob screw, specifically, the bearing member 5 is also a T-shaped steel pipe, the bearing member 5 includes a second vertical pipe 56 sleeved on the blocking pipe and a second horizontal pipe 55 disposed on the second vertical pipe 56, the second vertical pipe 56 is fixed on the blocking pipe by the knob screw, and the distance between the bearing member 5 and the inner pipe 11 is adjusted to adjust the height of the supporting surface of the bearing member 5, so as to be suitable for carrying the unmanned aerial vehicles 7 with different heights.

In other embodiments, the bearing member 5 is in threaded connection with the limiting member 2, specifically, the limiting member 2 is a screw rod, specifically, the first vertical tube 22 is a screw rod, the bearing member 5 is a supporting block 57 in threaded connection with the screw rod, a baffle 58 is disposed on the supporting block 57, a placement groove 59 for placing the rotor arm 72 is formed between the baffle 58 and the screw rod, after the rotor arm 72 is placed in the placement groove 59, the baffle 58 can cooperate with the rotor arm 72 to prevent the supporting block 57 from rotating, so that the stability of the supporting block 57 staying at the current position and the stability of the rotor arm 72 placed on the bearing block 57 are ensured.

Specifically, as shown in fig. 1 and 3, in the present embodiment, the handle 4 is integrally formed with the inner tube 11, and two handles 4 are provided, so that the handle 4 does not need to be manufactured and installed separately, thereby saving manufacturing time and cost. Specifically, each handle 4 is provided with a strap 6, and the straps 6 are respectively used for being hung on the shoulders of workers and reducing the force and gas applied to the handles 4 by the hands of the workers, so that the labor intensity of the workers for pulling or lifting the carrier can be reduced, and the labor force is saved. The handle 4 can be further provided with an anti-slip sleeve, the anti-slip sleeve is made of rubber or plastic materials and used for increasing the friction force between a hand and the handle 4, and anti-slip convex points or anti-slip grooves can be further arranged on the anti-slip sleeve so as to ensure the stability of a worker holding the handle 4.

In this embodiment, the traveling wheels 3 are preferably pneumatic wheels, so that the truck can be applied to rough road surfaces, and has good shock absorption effect and light weight. A shock absorbing pad such as a rubber pad may also be provided on carrier 5 to increase the stability of the placement of the rotor arm 72 on carrier 5 and to prevent friction between the rotor arm 72 and carrier 5 from scratching the rotor arm 72. Of course, when the carrier is applied to the transfer of articles in the warehouse, the traveling wheels 3 adopt silent rubber wheels, so that the noise in the warehouse can be reduced. Of course, walking wheel 3 can also adopt brake type universal wheel, when climbing the transport, when the workman has tired, can also stably stop on domatic, makes things convenient for the workman to have a rest. In this embodiment, the traveling wheels 3 are very convenient to install, so that different kinds of traveling wheels 3 can be selected according to practical application scenarios.

In this embodiment, the size of walking wheel 3 can be selected according to unmanned aerial vehicle 7's size, and when rotor arm 72 was higher apart from ground, the great walking wheel 3 of diameter was selected to walking wheel 3, and when rotor arm 72 was lower apart from ground, the less walking wheel 3 of diameter was selected to walking wheel 3. The diameter of the road wheels 3 is sized to pass under the rotor arms 72.

In this embodiment, can be applicable to the unmanned aerial vehicle 7 of transport equidimension not through the size that changes walking wheel 3, the interval between two inner tubes 11, horizontal pole 13 to the interval of walking wheel 3, the length of locating part 2 and apart from walking wheel 3 to the position and the height that holds carrier 5 for this carrier has adaptability reinforce, change mode polytype's advantage.

The carrier provided by the embodiment of the utility model has the advantages of simple structure, easy operation and low processing cost; meanwhile, when the carrier is used, the unmanned aerial vehicle 7 can be easily carried by only one person, and the unmanned aerial vehicle 7 can be carried to the carrier by multiple persons, so that labor and force are saved; the carrier adopts a lever principle, takes the two walking wheels 3 as pivots, and the distance between the handle 4 and the walking wheels 3 is far greater than the distance from the gravity center of the unmanned aerial vehicle 7 to the walking wheels 3, so that the multi-rotor 73 unmanned aerial vehicle 7 can be easily lifted to a certain height, a foot rest on the unmanned aerial vehicle body 71 is enabled to be away from the ground, and then the carrier can be pushed or pulled by hand to walk; through two travelling wheels 3 and braces 6, the carrier can be pushed and pulled, has high moving speed and flexible steering, and saves strength.

The above description is only exemplary of the present invention and should not be taken as limiting the scope of the present invention, as any modifications, equivalents, improvements and the like made within the spirit and principles of the present invention are intended to be included within the scope of the present invention.

Claims (10)

1. A cart for a drone, the drone comprising: unmanned aerial vehicle body and rotor arm, its characterized in that includes: be used for carrying the frame of rotor arm with locate locating part on the frame, the one end of frame has and supplies the exit of accessible business turn over of unmanned aerial vehicle body, the other end of frame is equipped with the handle, keep away from on the frame the one end of handle is equipped with running gear, based on same reference surface, the height that highly is less than the rotor arm of treating transport unmanned aerial vehicle of frame, the locating part is used for will during the frame slope the rotor arm restriction is in so that unmanned aerial vehicle hangs on the frame.

2. The cart for unmanned aerial vehicle according to claim 1, wherein: the frame includes: the two inner pipes are arranged at intervals and are positioned between the two outer pipes, and the two inner pipes and the two outer pipes are connected through the plurality of cross rods, so that the inlet and the outlet are formed between the two inner pipes.

3. The cart for unmanned aerial vehicle of claim 2, wherein: the two inner tubes are parallel, the two outer tubes are parallel, the inner tubes are parallel to the outer tubes, and the inner tubes and the outer tubes are perpendicular to the cross rod.

4. The cart for unmanned aerial vehicle of claim 3, wherein: the cross bar is welded with the inner pipe and/or the outer pipe; or the cross bar is movably connected with the inner pipe and/or the outer pipe, so that the fixed positions of the cross bar and the inner pipe and/or the outer pipe can be adjusted, and the width of the inlet and the outlet can be adjusted.

5. The cart for unmanned aerial vehicle of claim 3, wherein: the inner pipes are arranged at intervals with the adjacent outer pipes, and the two walking mechanisms are respectively arranged between the adjacent inner pipes and the adjacent outer pipes.

6. The cart for unmanned aerial vehicle of claim 2, wherein: the frame is also provided with a plurality of bearing parts capable of supporting the rotor arms, and the bearing parts are connected with the limiting parts.

7. The cart for unmanned aerial vehicle of claim 6, wherein: the locating part is for stopping the pipe, the one end that stops the pipe is located on the frame, hold carrier one end and locate on the frame, the other end locate stop on the pipe and with stop and form the step that is used for supporting between the pipe the rotor arm.

8. The cart for unmanned aerial vehicle of claim 7, wherein: the carrier includes: first riser and the second riser that is parallel to each other to and first diaphragm and the second diaphragm that is parallel to each other, the one end of first riser is connected on the frame, the other end of first riser with the one end of first diaphragm is connected, the other end of first diaphragm with the one end of second riser is connected, the other end of second riser with the one end of second diaphragm is connected, keep away from the pipe the one end of frame is passed first diaphragm and butt are in on the second diaphragm.

9. The cart for unmanned aerial vehicle of claim 6, wherein: the handle and the inner tube are integrally formed, and a strap is arranged on the handle.

10. The cart for unmanned aerial vehicle of claim 6, wherein: the locating part is arranged on the frame in a sliding mode and is fixed in position through a fastener, the bearing part is arranged on the locating part in a sliding mode and is fixed in position through the fastener, or the bearing part is in threaded connection with the locating part.

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