CN114162310A

CN114162310A - Unmanned aerial vehicle with self-adaptation undercarriage

Info

Publication number: CN114162310A
Application number: CN202210061071.7A
Authority: CN
Inventors: 陆俏; 李多姿
Original assignee: Shenzhen Liyi Technology Co ltd
Current assignee: Shenzhen Liyi Technology Co ltd
Priority date: 2022-01-19
Filing date: 2022-01-19
Publication date: 2022-03-11

Abstract

The invention belongs to the technical field of unmanned aerial vehicles, and discloses an unmanned aerial vehicle with a self-adaptive undercarriage. This unmanned aerial vehicle with self-adaptation undercarriage, including unmanned aerial vehicle, the equal fixed mounting in both ends has the undercarriage, two about the lower surface in the unmanned aerial vehicle all be provided with floating mechanism on the undercarriage, two the left and right sides of undercarriage all is provided with fixed establishment, two both sides all are provided with buffer gear around the undercarriage. This unmanned aerial vehicle with self-adaptation undercarriage, the person of controlling control rectangular plate cooperation hinge after the lapse, start the aspiration pump, inflate the air cushion, descend behind the pond as unmanned aerial vehicle, electronic slide bar top shoe drives waterproof box and moves down, operating personnel starts the motor and cooperates the transfer line to drive the running wheel and rotate, key control removes unmanned aerial vehicle to the bank on through the control handle, avoid unmanned aerial vehicle to descend and appear in the unable circumstances of picking up of aquatic, unmanned aerial vehicle has also been realized descending in aquatic.

Description

Unmanned aerial vehicle with self-adaptation undercarriage

Technical Field

The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle with a self-adaptive undercarriage.

Background

An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.

Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.

But most unmanned aerial vehicle now does not have level ground when usual landing when carrying out field shooting, irregular ground such as mountain region, sloping ground, pond can appear, unmanned aerial vehicle undercarriage in the past can only adapt to land in the level land, comparatively single, and when the level land is descended, because of most current undercarriage does not possess the buffering effect, can cause the damage to unmanned aerial vehicle inner member, consequently, we need an unmanned aerial vehicle who has self-adaptation undercarriage urgently.

Disclosure of Invention

The invention aims to provide an unmanned aerial vehicle with a self-adaptive undercarriage, which is suitable for landing on various grounds and has a buffering effect on landing of the unmanned aerial vehicle.

In order to achieve the purpose, the invention is realized by the following technical scheme: the utility model provides an unmanned aerial vehicle with self-adaptation undercarriage, includes unmanned aerial vehicle, the equal fixed mounting in both ends has the undercarriage, two about the lower surface in the unmanned aerial vehicle all be provided with floating mechanism on the undercarriage, two the left and right sides of undercarriage all is provided with fixed establishment, two both sides all are provided with buffer gear around the undercarriage.

Preferably, including the rectangular block, two in the floating mechanism the equal fixed mounting of rectangular block is at the lower surface of undercarriage, two the U-shaped groove has all been seted up in the rectangular block, two the left and right sides in the U-shaped inslot all is provided with the rectangular plate, and four one side that the rectangular plate just corresponds U-shaped inslot wall all is through hinge and U-shaped inslot wall swing joint, four the sliding tray has all been seted up in one side of rectangular plate and be close to U-shaped inslot wall.

Preferably, sliding connection has the slider in the sliding tray, the slider just is close to the equal fixed mounting in one side of U-shaped inslot wall has the go-between, the upper end of U-shaped inslot left and right sides inner wall all is provided with go-between one, be provided with the spring stay cord between go-between and the go-between one, and the both ends of spring stay cord respectively with go-between and go-between swing joint, two the rectangle board just keeps away from one of U-shaped inslot wall and serves equal fixed mounting and have the magnetism gag lever post, the magnetism spacing groove has all been seted up on U-shaped inslot left and right sides inner wall upper end and the corresponding magnetism gag lever post.

Preferably, a first cavity is formed in each of the two rectangular plates, an inflator pump is fixedly connected in each of the two first cavities through a support rod, air cushions are fixedly mounted at one ends of the two rectangular plates, which are far away from the U-shaped groove, and are in a square design, air inlets are fixedly communicated with the output ends of the air pumps and the corresponding air cushions, air outlet valves are respectively arranged on the two air cushions, a vertical rod is fixedly mounted at the rear side of the unmanned aerial vehicle, an electric slide rod is arranged on the vertical rod, a first slide block is connected on the electric slide rod in a sliding manner, the rear end of the first slide block is movably connected with a waterproof box through a movable rod, a motor is fixedly connected in the waterproof box through a support rod, and a magnetic limit rod is arranged, so that an operator can conveniently reset fast elements when resetting, the recovery time is saved, and the stability of the magnetic limit rod is high, the falling-off condition can not occur.

Preferably, the output end of the motor is fixedly connected with one end of a transmission rod through a coupler, the other end of the transmission rod extends outwards through an inner bearing with a corresponding through hole arranged on the waterproof box and is fixedly connected with a rotating wheel, the fixing mechanism comprises two transverse plates which are respectively and fixedly arranged at the left side and the right side of the bracket, two cavities II are respectively arranged in the two transverse plates, electric slide rails I are respectively arranged at the front end and the rear end in the two cavities II, slide blocks II are respectively and slidably connected in the two electric slide rails I, driving plates are respectively and fixedly connected at the opposite side surfaces of the two slide blocks II, dust covers are fixedly arranged on the upper surfaces of the two transverse plates and the rear ends of the two transverse plates, and rotating wheels are arranged, can make unmanned aerial vehicle descend behind the aquatic, can carry out the control of marcing all around to unmanned aerial vehicle through the handle, can make things convenient for the operator to retrieve the unmanned aerial vehicle of descending in the aquatic.

Preferably, there is a first motor through a second fixed mounting of the bracket in the dust cover, the output end of the first motor is connected with the top of the first transmission rod through a first coupling, and the bottom of the first transmission rod is connected with a second hydraulic rod through a first inner bearing of the corresponding through hole and extending downwards, the output end of the hydraulic rod is connected with the second inner bearing of the mounting bearing seat of the corresponding through hole on the driving plate in a rotating manner, the bottom end of the hydraulic rod is fixedly provided with a first bevel gear below the driving plate, the inner walls of the front side and the rear side of the transverse plate are provided with a second sliding groove and a third sliding block in the second sliding groove in a sliding manner, the inner bottom wall of the second sliding groove is fixedly provided with one end of a spring, and the other end of the spring is fixedly mounted with the third sliding block.

Preferably, be provided with the dwang between two slider three and be located the diaphragm, and the both ends of dwang all with correspond the slider three go up to set up and correspond three inner bearing of through-hole and rotate and be connected, be provided with a plurality of bevel gear two on the dwang, and be located left first bevel gear two and bevel gear meshing, a plurality of bevel gear two's below all meshes bevel gear three, all is provided with the staple in a plurality of bevel gear three, the lower surface of diaphragm just corresponds the staple position and all is provided with the export, through setting up a plurality of staples, can descend when topography such as mountain region, and the cooperation motor drives and drills ground to guarantee the stability that unmanned aerial vehicle descended at mountain region topography.

Preferably, both sides all are provided with electronic slide rail three around the diaphragm, and two equal sliding connection has the mount in the electronic slide rail three, including the support frame in the buffer gear, both ends, two around the support frame is fixed mounting respectively in the support the equal fixed mounting of lower surface of support frame has the hydraulic stem, two the equal fixedly connected with spring plate of output of hydraulic stem, the lower fixed surface of spring plate installs the slipmat, through setting up the spring plate, can obtain a fine buffering when descending, and the slipmat can increase the friction with ground to guarantee the more steady descending of unmanned aerial vehicle.

Preferably, unmanned aerial vehicle's lower surface is provided with the observation pole, the bottom of observation pole is provided with the camera, unmanned aerial vehicle's lower surface just is located the observation pole rear side and is provided with the data control case, all equal electric wires of unmanned aerial vehicle component and output control case electric connection, unmanned aerial vehicle upper element all is equipped with water proof coating, the observation pole adopts for electric putter, through control box transmission data to handle back, and flexible from top to bottom through handle control observation pole sets up the observation pole and can effectually observe descending topography to the person of conveniently controlling is to unmanned aerial vehicle's control.

By adopting the technical scheme, the invention has the beneficial effects that:

1. this unmanned aerial vehicle with self-adaptation undercarriage, when unmanned aerial vehicle descends when the pond, the camera observes behind the waters on the observation pole, with data transmission behind the data control case and transmit behind the liquid crystal display on the person's of controlling control handle, person's of controlling control rectangular plate cooperation hinge lapse and contact back, start the aspiration pump, inflate the air cushion, descend behind the pond when unmanned aerial vehicle, electronic slide bar top shoe drives the waterproof box lapse, operating personnel starts the motor and cooperates the transfer line to drive and rotate the wheel rotation, it removes unmanned aerial vehicle to the bank to pass through button control on the control handle, avoid the condition that unmanned aerial vehicle descending can't be picked up in aqueous to appear, unmanned aerial vehicle has also been realized descending in aqueous.

2. This unmanned aerial vehicle with self-adaptation undercarriage, when unmanned aerial vehicle descends in the ground that has the inclination such as hillside, observe behind the hillside on the pole camera, with data transmission behind the data control case and transmit behind the LCD screen on the person's of controlling control handle, when operating personnel controlled in the diaphragm on the electronic slide rail one drive the board downstream on two, with the output downstream of hydraulic stem, and starter motor one, motor one drives a plurality of bevel gears and rotates, move the staple out behind the diaphragm, and rotate the soil, it is fixed to form, both sides are fixed around to three mounts on the outside electronic slide rail, avoid the unmanned aerial vehicle landing, thereby realized the landing of unmanned aerial vehicle on the inclined land such as hillside, thereby avoid the unmanned aerial vehicle landing to lead to the condition appearance of damage.

3. This unmanned aerial vehicle with self-adaptation undercarriage when needs descend, the operating personnel with hydraulic stem downstream on the support frame, the last slipmat contact ground of spring board to play the cushioning effect, avoid unmanned aerial vehicle overweight and the condition that leads to the internal component to damage when descending takes place.

Drawings

FIG. 1 is a schematic view of the overall structure of the present invention;

FIG. 2 is a schematic diagram of a rectangular block structure according to the present invention;

FIG. 3 is a schematic view of a vertical bar according to the present invention;

FIG. 4 is a schematic diagram of a cross plate structure according to the present invention.

In the figure: 1 unmanned aerial vehicle, 2 landing gear, 3 floating mechanism, 4 fixing mechanism, 5 buffer mechanism, 31 rectangular block, 32U-shaped groove, 33 rectangular plate, 34 sliding groove, 35 sliding block, 36 connecting ring, 37 connecting ring I, 38 spring pull rope, 39 magnetic limiting rod, 310 magnetic limiting groove, 311 cavity I, 312 air pump, 313 air cushion, 314 air outlet valve, 315 vertical rod, 316 electric sliding rod, 317 sliding block I, 318 waterproof box, 319 motor, 320 transmission rod, 321 rotating wheel, 41 horizontal plate, 42 cavity II, 43 electric sliding rail I, 44 sliding block II, 45 driving plate, 46 dust cover, 47 motor I, 48 transmission rod I, 49 hydraulic rod, 410 bevel gear I, 411 sliding block II, 412 sliding block III, 413 spring, rotating rod, 415 bevel gear II, 416 bevel gear III, 417 fixing nail, 418 outlet, 419 electric sliding rail III, 420 fixing frame, 51 supporting frame, 52 hydraulic rod, 53 spring plate, 54 antiskid pad, 6 observation poles, 7 cameras, 8 data control boxes.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

In the description of the present invention, it is to be understood that the terms "central," "longitudinal," "lateral," "length," "width," "thickness," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," "clockwise," "counterclockwise," "axial," "radial," "circumferential," and the like are used in the orientations and positional relationships indicated in the drawings for convenience in describing the invention and to simplify the description, and are not intended to indicate or imply that the referenced devices or elements must have a particular orientation, be constructed and operated in a particular orientation, and are therefore not to be considered limiting of the invention.

In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," "secured," and the like are to be construed broadly and can, 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 meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.

Referring to fig. 1-4, the present invention provides a technical solution: an unmanned aerial vehicle with a self-adaptive landing gear comprises an unmanned aerial vehicle 1, landing gears 2 are fixedly arranged at the left end and the right end of the inner lower surface of the unmanned aerial vehicle 1, floating mechanisms 3 are arranged on the two landing gears 2, fixing mechanisms 4 are arranged at the left side and the right side of the two landing gears 2, buffer mechanisms 5 are arranged at the front side and the rear side of the two landing gears 2, rectangular blocks 31 are arranged in the floating mechanisms 3, two rectangular blocks 31 are fixedly arranged on the lower surface of the landing gears 2, U-shaped grooves 32 are formed in the two rectangular blocks 31, rectangular plates 33 are arranged at the left side and the right side of the two U-shaped grooves 32, one sides of the four rectangular plates 33 corresponding to the inner walls of the U-shaped grooves 32 are movably connected with the inner walls of the U-shaped grooves 32 through hinges, sliding grooves 34 are formed in one sides of the four rectangular plates 33 and close to the inner walls of the U-shaped grooves 32, sliding blocks 35 are connected in the sliding grooves 34 in a sliding mode, connecting rings 36 are fixedly arranged at one sides of the sliding blocks 35 and close to the inner walls of the U-shaped grooves 32, the upper ends of the inner walls of the left side and the right side of the U-shaped groove 32 are respectively provided with a connecting ring I37, a spring pull rope 38 is arranged between the connecting ring 36 and the connecting ring I37, two ends of the spring pull rope 38 are respectively movably connected with the connecting ring 36 and the connecting ring I37, one ends of the two rectangular plates 33 far away from the inner wall of the U-shaped groove 32 are respectively and fixedly provided with a magnetic limiting rod 39, the upper ends of the inner walls of the left side and the right side of the U-shaped groove 32 are respectively provided with a magnetic limiting groove 310 corresponding to the magnetic limiting rod 39, two rectangular plates 33 are respectively provided with a cavity I311, two cavities I311 are respectively and fixedly connected with an inflator pump 312 through a support rod, one ends of the two rectangular plates 33 far away from the U-shaped groove 32 are respectively and fixedly provided with air cushions 313, the two air cushions 313 are in a square design, the output end of the ejector pump 312 is fixedly communicated with the corresponding air cushion 313, two air cushions 313 are respectively provided with an air outlet valve 314, the rear side of the unmanned aerial vehicle 1 is fixedly provided with a vertical rod 315, an electric slide bar 316 is arranged on the vertical bar 315, a first slide block 317 is connected on the electric slide bar 316 in a sliding way, the rear end of the first sliding block 317 is movably connected with a waterproof box 318 through a movable rod, a motor 319 is fixedly connected in the waterproof box 318 through a first supporting rod, the output end of the motor 319 is fixedly connected with one end of a transmission rod 320 through a coupling, the other end of the transmission rod 320 extends outwards through a bearing in the corresponding through hole formed in the waterproof box 318 and is fixedly connected with a rotating wheel 321, the fixing mechanism 4 comprises two transverse plates 41, the two transverse plates 41 are respectively and fixedly installed on the left side and the right side of the support 1, two cavities 42 are formed in the two transverse plates 41, electric sliding rails 43 are arranged at the front end and the rear end in the two cavities 42, sliding blocks 44 are connected in the two electric sliding rails 43 in a sliding mode, driving plates 45 are fixedly connected to opposite side faces of the two sliding blocks 44, and dust covers 46 are fixedly installed on the upper surfaces of the two transverse plates 41 and the rear ends of the two transverse plates 41;

a first motor 47 is fixedly arranged in the dust cover 46 through a second bracket, the output end of the first motor 47 is fixedly connected with the top end of a first transmission rod 48 through a first coupling, the bottom end of the first transmission rod 48 is provided with a corresponding through hole, a first inner bearing, which extends downwards, and is fixedly connected with a hydraulic rod 49, the output end of the hydraulic rod 49 is rotatably connected with a second inner bearing, which is provided with a corresponding through hole, on the driving plate 45, the bottom end of the hydraulic rod 49 is fixedly provided with a first bevel gear 410 below the driving plate 45, the inner walls of the front side and the rear side of the transverse plate 41 and is positioned below the first electric slide rail 43 are provided with a second slide block 411, a third slide block 412 is slidably connected in the two second slide blocks 411, one end of a spring 413 is fixedly arranged on the inner bottom walls of the two slide blocks 411, the other end of the spring 413 is fixedly arranged with the corresponding third slide block 412, a rotating rod 414 is arranged between the two slide blocks 412 and is arranged in the transverse plate 41, two ends of the rotating rod 414 are rotatably connected with three inner bearings with corresponding through holes arranged on a corresponding slider three 412, a plurality of bevel gear two 415 are arranged on the rotating rod 414, the first bevel gear two 415 positioned on the left side is meshed with the bevel gear one 410, bevel gear three 416 is meshed below the bevel gear two 415, fixing nails 417 are arranged in the bevel gear three 416, outlets 418 are arranged on the lower surface of the transverse plate 41 and corresponding to the fixing nails 417, electric slide rails three 419 are arranged on the front side and the rear side of the transverse plate 41, fixing frames 420 are slidably connected in the two electric slide rails three 419, a supporting frame 51 is arranged in the buffering mechanism 5, the supporting frame 51 is fixedly arranged at the front end and the rear end of the bracket 1 respectively, hydraulic rods 52 are fixedly arranged on the lower surfaces of the two supporting frames 51, spring plates 53 are fixedly connected at the output ends of the two hydraulic rods 52, and anti-skid pads 54 are fixedly arranged on the lower surfaces of the spring plates 53, unmanned aerial vehicle 1's lower surface is provided with observation pole 6, and the bottom of observation pole 6 is provided with camera 7, and unmanned aerial vehicle 1's lower surface just is located 6 rear sides of observation pole and is provided with data control box 8, and the equal electric wire of 1 all components of unmanned aerial vehicle and 8 electric connection of output control box, the component all is equipped with water proof coating on unmanned aerial vehicle 1, and observation pole 6 adopts for electric putter.

When the unmanned aerial vehicle with the self-adaptive landing gear works, when the unmanned aerial vehicle 1 lands on a pond, after the camera 7 on the observation rod 6 observes a water area, data is transmitted to the data control box 8 and is transmitted to the liquid crystal screen on the control handle of an operator, the operator controls the rectangular plate 33 to be matched with the hinge to move downwards and then is connected with the hinge, the air suction pump 312 is started to inflate the air cushion 313, when the unmanned aerial vehicle 1 lands on the pond, the sliding block I317 on the electric sliding rod 316 drives the waterproof box 318 to move downwards, an operator starts the motor 319 and is matched with the transmission rod 320 to drive the rotating wheel 321 to rotate, the unmanned aerial vehicle is moved to the shore through the control of the key on the control handle, after the unmanned aerial vehicle is taken out, the air outlet valve 314 on the air cushion 313 is opened to deflate, the element is reset, when the unmanned aerial vehicle 1 lands on the ground with inclination such as a hillside, after the camera 7 on the observation rod 6 observes the hillside, the data is transmitted to the data control box 8 and is transmitted to the liquid crystal screen on the control handle of the operator, when an operator controls the driving plate 45 on the inner sliding block two 44 of the electric sliding rail one 43 in the transverse plate 41 to move downwards, the output end of the hydraulic rod 49 moves downwards, the motor one 47 is started, the motor one 47 drives the bevel gears to rotate, the fixing nail 417 is moved out of the transverse plate 41 and rotates the soil to form fixation, the fixing frame 420 on the outer electric sliding rail three 419 fixes the front side and the rear side, when the operator needs to descend, the hydraulic rod 52 on the supporting frame 51 moves downwards, and the anti-skid pad on the spring plate 53 contacts the ground.

It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. An unmanned aerial vehicle with adaptive undercarriage, includes unmanned aerial vehicle (1), its characterized in that: the unmanned aerial vehicle is characterized in that landing gears (2) are fixedly mounted at the left end and the right end of the inner lower surface of the unmanned aerial vehicle (1), two floating mechanisms (3) are arranged on the landing gears (2), two fixing mechanisms (4) are arranged on the left side and the right side of the landing gears (2), and two buffering mechanisms (5) are arranged on the front side and the rear side of the landing gears (2).

2. A drone with an adaptive landing gear according to claim 1, characterised in that: float including rectangular block (31), two in the mechanism (3) equal fixed mounting in rectangular block (31) is at the lower surface of undercarriage (2), two U-shaped groove (32), two have all been seted up in rectangular block (31) the left and right sides in U-shaped groove (32) all is provided with rectangular plate (33), and four one side that rectangular plate (33) and corresponding U-shaped groove (32) inner wall all is through hinge and U-shaped groove (32) inner wall swing joint, four sliding tray (34) have all been seted up in one side that just is close to U-shaped groove (32) inner wall of rectangular plate (33).

3. A drone with an adaptive landing gear according to claim 2, characterised in that: sliding connection has slider (35) in sliding tray (34), the equal fixed mounting in one side that slider (35) just are close to U-shaped groove (32) inner wall has go-between (36), the upper end of U-shaped groove (32) left and right sides inner wall all is provided with go-between (37), be provided with spring stay cord (38) between go-between (36) and go-between (37), and the both ends of spring stay cord (38) respectively with go-between (36) and go-between (37) swing joint, two equal fixed mounting has magnetism gag lever post (39) on rectangular plate (33) and the one end of keeping away from U-shaped groove (32) inner wall, all seted up magnetism gag lever post (310) on U-shaped groove (32) left and right sides inner wall upper end and the corresponding magnetism gag lever post (39).

4. A drone with an adaptive landing gear according to claim 3, characterised in that: the two rectangular plates (33) are internally provided with a first cavity (311), the two first cavities (311) are fixedly connected with an inflator pump (312) through a support rod, air cushions (313) are fixedly arranged at one ends of the two rectangular plates (33) far away from the U-shaped groove (32), the two air cushions (313) are designed in a square shape, the output end of the air pump (312) is fixedly communicated with the air inlets formed on the corresponding air cushions (313), the two air cushions (313) are both provided with air outlet valves (314), a vertical rod (315) is fixedly installed on the rear side of the unmanned aerial vehicle (1), an electric sliding rod (316) is arranged on the vertical rod (315), a first sliding block (317) is connected onto the electric sliding rod (316) in a sliding manner, the rear end of the first sliding block (317) is movably connected with a waterproof box (318) through a movable rod, the waterproof box (318) is internally fixedly connected with a motor (319) through a support rod.

5. A drone with an adaptive landing gear according to claim 4, characterised in that: the output end of the motor (319) is fixedly connected with one end of a transmission rod (320) through a coupling, the other end of the transmission rod (320) is provided with a corresponding through hole through the waterproof box (318), the inner bearing extends outwards and is fixedly connected with a rotating wheel (321), including two diaphragm (41), two in fixed establishment (4) diaphragm (41) fixed mounting is respectively in the left and right sides of support (1), two cavity two (42), two have all been seted up in diaphragm (41) both ends all are provided with electronic slide rail one (43), two around in cavity two (42) equal sliding connection has slider two (44), two in electronic slide rail one (43) the equal fixedly connected with in the opposite flank of slider two (44) drives movable plate (45), two fixed mounting has dust cover (46) on the upper surface of diaphragm (41) just is located the rear end.

6. A drone with an adaptive landing gear according to claim 5, characterised in that: a first motor (47) is fixedly installed in the dust cover (46) through a second support, the output end of the first motor (47) is fixedly connected with the top end of a first transmission rod (48) through a first coupler, the bottom end of the first transmission rod (48) is provided with a first inner bearing corresponding to a through hole and fixedly connected with a hydraulic rod (49) in a downward extending manner through a transverse plate (41), the output end of the hydraulic rod (49) is rotatably connected with a second inner bearing corresponding to a through hole and arranged in a bearing seat arranged on a driving plate (45), the bottom end of the hydraulic rod (49) is fixedly installed below the driving plate (45) and provided with a first bevel gear (410), the inner walls of the front side and the rear side of the transverse plate (41) are provided with a second sliding groove (411) below an electric sliding rail (43), a third sliding block (412) is slidably connected in the two sliding grooves (411), and one end of a spring (413) is fixedly installed on the inner bottom wall of the two sliding grooves (411), and the other end of the spring (413) is fixedly installed with the corresponding sliding block III (412).

7. A drone with an adaptive landing gear according to claim 6, characterised in that: between two slider three (412) and be located diaphragm (41) and be provided with dwang (414), and the both ends of dwang (414) all with correspond to set up on slider three (412) and correspond three inner bearing three rotation connection of through-hole, be provided with a plurality of bevel gear two (415) on dwang (414), and be located left first bevel gear two (415) and bevel gear one (410) meshing, a plurality of the below of bevel gear two (415) all meshes bevel gear three (416), all is provided with staple (417) in a plurality of bevel gear three (416), the lower surface of diaphragm (41) just corresponds staple (417) position and all is provided with export (418).

8. A drone with an adaptive landing gear according to claim 7, characterised in that: all be provided with three (419) of electronic slide rail around diaphragm (41), and two equal sliding connection has mount (420) in three (419) of electronic slide rail, including support frame (51) in buffer gear (5), both ends, two around support frame (51) fixed mounting is in support (1) respectively the lower surface of support frame (51) is equal fixed mounting has hydraulic stem (52), two the equal fixedly connected with spring plate (53) of output of hydraulic stem (52), the lower fixed mounting of spring plate (53) has slipmat (54).

9. A drone with an adaptive landing gear according to claim 1, characterised in that: the lower surface of unmanned aerial vehicle (1) is provided with observation pole (6), the bottom of observation pole (6) is provided with camera (7), the lower surface of unmanned aerial vehicle (1) just is located observation pole (6) rear side and is provided with data control box (8), the equal electric wire of all components of unmanned aerial vehicle (1) and output control box (8) electric connection, the component all is equipped with water proof coating on unmanned aerial vehicle (1), observation pole (6) adopt for electric putter.