CN115783287A - Fixed electric full-automatic vertical fixed wing airport with centering mechanism - Google Patents

Abstract

The invention relates to an unmanned aerial vehicle airport, and discloses a fixed electric full-automatic vertical fixed wing airport with a centering mechanism, which comprises an airport body, wherein an airport door is arranged on one side of the airport body, an apron body capable of being horizontally moved out from the airport door is arranged in the airport, the apron body comprises an apron base in a square frame shape, an apron bottom plate is arranged in the middle of the apron base, an unmanned aerial vehicle centering mechanism is arranged on the apron base, and the unmanned aerial vehicle centering mechanism comprises a transverse push rod mechanism and a longitudinal push rod mechanism which can push an unmanned aerial vehicle to the center of the apron body. The unmanned aerial vehicle in the airport can be pushed to a required position, so that the unmanned aerial vehicle is effectively ensured to be positioned in the central position of the parking apron body in the airport, and an effective precondition guarantee is provided for the follow-up battery replacement of the unmanned aerial vehicle.

Description

Fixed type electric full-automatic vertical fixed wing airport with centering mechanism

Technical Field

The invention relates to an unmanned aerial vehicle airport, in particular to a fixed type electric full-automatic vertical fixed wing airport with a centering mechanism.

Background

According to unmanned aerial vehicle's flight principle and structure, can roughly divide into many rotor unmanned aerial vehicle and fixed wing unmanned aerial vehicle. Fixed wing unmanned aerial vehicle occupies very big advantage in unmanned aerial vehicle's field because of structural advantage to and the advantage on the flight principle.

In order to avoid unmanned aerial vehicle to take off and land the influence design of in-process ground effect to unmanned aerial vehicle in the prior art and have the special airport that is used for accomodating vertical take-off and landing fixed wing unmanned aerial vehicle, be provided with the air park body in the airport, unmanned aerial vehicle descends and is accomodate to the unmanned aerial vehicle in the airport after on the air park body, unmanned aerial vehicle is in the position on the air park body unfixed in the current unmanned aerial vehicle, need rely on operating personnel to have comparatively accurate operation when stopping and landing unmanned aerial vehicle, just can guarantee that follow-up unmanned aerial vehicle is in the airport and accomodate the regulation position of intracavity, this kind of mode requires higher to the operating personnel who controls unmanned aerial vehicle take off and land, and control is inconvenient, be difficult to guarantee accurate positioning.

Disclosure of Invention

The invention provides a fixed electric full-automatic vertical fixed wing airport with a centering mechanism, aiming at the problems of an unmanned aerial vehicle airport in the prior art.

In order to solve the technical problem, the invention is solved by the following technical scheme:

fixed full-automatic fixed wing airport that hangs down of fixed electric power with centering mechanism, including the airport body, its characterized in that: one side of airport body is equipped with the airport door, is equipped with the air park body that can shift out from airport door department level in the airport, and the air park body is equipped with the air park bottom plate including the air park base that is square frame form at the air park base middle part, air park base, and the air park base is equipped with unmanned aerial vehicle centering mechanism, and unmanned aerial vehicle centering mechanism is including horizontal push rod mechanism and the vertical push rod mechanism that can push away unmanned aerial vehicle to air park body central point department.

Preferably, the transverse pushing rod mechanism comprises two transverse pushing rods which are arranged along the length direction of the parking apron body in the length direction and can move in the opposite direction or the back direction along the width direction of the parking apron body, and the longitudinal pushing rod mechanism comprises two longitudinal pushing rods which are arranged along the width direction of the parking apron body in the length direction and can move in the opposite direction or the back direction along the length direction of the parking apron body.

Preferably, the push rod driving mechanism comprises two groups of push rod driving mechanisms used for respectively driving the transverse push rods and the longitudinal push rods to move, each push rod driving mechanism comprises two drive rod assemblies which are arranged in parallel relatively, two ends of each transverse push rod or each longitudinal push rod are respectively connected to the drive rod assemblies at two corresponding sides, each drive rod assembly comprises a push rod driving wheel and a left-handed screw rod and a right-handed screw rod which are arranged at two sides of the corresponding push rod driving wheel and connected through a coupler, and the two transverse push rods or the two longitudinal push rods which move oppositely or reversely are respectively in threaded connection with the left-handed screw rods and the right-handed screw rods. The mode of screw rod transmission can make the promotion of push rod more accurate, guarantees the push rod to the accurate nature of unmanned aerial vehicle promotion stroke.

Preferably, the push rod driving mechanism comprises a push rod driving motor, a driving rotating shaft is connected to a motor shaft of the push rod driving motor, two driving synchronizing wheels are arranged on the driving rotating shaft, the push rod driving mechanism further comprises a driven rotating shaft, two driven synchronizing wheels are arranged on the driven rotating shaft, one driving synchronizing wheel and one driven synchronizing wheel are respectively connected with the push rod driving wheels on the driving rod assemblies on the two sides through a synchronizing belt, and the other driving synchronizing wheel is connected with the other driven synchronizing wheel through another synchronizing belt. The push rod driving motor drives the two push rods in the same direction to move synchronously, so that cost is effectively saved, and control is simpler.

Preferably, a linkage synchronizing wheel is further arranged between the two driving synchronizing wheels on the driving rotating shaft, a motor shaft of the push rod driving motor is connected with the linkage synchronizing wheel through a synchronizing belt, and the linkage synchronizing wheel is arranged to enable the transmission of the push rod driving motor to be more stable.

Preferably, the push rod driving mechanism further comprises two lead screw installation seats used for installing a left-handed lead screw and a right-handed lead screw, each lead screw installation seat comprises two installation plates which are arranged oppositely, two ends of the left-handed lead screw or the right-handed lead screw are respectively connected to the two installation plates in a rotating mode, a guide plate which is horizontally arranged is connected between the two installation plates, a push rod slide rail is arranged on the upper end face of the guide plate, a threaded connection seat connected with the left-handed lead screw or the right-handed lead screw is arranged at the end portion of a transverse push rod or a longitudinal push rod, a push rod slide block capable of sliding on the push rod slide rail is arranged at the bottom of the threaded connection seat, and a push rod slide groove matched with the push rod slide rail is arranged on the lower end face of the push rod slide block. The cooperation of push rod spout and push rod slider not only has the guide effect to the push rod, can also make the push rod motion more stable, smooth and easy.

Preferably, the middle part of the transverse push rod or the longitudinal push rod is provided with a push frame with a longitudinally extending push surface.

Preferably, the pushing frame comprises two transverse connecting rods connected with the transverse push rods or the longitudinal push rods, a U-shaped frame with a downward opening is connected onto the two transverse connecting rods, and the end face, facing the center of the apron body, of the U-shaped frame forms a longitudinally extending pushing face.

The setting that pushes away the frame can provide one for the push rod and push away the face to the vertical of unmanned aerial vehicle promotion to make the push rod can be better promote unmanned aerial vehicle to the required position department of air park body.

Preferably, the apron bottom plate is a light-transmitting plate and the lamp plate is arranged on the surface of the lower end of the apron bottom plate. The lamp plate can guarantee that unmanned aerial vehicle is normal descending at night.

Preferably, a two-dimensional code board is arranged on the upper surface of the apron bottom board, and a two-dimensional code is arranged on the two-dimensional code board, so that no one can locate and land by scanning the two-dimensional code. The setting of two-dimensional code can realize unmanned aerial vehicle's accurate location.

Preferably, be equipped with on the pushing frame and carry out spacing clamp plate and be used for driving the clamp plate motor that the clamp plate rotated to unmanned aerial vehicle.

Preferably, the clamp plate is L shape, and one end is connected on the motor shaft of clamp plate motor, and the other end constitutes the spacing end to unmanned aerial vehicle.

The setting of clamp plate can realize spacing to unmanned aerial vehicle for unmanned aerial vehicle can not take place to shift when the last battery of unmanned aerial vehicle is got by the clamp.

Due to the adoption of the technical scheme, the invention has the remarkable technical effects that:

the invention provides a fixed type electric full-automatic vertical fixed wing airport with a centering mechanism, wherein the centering mechanism of an unmanned aerial vehicle capable of pushing the unmanned aerial vehicle in the airport to a required position is arranged in the airport, so that the unmanned aerial vehicle can be effectively ensured to be positioned in the center of an apron body in the airport, and an effective precondition guarantee is provided for the follow-up battery replacement of the unmanned aerial vehicle.

Drawings

Fig. 1 is a schematic structural view of embodiment 1 of the present invention.

Fig. 2 is an exploded view of fig. 1.

Fig. 3 is a schematic structural view of the opened state of the front door mechanism in fig. 1.

Fig. 4 is a schematic view of the internal structure of fig. 1.

Fig. 5 is a schematic view of the structure of the front door mechanism in the present invention.

Fig. 6 is a schematic structural view of another state of the front door mechanism of the present invention.

Fig. 7 is a schematic view of the connection structure of the apron and the multi-stage telescopic rail mechanism in fig. 4.

Fig. 8 is a schematic view of the structure of the apron of fig. 7.

Fig. 9 is a schematic structural diagram of the centering mechanism of the drone in fig. 8.

Fig. 10 is a schematic view of the multi-stage telescoping rail mechanism of fig. 7 in a retracted state.

Fig. 11 is a schematic structural view of the multi-stage telescopic rail mechanism of fig. 7 in a deployed state.

Fig. 12 is a schematic structural diagram of the motor field switching mechanism in fig. 7.

Fig. 13 is a schematic diagram of a state that the battery replacing clamping jaws clamp the battery in fig. 12.

FIG. 14 is a schematic diagram of the current swapping clamping jaw of FIG. 13.

Fig. 15 is a cross-sectional view of fig. 14.

Fig. 16 is a schematic view of the structure of the battery of fig. 4.

Fig. 17 is a partial schematic view of the structure of fig. 16.

Figure 18 is a cross-sectional view of figure 17.

Fig. 19 is a schematic structural view of the movable latch of fig. 16.

Fig. 20 is a schematic structural view of the battery compartment of the robot in the present embodiment.

Fig. 21 is a schematic view of a state in which the pressing plate presses the drone in the present embodiment.

Fig. 22 is a partial structural schematic view of the multistage telescopic rail mechanism in the present embodiment.

Fig. 23 is a schematic structural diagram of the camera head in fig. 1.

Fig. 24 is a schematic structural view of the camera stand of fig. 1.

Detailed Description

The present invention will be described in further detail with reference to the accompanying drawings and examples.

Example 1

A fixed-wing airport, as shown in fig. 1-24, includes an airport body, one side of the airport body is provided with an airport door, the airport door includes a front door mechanism 1, the front door mechanism 1 includes a door body 101, the door body 101 is connected to the airport body through a link mechanism 102 and can be opened by swinging upwards under the action of the link mechanism 102; this internal air park body 2 that can shift out from door body 101 department level that is equipped with of airport, air park body 2 sets up in the airport this internally through a multistage flexible guide rail mechanism 3.

In this embodiment, the front door mechanism 1 includes a door frame 103 disposed on the front side of the fixed wing airport frame, a door body 101 is disposed on the door frame 103 through a link mechanism 102, and the door body 101 swings upward and downward to open through the link mechanism 102.

The link mechanism 102 includes a driving rod 104 with two ends rotatably connected to the fixed-wing airport frame, a bearing seat 112 is disposed at an end of the driving rod 104, a bearing connected to the driving rod 104 is disposed in the bearing seat 112, the driving rod 104 is mounted on the fixed-wing airport frame through the bearing seat 112, and the bearing seat 112 is mounted at an upper end of the fixed-wing airport frame through a bolt or a screw. Both ends of the driving rod 104 are hinged with a connecting rod 105, one end of the connecting rod 105 is hinged at the end part of the driving rod 104, the other end of the connecting rod 105 is hinged on the door body 101, the connecting rod 105 is a bent rod which is bent back to the door body 101 when the door body 101 is closed, and the end part of the connecting rod 105 hinged with the driving rod 104 is positioned above the end part hinged with the door body 101 when the door body 101 is closed.

A front door driving mechanism 107 is further included in the embodiment, the front door driving mechanism 107 includes a front door driving motor 108 for realizing the rotation of the driving rod 104,

a front door driving motor 108 is installed on the fixed wing airport frame, a front door driving gear 109 is installed on a driving shaft of the front door driving motor 108, and a front door driven gear 110 meshed with the driving gear is arranged on the driving rod 104.

When the door is opened, the front door driving motor 108 is started, the front door driving gear 109 drives the front door driven gear 110, the front door driven gear 110 drives the driving rod 104 to rotate, the driving rod 104 drives the connecting rods 105 at two ends of the driving rod to rotate anticlockwise, the connecting rods 105 can push the door body 101 outwards firstly and drive the door body 101 to move upwards at the same time, the door body 101 swings upwards until the door body 101 moves to the position above the fixed-wing airport frame, the door body 101 is completely opened, and the end part, hinged to the driving rod 104, of the connecting rod 105 is located below the end part hinged to the door body 101.

When the door is closed, the front door driving motor 108 rotates reversely, so that the connecting rod 105 rotates clockwise, and the connecting rod 105 drives the door body 101 to move downwards and towards the door frame 103 until the door body 101 is completely positioned in the door frame 103, thereby closing the door body 101.

In this embodiment, the link mechanism 102 further includes a side link 111 having one end hinged to the fixed-wing airport frame and the other end hinged to the door 101, and a hinge point between the side link 111 and the door 101 is located below a hinge point between the link 105 and the door 101. The stability that door body 101 lid closed in door frame 103 department can be further strengthened when the setting of connecting rod can realize door body 101 and close, and when door body 101 was opened, play the further supporting role to door body 101, effectively strengthen the stability of being connected between door body 101 and the fixed wing airport frame.

In this embodiment, a sealing strip for sealing a gap between the door body 101 and the door frame 103 is arranged between the door frame 103 and the door body 101, and the sealing strip can achieve a waterproof effect at the door body 101, so that rainwater is prevented from entering an airport through the opening and closing position of the door body 101.

In this embodiment, set up in the leading flank of fixed wing airport frame through the door body 101, and the mode through connecting rod 105 realizes opening and shutting of the door body 101, the door body 101 is in airport one side, can not collect foreign matters such as leaf or snow on the door body surface, the in-process of opening and shutting can effectively solve the switch door and smuggle the problem that the foreign matter got into the internal portion of cabinet secretly, whole door body 101 only is in on the leading flank simultaneously, no matter door body 101 itself or the required stroke of opening and shutting of door body 101, its shared space is all less, can practice thrift the space greatly, the while still has whole preparation, the equal comparatively simple characteristics of assembly.

Being equipped with the air park body 2 that can shift out from airport door department level in the airport in this embodiment, air park body 2 is equipped with air park bottom plate 202 including the air park base 201 that is the square frame form in the middle part of the air park base 201, air park base 201 is equipped with unmanned aerial vehicle centering mechanism 203, and unmanned aerial vehicle centering mechanism 203 is including can pushing away the horizontal push rod mechanism 204 and the vertical push rod mechanism 205 of 2 central points of air park body department with unmanned aerial vehicle.

In this embodiment, the transverse pushing rod mechanism 204 includes two transverse pushing rods 206 whose length directions are arranged along the length direction of the apron body 2 and can move toward or away from each other along the width direction of the apron body 2, and the longitudinal pushing rod mechanism 205 includes two longitudinal pushing rods 207 whose length directions are along the width direction of the apron body 2 and can move toward or away from each other along the length direction of the apron body 2; the push rod driving mechanism comprises two opposite driving rod assemblies 208 which are arranged in parallel, two ends of the transverse push rod 206 or the longitudinal push rod 207 are connected to the corresponding driving rod assemblies 208 on two sides respectively, each driving rod assembly 208 comprises a push rod driving wheel 209 and a left-handed screw rod 210 and a right-handed screw rod 211 which are arranged on two sides of the push rod driving wheel 209 and connected through a coupler, the transverse push rod 206 or the longitudinal push rod 207 which move in opposite directions or in opposite directions are connected to the left-handed screw rod 210 and the right-handed screw rod 211 in a threaded mode respectively, and the left-handed screw rod 210 and the right-handed screw rod 211 are trapezoidal screw rods or ball screw rods.

Realize horizontal push rod 206 and vertical push rod 207's removal under push rod actuating mechanism's effect to promote descending unmanned aerial vehicle on air park bottom plate 202 to required position department, through the rotation of control system control levogyration lead screw 210 and dextrorotation lead screw 211, then can accurate control push rod promote unmanned aerial vehicle's stroke, guarantee that final unmanned aerial vehicle can accurate location.

In this embodiment, the push rod driving mechanism includes a push rod driving motor 212, a driving rotating shaft 213 is connected to a motor shaft of the push rod driving motor 212, two driving synchronizing wheels 214 are disposed on the driving rotating shaft 213, and the push rod driving mechanism further includes a driven rotating shaft 215, two driven synchronizing wheels 216 are disposed on the driven rotating shaft 215, one of the driving synchronizing wheels 214 and one of the driven synchronizing wheels 216 are respectively connected to the push rod driving wheels 209 on the two side driving rod assemblies 208 through a synchronous belt, and the other driving synchronizing wheel 214 is connected to the other driven synchronizing wheel 216 through another synchronous belt.

For stability and reliability of transmission, a linkage synchronizing wheel 217 is further disposed between the two driving synchronizing wheels 214 on the driving rotating shaft 213, and a motor shaft of the push rod driving motor 212 is connected to the linkage synchronizing wheel 217 through a synchronous belt.

In this embodiment, synchronous motion of push rods on two sides in the same direction is realized through one push rod driving motor 212, so that efficiency of the unmanned aerial vehicle centering process is improved, cost is saved, resource waste is avoided, and compared with double-motor driving, the single-motor driving mode can effectively simplify a synchronous control system program.

The push rod driving mechanism in the embodiment further comprises two lead screw installation seats 218 used for installing the left-handed lead screw 210 and the right-handed lead screw 211, each lead screw installation seat 218 comprises two lead screw installation plates 219 which are arranged oppositely, two ends of the left-handed lead screw 210 or the right-handed lead screw 211 are respectively connected to the two lead screw installation plates 219 in a rotating mode, a guide plate 220 which is arranged horizontally is connected between the two lead screw installation plates 219, a push rod sliding rail 221 is arranged on the upper end face of the guide plate 220, a threaded connection seat 222 which is connected with the left-handed lead screw 210 or the right-handed lead screw 211 is arranged at the end portion of the transverse push rod 206 or the longitudinal push rod 207, a push rod sliding block 223 which can slide on the push rod sliding rail 221 is arranged at the bottom of the threaded connection seat 222, and a push rod sliding groove 224 which is matched with the push rod sliding rail 221 is arranged on the lower end face of the push rod sliding block 223. The arrangement of the push rod sliding groove 224 and the push rod sliding block 223 can guide the moving process of the transverse push rod 206 or the longitudinal push rod 207, and can make the movement of the transverse push rod 206 or the longitudinal push rod 207 more stable and smoother.

In this embodiment, a pushing frame 225 with a longitudinally extending pushing surface is arranged in the middle of the transverse pushing rod 206 or the longitudinal pushing rod 207, the pushing frame 225 comprises two transverse connecting rods 226 connected with the transverse pushing rod 206 or the longitudinal pushing rod 207, a U-shaped frame 227 with a downward opening is connected to the two transverse connecting rods 226, and the end surface of the U-shaped frame 227 facing the center of the tarmac body 2 forms the longitudinally extending pushing surface. Push away the setting of frame 225 and provide one and vertically push away the face for the push rod can be better promote unmanned aerial vehicle.

In addition, be equipped with on pushing away frame 225 and carry out spacing clamp plate 230 and be used for driving clamp plate 230 pivoted clamp plate motor 231 to unmanned aerial vehicle, clamp plate motor 231 is direct current motor, and clamp plate 230 is L shape, and one end is connected on clamp plate motor 231's motor shaft, and the other end constitutes the spacing end to unmanned aerial vehicle, and unmanned aerial vehicle location back, direct current motor rotate to drive clamp plate 230 and push down unmanned aerial vehicle and guarantee that unmanned aerial vehicle can not shift when pulling out battery 6.

Apron bottom plate 202 is the light-passing board and is equipped with lamp plate 228 on the lower extreme surface in this embodiment to can guarantee that unmanned aerial vehicle is normal descending night. In addition, a two-dimensional code board 229 is arranged on the upper surface of the apron bottom plate 202, and two-dimensional codes are arranged on the two-dimensional code board 229, so that no one can locate and land by scanning the two-dimensional codes.

In this embodiment, the apron body 2 is disposed in the airport body through a multi-stage telescopic rail mechanism 3, and the apron body 2 can be pushed out of the airport body through the horizontal line of the door 101 under the action of the multi-stage telescopic rail mechanism 3.

The multistage telescopic guide rail mechanism 3 in this embodiment includes the guide rail fixing base 301, guide rail fixing base 301 fixed mounting is in the fixed wing airport frame in this embodiment, and the relative position in the airport is unchangeable, it can directly fix guide rail fixing base 301 on the lower bottom surface of airport frame through the bolt to specifically this embodiment, guide rail fixing base 301 includes fixing base body 320, one-level guide rail chute seat 304 sets up on fixing base body 320, guide rail fixing base 301 still includes two first fixed plates 321 fixed relative to fixing base body 320, two first fixed plates 321 set up respectively in the both ends of 2 directions of motion of parking apron body, when parking apron body 2 retracts in the airport completely, two first fixed plates 321 are located the position department at 2 both ends of parking apron body respectively.

Be equipped with the one-level guide rail 302 that can horizontal linear motion on the guide rail fixing base 301, be equipped with the second grade guide rail 303 that can horizontal linear motion on the one-level guide rail 302, the direction of motion of one-level guide rail 302 and second grade guide rail 303 is the same, air park body 2 sets up on second grade guide rail 303, air park body 2 can realize that the two-stage is flexible under the combined action of one-level guide rail 302 and second grade guide rail 303, thereby can solve because of the limited longer guide rail of unable installation of airport whole length scope leads to air park body 2 to stretch out the short problem of airport distance, make final air park can stretch out longer distance, can not shelter from because of the airport structure production when guaranteeing the fixed wing take off and land, interfere.

Specifically, in this embodiment, the guide rail fixing seat 301 is provided with a primary guide rail sliding groove seat 304, the upper end surface of the primary guide rail sliding groove seat 304 is provided with a primary guide rail sliding groove 305, the primary guide rail 302 includes a primary moving plate 306, and the lower end surface of the primary moving plate 306 is provided with a primary guide rail sliding block 307 capable of sliding in the primary guide rail sliding groove 305; a secondary guide rail sliding groove seat 308 is arranged on the upper end face of the primary moving plate 306, a secondary guide rail sliding groove 309 is arranged on the upper end face of the secondary guide rail sliding groove seat 308, a secondary guide rail sliding block 310 capable of sliding in the secondary guide rail sliding groove 309 is arranged on the lower end face of the secondary guide rail 303, and the lower end face of the apron body 2 is fixed on the upper end face of the secondary guide rail 303.

The lower end face of the first-stage moving plate 306 is provided with a guide rail rack 311 which is arranged along the moving direction of the first-stage guide rail 302 along the length direction, and the lower end face of the first-stage moving plate further comprises a guide rail driving motor 312, and a guide rail gear 313 which is meshed with the guide rail rack 311 and is used for driving the first-stage guide rail 302 to move is connected to a driving shaft of the guide rail driving motor 312. The primary extension and retraction of apron body 2 can be realized by the cooperation of rail gear 313 and rail rack 311.

The embodiment provides a specific structure of two-stage expansion: that is, the upper end face of the first-stage moving plate 306 is further provided with an extending mechanism for driving the second-stage guide rail 303 to extend, the extending mechanism comprises a first rotating shaft 314 arranged at the front end part of the extending direction of the first-stage moving plate 306, the first rotating shaft 314 is provided with a first synchronizing wheel 315 capable of rotating, the first synchronizing wheel 315 is meshed with a first double-face synchronous belt 316, the middle part of the first double-face synchronous belt 316 is wound around the first synchronizing wheel 315 and is meshed with the first synchronizing wheel 315, two ends of the first double-face synchronous belt 316 extend towards the rear end part of the extending direction of the first-stage moving plate 306, one end of the first double-face synchronous belt is connected to the rear end part of the second-stage guide rail 303 along the extending direction, and the other end of the first double-face synchronous belt is connected to the guide rail fixing seat 301.

Still be equipped with the recovery mechanism that is used for driving secondary guide rail 303 to retract on the up end of one-level moving plate 306, recovery mechanism is including setting up the second pivot at one-level moving plate 306 orientation rear end portion, be equipped with on the second pivot can pivoted second synchronizing wheel 318, the meshing has second double-sided hold-in range 319 on the second synchronizing wheel 318, second double-sided hold-in range 319 middle part is walked around second synchronizing wheel 318 and is meshed with second synchronizing wheel 318, the both ends of second double-sided hold-in range 319 all extend towards the front end portion that one-level moving plate 306 orientation stretches out and one end is connected at the front end portion along the orientation that stretches out of secondary guide rail 303, the other end is connected on guide rail fixing base 301.

The first double-sided timing belt 316 and the second double-sided timing belt 319 have ends respectively connected to the first fixing plates 321 at both ends. The front and rear ends of the secondary guide rail 303 are respectively provided with a second fixing plate 322, and the other ends of the first double-sided synchronous belt 316 and the second double-sided synchronous belt 319 are respectively connected to the two second fixing plates 322.

The second grade telescopic machanism in this embodiment realizes through hold-in range and synchronizing wheel, follow the motion of one-level movable plate 306 when the synchronizing wheel under the drive of one-level movable plate 306, hold-in range one end on the synchronizing wheel is because being connected with guide rail fixing base 301 and therefore can keeping the position unchangeable, because the whole length of hold-in range is unchangeable, therefore the other end then can drive second grade guide rail 303 and follow the motion of one-level guide rail 302 under the effect of synchronizing wheel, the stroke of hold-in range tip motion is the twice of synchronizing wheel motion stroke, therefore second grade guide rail 303 can continue to move towards the direction of stretching out or retracting relative one-level guide rail 302, realize the second grade stroke of air park, fully guarantee finally that air park body 2 can move to the position far enough relative airport, avoid the airport to interfere the stationary vane to take off and land.

Meanwhile, the two-stage stretching is not realized by independent driving, but is realized by skillfully utilizing the driving of the one-stage stretching movement, so that the driving mechanism can be effectively reduced, the resource is saved, and the cost is saved.

In addition, be equipped with the airport in this embodiment and trade electric mechanism 4, the airport trades electric mechanism 4 and fills electric pile 5 including being the cuboid form, fills electric pile 5 department and deposits a plurality of batteries 6, still includes can press from both sides the clamping jaw 401 that trades that gets unmanned aerial vehicle battery storehouse 617 department and fill electric pile 5 department battery 6 and is used for installing the clamping jaw installation mechanism 402 that trades electric jaw 401, is equipped with on the clamping jaw installation mechanism 402 to be used for driving to trade electric jaw 401 along filling the three direction motion of electric pile 5 length, width and height.

Wherein, clamping jaw installation mechanism 402 includes two first guide rails 404 that are parallel to each other and length direction sets up along filling 5 length direction of electric pile, be connected with the second guide rail 405 perpendicular and the level setting with first guide rail 404 between two first guide rails 404, second guide rail 405 can slide along first guide rail 404 length direction on first guide rail 404, be connected with on the second guide rail 405 and follow the gliding third guide rail 406 of second guide rail 405 length direction, the vertical setting of third guide rail 406 length direction, trade electric clamping jaw 401 and connect on third guide rail 406 and can follow third guide rail 406 and slide from top to bottom.

The clamping jaw driving mechanism comprises a first screw rod, a second screw rod and a third screw rod which are respectively arranged on a first guide rail 404, a second guide rail 405 and a third guide rail 406, and the axial directions of the first screw rod, the second screw rod and the third screw rod are respectively the same as the axial directions of the first guide rail 404, the second guide rail 405 and the third guide rail 406;

the first guide rail 405, the third guide rail 406 and the battery replacement clamping jaw 401 are respectively provided with a first sliding block, a second sliding block and a third sliding block which can slide along the first guide rail 404, the second guide rail 405 and the third guide rail 406, and the first sliding block, the second sliding block and the third sliding block are respectively in threaded connection with the first guide rail, the second guide rail and the third guide rail and can respectively axially move along the first guide rail, the second guide rail and the third guide rail.

The embodiment provides a battery replacing clamping jaw 401 in a fixed wing airport, which comprises a clamping jaw body 407 arranged in the fixed wing airport, wherein the clamping jaw body 407 comprises a pressing rod 408 which can move in the vertical direction and press the upper end surface of a battery 6 on the unmanned aerial vehicle, and a clamping plate 409 which can move relatively in the horizontal direction and clamp two sides of the battery 6 on the unmanned aerial vehicle, wherein the clamping jaw body 407 comprises a clamping jaw mounting plate 410 which is horizontally arranged, one end of the clamping jaw mounting plate 410 is provided with a vertically arranged sliding block mounting plate 411, a third sliding block is mounted on the sliding block mounting plate 411, the upper end of the clamping plate 409 forms a connecting end mounted on the clamping jaw mounting plate 410, and the lower end forms a clamping end for clamping the battery 6,

all be equipped with locating pin 425 on the clamping end of two grip blocks 409 and the relative face, the last battery 6 side of unmanned aerial vehicle is equipped with and supplies locating pin 425 male battery locating hole 601. When clamping the unmanned aerial vehicle battery 6, the positioning pin 425 can be clamped into the battery positioning hole 601, and then the battery 6 can be stably clamped under the clamping action of the two clamping plates 409 and the pressing action of the pressing rod 408.

Be equipped with the grip block actuating mechanism who installs on the lower surface of clamping jaw mounting panel 410 between two grip blocks 409, two grip blocks 409 are installed respectively in grip block actuating mechanism's both sides and are realized two grip blocks 409 in the horizontal direction through grip block actuating mechanism and move in opposite directions or dorsad, wherein the grip block actuating mechanism in this embodiment is two-way lead screw motor, two-way lead screw motor's upper end passes through the connecting plate (not shown in the figure) to be fixed on the lower surface of clamping jaw mounting panel 410, two grip blocks 409 are connected respectively in the drive shaft of two-way lead screw motor both sides, can realize two grip blocks 409 and get the stable clamp of battery 6 under two-way lead screw motor's effect, then realize the change to unmanned aerial vehicle battery 6.

Be equipped with the horizontal arrangement on the lower surface of clamping jaw mounting panel 410 in this embodiment and length direction along the grip block slide rail 426 that the grip block 409 direction of motion set up, grip block 409 upper end is connected on grip block slide rail 426, grip block 409 can slide along grip block slide rail 426 length direction on grip block slide rail 426, it is spacing along grip block 409 length direction, grip block slide rail 426 can realize the centre gripping guide effect to two grip blocks 409 with the cooperation of grip block 413, guarantee that two grip blocks 409 can carry out horizontal centre gripping to battery 6, guarantee that locating pin 425 can get into in the battery locating hole 601 smoothly, guarantee the homogeneity of grip block 409 to battery 6 side clamping-force simultaneously, the realization is to the stable centre gripping of battery 6.

The two sides of the clamping plate slide rail 426 are both provided with a long-strip-shaped slide rail limiting groove 412 arranged along the length direction of the clamping plate slide rail 426, the upper end of the clamping plate 409 is provided with a clamping plate slide block 413 matched with the clamping plate slide rail 426, and the inner side surface of the clamping plate slide block 413 is provided with a slide block limiting protrusion 414 matched with the slide rail limiting groove 412. The cooperation of the slide rail limiting groove 412 and the slide block limiting protrusion 414 can realize the positioning effect on the upper end of the clamping plate 409, and the clamping plate 409 is prevented from being separated from the slide rail in the vertical direction.

In this embodiment, a pressing rod mounting assembly is disposed on the clamping jaw mounting plate 410, the pressing rod mounting assembly includes a pressing rod linear bearing 403 mounted on the clamping jaw mounting plate 410, the pressing rod 408 is slidably disposed in the pressing rod linear bearing 403, the pressing rod mounting assembly further includes a spring extrusion piece 415 disposed at a lower end portion of the pressing rod 408, and a pressing rod spring 416 which is sleeved on the pressing rod 408 and can extrude the pressing rod 408 downward is disposed between the spring extrusion piece 415 and the pressing rod linear bearing 403. When the battery 6 needs to be compressed, the pressing rod 408 moves downwards under the action of the pressing rod spring 416 pressing the spring pressing piece 415 until abutting against the upper end face of the battery 6, so that the pressing rod 408 compresses the battery 6.

In this embodiment, the number of the two pressing rods 408 is two, the two pressing rods 408 can respectively press two ends of the battery 6 along the length direction, and it is ensured that the pressing rods 408 can uniformly stabilize the force applied to the battery 6, in addition, the upper end of the pressing rod 408 can move above the clamping jaw mounting plate 410, the pressing rod mounting assembly further comprises a pressing rod limiting plate 417 connected between the upper ends of the two pressing rods 408, the pressing rod limiting plate 417 is disposed above the clamping jaw mounting plate 410, the pressing rods 408 at two ends are connected through the pressing rod limiting plate 417, on one hand, axial limitation on the pressing rods 408 can be realized, the pressing rods 408 are prevented from being separated from the pressing rod linear bearing 403 under the action of gravity, on the other hand, the movement synchronization of the pressing rods 408 at two ends can also be ensured, so that the pressing rods 408 at two ends can uniformly press and apply the force to the two ends of the battery 6, and the pressing stability of the battery 6 is ensured.

In order to realize the elastic force adjustment of the compression bar spring 416, the outer wall of the lower end part of the compression bar 408 is provided with an external thread, the spring extrusion part 415 is arranged to be an adjusting nut which is in threaded connection with the lower end part of the compression bar 408, the lower end part of the compression bar spring 416 abuts against the adjusting nut, the compression of the compression bar spring 416 in different degrees is realized by changing the position of the adjusting nut on the compression bar 408, then the elastic force of the compression bar spring 416 is changed, then the downward movement stroke of the lower end of the compression bar 408 is adjusted, and the compression bar 408 is ensured to compress the batteries 6 with different heights.

In this embodiment can stabilize to get battery 6 clamp on unmanned aerial vehicle in order to guarantee the clamping jaw, still be equipped with clamping jaw positioning component 418, clamping jaw positioning component 418 is including setting up reference column 619 on unmanned aerial vehicle, wherein reference column 619 is cylindricly, it can install additional on unmanned aerial vehicle's the up end that is close to battery compartment department through screw or welded mode, still including setting up on clamping jaw mounting panel 410 and can follow vertical direction up-and-down motion's guide bar 419, guide bar 419's lower tip is equipped with locating piece 420, be equipped with on the locating piece 420 with unmanned aerial vehicle on reference column 619 complex clamping jaw locating hole 421.

The clamping jaw positioning assembly 418 includes a positioning linear bearing 422 installed on the lower surface of the clamping jaw mounting plate 410, a guide rod 419 is slidably disposed in the positioning linear bearing 422, the upper end of the guide rod 419 can move above the clamping jaw mounting plate 410, a limit flange 423 is disposed at the upper end of the guide rod 419, a positioning recovery spring 424 disposed between the positioning block 420 and the positioning linear bearing 422 is sleeved on the guide rod 419, in addition, a sensor for detecting whether the positioning column 619 is inserted into the clamping jaw positioning hole 421 is further disposed at the upper end of the guide rod 419, the sensor in this embodiment is a groove-shaped photoelectric sensor for detecting the descending distance of the guide rod 419 to determine whether the positioning column 619 is inserted into the clamping jaw positioning hole 421.

When needs are changed unmanned aerial vehicle's battery 6, will trade battery clamping jaw 401 and move unmanned aerial vehicle's battery compartment department through clamping jaw actuating mechanism, make clamping jaw locating hole 421 on the locating plate aim at reference column 619 on the unmanned aerial vehicle, then top-down will trade battery clamping jaw 401 and move down, go into in clamping jaw locating hole 421 until reference column 619 location, because locating piece 420 is connected through guide bar 419 that can move about from top to bottom, because locating piece 420 can adapt to and the unmanned aerial vehicle of co-altitude not, guarantee locating piece 420 can be smoothly at unmanned aerial vehicle surface location, realize trading the first time location between battery clamping jaw 401 and unmanned aerial vehicle battery compartment 617 after reference column 619 inserts clamping jaw locating hole 421, get ready the prerequisite guarantee for follow-up to battery 6 presss from both sides.

Then, the lower end part of the pressing rod 408 is pressed on the upper end face of the battery 6 under the action of the pressing rod spring 416, the clamping plate 409 moves oppositely under the action of the clamping plate driving mechanism to clamp the side face of the battery 6, the positioning pin 425 is inserted into the battery positioning hole 601, the second positioning of the battery replacing clamping jaw 401 on the battery 6 is realized, and the stability of clamping the battery 6 by the battery replacing clamping jaw 401 and the accuracy of replacing the battery 6 between the unmanned aerial vehicle battery bin 617 and the battery replacing bin 617 in the battery replacing process can be fully guaranteed through the twice positioning, the pressing of the pressing rod 408 and the clamping of the clamping plate 409.

Trade electric clamping jaw 401 and battery 6 and fix a position completely and to the stable back of battery 6 centre gripping, rethread clamping jaw actuating mechanism makes trade electric clamping jaw 401 rise, then will trade electric clamping jaw 401 and move to fill electric pile 5 top and make battery 6 with fill the battery jar that does not place battery 6 on the electric pile 5 and aim at, then make trade electric clamping jaw 401 descend, put into the battery jar with battery 6 and charge.

And then clamping the fully charged battery 6 on the charging pile 5 by adopting the same method, and moving the battery 6 into a battery compartment of the unmanned aerial vehicle to finish the electricity changing work of the unmanned aerial vehicle.

Wherein, this internal electric pile 5 that fills that is equipped with in unmanned aerial vehicle airport in this embodiment, it is equipped with a plurality of battery jars that are used for placing battery 6 on the 5 up end of electric pile to fill, be equipped with the battery 6 that is used for unmanned aerial vehicle in the battery jar, battery 6 includes battery body 602, all be equipped with on battery body 602's the both sides face along length direction by clamping part 603, wherein, the surface by clamping part 603 constitutes to be the cockscomb structure by the clamping face, the intermediate position department by clamping part 603 is equipped with axial perpendicular to battery body 602 side and opening towards the outside battery locating hole 601 of battery body 602.

When changing battery 6, trade grip block 409 on the electric clamping jaw 401 and can be to the portion 603 of being gripped of battery 602 both sides, simultaneously grip block 409 go up with battery locating hole 601 complex locating pin 425 can be located the battery locating hole 601 of battery 6 side, the setting up of battery locating hole 601 can make unmanned aerial vehicle change in the airport in with trade the locating pin 425 cooperation on the electric clamping jaw 401, when getting unmanned aerial vehicle battery 6, trade the locating pin 425 on the electric clamping jaw 401 and can block in the battery locating hole 601, guarantee to carry out stable clamp to battery 6 and get, and the jagged face of being gripped can further improve trade electric clamping jaw 401 and by the frictional force between the portion 603, further improve the stability that battery 6 was got by the clamp.

In this embodiment, in order to ensure the stability of the clamp for the battery 6, the clamped portions 603 on the two sides of the battery body 602 are symmetrically arranged, and the clamped portions 603 are located on the central line of the battery body 602 in the length direction, so that the battery 6 can be uniformly stressed when being clamped.

In this embodiment, the clamped portion 603 includes a latch frame 604 disposed on the outer side of the battery body 602 and a movable latch 605 disposed in the latch frame 604, the latch frame 604 and the outer side of the battery body 602 together form a latch installation slot 606, the outer end surface of the movable latch 605 forms a serrated clamped surface and protrudes out of the latch installation slot 606, the upper end portion of the movable latch 605 is provided with a connection shaft 607, the lower end portion of the movable latch 605 is provided with a battery latching portion 608, the lower side wall of the latch frame 604 is provided with a latching portion limiting hole 609 extending from the latch installation slot 606 for supplying power to Chi Kouge, the movable latch 605 can rotate around the connection shaft 607 towards the inside of the latch installation slot 606 under the external force, a return spring 610 for driving the movable latch 605 to rotate towards the outside of the latch installation slot 606 is disposed between the movable latch 605 and the outer side of the battery body 602, wherein a spring column 611 disposed perpendicular to the outer side of the battery body 602 is disposed on the inner side surface of the movable latch 605, the return spring column 611 is disposed, one end of the return spring column 611 abuts against the outer side of the battery body 602, and the other end abuts against the outer side of the battery body 602.

In addition, the upper end portions of the two side walls of the locking and installing groove 606 are both provided with a connecting shaft groove 612 with an upward opening, two ends of the connecting shaft 607 are inserted into the connecting shaft groove 612 from top to bottom, and the upper end portion of the locking and installing groove 606 is provided with a locking and installing cover plate 614. The lock catch cover plate 614 comprises a press plate main body 615, protruding parts 616 which stretch into the lock catch mounting grooves 606 and block openings of the connecting shaft grooves 612 are arranged at two ends of the lower end face of the press plate main body 615, two ends of the press plate main body 615 are connected with the battery body 602 through pins, the lock catch cover plate 614 can effectively prevent the connecting shaft 607 from being separated from the connecting shaft grooves 612, and the structural stability of the whole lock catch structure is guaranteed.

When the unmanned aerial vehicle enters an airport and needs to replace the battery 6, the clamping jaw positioning hole 421 of the positioning block 420 on the clamping jaw positioning assembly 418 is aligned with the positioning column 619 on the unmanned aerial vehicle, then the battery replacement clamping jaw 401 is moved downwards from top to bottom until the positioning column 619 is positioned in the clamping jaw positioning hole 421, and the battery replacement clamping jaw 401 is positioned at the unmanned aerial vehicle battery bin 617; then, the positioning pin 425 on the clamping plate 409 is inserted into the battery positioning hole 601 on the side wall of the battery 6 to realize the positioning between the battery replacing clamping jaw 401 and the battery 6, then the clamping plate 409 applies force to the outer surface of the movable lock 605 to enable the movable lock 605 to rotate around the connecting shaft 607 against the action of the return spring 610, at this time, the battery buckling part 608 at the lower end of the movable lock 605 moves towards the inner side of the battery 6 along with the movable lock 605 to realize the unlocking between the battery buckling part 608 and the unmanned aerial vehicle buckling part 618 in the unmanned aerial vehicle battery compartment 617, at this time, the battery 6 can be taken out from the unmanned aerial vehicle battery compartment 617 by the battery replacing clamping jaw 401, and the battery can be moved into an airport battery compartment in the airport to be charged after being taken out. Through cooperating jointly battery 6 itself and trade electric clamping jaw 401, realized promptly to the unblock between battery 6 and the unmanned aerial vehicle battery compartment 617, realized getting again battery 6's clamp.

The fixed wing airport in this embodiment has a detachable wing storage cavity, wherein the airport body of the fixed wing airport includes an airport main body 7, a main body storage cavity 701 for horizontal entering of the unmanned aerial vehicle and for storing the main body part of the unmanned aerial vehicle is arranged in the airport main body 7, detachable wing storage shells 702 are symmetrically connected to two sides of the airport main body 7, and the wing storage cavities 703 communicated with the main body storage cavity 701 and used for storing the wing part of the unmanned aerial vehicle are formed inside the wing storage shells 702.

Design into detachable construction with the airport body in this embodiment, realize separately transporting when transporting to the airport, when satisfying effective fixed wing unmanned aerial vehicle wing and the paddle of accomodating, can also reach and reduce airport volume and quality, reduce area through the mode of dismantling to can dismantle the purpose of convenient transportation.

The front end face of the main body containing cavity 701 and the front end face of the wing containing cavity 703 jointly form an unmanned aerial vehicle inlet and outlet 704, the frame of the unmanned aerial vehicle inlet and outlet 704 forms a door frame 103, a door body 101 is arranged at the position of the door frame 103, and the door body 101 comprises a main door body 705 capable of covering the front end face of the main body containing cavity 701 and auxiliary door bodies 706 which are detachably arranged on two sides of the main door body 705 and capable of respectively covering the front end faces of the wing containing cavities 703 at two sides. The door body also designs into detachable mode, can further realize further lightening airport weight and volume to the dismantlement at unmanned aerial vehicle airport, reduces the transportation degree of difficulty and cost, promotes the transportation convenience.

In this embodiment, in order to achieve the connection stability of the detachment part on the airport, the main body storage cavity 701 is a U-shaped storage cavity with an open front end face, the two side walls of the main body storage cavity 701 are both provided with a housing mounting opening 707 with a front end part extending to the front end face of the main body storage cavity 701 to form a front end opening, the end part of the wing storage housing 702 connected with the airport main body 7 is a housing open end 708 corresponding to the housing mounting opening 707, and the housing open end 708 is connected with the housing mounting opening 707 through a bolt.

Meanwhile, a first mounting frame strip 709 is vertically arranged on the inner wall of the housing mounting opening 707, the first mounting frame strip 709 and the inner wall of the housing mounting opening 707 jointly form a mounting stepped groove, a second mounting frame strip 711 which can be clamped into the mounting stepped groove and is attached to the first mounting frame strip 709 is arranged at the opening end 708 of the housing, the first mounting frame strip 709 and the second mounting frame strip 711 are connected through bolts, and the secondary door body 706 and the main door body 705 are connected through bolts.

The mode through the bolt realizes dismantling the connection of department, makes its assembly all very convenient with the dismantlement, still is equipped with the installation department of mutually supporting between wing storage housing 702 and the airport main part 701 in addition, can make the assembly between the two more stable, guarantees airport overall structure's stability.

The front end face of the door frame 103 in this embodiment is provided with an end-to-end U-shaped clamping groove 712 with an outward opening, the edge of the rear end face of the door body is provided with an end-to-end U-shaped protruding strip 710 which can be clamped into the U-shaped clamping groove 712, a sealing strip for sealing a gap between the door body 101 and the door frame 103 is arranged between the U-shaped clamping groove 712 and the U-shaped protruding strip 710, the sealing strip is arranged to realize the waterproof function of the door body 101, and rainwater is prevented from entering the airport through the opening of the door body 101.

The main door body 705 is connected to the front end face of the main body accommodating cavity 701 through a connecting rod mechanism 102 and can swing upwards to be opened, the door body 101 or the door body 101 can be opened and closed in the opening and closing mode in a required stroke, the occupied space is small, the space can be greatly saved, and meanwhile the door body has the advantages of being simple in whole manufacturing and assembly.

The fixed wing airport in this embodiment has a monitoring system, wherein the airport body includes an airport housing 8, an unmanned aerial vehicle entrance 704 is arranged on the airport housing 8, a weather station 801 for detecting weather data outside the airport and a video monitoring module 802 for monitoring the unmanned aerial vehicle entrance 704 are arranged outside the airport housing 8; a fire prevention module and a temperature control module are arranged inside the airport shell 8.

Wherein video monitor module 802 includes can be towards the camera 803 of unmanned aerial vehicle import and export 704, and temperature control module is used for carrying out radiating radiator fan in airport casing 8 according to the temperature that temperature sensor detected including the temperature sensor who is used for detecting the inside temperature of airport casing 8 with setting up in airport casing 8, is equipped with heat dissipation vent 816 on airport casing 8's the trailing flank. The fire protection module comprises a smoke sensor which is arranged on the upper end face of the airport housing 8 and in the middle of the airport housing 8. The weather station 801 includes a mast 817 mounted on the airport housing 8 and a microclimate module 818 disposed on the mast 817, the microclimate module 818 including a temperature sensor, a humidity sensor, an air pressure sensor, a wind speed sensor, a wind direction sensor and a rain sensor capable of detecting temperature, humidity, air pressure, wind speed, wind direction and rain, respectively.

Through set up meteorological station 801 on the fixed wing airport, video monitoring module 802, the monitored control system that fire prevention module and temperature control module constitute, the realization is to the control of all aspects of fixed wing airport, and this monitoring data can communicate for airport controller, backstage control terminal can be uploaded to airport controller, can obtain real-time information through this kind of mode technical staff, not only can realize meteorological monitoring according to the information that detects, video monitoring, the fire prevention early warning, temperature regulation and control etc. can also maintain the fixed wing airport according to real-time information.

In this embodiment, unmanned aerial vehicle import and export 704 sets up on airport casing 8's leading flank, unmanned aerial vehicle import and export 704 department is equipped with the door body, video monitoring module 802 sets up on airport casing 8's the tip top surface that is close to unmanned aerial vehicle import and export 704, wherein, video monitoring module 802 still includes camera support 804, camera support 804 is including installing lower fixing base 805 on airport casing 8 surface and installing last fixing base 806 on fixing base 805 down, camera 803 is installed on last fixing base 806, it can rotate in order to realize the rotation of camera 803 fore-and-aft direction to go up fixing base 806 fixing base 805 down relatively.

The upper fixing seat 806 and the lower fixing seat 805 are both U-shaped plates, the U-shaped openings are oppositely arranged, the side walls of the U-shaped openings are semicircular, the outer surface of the side wall of the lower fixing seat 805 is in sliding fit with the inner surface of the side wall of the upper fixing seat 806, the side wall of the lower fixing seat 805 is rotationally connected with the side wall of the upper fixing seat 806 through a rotating pin 807, an arc-shaped limiting hole 808 which bends towards the rotating position of the rotating pin 807 is further formed in the side wall of the upper fixing seat 806, and a fixing pin 809 which is connected in the arc-shaped limiting hole 808 and limits the rotation of the upper fixing seat 806 is arranged on the side wall of the lower fixing seat 805.

Go up the long banding movable mounting hole 810 that two intervals set up and length direction set up along camera 803 fore-and-aft direction on the up end wall of fixing base 806, be equipped with a fixed mounting hole 811 between two movable mounting holes 810, the camera 803 bottom is fixed with camera mounting panel 812, is equipped with two camera mounting holes 813 that can correspond with movable mounting hole 810 and fixed mounting hole 811 respectively and be connected on the camera mounting panel 812.

In this embodiment, the camera 803 is installed on the airport housing 8 through the camera support 804, wherein the camera support 804 is formed by connecting an upper fixing seat 805 and a lower fixing seat 805, and the camera support can rotate relatively to enable the orientation of the camera 803 to be adjusted according to actual needs, and the camera support can also be limited through the fixing pins 809 after being adjusted to a required angle, so as to ensure the shooting stability of the camera 803.

In addition, a bracket mounting hole 814 and a plurality of arc-shaped elongated holes 815 uniformly arranged around the bracket mounting hole 814 are provided at the center position of the lower end wall of the lower fixing base 805. When camera support 804 is installed on the airport body, through support mounting hole 814 and a plurality of arc rectangular holes 815 around support mounting hole 814 evenly arranged realize the installation, support mounting hole 814 realizes the location of camera support 804 on airport casing 8, arc rectangular hole 815 realizes the stable installation of camera support 804 on airport casing 8, and the mode of setting up of arc rectangular hole 815 can make camera support 804 very nimble in the installation on airport casing 8, can select bolt fixed position according to actual need, can adapt to the airport casing 8 of different shapes.

When the camera 803 of this embodiment is mounted on the camera support 804, the camera is mounted through two camera mounting holes 813 on the camera mounting plate 812, the distances between the camera mounting holes 813 on different cameras 803 are different, in order to adapt to the mounting of different cameras 803, in this embodiment, two strip-shaped movable mounting holes 810 are provided on the upper end wall of the upper fixing base 806, the intervals are set, and the length direction is set along the front-back direction of the camera 803, a fixed mounting hole 811 is provided between the two movable mounting holes 810, so that one of the camera mounting holes 813 is connected with the fixed mounting hole 811, the other camera mounting hole 813 and the strip-shaped movable mounting hole 810 can make the bolt be in different positions of the movable mounting hole 810 according to the distance between the two camera mounting holes 813, so that the camera support 804 can be more flexibly adapted to the mounting of different cameras 803.

In summary, the above-mentioned embodiments are only preferred embodiments of the present invention, and all equivalent changes and modifications made in the claims of the present invention should be covered by the claims of the present invention.

Claims (12)

1. Fixed full-automatic fixed wing airport that hangs down of fixed electric power with centering mechanism, including the airport body, its characterized in that: one side of airport body is equipped with the airport door, be equipped with air park body (2) that can shift out from airport door department level in the airport, air park body (2) are including air park base (201) that is square frame form, air park base (201) middle part is equipped with air park bottom plate (202), air park base (201) are equipped with unmanned aerial vehicle centering mechanism (203), unmanned aerial vehicle centering mechanism (203) are including horizontal push rod mechanism (204) and vertical push rod mechanism (205) that can push away unmanned aerial vehicle to air park body (2) central point department of putting.

2. The stationary electric fully-automatic vertical fixed-wing airport with centering mechanism of claim 1, wherein: the transverse push rod mechanism (204) comprises two transverse push rods (206) which are arranged along the length direction of the apron body (2) in the length direction and can move towards or away from the width direction of the apron body (2), and the longitudinal push rod mechanism (205) comprises two longitudinal push rods (207) which are arranged along the width direction of the apron body (2) in the length direction and can move towards or away from the length direction of the apron body (2).

3. The stationary electric power full-automatic vertical fixed wing airport with centering mechanism of claim 2, wherein: the automatic push rod mechanism is characterized by further comprising two groups of push rod driving mechanisms used for respectively driving the transverse push rods (206) and the longitudinal push rods (207) to move, each push rod driving mechanism comprises two driving rod assemblies (208) arranged in parallel, the two ends of each transverse push rod (206) or each longitudinal push rod (207) are respectively connected to the corresponding driving rod assemblies (208) on the two sides, each driving rod assembly (208) comprises a push rod driving wheel (209) and a left-handed screw rod (210) and a right-handed screw rod (211) which are arranged on the two sides of the corresponding push rod driving wheel (209) and connected through a coupler, and the transverse push rods (206) or the longitudinal push rods (207) moving in opposite directions or opposite directions are respectively in threaded connection with the left-handed screw rods (210) and the right-handed screw rods (211).

4. The stationary electric fully-automatic droop fixed-wing airport with centering mechanism of claim 3, wherein: the push rod driving mechanism comprises a push rod driving motor (212), a driving rotating shaft (213) is connected to a motor shaft of the push rod driving motor (212), two driving synchronous wheels (214) are arranged on the driving rotating shaft (213), the push rod driving mechanism further comprises a driven rotating shaft (215), two driven synchronous wheels (216) are arranged on the driven rotating shaft (215), one of the driving synchronous wheels (214) and one of the driven synchronous wheels (216) are respectively connected with push rod driving wheels (209) on the driving rod assemblies (208) on two sides through a synchronous belt, and the other driving synchronous wheel (214) is connected with the other driven synchronous wheel (216) through another synchronous belt.

5. The stationary electric power fully-automatic droop fixed-wing airport with centering mechanism of claim 4, wherein: a linkage synchronizing wheel (217) is further arranged between the two driving synchronizing wheels (214) on the driving rotating shaft (213), and a motor shaft of the push rod driving motor (212) is connected with the linkage synchronizing wheel (217) through a synchronous belt.

6. The stationary electric power fully-automatic droop fixed-wing airport with centering mechanism of claim 4, wherein: the push rod driving mechanism further comprises two lead screw installation bases (218) used for installing a left-handed lead screw (210) and a right-handed lead screw (211), each lead screw installation base (218) comprises two lead screw installation plates (219) which are arranged oppositely, two ends of the left-handed lead screw (210) or the right-handed lead screw (211) are respectively connected to the two lead screw installation plates (219) in a rotating mode, a guide plate (220) which is arranged horizontally is connected between the two lead screw installation plates (219), a push rod sliding rail (221) is arranged on the upper end face of the guide plate (220), a threaded connection base (222) connected with the left-handed lead screw (210) or the right-handed lead screw (211) is arranged at the end portion of a transverse push rod (206) or a longitudinal push rod (207), a push rod sliding block (223) capable of sliding on the push rod sliding rail (221) is arranged at the bottom of the threaded connection base (222), and a push rod sliding groove (224) matched with the push rod sliding rail (221) is arranged on the lower end face of the push rod sliding block (223).

7. The stationary electric power full-automatic vertical fixed wing airport with centering mechanism of claim 3, wherein: the middle part of the transverse push rod (206) or the longitudinal push rod (207) is provided with a push frame (225) with a longitudinally extending push surface.

8. The stationary electric fully-automatic droop fixed-wing airport with centering mechanism of claim 7, wherein: the pushing frame (225) comprises two transverse connecting rods (226) connected with the transverse pushing rod (206) or the longitudinal pushing rod (207), a U-shaped frame (227) with a downward opening is connected onto the two transverse connecting rods (226), and the end face, facing the center of the apron body (2), of the U-shaped frame (227) forms a longitudinally extending pushing face.

9. The stationary electric fully-automatic vertical fixed-wing airport with centering mechanism of claim 1, wherein: the apron bottom plate (202) is a light-transmitting plate and a lamp plate (228) is arranged on the surface of the lower end of the apron bottom plate.

10. The fixed type electric full-automatic vertical fixed wing airport with the centering mechanism according to claim 1 or 9, wherein a two-dimension code board (229) is arranged on the upper surface of the apron bottom board (202), a two-dimension code is arranged on the two-dimension code board (229), and no one can locate and land by scanning the two-dimension code.

11. The stationary electric power fully-automatic droop fixed-wing airport with centering mechanism of claim 7 or 8, wherein: be equipped with on pushing away frame (225) and carry out spacing clamp plate (230) and be used for driving clamp plate (230) pivoted clamp plate motor (231) to unmanned aerial vehicle.

12. The stationary electric power full-automatic droop fixed-wing airport with centering mechanism of claim 11, wherein: clamp plate (230) are L shape, and one end is connected on the motor shaft of clamp plate motor (231), and the other end constitutes the spacing end to unmanned aerial vehicle.

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