CN114789797A - Multistation type unmanned aerial vehicle-mounted departure vehicle with unmanned aerial vehicle capable of independently receiving and transmitting - Google Patents
Multistation type unmanned aerial vehicle-mounted departure vehicle with unmanned aerial vehicle capable of independently receiving and transmitting Download PDFInfo
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- CN114789797A CN114789797A CN202210364676.3A CN202210364676A CN114789797A CN 114789797 A CN114789797 A CN 114789797A CN 202210364676 A CN202210364676 A CN 202210364676A CN 114789797 A CN114789797 A CN 114789797A
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- 230000007306 turnover Effects 0.000 claims abstract description 22
- 238000005381 potential energy Methods 0.000 claims abstract description 10
- 230000002457 bidirectional effect Effects 0.000 claims description 22
- 238000001125 extrusion Methods 0.000 claims description 8
- 230000005540 biological transmission Effects 0.000 claims description 7
- 230000000149 penetrating effect Effects 0.000 claims description 4
- 230000006978 adaptation Effects 0.000 claims description 3
- 238000004891 communication Methods 0.000 claims description 3
- 230000007246 mechanism Effects 0.000 claims description 3
- 238000000034 method Methods 0.000 abstract description 10
- 230000008569 process Effects 0.000 abstract description 9
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- 238000010586 diagram Methods 0.000 description 4
- 230000009286 beneficial effect Effects 0.000 description 1
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/007—Helicopter portable landing pads
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/04—Ground or aircraft-carrier-deck installations for launching aircraft
- B64F1/06—Ground or aircraft-carrier-deck installations for launching aircraft using catapults
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Abstract
The invention relates to an unmanned aerial vehicle auxiliary tool, in particular to a multistation type unmanned aerial vehicle-mounted departure vehicle with an unmanned aerial vehicle capable of independently receiving and sending, wherein a lifting plate is arranged in a box body; one end of the overturning part is rotatably connected with the lifting plate, and a force storage assembly is arranged on the overturning part; the lifting structure is arranged at the bottom of the box body and connected with the lifting plate, the inclined turnover structure is arranged between the turnover part and the inner wall of the box body, and the locking assembly is arranged on the turnover part. The lifting plate is driven to be lifted from the bottom of the box body through the lifting structure, the overturning part is driven to be lifted in the lifting process, one end of the overturning part is driven to rotate around the lifting plate through the inclined overturning structure, the overturning part is enabled to rotate to incline from the parallel lifting plate, and the take-off posture is adjusted; at the relative lifting plate pivoted in-process of upset piece, utilize and hold power subassembly storage elastic potential energy, after unmanned aerial vehicle held in the palm completely and adjusted the gesture from the box, through helping flying to unmanned aerial vehicle under the elastic potential energy effect of holding power subassembly storage to the locking subassembly unblock.
Description
Technical Field
The invention relates to an auxiliary tool for an unmanned aerial vehicle, in particular to a multistation type unmanned aerial vehicle-mounted departure vehicle with an unmanned aerial vehicle capable of independently receiving and transmitting.
Background
Unmanned aerial vehicle's a great variety, usage are extensive, and some unmanned aerial vehicles still have multiple use, and some unmanned aerial vehicle have the wing, and some unmanned aerial vehicle wings are from surperficial and can not see, for example military unmanned aerial vehicle, can not see the rotor from the appearance. The unmanned aerial vehicle without the rotor wing type takes off and lands without a launcher, and the unmanned aerial vehicle without the rotor wing type needs to help flying by means of an undercarriage.
Most of the existing landing gears have single station and do not have the function of assisting flight, and the existing landing gears are very inconvenient to launch.
Disclosure of Invention
The invention aims to provide a multistation type unmanned aerial vehicle-mounted departure vehicle with independent receiving and sending functions of an unmanned aerial vehicle, and aims to solve the problems in the background technology.
In order to achieve the purpose, the invention provides the following technical scheme:
a multistation formula unmanned aerial vehicle that unmanned aerial vehicle received and dispatched independently carries out car includes:
the bicycle frame is fixedly provided with a box body with an opening at the upper end;
the lifting plate is horizontally arranged and movably arranged in the box body along the height direction of the box body;
the overturning device comprises an overturning piece, a lifting plate and a lifting mechanism, wherein one end of the overturning piece is rotatably connected with the lifting plate, a force storage component is arranged on the overturning piece, and the force storage component stores elastic potential energy when the overturning piece rotates to incline from parallel to the lifting plate relative to the lifting plate;
the lifting structure is arranged at the bottom of the box body and connected with the lifting plate, and the lifting structure is used for driving the lifting plate to move along the height direction of the box body;
the inclined overturning structure is arranged between the overturning part and the inner wall of the box body, and drives the overturning part to rotate relative to the lifting plate when the lifting plate moves along the height direction of the box body;
the locking assembly is arranged on the overturning part and matched with the power accumulating assembly to fix the unmanned aerial vehicle on the overturning part.
The multi-station unmanned aerial vehicle-mounted departure with independent receiving and sending of the unmanned aerial vehicle comprises the following steps: the elevation structure includes:
the bidirectional screw rod is horizontally and rotatably arranged at the bottom of the box body, and external threads with opposite thread turning directions are symmetrically arranged on two sides of the bidirectional screw rod;
the two screw sleeves are respectively matched with the external threads on the two sides of the bidirectional screw rod;
the two connecting rods are symmetrically arranged, and one end of one connecting rod, which is close to the bidirectional screw rod, is rotationally connected with one of the turnbuckles; one end of the other connecting rod, which is close to the bidirectional screw rod, is rotatably connected with the other thread sleeve, and the other ends of the two connecting rods are rotatably connected with the lifting plate.
The multi-station unmanned aerial vehicle-mounted departure with independent receiving and sending of the unmanned aerial vehicle comprises the following steps: the two groups of lifting structures are connected through transmission parts, and the two-way screw rods in the two groups of lifting structures are connected through the transmission parts;
one end of a bidirectional screw rod in one group of lifting structures penetrates out of the side wall of the box body and is connected with the side wall of the box body in a rotating mode, and one end of the bidirectional screw rod penetrating out of the side wall of the box body is connected with a motor output end fixed on the outer wall of the box body.
The multi-station unmanned aerial vehicle that unmanned aerial vehicle independently received and dispatched as described above carries the departure: a sliding groove arranged along the height of the box body is fixed on the inner wall of the box body, and a bulge in sliding fit with the sliding groove is integrally arranged on the side wall of the lifting plate;
the upper portion of box rotates and is provided with the case lid of the last port looks adaptation of box, and just be in below one side of frame is provided with a set of universal wheel, and the opposite side is provided with a set of removal wheel.
The multi-station unmanned aerial vehicle-mounted departure with independent receiving and sending of the unmanned aerial vehicle comprises the following steps: the structure of turning over to one side includes:
the fixed shaft is fixed with one end of the overturning piece;
the gear is fixed on the fixed shaft;
the toothed plate is fixed on the inner wall of the box body along the height direction of the box body, and the toothed plate is meshed with the gear.
The multi-station unmanned aerial vehicle-mounted departure with independent receiving and sending of the unmanned aerial vehicle comprises the following steps: the power storage assembly includes:
the sleeve is horizontally fixed on the turnover part, and two ends of the sleeve are communicated;
one end of the push rod extends into the sleeve from one end of the sleeve and is connected with the sleeve in a sliding mode;
one end of the boosting rod extends into the sleeve from the other end of the sleeve and is connected with the sleeve in a sliding manner;
the spring is arranged in the sleeve, one end of the spring is abutted to one end, extending into the sleeve, of the boosting rod, and the other end of the spring is abutted to one end, extending into the sleeve, of the push rod;
the extrusion piece is fixed at one end of the push rod extending out of the sleeve;
the flying assisting plate is fixed at one end of the boosting rod, which extends out of the sleeve;
the pulling structure is arranged between the extrusion part and the lifting plate and drives the push rod to further extend into the sleeve to extrude the spring when the overturning part rotates around the axis of the fixed shaft;
the flight assisting plate is matched with the locking assembly to fix the rear wheel of the unmanned aerial vehicle.
The multi-station unmanned aerial vehicle-mounted departure with independent receiving and sending of the unmanned aerial vehicle comprises the following steps: the pulling structure comprises:
one end of the force storage rod is rotatably connected with the lifting plate;
the through groove is formed in one side, close to the fixed shaft, of the turnover piece;
the sliding plate penetrates through the through groove and is in sliding embedded with the through groove, and the other end of the force storage rod is rotatably connected with one end of the sliding plate, which penetrates through the through groove;
wherein the extrusion is fixed with the slide plate.
The multi-station unmanned aerial vehicle-mounted departure with independent receiving and sending of the unmanned aerial vehicle comprises the following steps: the upper parts of two sides of the sliding plate are provided with convex blocks, the lower parts of two sides are also provided with convex blocks, the convex blocks on the upper parts are in sliding fit with the upper surface of the overturning part, and the convex blocks on the lower parts are in sliding fit with the lower surface of the overturning part.
The multi-station unmanned aerial vehicle-mounted departure with independent receiving and sending of the unmanned aerial vehicle comprises the following steps: the locking assembly comprises a stop block, and the stop block penetrates through a lock hole formed in the turnover piece along the height direction of the box body;
the stopping blocks are connected with the overturning part through a driving structure, the number of the stopping blocks is three, two of the stopping blocks are close to the fixed shaft, the other stopping block is far away from the fixed shaft, and the two stopping blocks close to the fixed shaft are collinear in the width direction of the overturning part.
The multi-station unmanned aerial vehicle-mounted departure with independent receiving and sending of the unmanned aerial vehicle comprises the following steps: the driving structure comprises a lifter, a driving piece and a connecting piece, wherein the lifter is arranged on one surface of the overturning piece, which is far away from the power storage assembly, the driving piece is connected with the output end of the lifter, and the connecting piece is fixed at one end of the driving piece and is fixed with the stop block;
wherein a receiver in signal communication with the riser is mounted on the lift plate.
Compared with the prior art, the invention has the beneficial effects that: the lifting plate is driven by the lifting structure to be lifted from the bottom of the box body, the lifting plate drives the overturning part to lift along with the lifting plate in the lifting process, and in the lifting process, the tilting structure is utilized to drive one end of the overturning part to rotate around the lifting plate, so that the overturning part rotates to incline from the parallel lifting plate, the unmanned aerial vehicle fixed on the overturning part is lifted from the box body and inclines upwards at the same time, and the take-off posture is adjusted;
in addition, in the process that the turnover part rotates relative to the lifting plate, the force storage component is used for storing elastic potential energy, and after the unmanned aerial vehicle is completely lifted out of the box body and the posture of the unmanned aerial vehicle is adjusted, the locking component is unlocked to help the unmanned aerial vehicle fly under the action of the elastic potential energy stored by the force storage component;
the device can adjust unmanned aerial vehicle's the height of taking off and angle according to the actual demand, reaches the multistation and carries out the effect.
Drawings
Fig. 1 is a schematic structural view of a multistation type unmanned aerial vehicle-mounted departure with independent transceiving of an unmanned aerial vehicle.
Fig. 2 is a schematic structural diagram of a multi-station unmanned aerial vehicle with a detachable cover for independent receiving and transmitting of the unmanned aerial vehicle.
Fig. 3 is a schematic structural view of the case cut away in part on the basis of fig. 2.
Fig. 4 is a schematic structural diagram of a lifting structure and a lifting plate in a multistation type unmanned aerial vehicle-mounted departure with independent transceiving of an unmanned aerial vehicle.
Fig. 5 is a schematic structural diagram of the multi-station unmanned aerial vehicle-mounted departure vehicle-mounted power storage rod and the lifting plate when being disassembled, wherein the multi-station unmanned aerial vehicle-mounted departure vehicle-mounted power storage rod and the lifting plate are independently received and transmitted by the unmanned aerial vehicle.
FIG. 6 is a schematic illustration of the construction of the power storage assembly when detached from the flipper.
Fig. 7 is a schematic structural diagram of a power accumulating assembly in a multistation type unmanned aerial vehicle-mounted departure system with independent transceiving of an unmanned aerial vehicle.
Fig. 8 is a schematic view of the driving structure on the back side of the flipper.
Fig. 9 is a partially enlarged view of a point a in fig. 8.
In the figure: 1-a vehicle frame; 2-a box body; 3-box cover; 4-lifting the plate; 5-bulge; 6-a chute; 7-a motor; 8-a bidirectional screw rod; 9-thread sleeve; 10-a connecting rod; 11-a flip-over member; 12-a stationary shaft; 13-a gear; 14-toothed plate; 15-a transmission member; 16-an accumulator rod; 17-a slide plate; 18-an extrusion; 19-a push rod; 20-a sleeve; 21-a booster rod; 22-a flight aid plate; 23-a spring; 24-a stop block; 25-a lifter; 26-a drive member; 27-a connector; 28-a receiver; 29-through groove.
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.
Referring to fig. 1 to 9, as an embodiment of the present invention, the multi-station type unmanned aerial vehicle for unmanned aerial vehicle independent transceiving sends out includes:
the bicycle frame comprises a frame 1, wherein a box body 2 with an opening at the upper end is fixed on the frame 1;
the lifting plate 4 is horizontally arranged, and the lifting plate 4 is movably arranged in the box body 2 along the height direction of the box body 2;
the overturning part 11, one end of the overturning part 11 is rotationally connected with the lifting plate 4, and the overturning part 11 is provided with a force storage component which stores elastic potential energy when the overturning part 11 rotates to incline from parallel to the lifting plate 4;
the lifting structure is arranged at the bottom of the box body 2 and is connected with the lifting plate 4, and the lifting structure is used for driving the lifting plate 4 to move along the height direction of the box body 2;
the inclined overturning structure is arranged between the overturning part 11 and the inner wall of the box body 2, and drives the overturning part 11 to rotate relative to the lifting plate 4 when the lifting plate 4 moves along the height direction of the box body 2;
the locking assembly is arranged on the overturning piece 11, and the locking assembly is matched with the power accumulating assembly to fix the unmanned aerial vehicle on the overturning piece 11.
The lifting plate 4 is driven to be lifted from the bottom of the box body 2 through the lifting structure, the lifting plate 4 drives the overturning part 11 to lift along with the lifting plate 4 in the lifting process, and in the lifting process, the inclined overturning structure is utilized to drive one end of the overturning part 11 to rotate around the lifting plate 4, so that the overturning part 11 rotates to incline from the parallel lifting plate 4, the unmanned aerial vehicle fixed on the overturning part 11 is inclined upwards while being lifted from the box body 2, and the take-off posture is well adjusted;
in addition, in the process that the turnover piece 11 rotates relative to the lifting plate 4, the force storage component is used for storing elastic potential energy, and after the unmanned aerial vehicle is completely lifted out of the box body 2 and the posture is adjusted, the locking component is unlocked to help the unmanned aerial vehicle fly under the action of the elastic potential energy stored by the force storage component;
the device can adjust unmanned aerial vehicle's take-off height and angle according to the actual demand, reaches the multistation and carries and send out the effect.
As a further scheme of the present invention, referring to fig. 3, the lifting structure includes:
the bidirectional screw rod 8 is horizontally and rotatably arranged at the bottom of the box body 2, and external threads with opposite thread turning directions are symmetrically arranged on two sides of the bidirectional screw rod 8;
two screw sleeves 9 are arranged and are respectively matched with the external threads on the two sides of the bidirectional screw rod 8;
the two connecting rods 10 are symmetrically arranged, and one end of one connecting rod 10 close to the bidirectional screw rod 8 is rotatably connected with one thread sleeve 9; one end of the other connecting rod 10 close to the bidirectional screw rod 8 is rotatably connected with the other threaded sleeve 9, and the other ends of the two connecting rods 10 are rotatably connected with the lifting plate 4.
In the embodiment, when the bidirectional screw 8 rotates, the screw sleeves 9 on the two sides are driven to mutually approach or separate, so that the Lijiagan 10 on the two sides drives the lifting plate 4 to move upwards and downwards along the height direction of the box body 2, and the lifting plate 4 is lifted from the box body 2 or falls into the box body 2.
As a further scheme of the present invention, please refer to fig. 4, the two sets of lifting structures are provided, and the two-way screws 8 in the two sets of lifting structures are connected through a transmission member 15;
one end of a bidirectional screw rod 8 in one group of lifting structures penetrates through the side wall of the box body 2 and is rotatably connected with the side wall of the box body 2, and one end of the bidirectional screw rod 8 penetrating through the side wall of the box body 2 is connected with an output end of a motor 7 fixed on the outer wall of the box body 2.
In the embodiment, the two groups of lifting structures are arranged, so that the stability of the lifting plate 4 can be improved, the pressure of a single group of lifting structure can be shared, the two-way screw rods 8 in the two groups of lifting structures are connected through the transmission part 15, and the motor 7 is not required to be additionally arranged;
the connecting rod 10 is driven by adopting thread transmission to support the lifting plate 4, so that the lifting plate has the characteristics of labor saving and low requirement on the torque of the motor 7, and has a self-locking function to prevent the lifting plate 4 from falling after being supported to a set height.
As a further scheme of the present invention, please refer to fig. 1 and 3, a sliding groove 6 is fixed on the inner wall of the box body 2 along the height thereof, and a protrusion 5 in sliding fit with the sliding groove 6 is integrally arranged on the side wall of the lifting plate 4;
the upper portion of box 2 rotates and is provided with the case lid 3 of the last port looks adaptation of box 2, and be in frame 1's below one side is provided with a set of universal wheel, and the opposite side is provided with a set of removal wheel.
In this embodiment, the moving direction of the whole vehicle-mounted can be adjusted through the arranged universal wheels, and the vehicle-mounted can be moved to the launching position through matching with the moving wheels.
In addition, the lifting plate 4 can be kept to be always horizontally positioned in the box body 2 through the matching of the arranged sliding groove 6 and the protrusion 5, and the side turning cannot occur.
As a still further solution of the present invention, referring to fig. 2, fig. 3 and fig. 4, the flip structure includes:
the fixed shaft 12 is fixed with one end of the overturning part 11;
a gear 13, wherein the gear 13 is fixed on the fixed shaft 12;
a toothed plate 14, wherein the toothed plate 14 is fixed on the inner wall of the box body 2 along the height direction of the box body 2, and the toothed plate 14 is meshed with the gear 13.
When the lifting plate 4 moves along the height direction of the box body 2, the fixed shaft 12 is driven to move upwards along with the lifting plate, the gear 13 is driven to rotate by the action of the gear 13 and the fixed toothed plate 14 in the process of moving upwards, the gear 13 drives the fixed shaft 12 and the turnover part 11 to rotate, and therefore the turnover part 11 is turned to be inclined from a position parallel to the lifting plate 4.
As a still further aspect of the present invention, referring to fig. 3, 6 and 7, the power storage assembly comprises:
the sleeve 20 is horizontally fixed on the turnover part 11, and two ends of the sleeve 20 are communicated;
a push rod 19, one end of the push rod 19 extends into the sleeve 20 from one end of the sleeve 20 and is connected with the sleeve 20 in a sliding mode;
the power assisting rod 21 extends into the sleeve 20 from the other end of the sleeve 20 at one end of the power assisting rod 21 and is connected with the sleeve 20 in a sliding mode;
the spring 23 is arranged in the sleeve 20, one end of the spring 23 is abutted with one end of the boosting rod 21 extending into the sleeve 20, and the other end of the spring 23 is abutted with one end of the push rod 19 extending into the sleeve 20;
an extruding part 18, wherein the extruding part 18 is fixed at one end of the push rod 19 extending out of the sleeve 20;
the flying assisting plate 22 is fixed at one end of the boosting rod 21, which extends out of the sleeve 20;
a pulling structure arranged between the extrusion part 18 and the lifting plate 4, wherein the pulling structure drives the push rod 19 to further extend into the sleeve 20 to squeeze the spring 23 when the turnover part 11 rotates around the axis of the fixed shaft 12;
the flight assistance board 22 cooperates with the locking assembly for securing the rear wheels of the drone.
When the turnover part 11 rotates around the axis of the fixed shaft 12 relative to the lifting plate 4, one end of the push rod 19 extending into the sleeve 20 is driven by the traction structure to extrude the spring 23, so that the spring 23 stores elastic potential energy; after the locking subassembly unblock, utilize spring 23's elastic force to drive helping hand pole 21 to promote and help flying board 21 to launch fast to the driving unmanned aerial vehicle rear wheel removes along the incline direction of upset piece 11, plays and helps flying the function.
As a still further aspect of the present invention, referring to fig. 5 and 6, the pulling structure includes:
the power storage rod 16, one end of the power storage rod 16 is rotatably connected with the lifting plate 4;
the through groove 29 is formed in one side, close to the fixed shaft 12, of the overturning part 11, and the through groove 29 is formed in the other side;
a slide plate 17, wherein the slide plate 17 passes through the through groove 29 and is in sliding fit with the through groove, and the other end of the force storage rod 16 is rotatably connected with one end of the slide plate 17 passing through the through groove 29;
the extrusion part 18 is fixed with the sliding plate 17, the upper parts of two sides of the sliding plate 17 are provided with convex blocks, the lower parts of two sides are also provided with convex blocks, the convex blocks on the upper parts are in sliding fit with the upper surface of the turnover part 11, and the convex blocks on the lower parts are in sliding fit with the lower surface of the turnover part 11.
During the process of the tilting element 11 relative to the lifting plate 4, the force storage rod 16 drives the sliding plate 17 to slide along the through groove 29 and away from the fixed shaft 12, the sliding plate 17 drives the extrusion element 18 to move in the direction away from the fixed shaft 12, and drives the push rod 19 to continuously extrude into the sleeve 20 to compress the spring 23.
As a further aspect of the present invention, referring to fig. 6, 8 and 9, the locking assembly includes a stop block 24, and the stop block 24 passes through a lock hole formed on the flip member 11 along the height direction of the box body 2;
the stop blocks 24 are connected with the flip member 11 through a driving structure, wherein the number of the stop blocks 24 is three, two of the stop blocks are close to the fixed shaft 12, the other stop block is far away from the fixed shaft 12, and the two stop blocks 24 close to the fixed shaft 12 are collinear in the width direction of the flip member 11.
After upset piece 11 held up and slope from box 2, utilize drive structure to drive backstop 24 and slide to flushing with upset piece 11 along the lockhole, drive helping hand pole 21 and help flying board 22 and promote the unmanned aerial vehicle rear wheel slant and upwards bounce fast under the spring action of spring 23 this moment, reach and help and fly the effect.
As a further aspect of the present invention, referring to fig. 9, the driving structure includes a lifter 25 mounted on a side of the flip member 11 away from the power storage assembly, a driving member 26 connected to an output end of the lifter 25, and a connecting member 27 fixed to an end of the driving member 26 and fixed to the stop block 24;
wherein a receiver 28 is mounted on the lifting plate 4 in signal communication with the riser 25.
The lifter 25 includes but not limited to a pneumatic lifter, a hydraulic lifter, an electromagnetic lifter, and belongs to the application of the prior art, after the turnover part 11 is lifted from the box body 2 and is inclined to a predetermined height and angle, an unlocking signal is sent to the receiver 28 through a remote controller, the receiver 28 controls the lifter 25 to drive the driving part 26 to move, the connecting part 27 drives the stopping block 24 to move in a direction away from the power storage assembly, and when the stopping block 24 slides along a lock hole to be flush with the turnover part 11, the flying assisting plate 22 bounces the rear wheel of the unmanned aerial vehicle to assist flying.
The above embodiments are exemplary rather than limiting, and embodiments of the invention may be embodied in other specific forms without departing from the spirit or essential characteristics thereof.
Claims (9)
1. The utility model provides an unmanned aerial vehicle independently receives and dispatches multistation formula unmanned aerial vehicle carries departure which characterized in that includes:
the bicycle frame comprises a bicycle frame (1), wherein a box body (2) with an opening at the upper end is fixed on the bicycle frame (1);
the lifting plate (4) is horizontally arranged and movably arranged in the box body (2) along the height direction of the box body (2);
the overturning device comprises an overturning part (11), wherein one end of the overturning part (11) is rotatably connected with the lifting plate (4), a force storage component is arranged on the overturning part (11), and the force storage component stores elastic potential energy when the overturning part (11) rotates to incline from parallel relative to the lifting plate (4);
the lifting structure is arranged at the bottom of the box body (2) and is connected with the lifting plate (4);
the inclined overturning structure is arranged between the overturning part (11) and the inner wall of the box body (2), and drives the overturning part (11) to rotate relative to the lifting plate (4) when the lifting plate (4) moves along the height direction of the box body (2);
a locking assembly provided on the flipper (11).
2. The multi-station unmanned aerial vehicle that unmanned aerial vehicle independently transceives carries out departure from a vehicle of claim 1, wherein the elevation structure comprises:
the bidirectional screw rod (8) is horizontally and rotatably arranged at the bottom of the box body (2), and external threads with opposite thread turning directions are symmetrically arranged on two sides of the bidirectional screw rod (8);
the number of the screw sleeves (9) is two, and the two screw sleeves (9) are respectively matched with the external threads on the two sides of the bidirectional screw rod (8);
the two connecting rods (10) are symmetrically arranged, one end of one connecting rod (10) close to the bidirectional screw rod (8) is rotatably connected with one threaded sleeve (9); one end of the other connecting rod (10) close to the two-way screw rod (8) is rotatably connected with the other threaded sleeve (9), and the other ends of the two connecting rods (10) are rotatably connected with the lifting plate (4).
3. The multi-station unmanned aerial vehicle that is independently transceived by an unmanned aerial vehicle carries a departure car according to claim 2, wherein the lifting mechanisms are two sets, and the two-way screws (8) of the two sets of lifting mechanisms are connected by a transmission member (15);
one end of a bidirectional screw rod (8) in one group of lifting structures penetrates out of the side wall of the box body (2) and is rotationally connected with the side wall of the box body, and one end of the bidirectional screw rod (8) penetrating out of the side wall of the box body (2) is connected with an output end of a motor (7) fixed on the outer wall of the box body (2).
4. The multi-station unmanned aerial vehicle-mounted departure cart capable of being independently transceived by unmanned aerial vehicles according to claim 1, wherein a sliding groove (6) is fixed on the inner wall of the box body (2) along the height of the box body, and a protrusion (5) which is in sliding fit with the sliding groove (6) is integrally arranged on the side wall of the lifting plate (4);
the upper portion of box (2) rotates and is provided with case lid (3) of the last port looks adaptation of box (2), and be in frame (1) below one side is provided with a set of universal wheel, and the opposite side is provided with a set of removal wheel.
5. The unmanned aerial vehicle independent transceiving multistation unmanned aerial vehicle-mounted departure car of claim 1, wherein said tilt structure comprises:
the fixed shaft (12), the said fixed shaft (12) is fixed with one end of the said turning member (11);
a gear (13), said gear (13) being fixed to said stationary shaft (12);
the toothed plate (14), the toothed plate (14) is fixed on the inner wall of the box body (2) along the height direction of the box body (2), and the toothed plate (14) is meshed with the gear (13).
6. The unmanned aerial vehicle multi-station unmanned aerial vehicle that independently transceives of claim 5, wherein the power storage assembly comprises:
the sleeve (20), the said sleeve (20) is fixed on said turning part (11) horizontally, both ends of the said sleeve (20) are run through;
the push rod (19), one end of the push rod (19) stretches into the sleeve (20) from one end of the sleeve (20) and is connected with the sleeve (20) in a sliding mode;
the power-assisted rod (21), one end of the power-assisted rod (21) extends into the sleeve (20) from the other end of the sleeve (20) and is connected with the sleeve (20) in a sliding manner;
the spring (23) is arranged in the sleeve (20), one end of the spring (23) abuts against one end, extending into the sleeve (20), of the boosting rod (21), and the other end of the spring (23) abuts against one end, extending into the sleeve (20), of the push rod (19);
a pressing piece (18), wherein the pressing piece (18) is fixed at one end of the push rod (19) extending out of the sleeve (20);
the auxiliary flying plate (22), the auxiliary flying plate (22) is fixed at one end of the boosting rod (21) extending out of the sleeve (20);
a pulling structure arranged between the extrusion part (18) and the lifting plate (4), and the pulling structure drives the push rod (19) to further extend into the sleeve (20) to extrude a spring (23) when the overturning part (11) rotates around the axis of the fixed shaft (12);
the flight assisting plate (22) is matched with the locking assembly to fix a rear wheel of the unmanned aerial vehicle;
the pulling structure comprises:
one end of the power storage rod (16) is rotatably connected with the lifting plate (4);
the through groove (29) is formed in one side, close to the fixed shaft (12), of the turnover piece (11);
the sliding plate (17) penetrates through the through groove (29) and is in sliding fit with the through groove, and the other end of the force storage rod (16) is rotatably connected with one end, penetrating through the through groove (29), of the sliding plate (17);
wherein the pressing part (18) is fixed with the sliding plate (17).
7. The unmanned aerial vehicle of claim 6, wherein the unmanned aerial vehicle is capable of receiving and dispatching multiple unmanned aerial vehicles independently,
the upper parts of two sides of the sliding plate (17) are provided with convex blocks, the lower parts of two sides are also provided with convex blocks, the convex blocks on the upper parts are in sliding fit with the upper surface of the turnover part (11), and the convex blocks on the lower parts are in sliding fit with the lower surface of the turnover part (11).
8. The multi-station unmanned aerial vehicle that unmanned aerial vehicle receives and dispatches independently carries out departure from machine of claim 1, characterized in that, the locking assembly includes backstop (24), stop (24) along the direction of height of box (2) pass set up in the lockhole on upset piece (11);
the stop blocks (24) are connected with the turnover part (11) through a driving structure, the number of the stop blocks (24) is three, two of the stop blocks are close to the fixed shaft (12), the other stop block is far away from the fixed shaft (12), and the two stop blocks (24) close to the fixed shaft (12) are collinear in the width direction of the turnover part (11).
9. The unmanned aerial vehicle multi-station unmanned aerial vehicle-mounted departure cart independent of unmanned aerial vehicle transceiving according to claim 8, wherein said driving structure comprises a lifter (25) mounted on a side of said flip member (11) facing away from said power accumulating assembly, a driving member (26) connected to an output end of said lifter (25), and a connecting member (27) fixed to one end of said driving member (26) and fixed to said stop block (24);
wherein a receiver (28) in signal communication with the riser (25) is mounted on the lifting plate (4).
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