CN216659710U - A fixed equipment that is used for emergent unmanned aerial vehicle in removing command car - Google Patents
A fixed equipment that is used for emergent unmanned aerial vehicle in removing command car Download PDFInfo
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- CN216659710U CN216659710U CN202123076919.3U CN202123076919U CN216659710U CN 216659710 U CN216659710 U CN 216659710U CN 202123076919 U CN202123076919 U CN 202123076919U CN 216659710 U CN216659710 U CN 216659710U
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
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- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
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Abstract
The utility model provides a fixing device for an unmanned aerial vehicle in an emergency mobile command vehicle, which comprises: the fixed platform comprises a box body and a table board, notches are formed in the four edges of the table board, and a transmission device is arranged in the box body; the transmission device comprises a pair of guide shafts which are vertically arranged in a staggered manner and are arranged close to the edge of the box body, and a bearing seat is arranged at the center of each guide shaft; the servo motor is arranged in parallel with the guide shaft and is connected with the guide shaft through a first synchronous belt; the second synchronous belts are arranged at two ends of the guide shaft, one ends of the second synchronous belts are connected with the end parts of the guide shaft, the other ends of the second synchronous belts are connected with the supporting columns, and the supporting columns are arranged on the side walls of the box body; the pair of synchronous belt connecting pieces are symmetrically arranged at the upper part and the lower part of the second synchronous belt; one end of the push rod fixing piece is fixedly connected with the synchronous belt connecting piece; the clamping push rod is fixedly arranged at the other end of the push rod fixing piece; the other end of the push rod fixing piece extends out of the notch, and the clamping push rod is positioned on the table board. Can be with accurate location of falling in the middle of unmanned aerial vehicle.
Description
Technical Field
The utility model relates to the technical field of auxiliary equipment of unmanned aerial vehicles, in particular to fixing equipment for an unmanned aerial vehicle in an emergency mobile command vehicle.
Background
With the application of the unmanned aerial vehicle industry in various fields becoming more and more extensive, the control distance of the unmanned aerial vehicle and the flight distance limited by the electric quantity also gradually become a worldwide difficult problem, so the unmanned aerial vehicle emergency command vehicle is also gradually applied in various fields. Through set up fixed equipment in the emergent car that removes the command car of unmanned aerial vehicle, can realize taking off of unmanned aerial vehicle in emergent removal command car.
Because there are certain deviation and declination when unmanned aerial vehicle descends, unmanned aerial vehicle's wing is great moreover a bit, leads to the unmanned aerial vehicle to descend to the emergent locomotive in can't smoothly behind the roof platform.
Therefore, there is a need to develop a fixing device for an unmanned aerial vehicle in an emergency mobile command car, which can accurately position the unmanned aerial vehicle, and further realize the function of flying the unmanned aerial vehicle in the emergency mobile command car.
SUMMERY OF THE UTILITY MODEL
The present invention is directed to solving one of the technical problems of the prior art or the related art.
Therefore, the utility model provides a fixing device for an unmanned aerial vehicle in an emergency mobile command vehicle.
In view of the above, the present invention provides a fixing device for an unmanned aerial vehicle in an emergency mobile command vehicle, including:
the fixed platform comprises a box body and a table top fixed on the box body, wherein notches are formed in four sides of the table top, and a transmission device is arranged in the box body; wherein the transmission comprises:
the pair of guide shafts is vertically arranged in a staggered manner, the guide shafts are arranged close to the edge of the box body, a bearing seat is arranged at the center of each guide shaft, and the bottom of each bearing seat is fixedly connected with the bottom wall of the box body;
the servo motor is arranged in parallel with the guide shaft and is connected with the guide shaft through a first synchronous belt;
the second synchronous belts are arranged at two ends of the guide shaft, one ends of the second synchronous belts are connected with the end parts of the guide shaft, the other ends of the second synchronous belts are connected with the supporting columns, and the supporting columns are arranged on the side walls of the box body;
the pair of synchronous belt connecting pieces are symmetrically arranged at the upper part and the lower part of the second synchronous belt;
the push rod fixing piece is fixedly connected with one end of the push rod fixing piece and the synchronous belt connecting piece;
the clamping push rod is fixedly arranged at the other end of the push rod fixing piece;
the other end of the push rod fixing piece extends out of the notch, and the clamping push rod is located on the table top.
Further, the transmission device further includes:
the rail is arranged on the side wall of the box body;
the linear sliding block is arranged on the track and fixedly connected with the synchronous belt connecting piece.
Further, the transmission device further includes:
and the speed reducer is arranged between the servo motor and the first synchronous belt.
Further, the transmission device further includes:
and the anti-collision blocks are respectively positioned at the two ends of the second synchronous belt and at the central position of the second synchronous belt, and the anti-collision blocks are fixedly connected with the side wall of the box body.
Further, the fixing apparatus further includes:
fixing device, set up in centre department of centre gripping push rod, fixing device includes:
the fixing seat is fixedly connected with the clamping push rod;
the fixing clamp is hinged with the fixing seat;
the locating pin runs through set up in the direction of height of fixing base, the fixation clamp with when the fixing base is parallel, the locating pin can also run through the fixation clamp.
Further, a magnet is arranged on one side, deviating from the clamping push rod, of the fixing seat, and the magnet is fixed on the fixing seat through special glue.
Further, hold-in range connecting piece include, first diaphragm and with the L shaped plate that first diaphragm set up perpendicularly, first diaphragm pass through the bolt with second hold-in range fixed connection, the shaped plate with first diaphragm forms an holding tank.
Further, the push rod mounting includes a pair of second diaphragm of parallel arrangement and the swash plate of connecting a pair of second diaphragm, one of them the second diaphragm with hold-in range connecting piece fixed connection, another the second diaphragm with centre gripping push rod fixed connection.
Further, the table-board is a carbon fiber table-board.
The technical scheme provided by the utility model can have the following beneficial effects:
can drive the centre gripping push rod through transmission and remove, realize that a plurality of centre gripping push rods remove or remove all around to the box to the center simultaneously, and then realize returning in to the centre of unmanned aerial vehicle on fixed platform, can be with the accurate location of unmanned aerial vehicle, and then realize that unmanned aerial vehicle flies the function in emergent removal command car, can provide one for unmanned aerial vehicle and take off, descend the platform, and need not to take to look for suitable landing environment of taking off outside the car.
It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory only and are not restrictive of the utility model, as claimed.
Drawings
The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate embodiments consistent with the utility model and together with the description, serve to explain the principles of the utility model.
In order to more clearly illustrate the embodiments or technical solutions in the prior art of the present invention, the drawings used in the description of the embodiments or prior art will be briefly described below, and it is obvious for those skilled in the art that other drawings can be obtained based on these drawings without creative efforts.
Fig. 1 shows a schematic view of a fixture for an unmanned aerial vehicle in an emergency mobile command vehicle according to one embodiment of the utility model;
FIG. 2 shows a schematic view of the interior of a cabinet according to one embodiment of the utility model;
FIG. 3 shows a top view of the interior of a cabinet according to one embodiment of the utility model;
FIG. 4 shows an enlarged view at A of FIG. 2 in accordance with the present invention;
FIG. 5a illustrates a schematic non-operational state of a fixation device according to an embodiment of the present invention;
FIG. 5b illustrates a schematic view of the working state of a fixture according to one embodiment of the present invention;
figure 6 shows a schematic diagram of a synchronous belt connection according to one embodiment of the present invention;
FIG. 7 shows a schematic view of a putter holder according to one embodiment of the present invention.
Wherein, the correspondence between the reference numbers and the part names in fig. 1 to 7 is:
100 fixed equipment, 110 fixed platform, 1101 box, 1102 mesa, 1103 notches, 120 transmission, 1201 guiding axle, 1202 bearing seat, 1203 servo motor, 1204 speed reducer, 1205 first synchronous belt, 1206 second synchronous belt, 1207 support column, 1208 synchronous belt connecting piece, 1208a first horizontal plate, 1208bL shaped plate, 1208c holding tank, 1209 push rod fixing piece, 1209a second horizontal plate, 1209b swash plate, 1210 centre gripping push rod, 1211 straight line slider, 1212 anticollision piece, 1213 track, 130 fixing device, 1301 fixing base, 1302 fixing clip, 1303 locating pin, 1304 magnet, 200 unmanned aerial vehicle.
Detailed Description
Reference will now be made in detail to the exemplary embodiments, examples of which are illustrated in the accompanying drawings. When the following description refers to the accompanying drawings, like numbers in different drawings represent the same or similar elements unless otherwise indicated. The embodiments described in the following exemplary embodiments do not represent all embodiments consistent with the present invention. Rather, they are merely examples of apparatus and methods consistent with certain aspects of the utility model, as detailed in the appended claims.
Examples
Fig. 1 shows a schematic view of a fixture for an unmanned aerial vehicle in an emergency mobile command vehicle according to one embodiment of the utility model; FIG. 2 shows a schematic view of the interior of a cabinet according to one embodiment of the utility model; FIG. 3 shows a top view of the interior of a cabinet according to one embodiment of the utility model.
As shown in fig. 1 to 3, the present embodiment provides a fixing device for a drone in an emergency mobile command vehicle, where the fixing device 100 includes:
the fixed platform 110 comprises a box 1101 and a table 1102 fixed on the box 1101, notches 1103 are arranged at four sides of the table 1102, and the transmission device 120 is arranged in the box 1101; wherein the transmission 120 includes:
the guide shafts 1201 are vertically staggered, the guide shafts 1201 are arranged close to the side parts of the box body 1101, a bearing seat 1202 is arranged at the center of each guide shaft 1201, and the bottom of each bearing seat 1202 is fixedly connected with the bottom wall of the box body 1101;
a servo motor 1203 arranged in parallel with the guide shaft 1201, the servo motor 1203 being connected to the guide shaft 1201 through a first synchronization belt 1205;
the second synchronous belts 1206 are arranged at two ends of the guide shaft 1201, one end of each second synchronous belt 1206 is connected with the end of the guide shaft 1201, the other end of each second synchronous belt 1206 is connected with a support column 1207, and the support columns 1207 are arranged on the side walls of the box body 1101;
a pair of synchronous belt connectors 1208 are symmetrically arranged at the upper and lower parts of the second synchronous belt 1206;
the push rod fixing piece 1209, one end of the push rod fixing piece 1209 is fixedly connected with the synchronous belt connecting piece 1208;
a clamping push rod 1210 fixedly arranged at the other end of the push rod fixing member 1209;
wherein the other end of the pushrod mount 1209 extends out of the notch 1103 and the clamping pushrod 1210 is positioned on the tabletop 1102.
Can drive centre gripping push rod 1210 through transmission 120 and remove, realize that a plurality of centre gripping push rods 1210 remove simultaneously or remove all around to box 1101 to the center, and then realize getting in the middle of unmanned aerial vehicle 200 on fixed platform 110, can be with the accurate location of unmanned aerial vehicle 200, and then realize that unmanned aerial vehicle 200 flies the function in emergent removal command car, can provide one for unmanned aerial vehicle 200 and take off, the landing platform, and need not to take out the car and look for suitable landing environment of taking off.
Specifically, as shown in fig. 3, for example, the guide shaft 1201 in the X-axis direction is taken as an example, the servo motor 1203 rotates forward to drive the first synchronous belt 1205 to rotate clockwise, the first synchronous belt 1205 drives the guide shaft 1201 in the X-axis direction to rotate clockwise, the guide shaft 1201 rotates clockwise to drive the second synchronous belts 1206 at both ends to rotate clockwise, the second synchronous belt 1206 rotates clockwise to drive the synchronous belt connectors 1208 at the lower end to move leftward and simultaneously drive the synchronous belt connectors 1208 at the upper end to move rightward, two push rod fixing members 1209 are respectively fixed on the synchronous belt connectors 1208 at the upper end and the synchronous belt connectors 1208 at the lower end, the clamping push rods 1210 are fixed on the push rod fixing members 1209 on the second conveyor belts at both ends of the guide shaft 1201 in the X-axis direction, so that the clamping push rods 1210 move to both sides of the box 1101, i.e. an open state, when the servo motor 1203 rotates reversely, the two clamping push rods 1210 move to the center of the box 1101, i.e. the closed state. Similarly, when the servo motor 1203 on the guide shaft 1201 in the Y-axis direction rotates forward, the two clamping push rods 1210 are in an open state, and when the servo motor 1203 on the guide shaft 1201 in the Y-axis direction rotates backward, the two clamping push rods 1210 are in a closed state.
It should be noted that the heights of the shaft fixing members 1209 extending out of the notches 1103 are different, so that the two sets of holding shafts 1210 are arranged in a staggered manner, and interference is avoided, the notches 1103 are arranged at two ends of four sides of the table top 1102, that is, two notches 1103 are arranged on each side, and the edges of the notches 1103 have a limited effect on the moving position of the holding shafts 1210.
Wherein, servo motor 1203 is 200W's servo motor 1203, guiding axle 1201 supports through bearing frame 1202 and can guarantee that guiding axle 1201 can not warp because of receiving the external force influence, and the structural strength is improved, the guiding axle 1201 both ends all are equipped with second hold-in range 1206, then four second hold-in range 1206 altogether, be equipped with two hold-in range connecting pieces 1208 on every second hold-in range 1206, then total eight hold-in range connecting pieces 1208, and then there are eight push rod mounting 1209, can fix four centre gripping push rods 1210, four centre gripping push rods 1210 form the groined type setting.
Fig. 4 shows an enlarged view at a of fig. 2 according to the present invention.
As shown in fig. 4, the transmission 120 further includes:
a rail 1213 provided on a side wall of the case 1101;
and the linear slider 1211 is arranged on the track 1213, and the linear slider 1211 is fixedly connected with the synchronous belt connecting piece 1208.
It should be noted that, by arranging the linear slider 1211 on the track 1213, fixing the synchronous belt connector 1208 and the linear slider 1211, and rotating the second synchronous belt 1206, the synchronous belt connector 1208 and the linear slider 1211 can be driven to move on the track 1213, so that the synchronous belt connector 1208 can move repeatedly on the track 1213 very smoothly, and the stability of movement and the service life are ensured.
Further, the transmission 120 further includes:
the speed reducer 1204 is provided between the servo motor 1203 and the first timing belt 1205.
Wherein, speed reducer 1204 sets up between servo motor 1203 and first synchronous belt 1205, and the speed reducer 1204 of collocation through servo motor 1203 is first synchronous belt 1205 transmission power, can reduce the translation rate of centre gripping push rod 1210 to improve the thrust of centre gripping push rod 1210, in order to reach and promote the purpose placed in the middle with unmanned aerial vehicle 200.
It should be noted that the rotation speed and the torque of the motor are in an inverse relationship, and the larger the speed is, the smaller the torque is, the smaller the speed is, the driving shaft inside the speed reducer 1204 drives the pinion gear, and the pinion gear drives the gearwheel to achieve the purpose of speed reduction, so as to improve the torque of the motor and achieve the purpose of increasing the thrust.
In this embodiment, the reducer 1204 is a 1:10 reducer.
Further, the transmission 120 further includes:
the anti-collision blocks 1212 and the anti-collision blocks 1212 are respectively located at two ends of the second synchronous belt 1206 and at a center of the second synchronous belt 1206, and the anti-collision blocks 1212 are fixedly connected with the side wall of the box 1101.
It should be noted that, the two ends of the second synchronous belt 1206 and the center of the second synchronous belt 1206 are respectively provided with an anti-collision block 1212, so that there are 12 anti-collision blocks 1212 in total, when the servo motor 1203 fails and cannot stop or reverse in time, the push rod fixing member 1209 may collide with the anti-collision block 1212, and the anti-collision block 1212 is soft and can play a role in buffering, thereby ensuring that the fixing device is not damaged.
Wherein, the anti-collision block 1212 is a polyurethane anti-collision block.
FIG. 5a illustrates a schematic non-operational state of a fixation device according to an embodiment of the present invention; fig. 5b shows a schematic view of the working state of the fixation device according to an embodiment of the utility model.
As shown in fig. 5a and 5b, the fixing device 100 further includes:
a fixing device 130 disposed at the center of the clamping push rod 1210, the fixing device 130 comprising:
the fixing seat 1301 is fixedly connected with the clamping push rod 1210;
the fixing clamp 1302 is hinged with the fixing seat 1301;
the positioning pin 1303 is disposed through the fixing base 1301 in the height direction, and when the fixing clip 1302 is parallel to the fixing base 1301, the positioning pin 1303 may also penetrate through the fixing clip 1302.
Wherein, be equipped with magnet 1304 on the one side that fixing base 1301 deviates from centre gripping push rod 1210, magnet 1304 is fixed on fixing base 1301 through special glue.
After the unmanned aerial vehicle 200 is centered, the fixing device 130 is manually operated to further fix the unmanned aerial vehicle 200, the centered unmanned aerial vehicle 200 is in the state shown in fig. 5a, the fixing clamp 1302 is manually rotated to clamp the legs of the unmanned aerial vehicle 200, as shown in fig. 5b, and then the fixing clamp 1302 is gradually screwed into the fixing clamp 1302 through the positioning pin 1303, so that the fixing clamp 1302 cannot rotate, and the fixing pin abuts against the legs of the unmanned aerial vehicle 200, so that the unmanned aerial vehicle 200 is fixed on the fixing platform 110; when the unmanned aerial vehicle 200 is to be flown, the positioning pin 1303 is unscrewed, the fixing clip 1302 can be covered on the fixing base 1301 in a rotating manner, and the fixing clip 1302 is adsorbed by the magnet 1304 on the fixing base 1301.
Figure 6 shows a schematic diagram of a timing belt connection in accordance with one embodiment of the present invention.
As shown in fig. 6, the timing belt connecting member 1208 comprises a first transverse plate 1208a and an L-shaped plate 1208B vertically disposed on the first transverse plate 1208a, the first transverse plate 1208a is fixedly connected to the second timing belt 1206 through a bolt, and the plate and the first transverse plate 1208a form a holding groove 1208 c.
It should be noted that, when the synchronous belt connecting piece 1208 is located on the upper portion of the second synchronous belt 1206, the L-shaped plate 1208B is disposed downward, and when the synchronous belt connecting piece 1208 is located on the lower portion of the second synchronous belt 1206, the L-shaped plate 1208B is disposed upward (as shown in fig. 4), so that the linear slider 1211 can be located in the accommodating groove 1208c, and the linear slider 1211 and the synchronous belt connecting piece 1208 are fixedly connected.
FIG. 7 shows a schematic view of a putter holder according to one embodiment of the present invention.
As shown in fig. 7, the pusher holder 1209 includes a pair of second transverse plates 1209a and a sloping plate 1209b connecting the pair of second transverse plates 1209a, wherein one of the second transverse plates 1209a is fixedly connected to the timing belt connector 1208, and the other second transverse plate 1209a is fixedly connected to the clamping pusher 1210.
It should be noted that, because the pair of guide shafts 1201 are vertically arranged in a staggered manner, each component connected to the guide shafts 1201 has a staggered manner, that is, the highest position of the installed pushrod fixing member 1209 has a fall, so that the heights of the pushrod fixing members 1209 extending out of the notches 1103 can be different, and thus, the two groups of the clamping pushrods 1210 are arranged in a staggered manner, and interference is avoided.
Further, the mesa 1102 is a carbon fiber mesa 1102.
It should be noted that, the table top 1102 is a carbon fiber table top 1102, and each component in the box 1101 is enclosed in the box 1101, so that on one hand, the components in the box 1101 are not easily damaged, the appearance is more attractive, and on the other hand, the safety of an operator is also protected.
Wherein, the quality light in weight of carbon fiber mesa 1102, intensity is high, and what smooth surface can be better satisfies unmanned aerial vehicle 200's the demand of taking off and land.
Furthermore, the fixing device of the utility model is also provided with an emergency stop button, when the fixing device is in failure, the safety of an operator is threatened or the flight of the unmanned aerial vehicle 200 has potential safety hazard, the emergency stop button can be pressed to prevent accidents, the function of the emergency stop button is controlled by software, the motion of all electric devices such as motors and the like can be stopped after the emergency stop button is pressed, meanwhile, a start button is also arranged, the program can automatically complete all the actions of the unmanned aerial vehicle 200 in flying (namely the closing of the clamping push rod 1210), the processing efficiency of emergency events is improved, and the conventional setting of emergency stop and start of the existing electric devices is adopted, and the description is omitted here.
It should be noted that, in this embodiment, taking the M300 unmanned aerial vehicle 200 as an example, the fixing device in the present invention is connected to the lifting device of the emergency mobile command car, and after the unmanned aerial vehicle 200 is centered and fixed by the fixing device, the fixing device is retracted into the emergency mobile command car, or after the unmanned aerial vehicle is lifted out of the emergency mobile command car by the lifting device, the fixing device 130 and the clamping push rod 1210 are opened, so that the unmanned aerial vehicle 200 is released.
Other embodiments of the utility model will be apparent to those skilled in the art from consideration of the specification and practice of the utility model disclosed herein. This application is intended to cover any variations, uses, or adaptations of the utility model following, in general, the principles of the utility model and including such departures from the present disclosure as come within known or customary practice within the art to which the utility model pertains. It is intended that the specification and examples be considered as exemplary only, with a true scope and spirit of the utility model being indicated by the following claims.
It will be understood that the utility model is not limited to the precise arrangements that have been described above and shown in the drawings, and that various modifications and changes can be made without departing from the scope thereof. The scope of the utility model is limited only by the appended claims.
Claims (9)
1. A fixed equipment that is used for emergent unmanned aerial vehicle in mobile command car, its characterized in that, fixed equipment includes:
the fixed platform comprises a box body and a table top fixed on the box body, wherein notches are formed in four sides of the table top, and a transmission device is arranged in the box body; wherein the transmission comprises:
the pair of guide shafts is vertically arranged in a staggered manner, the guide shafts are arranged close to the edge of the box body, a bearing seat is arranged at the center of each guide shaft, and the bottom of each bearing seat is fixedly connected with the bottom wall of the box body;
the servo motor is arranged in parallel with the guide shaft and is connected with the guide shaft through a first synchronous belt;
the second synchronous belts are arranged at two ends of the guide shaft, one ends of the second synchronous belts are connected with the end parts of the guide shaft, the other ends of the second synchronous belts are connected with the supporting columns, and the supporting columns are arranged on the side walls of the box body;
the pair of synchronous belt connecting pieces are symmetrically arranged at the upper part and the lower part of the second synchronous belt;
the push rod fixing piece is fixedly connected with one end of the push rod fixing piece and the synchronous belt connecting piece;
the clamping push rod is fixedly arranged at the other end of the push rod fixing piece;
the other end of the push rod fixing piece extends out of the notch, and the clamping push rod is located on the table top.
2. The fixture for a drone in an emergency mobile command vehicle of claim 1, wherein the transmission further comprises:
the rail is arranged on the side wall of the box body;
the linear sliding block is arranged on the track and fixedly connected with the synchronous belt connecting piece.
3. The fixture for a drone in an emergency mobile command vehicle of claim 1, wherein the transmission further comprises:
and the speed reducer is arranged between the servo motor and the first synchronous belt.
4. The fixture for a drone in an emergency mobile command vehicle of claim 1, wherein the transmission further comprises:
and the anti-collision blocks are respectively positioned at the two ends of the second synchronous belt and at the central position of the second synchronous belt, and the anti-collision blocks are fixedly connected with the side wall of the box body.
5. The fixture for a drone in an emergency mobile command vehicle of claim 1, further comprising:
fixing device, set up in centre department of centre gripping push rod, fixing device includes:
the fixing seat is fixedly connected with the clamping push rod;
the fixing clamp is hinged with the fixing seat;
the locating pin runs through set up in the direction of height of fixing base, the fixation clamp with when the fixing base is parallel, the locating pin can also run through the fixation clamp.
6. The fixing device for the unmanned aerial vehicle in the emergency mobile command vehicle of claim 5, wherein a magnet is arranged on one side of the fixing seat, which faces away from the clamping push rod, and the magnet is fixed on the fixing seat through special glue.
7. The fixing device for the unmanned aerial vehicle in the emergency mobile command vehicle of any one of claims 1 to 6, wherein the synchronous belt connecting piece comprises a first transverse plate and an L-shaped plate arranged perpendicular to the first transverse plate, the first transverse plate is fixedly connected with the second synchronous belt through a bolt, and the shaped plate and the first transverse plate form a holding groove.
8. The fixing device for the unmanned aerial vehicle in the emergency mobile command vehicle of any one of claims 1 to 6, wherein the push rod fixing member comprises a pair of second transverse plates and an inclined plate, the second transverse plates are arranged in parallel, the inclined plate is connected with the pair of second transverse plates, one of the second transverse plates is fixedly connected with the synchronous belt connecting piece, and the other second transverse plate is fixedly connected with the clamping push rod.
9. The fixture for unmanned aerial vehicle in emergency mobile command vehicle of any one of claims 1 to 6, wherein the table top is a carbon fiber table top.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123076919.3U CN216659710U (en) | 2021-12-09 | 2021-12-09 | A fixed equipment that is used for emergent unmanned aerial vehicle in removing command car |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123076919.3U CN216659710U (en) | 2021-12-09 | 2021-12-09 | A fixed equipment that is used for emergent unmanned aerial vehicle in removing command car |
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| Publication Number | Publication Date |
|---|---|
| CN216659710U true CN216659710U (en) | 2022-06-03 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202123076919.3U Active CN216659710U (en) | 2021-12-09 | 2021-12-09 | A fixed equipment that is used for emergent unmanned aerial vehicle in removing command car |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115056702A (en) * | 2022-06-07 | 2022-09-16 | 北京机械设备研究所 | Automatic take-off and landing centering device of vehicle-mounted unmanned aerial vehicle |
| CN115214447A (en) * | 2022-06-07 | 2022-10-21 | 北京机械设备研究所 | Rescue fire truck based on unmanned aerial vehicle and control method thereof |
-
2021
- 2021-12-09 CN CN202123076919.3U patent/CN216659710U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115056702A (en) * | 2022-06-07 | 2022-09-16 | 北京机械设备研究所 | Automatic take-off and landing centering device of vehicle-mounted unmanned aerial vehicle |
| CN115214447A (en) * | 2022-06-07 | 2022-10-21 | 北京机械设备研究所 | Rescue fire truck based on unmanned aerial vehicle and control method thereof |
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