CN219172270U - Unmanned aerial vehicle transportation measurement and control integrated vehicle - Google Patents
Unmanned aerial vehicle transportation measurement and control integrated vehicle Download PDFInfo
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- CN219172270U CN219172270U CN202320129695.8U CN202320129695U CN219172270U CN 219172270 U CN219172270 U CN 219172270U CN 202320129695 U CN202320129695 U CN 202320129695U CN 219172270 U CN219172270 U CN 219172270U
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Abstract
An unmanned aerial vehicle transportation measurement and control integrated vehicle comprises a chassis vehicle and a shelter arranged on the chassis vehicle; a measurement and control space is arranged in front of the inside of the shelter, and a measurement and control system is arranged in the measurement and control space; the middle rear part inside the shelter is a storage and transportation space, the storage and transportation space is used for placing the unmanned aerial vehicle, and an unmanned aerial vehicle fixing bracket and a blade box are arranged in the storage and transportation space; the side part and the tail part of the shelter are respectively provided with a side door and a side-by-side door, the side door is used for getting on and off a vehicle by personnel, and the side-by-side door is used for the entrance and exit of an unmanned aerial vehicle; the tail of the chassis truck is also provided with a hydraulic loading and unloading mechanism, and the hydraulic loading and unloading mechanism is used for supporting the unmanned aerial vehicle and then vertically lifting. The utility model can realize quick shipment and integrate transportation and measurement and control.
Description
Technical Field
The utility model relates to a special vehicle for an unmanned aerial vehicle, in particular to an unmanned aerial vehicle transportation measurement and control integrated vehicle.
Background
The known unmanned helicopter, namely unmanned aerial vehicle for short, has the advantages of relatively low cost, risk of casualties of unmanned aerial vehicle, strong survivability, good maneuvering characteristics, convenient use and the like, and is widely applied to the fields including: the system comprises a plurality of fields such as aviation shooting, aviation photography, geological and landform mapping, forest fire prevention, earthquake investigation, border patrol, emergency disaster relief, poison banning, anti-terrorism, police investigation patrol, security monitoring, fire-fighting aerial investigation, communication relay, city planning and the like.
At present, because of limitation of space layout, two vehicles are adopted for transportation and measurement and control of the unmanned aerial vehicle, for example, an unmanned aerial vehicle transportation vehicle (CN 208291068U) and an unmanned aerial vehicle measurement and control vehicle (CN 206884847U), and two independent vehicles are needed to be used for carrying, so that the cost is high and the configuration is required to be optimized. Meanwhile, in the transportation operation of the existing unmanned aerial vehicle, before entering the vehicle, the unmanned aerial vehicle is always lifted up and down, and enters the vehicle by means of a loading and unloading tool in a lifting state, so that the stability is poor, the operation efficiency is affected, and the operation is time-consuming and labor-consuming.
Disclosure of Invention
In order to overcome the defects in the prior art, the utility model provides the unmanned aerial vehicle transportation measurement and control integrated vehicle, which can realize rapid transportation and can integrate transportation measurement and control.
The technical scheme adopted for solving the technical problems is as follows:
an unmanned aerial vehicle transportation measurement and control integrated vehicle comprises a chassis vehicle and a shelter arranged on the chassis vehicle; a measurement and control space is arranged in front of the inside of the shelter, and a measurement and control system is arranged in the measurement and control space; the middle rear part inside the shelter is a storage and transportation space, the storage and transportation space is used for placing the unmanned aerial vehicle, and an unmanned aerial vehicle fixing bracket and a blade box are arranged in the storage and transportation space; the side part and the tail part of the shelter are respectively provided with a side door and a side-by-side door, the side door is used for getting on and off a vehicle by personnel, and the side-by-side door is used for the entrance and exit of an unmanned aerial vehicle;
the tail of the chassis truck is also provided with a hydraulic loading and unloading mechanism, and the hydraulic loading and unloading mechanism is used for supporting the unmanned aerial vehicle and then vertically lifting.
Optionally, the hydraulic loading and unloading mechanism includes fixed bolster, drive assembly and supports the dull and stereotyped, the rear end of supporting the dull and stereotyped rotation and connecting drive assembly's front end, drive assembly's rear end rotation is connected on one side of fixed bolster, the opposite side fixed bolster is in the afterbody of chassis car.
Optionally, the supporting plate has an integrally inclined upper surface, and the thickness of the supporting plate gradually decreases from the rear end to the front end; and or the back of the back end of the supporting flat plate is provided with a reinforcing member.
Optionally, the central area of the support plate is provided with a centering mark, and the centering mark is a pattern matrix arranged on the surface of the support plate.
Optionally, the support plate comprises at least two sections of tail plates, the first section of tail plate is used for being connected with the driving assembly, the second section of tail plate is rotationally connected to the front end of the first section of tail plate, and the included angle range between the second section of tail plate and the front surface of the first section of tail plate is 0-180 degrees.
Optionally, the driving assembly comprises two groups of symmetrically arranged driving units, the driving units comprise lifting arms and a first oil cylinder which are arranged on the inner side and a second oil cylinder which is arranged on the outer side, and two ends of each lifting arm and each second oil cylinder are respectively hinged on the fixed support and the supporting flat plate; one end of the first oil cylinder is hinged to the middle lower portion of the lifting arm, and the other end of the first oil cylinder is hinged to the fixed support.
Optionally, the measurement and control system comprises a display control module and a seat which are arranged in the measurement and control space front and back, and a directional antenna arranged at the top of the shelter, wherein the directional antenna is associated with the display control module;
the display control module comprises a console and a cabinet which are vertically arranged up and down.
Optionally, the blade box is arranged on the bottom plate of the shelter and is positioned at the middle position in the width direction of the bottom plate; the length trend of the blade box is consistent with the length direction of the bottom plate.
Optionally, the shelter adopts a chamfer shelter; the chassis vehicle adopts a second type chassis.
Optionally, the front portion of shelter still is equipped with on-vehicle air conditioner, illumination mast and step on the top, the below of side door is equipped with collapsible or detachable step on the cabin.
Compared with the prior art, the unmanned aerial vehicle transportation measurement and control integrated vehicle has the advantages that the measurement and control space and the storage and transportation space are reasonably distributed in the cabin of the square cabin, so that the square cabin space of the vehicle is stronger in accommodating property, measurement and control equipment and large-scale equipment such as an unmanned aerial vehicle can be installed at the same time, and the measurement and control system and the blade box can be utilized, so that the unmanned aerial vehicle transportation measurement and control integrated vehicle is realized, and the emergency use requirement is more comprehensively met; meanwhile, based on the use of the hydraulic loading and unloading mechanism, the unmanned aerial vehicle can be rapidly and stably loaded and unloaded vertically.
Drawings
The utility model will be further described with reference to the drawings and examples.
Fig. 1 and 2 are perspective views of an integrated unmanned plane transportation and measurement and control vehicle according to an embodiment of the present utility model at different angles.
Fig. 3 is a schematic diagram of an external structure of a shelter in an integrated unmanned aerial vehicle transportation and measurement and control vehicle according to an embodiment of the present utility model.
Fig. 4 is a schematic diagram of an internal structure of a shelter in an integrated unmanned aerial vehicle transportation and measurement and control vehicle according to an embodiment of the present utility model.
Fig. 5 is a front view of a hydraulic loading and unloading mechanism in an unmanned aerial vehicle transportation and measurement and control integrated vehicle according to an embodiment of the utility model.
Fig. 6 is a top view of a hydraulic handling mechanism in an unmanned aerial vehicle transport measurement and control integrated vehicle in accordance with one embodiment of the present utility model.
Fig. 7 is a left side view of a hydraulic loading and unloading mechanism in an unmanned aerial vehicle transportation and measurement and control integrated vehicle according to an embodiment of the utility model.
Fig. 8 is a schematic diagram of a use process of an integrated unmanned plane transportation and measurement and control vehicle according to an embodiment of the utility model.
The reference numerals in the drawings illustrate:
100-an unmanned plane transportation measurement and control integrated vehicle; 200-unmanned aerial vehicle;
1-chassis turning; 2-shelter; 21-side door; 22-split door; 3-a measurement and control system; 31-a display control module; 311-console; 312-cabinet; 32-a seat; 33-directional antennas; 4-a blade box; 5-a hydraulic loading and unloading mechanism; 51-a fixed support; 52-a drive assembly; 521-a driving unit; 5211-lifting arms; 5212-a first cylinder; 5213-a second cylinder; 53-a support plate; 531-reinforcing members; 532-centering identification; 6-vehicle-mounted air conditioner; 7-illuminating the mast; 8-climbing a footstep; 9-boarding ladder.
Detailed Description
For the purpose of making the objects, technical solutions and advantages of the embodiments of the present utility model more apparent, the technical solutions of the embodiments of the present utility model will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present utility model, and it is apparent that the described embodiments are some embodiments of the present utility model, but not all embodiments of the present utility model. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to fall within the scope of the utility model.
Fig. 1 to 7 show a schematic structural diagram of a preferred embodiment of the present utility model, in which an integrated transport and measurement and control vehicle for an unmanned aerial vehicle includes a chassis 1 and a shelter 2 disposed on the chassis 1; a measurement and control space is arranged in front of the inside of the shelter 2, and a measurement and control system 3 is arranged in the measurement and control space; the middle rear part inside the shelter 2 is a storage and transportation space, the storage and transportation space is used for placing the unmanned aerial vehicle, and an unmanned aerial vehicle fixing bracket and a blade box 4 are arranged in the storage and transportation space; the side part and the tail part of the shelter 2 are respectively provided with a side door 21 and a side-by-side door 22, the side door 21 is used for getting on and off a vehicle by personnel, and the side-by-side door 22 is used for entering and exiting an unmanned aerial vehicle;
the tail of the chassis vehicle 1 is also provided with a hydraulic loading and unloading mechanism 5, and the hydraulic loading and unloading mechanism 5 is used for supporting the unmanned aerial vehicle and then vertically lifting.
In specific implementation, the chassis vehicle 1 can be a high-mobility type chassis with a free automobile, and a group of 12KW power generators are additionally arranged on the chassis to supply power for vehicle-mounted equipment. More specifically, the shelter 2 can be connected with the automobile chassis girder through the auxiliary frame, and the connection mode has the characteristics of quick disassembly and shipment, and can greatly improve the maneuverability and convenience of the mobile shelter 2.
On one hand, the measurement and control system 3 of the measurement and control space can meet the functional requirements of unmanned helicopter measurement, control and the like, and has the functions of monitoring, power supply, communication access and the like. On the other hand, the storage and transportation space is mainly the space for transporting and storing the unmanned helicopter, and the transportation requirement of the unmanned helicopter can be met by internally installing equipment such as the unmanned helicopter fixing bracket, the blade box 4 and the like. On the other hand, the hydraulic loading and unloading mechanism 5 arranged at the tail of the vehicle can meet the high-efficiency unloading requirement of unmanned helicopter loading by stretching and lifting. Therefore, the unmanned aerial vehicle transportation measurement and control integrated vehicle of this embodiment has both realized quick shipment, can collect transportation again and observe and control an organic wholely, and the emergent use needs of response fast finally can transport and put into use with fastest mode.
As a further optional implementation manner of this embodiment, the hydraulic loading and unloading mechanism 5 includes a fixed support 51, a driving assembly 52 and a supporting plate 53, the rear end of the supporting plate 53 is rotatably connected to the front end of the driving assembly 52, the rear end of the driving assembly 52 is rotatably connected to one side of the fixed support 51, and the other side of the fixed support 51 is fixedly connected to the tail of the chassis 1. The fixed support can be a square steel support.
As a further alternative of this embodiment, the support plate 53 has an integrally inclined upper surface, and the support plate 53 has a gradually decreasing thickness from the rear end to the front end; and or the rear end back surface of the support plate 53 is provided with a reinforcing member 531.
In a specific implementation, the reinforcing member 531 may be a reinforcing rib plate disposed near the connection portion, and the reinforcing rib plate may be in a right triangle shape, and the number of the reinforcing rib plates may be two pairs.
As a further alternative implementation of this embodiment, the central area of the support plate 53 is provided with a centering mark 532, and the centering mark 532 is a pattern matrix disposed on the surface of the support plate 53.
The centering mark 532 is used for indicating the parking position of the unmanned aerial vehicle as the name implies, and the pattern matrix can be used for highlighting the central position of the supporting plate 53 or positioning the optimal parking area of the unmanned aerial vehicle, so that the unmanned aerial vehicle can be prevented from taking too much time when being placed, and the loading and unloading accuracy is ensured.
As a further alternative of this embodiment, the support plate 53 includes at least two end plates, a first end plate for connecting with the driving assembly 52, and a second end plate rotatably connected to the front end of the first end plate, where an angle between the second end plate and the front surface of the first end plate is in a range of 0-180 °.
In application, the hydraulic loading and unloading mechanism 5 can select a 3-ton folding lengthened hydraulic tail plate, wherein the plate length of the first tail plate is 1.8 meters, and the plate length of the second tail plate is 1 meter. The downward inclination angle and the vertical lifting action of the positive and negative hydraulic tail plates can be controlled by controlling the expansion and contraction of the front hydraulic oil cylinder and the rear hydraulic oil cylinder.
As a further alternative implementation manner of the present embodiment, the driving assembly 52 includes two sets of driving units 521 symmetrically arranged, the driving units 521 include a lifting arm 5211 and a first cylinder 5212 disposed on the inner side and a second cylinder 5213 disposed on the outer side, and two ends of the lifting arm 5211 and the second cylinder 5213 are respectively hinged to the fixed support 51 and the supporting plate 53; one end of the first oil cylinder 5212 is hinged to the middle lower portion of the lifting arm 5211, and the other end of the first oil cylinder is hinged to the fixed support 51.
As a further optional implementation manner of this embodiment, the measurement and control system 3 includes a display control module 31 and a seat 32 disposed in the measurement and control space, and a directional antenna 33 disposed at the top of the shelter 2, where the directional antenna 33 is associated with the display control module 31;
the display control module 31 includes a console 311 and a cabinet 312 vertically arranged up and down. More specifically, the console 311 comprises 1 operation platform arranged at the front part of the cabin 2, when the operation platform meets the operation of 3 persons, the operation platform is matched with three seats 32, preferably aviation seats, three vehicle-mounted computers can be specifically arranged below the operation platform, and 6 22 inch displays are arranged on the upper part of the operation platform; the cabinet 312 is a three-set standard 16U cabinet installed at the lower part of the operation desk, and is used for storing devices such as computers, in addition, four LED lighting and air defense lamps can be installed at the top of the cabin of the shelter 2, so that the cabin can be used for lighting.
As a further alternative implementation of the embodiment, the blade box 4 is disposed on the bottom plate of the shelter 2 and is located at a central position in the width direction of the bottom plate; the length trend of the blade box 4 is consistent with the length direction of the bottom plate.
The blade box 4 is used for storing unmanned helicopter blades, the rest part of the rear part is the unmanned helicopter storage and transportation space, and two frames 3700 x 1050 x 1760 of unmanned helicopters can be stored and transported simultaneously.
As a further alternative implementation manner of this embodiment, the shelter 2 is a chamfer shelter; the chassis vehicle 1 adopts a second type chassis. More specifically, the chassis 1 may be a CTM131L chassis.
In a specific implementation, the specifications of the chamfer type shelter 2 can be set to be 5100mm×2438mm×2100mm in external dimensions. In terms of manufacturing, the whole shelter 2 can be made of a steel skeleton, the skin is made of aluminum, and polyurethane heat-insulating materials are filled in the skin. The whole overall dimension of the unmanned aerial vehicle transportation measurement and control integrated vehicle can be designed as (length x width x height): 9120mm×2500mm×3801 (including roof directional antenna 33), the roof directional antenna 33 can be removed in railway transportation, and the overall dimensions of the whole car are (length×width×height): 9120mm×2500mm×3401mm.
As a further optional implementation manner of this embodiment, the front part of the shelter 2 is further provided with a vehicle-mounted air conditioner 6, an illumination mast 7 and a boarding ladder 8, and a foldable or detachable boarding ladder 9 is arranged below the side door 21. The illumination mast 7 can be set to be a telescopic illumination mast, and can be combined with a hydraulic tail plate for use, so that the illumination mast can be better adapted to rapid vertical loading and unloading of different light environments. The boarding ladder 8 and the boarding ladder 9 are used to assist in entering the side doors 21 and the side-by-side doors 22.
Referring to fig. 8, in use, the loading of the unmanned helicopter is mainly completed through the hydraulic loading and unloading mechanism 5, the supporting plate 53 of the hydraulic loading and unloading mechanism 5 is put down at first when the loading work starts, the second tail plate of the supporting plate 53 is opened and placed on the ground, the side-by-side door 22 at the tail part of the shelter 2 is opened, then the unmanned helicopter is moved onto the supporting plate 53, when more than two thirds of the unmanned helicopter is on the supporting plate 53, the supporting plate 53 is controlled to be lifted to the height consistent with the bottom plate of the shelter 2, at this time, the unmanned helicopter can be moved into the shelter 2 and fixed, and the steps are repeated to load the second unmanned helicopter. The unmanned helicopter unloading process is opposite to the two-machine unloading process, and is not repeated here.
The foregoing description is only a preferred embodiment of the present utility model, and is not intended to limit the utility model in any way, but any simple modification and equivalent variation of the above embodiment according to the technical spirit of the present utility model falls within the scope of the present utility model.
Claims (10)
1. An unmanned aerial vehicle transportation measurement and control integrated vehicle comprises a chassis vehicle and a shelter arranged on the chassis vehicle; the method is characterized in that: a measurement and control space is arranged in front of the inside of the shelter, and a measurement and control system is arranged in the measurement and control space; the middle rear part inside the shelter is a storage and transportation space, the storage and transportation space is used for placing the unmanned aerial vehicle, and an unmanned aerial vehicle fixing bracket and a blade box are arranged in the storage and transportation space; the side part and the tail part of the shelter are respectively provided with a side door and a side-by-side door, the side door is used for getting on and off a vehicle by personnel, and the side-by-side door is used for the entrance and exit of an unmanned aerial vehicle;
the tail of the chassis truck is also provided with a hydraulic loading and unloading mechanism, and the hydraulic loading and unloading mechanism is used for supporting the unmanned aerial vehicle and then vertically lifting.
2. The unmanned aerial vehicle transportation measurement and control integrated vehicle according to claim 1, wherein: the hydraulic loading and unloading mechanism comprises a fixed support, a driving assembly and a supporting flat plate, wherein the rear end of the supporting flat plate is rotationally connected with the front end of the driving assembly, the rear end of the driving assembly is rotationally connected to one side of the fixed support, and the other side of the fixed support is fixedly connected to the tail of the chassis vehicle.
3. The unmanned aerial vehicle transportation measurement and control integrated vehicle according to claim 2, wherein: the supporting flat plate is provided with an integrally inclined upper surface, and the thickness of the supporting flat plate gradually decreases from the rear end to the front end; and or the back of the back end of the supporting flat plate is provided with a reinforcing member.
4. The unmanned aerial vehicle transportation measurement and control integrated vehicle of claim 3, wherein: the centering mark is arranged in the centering area of the supporting flat plate, and the centering mark is a pattern matrix arranged on the surface of the supporting flat plate.
5. The unmanned aerial vehicle transportation measurement and control integrated vehicle according to claim 4, wherein: the support flat plate comprises at least two sections of tail plates, a first section of tail plates is used for being connected with the driving assembly, a second section of tail plates are rotatably connected to the front ends of the first section of tail plates, and the included angle range between the front faces of the second section of tail plates and the front faces of the first section of tail plates is 0-180 degrees.
6. The unmanned aerial vehicle transportation measurement and control integrated vehicle according to claim 5, wherein: the driving assembly comprises two groups of symmetrically arranged driving units, the driving units comprise lifting arms and first oil cylinders which are arranged on the inner side and second oil cylinders which are arranged on the outer side, and two ends of each lifting arm and each second oil cylinder are respectively hinged on the fixed support and the supporting flat plate; one end of the first oil cylinder is hinged to the middle lower portion of the lifting arm, and the other end of the first oil cylinder is hinged to the fixed support.
7. The unmanned aerial vehicle transportation measurement and control integrated vehicle according to any one of claims 1 to 6, wherein: the measurement and control system comprises a display control module and a seat which are arranged in a measurement and control space front and back, and a directional antenna arranged at the top of the shelter, wherein the directional antenna is associated with the display control module;
the display control module comprises a console and a cabinet which are vertically arranged up and down.
8. The unmanned aerial vehicle transportation measurement and control integrated vehicle of claim 7, wherein: the blade box is arranged on the bottom plate of the shelter and is positioned at the middle position in the width direction of the bottom plate; the length trend of the blade box is consistent with the length direction of the bottom plate.
9. The unmanned aerial vehicle transportation measurement and control integrated vehicle of claim 8, wherein: the square cabin adopts a chamfer square cabin; the chassis vehicle adopts a second type chassis.
10. The unmanned aerial vehicle transportation measurement and control integrated vehicle of claim 9, wherein: the front part of the shelter is also provided with a vehicle-mounted air conditioner, an illumination mast and a boarding ladder, and a foldable or detachable boarding ladder is arranged below the side door.
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| Application Number | Priority Date | Filing Date | Title |
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| CN202320129695.8U CN219172270U (en) | 2023-01-17 | 2023-01-17 | Unmanned aerial vehicle transportation measurement and control integrated vehicle |
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| Application Number | Priority Date | Filing Date | Title |
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| CN202320129695.8U CN219172270U (en) | 2023-01-17 | 2023-01-17 | Unmanned aerial vehicle transportation measurement and control integrated vehicle |
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| CN219172270U true CN219172270U (en) | 2023-06-13 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116443302A (en) * | 2023-06-16 | 2023-07-18 | 成都庆龙航空科技有限公司 | Unmanned aerial vehicle comprehensive guarantee vehicle |
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- 2023-01-17 CN CN202320129695.8U patent/CN219172270U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116443302A (en) * | 2023-06-16 | 2023-07-18 | 成都庆龙航空科技有限公司 | Unmanned aerial vehicle comprehensive guarantee vehicle |
| CN116443302B (en) * | 2023-06-16 | 2023-09-05 | 成都庆龙航空科技有限公司 | Unmanned aerial vehicle comprehensive guarantee vehicle |
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