CN212313385U - Digital command shelter - Google Patents
Digital command shelter Download PDFInfo
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- CN212313385U CN212313385U CN201921993906.2U CN201921993906U CN212313385U CN 212313385 U CN212313385 U CN 212313385U CN 201921993906 U CN201921993906 U CN 201921993906U CN 212313385 U CN212313385 U CN 212313385U
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- cabin
- cabin body
- digital command
- door
- unmanned aerial
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Abstract
The utility model provides a digital command shelter, include the transport vechicle and install the cabin body on the transport vechicle, be provided with four fixing device on the transport vechicle, cabin body outside fixed mounting has air conditioning system, is provided with the business turn over door on the cabin body, the business turn over door is located the afterbody of transport vechicle, and both sides all are equipped with the daylighting window around the cabin body, the bottom of the cabin body is equipped with battery compartment and generator storehouse. The utility model discloses a fly unmanned many rotor crafts, can be faster more accurate acquire near the topography and landform of transport vechicle and monitor the transport vechicle surrounding environment, ensure the safety of the cabin body, can be more accurate acquire information to can assist the quick analysis of commander to judge.
Description
Technical Field
The utility model relates to a commander's shelter technical field, specifically speaking relates to a digital commander's shelter.
Background
In recent years, natural disasters frequently occur and military demonstration are increased in China, the complexity of the social situations of regions and different landforms are low, a mobile, flexible, portable, rapid and efficient digital command shelter is not available, effective control on various events and wartime conditions is not available, and the battle performance of troops and the safety of people are seriously affected.
At present, a chinese patent with patent application number 201620414102.2 discloses a digital multifunctional command shelter, which comprises a cabin body with an energy cabin, wherein a satellite antenna is arranged at the top of the energy cabin, and a television receiving antenna is arranged at the outer top of the cabin body; the right side outside the cabin body is provided with an access door, and the left side outside the cabin body is provided with a lighting window and a power supply input door; the rear end outside the cabin body is provided with a lifting rod; the outer top of the cabin body is provided with a tool box; the left side in the cabin is located and is provided with the time display between two daylighting windows, and the time display below is provided with the operation touch-control screen, and operation touch-control screen below is provided with video control system's side rack, and side rack both sides are provided with the drawer, and the both sides that the internal right side of cabin is located the business turn over door are provided with looks the video display screen frequently, look sideways at the video display screen below and are provided with the seat frequently, and both ends are provided with tip video display screen around the internal cabin.
Foretell multi-functional commander's cabin of digitization, can make commander's cabin obtain in the field flexibly, in a flexible way, light, quick commander's cabin, but equipment layout is unreasonable on this commander's cabin, can't carry unmanned aerial vehicle, and unmanned aerial vehicle can be more accurate acquisition information more fast in natural disasters frequently takes place and the military demonstration at present, thereby can assist the quick analysis and judgment of commander, along with the research and development of national unmanned aerial vehicle, unmanned aerial vehicle's effect in natural disasters frequently takes place and the military demonstration is more and more important.
SUMMERY OF THE UTILITY MODEL
In order to solve the defects of the prior art, the utility model aims to provide a digital command shelter, which overcomes the defects in the prior art.
In order to achieve the above object, the utility model provides a digital command shelter, which comprises a transport vehicle and a cabin body arranged on the transport vehicle, wherein the transport vehicle is provided with four fixing devices, the outer side of the cabin body is fixedly provided with an air conditioning system, the cabin body is provided with an access door, the access door is positioned at the tail part of the transport vehicle, the front side and the rear side of the cabin body are respectively provided with a lighting window, the bottom of the cabin body is provided with a battery cabin and a generator cabin, a storage battery pack is arranged in the battery cabin, a diesel generator set is arranged in the generator cabin and is used for charging the storage battery pack, the outer part of the cabin body is provided with a signal transceiver, the signal transceiver is arranged on an electric telescopic rod I, the fixed end of the electric telescopic rod I is fixedly arranged on the outer side wall of the cabin body, the central control system comprises a time display, an operation touch screen, a side cabinet, a side video display screen, an end video display screen, a server cabinet, an LED screen and a loudspeaker; the top of the cabin body is provided with an unmanned aerial vehicle cabin, and unmanned multi-rotor aircraft are placed in the unmanned aerial vehicle cabin.
Through the technical scheme, the utility model discloses an equipment overall arrangement on the digital command shelter is reasonable to set up unmanned aerial vehicle bin and can carry unmanned many rotor crafts, when natural disasters and military demonstration, can be faster more accurate acquisition information, can be faster more accurate acquire near the topography and geomorphology of transport vechicle and monitor the transport vechicle surrounding environment, ensure the safety of the cabin body.
As right digital command shelter further explain, preferably, fixing device includes hydraulic stem drive arrangement, hydraulic telescoping rod and bottom plate, four hydraulic telescoping rod is fixed mounting respectively at four turnings of transport vechicle, hydraulic telescoping rod's lower extreme fixedly connected with bottom plate, the bottom plate is used for increasing the area of contact of hydraulic telescoping rod with ground, hydraulic stem drive arrangement is used for controlling hydraulic telescoping rod's work.
Through the technical scheme, the four hydraulic telescopic rods can be controlled respectively, and the transport vehicle body can be adjusted to the horizontal position, so that personnel in the cabin can normally conduct commands.
As right the digital command shelter of the utility model further explain, preferably, the lighting window includes steel sheet and bullet-proof glass, fixed connection and bullet-proof glass on the inner wall of steel sheet, the upside of steel sheet articulates in the cabin body.
Through above-mentioned technical scheme, can rotate the steel sheet, open the daylighting window, realize the ventilation, can select to close air conditioning system according to actual conditions this moment to save the electric energy.
As to the further explanation of the digital command shelter of the present invention, preferably, a first solar panel is installed on the top of the cab of the transportation vehicle, and the first solar panel is used for charging the storage battery pack.
Through the technical scheme, the using amount of the diesel generator set can be reduced, and diesel is saved.
As right digital command shelter further explain, preferably, the both sides of the cabin body all are equipped with solar cell panel two, solar cell panel two's upper end articulates on the cabin body, and solar cell panel two is connected through electric telescopic handle two with the cabin body within a definite time, electric telescopic handle two's both ends articulate respectively on solar cell panel two and the cabin body, and electric telescopic handle two is used for propping up solar cell panel two.
Through the technical scheme, when the transport vehicle moves, the electric telescopic rod II is shortened, the solar cell panel II is close to the cabin body, after the transport vehicle is fixed through the fixing device, the electric telescopic rod II extends to support the solar cell panel II, the solar cell panel II can be fully contacted with sunlight, and the conversion rate of solar energy is improved.
As right digital command shelter further explain, preferably, unmanned aerial vehicle transmission slide rail is installed at the top of the cabin body, be provided with fixed wing unmanned aerial vehicle on the unmanned aerial vehicle transmission slide rail.
Through above-mentioned technical scheme, can launch fixed wing unmanned aerial vehicle, further increase strategic performance.
As right digital command shelter further explain, preferably, the unmanned aerial vehicle bin includes box, place the platform, hatch door, lifting device and mechanism of opening door, the box is upside open-ended square structure, and the inner wall sliding connection of box has place the platform, place unmanned many rotor crafts on the place the platform, the last lifting device that is provided with of place the platform, the lifting device is used for reciprocating of place the platform, the hatch door articulates the upside at the box, set up the mechanism of opening door on the hatch door, the mechanism of opening door is used for opening and shutting of hatch door.
Through above-mentioned technical scheme, the mechanism of opening the door opens the hatch door, and the lifting device will place the platform lifting to with the same height of hatch door, can carry out the remote control to unmanned many rotor crafts in the cabin body this moment and take off.
As to the further explanation of digital command shelter of the utility model, preferably, the hatch door comprises four triangle-shaped plates that the structure is the same, triangle-shaped plate is equilateral right triangle-shaped structure, four triangle-shaped plate articulates respectively the upside of four lateral walls of box.
Through above-mentioned technical scheme, four triangle-shaped boards have constituteed a landing platform with place the platform jointly, and the area of landing platform has increased one time than place the platform to make unmanned many rotor crafts's landing area bigger, descend more easily.
As a further explanation of the digital command shelter of the present invention, preferably, the lifting device is an electric telescopic rod.
As to the further explanation of digital command shelter of the utility model, preferably, four the equal fixedly connected with sealing strip in adjacent one side of triangle-shaped board extrudes each other between adjacent sealing strip.
Through above-mentioned technical scheme, realize waterproof effect, when avoiding raining, the rainwater gets into the unmanned aerial vehicle bin.
The utility model has the advantages as follows:
1. the four fixing devices are arranged on the transport vehicle, the vehicle is fixed on the ground by the fixing devices after the transport vehicle is stopped stably, the stability of the transport vehicle is ensured, and the body of the transport vehicle can be adjusted to be horizontal by respectively controlling the four hydraulic telescopic rods, so that personnel in the cabin can normally command;
2. by flying the unmanned multi-rotor aircraft, the landform and the geomorphic appearance near the transport vehicle can be acquired more quickly and accurately, the surrounding environment of the transport vehicle can be monitored, the safety of the cabin body is ensured, information can be acquired more quickly and accurately, and therefore rapid analysis and judgment of commanders can be assisted;
3. the cabin door is formed by the four triangular plates, the four triangular plates are respectively positioned on four edges of the placing platform, the four triangular plates and the placing platform jointly form a landing platform, and the area of the landing platform is doubled compared with that of the placing platform, so that the landing area of the unmanned multi-rotor aircraft is larger, and the unmanned multi-rotor aircraft can land more easily.
Drawings
Fig. 1 is a schematic structural view of a digital command shelter of the present invention;
fig. 2 is a top view of the middle chamber body of the present invention;
fig. 3 is a cross-sectional view of the unmanned aerial vehicle cabin of the present invention;
fig. 4 is a schematic view of the unmanned aerial vehicle cabin of the present invention after the cabin door is opened;
FIG. 5 is a schematic view of connection among a second solar panel, a second electric telescopic rod and a cabin body.
In the figure: transport vechicle 1, the cabin body 2, fixing device 3, air conditioning system 4, daylighting window 5, business turn over door 6, battery compartment 7, generator storehouse 8, signal transceiver 9, electric telescopic handle one 10, unmanned aerial vehicle storehouse 11, unmanned many rotor crafts 12, solar cell panel one 13, two 14 of solar cell panel, two 15 of electric telescopic handle, unmanned aerial vehicle transmission slide rail 16, fixed wing unmanned aerial vehicle 17, box 111, place the platform 112, hatch door 113, lifting device 114, mechanism 115 opens a door.
Detailed Description
In order to further understand the structure, characteristics and other objects of the present invention, the following detailed description is given with reference to the accompanying preferred embodiments, which are only used to illustrate the technical solution of the present invention and are not intended to limit the present invention.
As shown in fig. 1, the utility model provides a technical solution: a digital command shelter comprises a transport vehicle 1 and a cabin body 2 installed on the transport vehicle 1, wherein four fixing devices 3 are arranged on the transport vehicle 1, the fixing devices 3 are used for fixing the transport vehicle on the ground after the transport vehicle 1 is stopped stably, the stability of the transport vehicle 1 is ensured, an air conditioning system 4 is fixedly installed on the outer side of the cabin body 2, the air conditioning system 4 is used for controlling the temperature in the cabin body 2 and exchanging the internal air and the external air, an access door 6 is arranged on the cabin body 2, the access door 6 is positioned at the tail part of the transport vehicle 1, personnel enter the cabin body 2 through the access door 6, lighting windows 5 are arranged on the front side and the rear side of the cabin body 2, a battery cabin 7 and a generator cabin 8 are arranged at the bottom of the cabin body 2, a storage battery pack is installed in the battery cabin 7 and used for supplying power to all electric equipment in the cabin body 2, a diesel generator set, the outer part of the cabin body 2 is provided with a signal transceiver 9, the signal transceiver 9 is installed on a first electric telescopic rod 10, the fixed end of the first electric telescopic rod 10 is fixedly installed on the outer side wall of the cabin body 2, the first electric telescopic rod 10 can drive the signal transceiver 9 to ascend and descend, so that the signal coverage range of the signal transceiver 9 is wider, a central control system for digital command is arranged in the cabin body 2, and the central control system comprises a time display, an operation touch screen, a side cabinet, a side-view frequency display screen, an end video display screen, a server cabinet, an LED screen and a loudspeaker, and the specific installation mode is fully disclosed in a Chinese patent with the application number of 2016204141022 and is not described herein; the top of the cabin body 2 is provided with unmanned aerial vehicle bin 11, has placed unmanned many rotor crafts 12 in the unmanned aerial vehicle bin 11, through flying unmanned many rotor crafts 12, can be faster more accurate acquire the topography and geomorphology near transport vechicle 1 and monitor transport vechicle 1 surrounding environment, ensures the safety of the cabin body 2.
As an embodiment of the utility model, fixing device 3 includes hydraulic stem drive arrangement, hydraulic telescoping rod and bottom plate, four hydraulic telescoping rod respectively fixed mounting are at four turnings of transport vechicle 1, hydraulic telescoping rod's lower extreme fixedly connected with bottom plate, the bottom plate is used for increasing the area of contact of hydraulic telescoping rod and ground, hydraulic stem drive arrangement is used for controlling hydraulic telescoping rod's work, through controlling four hydraulic telescoping rod respectively, can transfer 1 automobile body of transport vechicle to the level, make the personnel in the cabin body 2 can be normal commander.
As an embodiment of the utility model, the lighting window 5 includes steel sheet and shellproof glass, fixed connection and shellproof glass on the inner wall of steel sheet, and the upside of steel sheet articulates in cabin body 2, can rotate the steel sheet, opens lighting window 5, realizes the ventilation, can select to close air conditioning system 4 according to actual conditions this moment to save the electric energy.
As an embodiment of the present invention, a first solar cell panel 13 is installed on the top of the cab of the transportation vehicle 1, and the first solar cell panel 13 is used for charging the storage battery.
As an embodiment of the present invention, as shown in fig. 1 and fig. 5, both sides of the cabin body 2 are equipped with two solar cell panels 14, the upper end of two solar cell panels 14 articulates on the cabin body 2, two solar cell panels 14 and the cabin body 2 are connected through two electric telescopic handle 15, two ends of two electric telescopic handle 15 articulate respectively on two solar cell panels 14 and the cabin body 2, two electric telescopic handle 15 are used for propping up two solar cell panels 14, when transport vechicle 1 is moving, two electric telescopic handle 15 shorten, make two solar cell panels 14 press close to the cabin body 2, after transport vechicle 1 passes through fixing device 3 and fixes, two electric telescopic handle 15 extend, prop up two solar cell panels 14, make two solar cell panels 14 can be abundant with the sunlight contact, improve the conversion rate of solar energy.
As an embodiment of the utility model, as shown in fig. 2, unmanned aerial vehicle transmission slide rail 16 is installed at the top of the cabin body 2, is provided with fixed wing unmanned aerial vehicle 17 on the unmanned aerial vehicle transmission slide rail 16, realizes fixed wing unmanned aerial vehicle 17's transmission.
As an embodiment of the present invention, as shown in fig. 3, unmanned aerial vehicle cabin 11 includes box 111, place the platform 112, hatch door 113, lifting device 114 and door opening mechanism 115, box 111 is the square structure of upside open-ended, the inner wall sliding connection of box 111 has place the platform 112, place unmanned multi-rotor aircraft 12 on the place the platform 112, be provided with lifting device 114 on the place the platform 112, lifting device 114 is used for reciprocating of place the platform 112, hatch door 113 articulates the upside at box 111, set up door opening mechanism 115 on the hatch door 113, door opening mechanism 115 is used for opening and shutting of hatch door 113, in operation, door opening mechanism 115 opens hatch door 113, lifting device 114 lifts place the platform 112 to the same height with hatch door 113, can carry out the remote control to unmanned multi-rotor aircraft 12 in cabin 2 this moment.
As an embodiment of the present invention, as shown in fig. 4, the hatch 113 is composed of four triangular plates with the same structure, the triangular plates are equilateral right triangle structures, the four triangular plates are respectively hinged on the upper sides of four side walls of the box 111, after the hatch 113 is opened, the four triangular plates are respectively located on four edges of the placement platform 112, the four triangular plates and the placement platform 112 jointly form a landing platform, the area of the landing platform is doubled compared with the placement platform 112, thereby the landing area of the unmanned multi-rotor aircraft 12 is larger, and the landing is easier.
As an embodiment of the present invention, the lifting device 114 is an electric telescopic rod.
As an embodiment of the utility model, the equal fixedly connected with sealing strip in one side that four triangle-shaped boards are adjacent extrudees each other between adjacent sealing strip, realizes waterproof effect, and when avoiding raining, the rainwater gets into unmanned aerial vehicle bin 11.
It should be noted that the above mentioned embodiments and embodiments are intended to demonstrate the practical application of the technical solution provided by the present invention, and should not be interpreted as limiting the scope of the present invention. Various modifications, equivalent substitutions and improvements will occur to those skilled in the art and are intended to be within the spirit and scope of the present invention. The protection scope of the present invention is subject to the appended claims.
Claims (10)
1. A digital command shelter comprises a transport vehicle (1) and a cabin body (2) installed on the transport vehicle (1), and is characterized in that four fixing devices (3) are arranged on the transport vehicle (1), an air conditioning system (4) is fixedly installed on the outer side of the cabin body (2), an access door (6) is arranged on the cabin body (2), the access door (6) is located at the tail of the transport vehicle (1), lighting windows (5) are arranged on the front side and the rear side of the cabin body (2), a battery cabin (7) and a generator cabin (8) are arranged at the bottom of the cabin body (2), a storage battery pack is installed in the battery cabin (7), a diesel generator set is installed in the generator cabin (8), the diesel generator set is used for charging the storage battery pack, a signal transceiver (9) is arranged outside the cabin body (2), and the signal transceiver (9) is installed on a first electric telescopic rod (10), the fixed end of the electric telescopic rod I (10) is fixedly arranged on the outer side wall of the cabin body (2), a central control system for digital command is arranged in the cabin body (2), and the central control system comprises a time display, an operation touch screen, a side cabinet, a side video display screen, an end video display screen, a server cabinet, an LED screen and a loudspeaker; the top of the cabin body (2) is provided with an unmanned aerial vehicle cabin (11), and an unmanned multi-rotor aircraft (12) is placed in the unmanned aerial vehicle cabin (11).
2. The digital command shelter of claim 1, wherein the fixing device (3) comprises a hydraulic rod driving device, four hydraulic telescopic rods and a bottom plate, the four hydraulic telescopic rods are respectively and fixedly installed at four corners of the transport vehicle (1), the bottom plate is fixedly connected to the lower ends of the hydraulic telescopic rods, the bottom plate is used for increasing the contact area between the hydraulic telescopic rods and the ground, and the hydraulic rod driving device is used for controlling the work of the hydraulic telescopic rods.
3. The digital command shelter according to claim 1, wherein the lighting window (5) comprises a steel plate and bulletproof glass, the bulletproof glass is fixedly connected to the inner wall of the steel plate, and the upper side of the steel plate is hinged to the shelter body (2).
4. A digital command shelter according to claim 1, characterized in that the top of the cab of the transport vehicle (1) is fitted with a first solar panel (13), the first solar panel (13) being used to charge the battery pack.
5. The digital command shelter according to claim 1, wherein two sides of the cabin body (2) are respectively provided with a second solar cell panel (14), the upper end of the second solar cell panel (14) is hinged to the cabin body (2), the second solar cell panel (14) is connected with the cabin body (2) through a second electric telescopic rod (15), and two ends of the second electric telescopic rod (15) are respectively hinged to the second solar cell panel (14) and the cabin body (2), so that the second solar cell panel (14) is supported by the second electric telescopic rod (15).
6. The digital command shelter according to claim 1, wherein the top of the shelter body (2) is provided with an unmanned aerial vehicle launching slide rail (16), and the unmanned aerial vehicle launching slide rail (16) is provided with a fixed wing unmanned aerial vehicle (17).
7. The digital command shelter of claim 1, wherein the unmanned aerial vehicle cabin (11) comprises a box body (111), a placement platform (112), a cabin door (113), a lifting device (114) and a door opening mechanism (115), the box body (111) is of a square structure with an opening on the upper side, the placement platform (112) is connected to the inner wall of the box body (111) in a sliding mode, the unmanned multi-rotor aircraft (12) is placed on the placement platform (112), the lifting device (114) is arranged at the bottom of the placement platform (112), the lifting device (114) is used for moving the placement platform (112) up and down, the cabin door (113) is hinged to the upper side of the box body (111), the door opening mechanism (115) is arranged on the cabin door (113), and the door opening mechanism (115) is used for opening and closing the cabin door (113).
8. A digital command shelter according to claim 7 characterized in that said hatch (113) is composed of four triangular plates of identical structure, said triangular plates being of equilateral right triangle structure, said four triangular plates being hinged on the upper side of the four side walls of the box (111), respectively.
9. The digital command shelter of claim 7, wherein the lifting device (114) is a three-pole electrical extension pole.
10. The digital command shelter of claim 8, wherein the adjacent sides of the four triangular plates are fixedly connected with sealing strips, and the adjacent sealing strips are mutually extruded.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921993906.2U CN212313385U (en) | 2019-11-18 | 2019-11-18 | Digital command shelter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921993906.2U CN212313385U (en) | 2019-11-18 | 2019-11-18 | Digital command shelter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212313385U true CN212313385U (en) | 2021-01-08 |
Family
ID=74029672
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921993906.2U Active CN212313385U (en) | 2019-11-18 | 2019-11-18 | Digital command shelter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212313385U (en) |
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2019
- 2019-11-18 CN CN201921993906.2U patent/CN212313385U/en active Active
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