CN211617529U - Special vehicle with hydraulic balance support system for mobile emergency command shelter - Google Patents
Special vehicle with hydraulic balance support system for mobile emergency command shelter Download PDFInfo
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- CN211617529U CN211617529U CN201921993818.2U CN201921993818U CN211617529U CN 211617529 U CN211617529 U CN 211617529U CN 201921993818 U CN201921993818 U CN 201921993818U CN 211617529 U CN211617529 U CN 211617529U
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Abstract
The utility model provides a special vehicle of a movable emergency command shelter with a hydraulic balance supporting system, which comprises a semi-trailer head and a vehicle body connected with the semi-trailer head through a pin bolt, wherein the vehicle body comprises a chassis, wheels, a command shelter and the hydraulic balance supporting system, the command shelter is provided with an access door which is positioned at the tail part of the vehicle body, and the front side and the rear side of the command shelter are both provided with lighting windows; the hydraulic balance supporting system comprises a hydraulic telescopic rod, an upper sleeve, a lower sleeve, a reinforcing rib, a rotating shaft, a limiting piece, a hinged rod and an adjusting component, the hydraulic balance supporting system is arranged on the semitrailer head, so that the semitrailer head can be stably fixed on the ground, the semitrailer head can be separated from the semitrailer head at the moment, the semitrailer head is applied to the transportation of other materials, the service efficiency of the semitrailer head is improved, and the semitrailer body can be rapidly and stably fixed on the ground under the condition that the semitrailer head is separated from the semitrailer body.
Description
Technical Field
The utility model relates to a commander shelter technical field, specifically speaking relates to a remove emergent commander shelter special type vehicle with hydraulic pressure balanced braced system.
Background
At present, for the conditions of anti-terrorism, emergency, disaster prevention, group events, large-scale security, high-level security police, and the like, a multifunctional special vehicle is urgently needed in public security police work, and the current emergency command vehicle has too single and simple function and cannot adapt to high-tech operation.
At present, a chinese patent with patent application number 201420714137.9 discloses a remove emergency command shelter special vehicle, which comprises a carriage body, be provided with the command cabin body in the automobile body, be provided with multi-functional folding official working platform in the command cabin body, the afterbody and the well door department of automobile body are provided with electronic footboard of getting on the bus, front end and the end at automobile body top are provided with high definition cloud platform respectively and make a video recording illumination platform, the central part of automobile body is provided with on-vehicle air conditioning system and satellite television receiving system and commands cabin body bottom and still is provided with on-vehicle power supply system and hydraulic pressure balanced braced system, the top of automobile body still is provided with warning light alarm system.
Foretell remove emergency command shelter special vehicle, can make the commander's cabin quick removal in the field, but this commander's cabin special vehicle has the overall arrangement unreasonable, can't carry unmanned aerial vehicle, and unmanned aerial vehicle can be more accurate acquisition information more fast in natural disasters frequently and military demonstration at present, and simultaneously, this vehicle locomotive and automobile body can't separate, under the most circumstances of emergent disaster prevention, need to transport a large amount of goods and materials to disaster area front line, the back is arranged to emergency command shelter, the locomotive can't break away from to do other things, work such as goods and materials transportation, the rate of utilization that has caused the locomotive falls, if can separate the locomotive, can accelerate the speed of transporting of goods and materials, transport front line with more goods and materials.
SUMMERY OF THE UTILITY MODEL
In order to solve the defects of the prior art, the utility model aims to provide a remove emergency command shelter special vehicle with hydraulic pressure balance braced system to overcome the defect among the prior art.
In order to achieve the purpose, the utility model provides a special vehicle with a hydraulic balance support system for a mobile emergency command shelter, which comprises a semitrailer head and a vehicle body connected with the semitrailer head through a pin bolt, wherein the vehicle body comprises a chassis, wheels, a command shelter and the hydraulic balance support system; wherein, hydraulic balance braced system includes hydraulic telescoping rod, the upper sleeve, the lower sleeve, the strengthening rib, the apparatus further comprises a rotating shaft, spacing piece, hinge bar and adjusting part, hydraulic telescoping rod fixed mounting is at the lateral wall on chassis, hydraulic telescoping rod's lower extreme fixedly connected with upper sleeve, be connected through cylindric strengthening rib between upper sleeve and lower sleeve, it is connected with spacing piece to rotate on the strengthening rib, the articulated one end that has the hinge bar on the spacing piece, the other end of hinge bar articulates in the pivot, the pivot is rotated through a plurality of bearings and is connected in upper sleeve and lower sleeve, lower telescopic lower extreme is the toper structure, adjusting part is connected with the pivot transmission, so that adjusting part can drive the pivot rotation.
Through above-mentioned technical scheme, can be under the condition that semitrailer head and automobile body break away from, quick and stable fix the automobile body on ground to adjust the balance of automobile body.
As a further explanation of the special vehicle of the mobile emergency command shelter of the present invention, preferably, the adjusting assembly includes a reduction gear set, a connecting rod and an inner hexagon bolt; the output end of the reduction gear set is fixedly connected with one end of a connecting rod, the other end of the connecting rod is fixedly connected with an inner hexagon bolt, a rotating shaft of the inner hexagon bolt penetrates through the upper sleeve, and the output end of the reduction gear set is fixedly connected with a rotating shaft.
Through above-mentioned technical scheme, can realize the rotation of pivot through rotating hexagon socket head cap screw, reduction gear set can reduce the required torsion of rotatory hexagon socket head cap screw.
As right the utility model discloses a remove further explanation of emergency command shelter special type vehicle, preferably, the top of commander's shelter is equipped with warning light alarm system.
Through above-mentioned technical scheme, can send the warning to the external world when using, warn other vehicles.
As right the further explanation of removal emergency command shelter special type vehicle, preferably, warning light alarm system includes the long row warning light of commander shelter top front end and the reddish blue utmost point light flashing light of commander shelter side.
Through above-mentioned technical scheme, can realize the warning effect of long row warning light and red blue aurora flashing light, can effectual warning other vehicles and personnel.
As right the further explanation of removal emergency command shelter special type vehicle of the utility model, preferably, one side that the pivot was kept away from to spacing piece is the cutting edge shape setting.
Through above-mentioned technical scheme, can reduce the resistance that spacing piece cut into in earth.
As right the further explanation of removal emergency command shelter special type vehicle, preferably, the top of commander's shelter is provided with unmanned aerial vehicle bin and on-vehicle air conditioning system, unmanned many rotor crafts have been placed in the unmanned aerial vehicle bin.
Through above-mentioned technical scheme, can release unmanned many rotor crafts to faster acquire the video information of front line, on-vehicle air conditioning system can control the temperature in the commander's cabin.
As right the further explanation of removal emergency command shelter special vehicle, preferably, the unmanned aerial vehicle bin includes box, place the platform, hatch door, lifting device and mechanism of opening the 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 the door on the hatch door, the mechanism of opening the door is used for opening and shutting of hatch door.
Through above-mentioned technical scheme, can realize depositing and retrieving of unmanned many rotor crafts.
As right the further explanation of removal emergency command shelter special type vehicle, preferably, the hatch door comprises four triangle-shaped plates that the structure is the same, the triangle-shaped plate is equilateral right triangle-shaped structure, four the 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 to the further explanation of the special vehicle for the mobile emergency command shelter of the present invention, preferably, the lifting device is an electric telescopic rod.
Compared with the prior art, the beneficial effects of the utility model are as follows:
1. the hydraulic balance supporting system is arranged on the semitrailer head, and after the semitrailer reaches a designated position, the hydraulic balance supporting system is started, the limiting piece can be screwed out, the contact area between the limiting piece and soil is increased, so that the semitrailer head can be stably fixed on the ground, the semitrailer head can be separated from the semitrailer head at the moment to be applied to conveying other materials, the use efficiency of the semitrailer head is improved, the semitrailer head can be quickly and stably fixed on the ground under the condition that the semitrailer head is separated from the semitrailer body, and when the hydraulic balance supporting system is pulled out of the ground, the limiting piece can be withdrawn only by adjusting the rotating shaft in the opposite direction, so that the lower sleeve can be quickly pulled out of the soil, and quick transfer is realized;
2. by flying the unmanned multi-rotor aircraft, the landform and the geomorphology near the semitrailer head can be acquired more quickly and accurately, the surrounding environment of the semitrailer head can be monitored, the safety of the cabin body is ensured, information can be acquired more quickly and accurately, and therefore quick 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 the present invention;
fig. 2 is a schematic structural view of the hydraulic balance support system of the present invention;
FIG. 3 is a cross-sectional view A-A of FIG. 2;
FIG. 4 is a schematic view of another operating state of FIG. 3;
FIG. 5 is a cross-sectional view taken along line B-B of FIG. 2;
fig. 6 is a cross-sectional view of the unmanned aerial vehicle cabin of the present invention;
fig. 7 is the utility model discloses well schematic diagram after the hatch door of unmanned aerial vehicle cabin is opened.
In the figure: the semi-trailer comprises a semi-trailer head 1, a trailer body 2, a chassis 21, wheels 22, a command shelter 23, an access door 24, a daylight window 25, a hydraulic balance supporting system 26, a hydraulic telescopic rod 261, an upper sleeve 262, a lower sleeve 263, reinforcing ribs 264, a rotating shaft 265, a limiting piece 266, a hinge rod 267, a reduction gear set 268, an inner hexagon bolt 269, a warning lamp alarm system 27, a vehicle-mounted air conditioning system 28, an unmanned aerial vehicle cabin 11, a multi-rotor aircraft 12, a box body 111, a placement platform 112, a cabin door 113, a lifting device 114 and a door opening mechanism 115.
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.
Referring to fig. 1, the present invention provides a technical solution: a special vehicle with a hydraulic balance support system for a movable emergency command shelter comprises a semitrailer head 1 and a vehicle body 2 connected to the semitrailer head 1 through a pin bolt, wherein the vehicle body 2 comprises a chassis 21, wheels 22, a command shelter 23 and a hydraulic balance support system 26, an access door 24 is arranged on the command shelter 23, the access door 24 is positioned at the tail part of the vehicle body 2, and lighting windows 25 are arranged on the front side and the rear side of the command shelter 23; wherein the content of the first and second substances,
referring to fig. 2-4, the hydraulic balance support system 26 includes a hydraulic telescopic rod 261, an upper sleeve 262, a lower sleeve 263, a reinforcing rib 264, a rotating shaft 265, a limiting piece 266, a hinge rod 267 and an adjusting assembly, the hydraulic telescopic rod 261 is fixedly installed on a side wall of the chassis 21, the lower end of the hydraulic telescopic rod 261 is fixedly connected with the upper sleeve 262, the upper sleeve 262 is connected with the lower sleeve 263 through a cylindrical reinforcing rib 264, the reinforcing rib 264 is rotatably connected with the limiting piece 266, the limiting piece 266 is hinged with one end of the hinge rod 267, the other end of the hinge rod 267 is hinged on the rotating shaft 265, the rotating shaft 265 is rotatably connected in the upper sleeve 262 and the lower sleeve 263 through a plurality of bearings, the lower end of the lower sleeve 263 is a conical structure, so that the lower sleeve 263 is rapidly inserted into the soil, the adjusting assembly is in transmission connection with the rotating shaft 265, so that the adjusting assembly can drive the, start hydraulic pressure balanced support system 26, control hydraulic telescoping rod 261 extension, make lower sleeve 263 insert in earth, drive pivot 265 anticlockwise rotation through adjusting part, make to rotate drive hinge rod 267 and unscrew spacing piece 266, the area of contact of spacing piece 266 with earth has been increased, thereby make fixing subaerial that automobile body 2 can be stable, can break away from semitrailer head 1 and locomotive this moment, go the transportation of being applied to other goods and materials, can be under the condition that semitrailer head 1 breaks away from with automobile body 2, quick and stable fix automobile body 2 on ground, when taking hydraulic pressure balanced support system 26 out ground, only need reverse direction regulation pivot 265, can withdraw spacing piece 266, thereby make lower sleeve 263 can be quick take out from earth, realize quick transfer.
Referring to fig. 5, as an embodiment of the present invention, the adjusting assembly includes a reduction gear set 268, a connecting rod and a socket head cap screw 269; one end of reduction gear set 268's output fixed connection connecting rod, hexagon socket head cap screw 269 in the other end fixedly connected with of connecting rod, interior hexagon socket head cap screw 269 pivot 265 runs through upper sleeve 262, reduction gear set 268's output fixed connection pivot 265, through the quick rotatory hexagon socket head cap screw 269 of electronic torque wrench, make reduction gear set 268 drive pivot 265 rotatory at a slow speed, pivot 265 drives hinge rod 267 and rotates, thereby realize spacing piece 266's back-out and screw in, reduction gear set 268 can reduce the required torsion of rotatory hexagon socket head cap screw 269.
Referring to fig. 1, as an embodiment of the present invention, a warning light alarm system 27 is disposed at the top of the command shelter 23, and can send out an alarm to the outside to warn other vehicles when in use.
As an embodiment of the utility model, warning lamp alarm system 27 is including the long row warning lamp of commander shelter 23 top front end and the reddish blue aurora that commander shelter 23 side explodes the flashing light, and the during operation, the light-emitting of long row warning lamp and reddish blue aurora explodes the flashing light, can other vehicles of effectual warning and personnel.
Referring to fig. 3-4, as an embodiment of the present invention, the side of the limiting piece 266 away from the rotating shaft 265 is a blade-shaped arrangement, which can reduce the resistance of the limiting piece 266 cutting into the soil.
Please refer to fig. 6, as an embodiment of the present invention, the top of the command shelter 23 is provided with an unmanned aerial vehicle cabin 11 and a vehicle-mounted air conditioning system 28, the unmanned aerial vehicle cabin 11 has an unmanned multi-rotor aircraft 12 placed therein, and the unmanned multi-rotor aircraft 12 can be released, so as to obtain the video information of the front line more quickly, and the vehicle-mounted air conditioning system 28 can control the temperature in the command shelter 23.
Please refer to fig. 7, as an embodiment of the present invention, the unmanned aerial vehicle cabin 11 includes a box 111, a placement platform 112, a cabin door 113, a lifting device 114 and a door opening mechanism 115, the box 111 is a square structure with an open upper side, the inner wall of the box 111 is slidably connected to the placement platform 112, the unmanned multi-rotor aircraft 12 is placed on the placement platform 112, the placement platform 112 is provided with the lifting device 114, the lifting device 114 is used for the vertical movement of the placement platform 112, the cabin door 113 is hinged to the upper side of the box 111, the cabin door 113 is provided with the door opening mechanism 115, the door opening mechanism 115 is used for the opening and closing of the cabin door 113, in operation, the door opening mechanism 115 opens the cabin door 113, the lifting device 114 lifts the placement platform 112 to the same height as the cabin door 113, and at this time, the unmanned multi-rotor aircraft 12 can be.
Please refer to fig. 7, as an embodiment of the present invention, the cabin door 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 cabin door 113 is opened, the four triangular plates are respectively located on four edges of the placing platform 112, the four triangular plates and the placing platform 112 jointly form a landing platform, the area of the landing platform is doubled compared with the placing 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. 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 (9)
1. A special vehicle with a hydraulic balance support system for a mobile emergency command shelter comprises a semitrailer head (1) and a vehicle body (2) connected to the semitrailer head (1) through a pin bolt, and is characterized in that,
the vehicle body (2) comprises a chassis (21), wheels (22), a commanding shelter (23) and a hydraulic balance supporting system (26), wherein an access door (24) is arranged on the commanding shelter (23), the access door (24) is positioned at the tail part of the vehicle body (2), and lighting windows (25) are arranged on the front side and the rear side of the commanding shelter (23); wherein the content of the first and second substances,
the hydraulic balance supporting system (26) comprises a hydraulic telescopic rod (261), an upper sleeve (262), a lower sleeve (263), a reinforcing rib (264), a rotating shaft (265), a limiting piece (266), a hinged rod (267) and an adjusting component, wherein the hydraulic telescopic rod (261) is fixedly installed on the side wall of the chassis (21), the lower end of the hydraulic telescopic rod (261) is fixedly connected with the upper sleeve (262), the upper sleeve (262) is connected with the lower sleeve (263) through the cylindrical reinforcing rib (264), the reinforcing rib (264) is rotatably connected with the limiting piece (266), the limiting piece (266) is hinged with one end of the hinged rod (267), the other end of the hinged rod (267) is hinged on the rotating shaft (265), the rotating shaft (265) is rotatably connected in the upper sleeve (262) and the lower sleeve (263) through a plurality of bearings, the lower end of the lower sleeve (263) is of a conical structure, and the adjusting component is in transmission connection with the rotating shaft (265, so that the adjusting component can drive the rotating shaft (265) to rotate.
2. The mobile emergency command shelter specialty vehicle of claim 1, wherein: the adjustment assembly includes a reduction gear set (268), a connecting rod and a socket head cap screw (269); the output end of reduction gear set (268) is fixed connection the one end of connecting rod, the other end fixed connection of connecting rod has hexagon socket head cap screw (269), and upper sleeve (262) is run through in hexagon socket head cap screw (269), output fixed connection pivot (265) of reduction gear set (268).
3. The mobile emergency command shelter specialty vehicle of claim 1, wherein: and the top of the command shelter (23) is provided with a warning lamp alarm system (27).
4. The mobile emergency command shelter specialty vehicle of claim 3, wherein: the warning lamp alarm system (27) comprises a long-row warning lamp at the front end of the top of the command shelter (23) and a red and blue extreme light flashing lamp on the side surface of the command shelter (23).
5. The mobile emergency command shelter specialty vehicle of claim 1, wherein: one side of the limiting sheet (266) far away from the rotating shaft (265) is arranged in a blade shape.
6. The mobile emergency command shelter specialty vehicle of claim 1, wherein: the top of commander shelter (23) is provided with unmanned aerial vehicle bin (11) and on-vehicle air conditioning system (28), unmanned many rotor crafts (12) have been placed in unmanned aerial vehicle bin (11).
7. The mobile emergency command shelter specialty vehicle of claim 6, wherein: unmanned aerial vehicle bin (11) are including box (111), place platform (112), hatch door (113), lifting device (114) and mechanism of opening door (115), box (111) is upside open-ended square structure, the inner wall sliding connection of box (111) has place platform (112), place unmanned many rotor crafts (12) on place platform (112), place platform (112) bottom is provided with lifting device (114), lifting device (114) are used for reciprocating of place platform (112), hatch door (113) articulate the upside at box (111), set up mechanism of opening door (115) on hatch door (113), mechanism of opening door (115) is used for opening and shutting of hatch door (113).
8. The special vehicle of a mobile emergency command shelter according to claim 7, characterized in that the hatch (113) consists of four triangular plates of identical structure, which are of equilateral right triangle structure and are hinged on the upper side of the four side walls of the box (111), respectively.
9. The mobile emergency command shelter specialty vehicle of claim 7, wherein said lifting device (114) is an electric telescopic rod.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921993818.2U CN211617529U (en) | 2019-11-18 | 2019-11-18 | Special vehicle with hydraulic balance support system for mobile emergency command shelter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921993818.2U CN211617529U (en) | 2019-11-18 | 2019-11-18 | Special vehicle with hydraulic balance support system for mobile emergency command shelter |
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| Publication Number | Publication Date |
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| CN211617529U true CN211617529U (en) | 2020-10-02 |
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| CN201921993818.2U Active CN211617529U (en) | 2019-11-18 | 2019-11-18 | Special vehicle with hydraulic balance support system for mobile emergency command shelter |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114771389A (en) * | 2022-04-22 | 2022-07-22 | 北京诚志北分机电技术有限公司 | Satellite communication command vehicle |
-
2019
- 2019-11-18 CN CN201921993818.2U patent/CN211617529U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114771389A (en) * | 2022-04-22 | 2022-07-22 | 北京诚志北分机电技术有限公司 | Satellite communication command vehicle |
| CN114771389B (en) * | 2022-04-22 | 2023-09-05 | 北京诚志北分机电技术有限公司 | Satellite communication command car |
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