Composite combat emergency command vehicle

Abstract

The utility model discloses a composite combat emergency command vehicle, and relates to the technical field of command vehicles. The vehicle comprises a vehicle body, a protective shell, a shielding assembly and a supporting plate, the protective shell is fixed to the top of the vehicle body, a glass plate is fixed to the top of the protective shell in a penetrating mode, an opening is formed in the top of the vehicle body along the transverse center line, the shielding assembly is arranged in the opening, and an electric push rod is fixed to the portion, in the protective shell, of the top of the vehicle body; reeds are symmetrically fixed to the top of the bottom plate, a supporting plate is fixed to the tops of the two reeds together, a wireless charger is vertically fixed in the supporting plate in a penetrating mode, and a solar panel is fixed to the portion, below the glass plate, in the protective shell. By arranging the vehicle body, the protective shell, the shielding assembly and the supporting plate, the problems that power supply power needs to be additionally increased when an emergency combat command vehicle uses an unmanned aerial vehicle, electric power shortage of the vehicle is easily caused, and after the unmanned aerial vehicle leaves, a wireless charger continues to work, and electric energy is wasted are solved.

Description

Technical Field

[0001] The utility model belongs to the technical field related to command vehicles, in particular to a synthetic combat emergency command vehicle. Background Art

[0002] The synthetic combat emergency command vehicle is a vehicle used for emergency command and combat, usually used in public security, armed police, firefighting, urban law enforcement and other scenarios. The synthetic combat emergency command vehicle is equipped with a variety of information collection equipment, such as electronic fences, radio detection scanning, image reconnaissance, intercom and ID card fingerprint reader listening, etc. The vehicle integrates a variety of advanced police equipment and technical systems, such as high-speed intelligent pan-tilt camera, intelligent linear undercarriage scanner, millimeter wave detection system, drone aerial electronic and image reconnaissance system, search and control system, individual combat system, poison gas detection system, laser dazzling blinding system, radar radio scanning system, etc. Among them, the drone is an important combat information collection tool on the vehicle, but it still has the following disadvantages in actual use:

[0003] Usually, the emergency operation environment is relatively harsh, so fuel vehicles are used as the main body. When setting up drones on combat vehicles, since most drones are powered by electricity, they need to be charged after returning, and the power on the vehicle is relatively tight. When additional power is supplied to the drone, it is easy to cause a shortage of power in the vehicle;

[0004] Secondly, on the emergency command vehicle, the operator needs to manually place the drone into the charging compartment to release it. In order to facilitate the stability of emergency operations, drones are usually charged wirelessly. Keeping wireless charging on at all times also consumes electricity, and it is not possible to cut off the power supply of the wireless charger after the drone leaves. Utility Model Content

[0005] The purpose of the utility model is to provide a synthetic combat emergency command vehicle. By arranging a vehicle body, a protective shell, a shielding component and a support plate, the utility model solves the problem that the emergency combat command vehicle needs to increase the power supply when using a drone, which easily causes power shortage of the vehicle, and the wireless charger continues to work and wastes electricity after the drone leaves.

[0006] In order to solve the above technical problems, the utility model is realized by the following technical solutions:

[0007] The utility model discloses a synthetic combat emergency command vehicle, comprising a vehicle body, a protective shell, a shielding assembly and a support plate, wherein the top of the vehicle body is fixed with a protective shell, the top of the protective shell is penetrated and fixed with a glass plate, the glass plate is arranged at a short side of the top of the vehicle body, the top of the vehicle body is provided with an opening along the transverse center line, the shielding assembly is arranged in the opening, the shielding assembly comprises a movable frame and a telescopic curtain, the movable frame is movably connected in the opening, a telescopic curtain is fixed on one side of the movable frame and the telescopic curtain is arranged on the top of the protective shell, the end of the telescopic curtain away from the sliding frame is fixed to the top of the protective shell, and the vehicle in the protective shell is provided with a movable frame. An electric push rod is fixed on the top of the body, and a bottom plate is fixed to the telescopic end of the electric push rod, and reeds are symmetrically fixed on the top of the bottom plate. A support plate is fixed to the top of the two reeds, and the support plate is arranged below the opening. A wireless charger is fixed vertically through the support plate, and a solar panel is fixed in the protective shell below the glass plate. When working, the protective shell and the electric push rod are fixed thereon through the body, and the body moves when working. When the protective shell is working, a drone can be accommodated therein, and the drone in the protective shell can be shielded by a shielding component, and the drone is supported and arranged in the protective shell by the support plate.

[0008] Furthermore, a skylight is provided on the top of the vehicle body, and the skylight is arranged on the outside of the support plate in a bird's-eye view. The vehicle body provides a function of placing the drone on the support plate inside the vehicle through the skylight.

[0009] Furthermore, a sliding bar is symmetrically fixed on the top of the protective shell with a center line parallel to the long side, and the sliding bar is arranged on both sides of the opening. When the protective shell is working, the sliding frame is movably connected through the sliding bar.

[0010] Furthermore, a storage battery is fixed at the bottom of the solar panel, and the solar panel is electrically connected to the storage battery, so that when the solar panel is working, the storage battery stores the electrical energy generated by the solar panel.

[0011] Furthermore, the shielding assembly also includes a connecting rope, a fixed pulley, an electric roller and a sliding frame. Two electric rollers are rotatably connected to the inner wall of the protective shell below the opening. The output ends of the two electric rollers are respectively fixedly connected to the inner wall of the protective shell. Two fixed pulleys are fixed on the two electric rollers. Two connecting ropes are fixed on the movable frame. The two ends of the two connecting ropes are placed on both sides of the movable frame. The two fixed pulleys are arranged below the position where the connecting ropes are connected on the movable frame in a top-down perspective. The same connecting rope is wound around the fixed pulleys at the same position of the two electric rollers. Sliding frames are fixed at the two short sides of the top of the movable frame. The sliding frames are movably connected to the outside of the sliding bar. The telescopic curtain is driven by the electric roller to cover and open the opening.

[0012] Furthermore, the top of the wireless charger is flush with the top of the support plate, a push switch is fixed in the center of the bottom end of the wireless charger, the bottom of the push switch is flush with the top of the base plate, the battery is electrically connected to the wireless charger, and when the push switch is pressed, the wireless charger is started to charge the drone.

[0013] The utility model has the following beneficial effects:

[0014] The utility model solves the problem that the emergency combat command vehicle needs to increase the power supply when using the drone, which easily causes power shortage of the vehicle, by providing a vehicle body, a protective shell and a support plate. During operation, when the vehicle body is in motion, the protective shell is driven to move. When the vehicle body moves to a sunny place, the sunlight passes through the glass plate on the top of the protective shell and is transmitted to the solar panel. After the solar panel generates electricity, the electric energy is transmitted to the battery, stored in the battery, and transmitted to the wireless charger for wireless charging of the drone, so that the drone does not need to increase the power supply on the command vehicle, thereby reducing the power shortage of the vehicle.

[0015] The utility model solves the problem of wasting electric energy by the wireless charger continuing to work after the UAV leaves the emergency combat command vehicle by arranging a vehicle body, a protective shell, a shielding component and a supporting plate. When the UAV is released, the electric roller is started to rotate again to fold the telescopic curtain so that the opening is opened to carry out the UAV release operation. After the UAV leaves, the switch is pressed and released under the rebound effect of the spring leaf to stop the power supply of the wireless charger, so that the wireless charger can be powered off in time after the UAV leaves the emergency combat command vehicle to prevent electric energy from being wasted. In addition, by using the wireless charger, the UAV does not need to be taken back into the vehicle for charging after it is retrieved. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] In order to more clearly illustrate the technical solutions of the embodiments of the utility model, the drawings required for describing the embodiments are briefly introduced below. Obviously, the drawings described below are only some embodiments of the utility model. For ordinary technicians in this field, other drawings can be obtained based on these drawings without creative work.

[0017] Figure 1 This is a three-dimensional diagram of the structure of a synthetic combat emergency command vehicle after partial cutaway;

[0018] Figure 2 The structural stereogram of the vehicle body is as follows;

[0019] Figure 3 The figure is a three-dimensional diagram of the structure of the protective shell;

[0020] Figure 4 A structural stereogram of a shielding assembly;

[0021] Figure 5 This is a structural stereogram of the support plate viewed from above;

[0022] Figure 6 This is a three-dimensional diagram of the assembly structure of a synthetic combat emergency command vehicle.

[0023] Reference numerals:

[0024] 1. Vehicle body; 101. Skylight window; 2. Protective shell; 201. Opening; 202. Sliding bar; 203. Glass plate; 204. Solar panel; 205. Battery; 3. Shielding assembly; 301. Movable frame; 302. Connecting rope; 303. Fixed pulley; 304. Electric roller; 305. Sliding frame; 306. Telescopic curtain; 4. Support plate; 401. Wireless charger; 402. Push switch; 403. Reed; 404. Bottom plate; 405. Electric push rod. DETAILED DESCRIPTION

[0025] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments of the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model. Specific embodiment 1

[0026] See also Figure 1-5The utility model is a synthetic combat emergency command vehicle, comprising a vehicle body 1, a protective shell 2, a shielding component 3 and a support plate 4. The protective shell 2 is fixed on the top of the vehicle body 1. When the vehicle body 1 is working, the protective shell 2 is fixed thereon, and the unmanned aerial vehicle supported on the support plate 4 is protected by the protective shell 2. A glass plate 203 is fixed through the top of the protective shell 2. When the glass plate 203 is working, sunlight is transmitted to the solar panel 204, and the solar panel 204 is used to supply power to the battery 205. The glass plate 203 is arranged on a short side of the top of the vehicle body 1. An opening 201 is provided at the top of the vehicle body 1 along the transverse center line, and a position for the support plate 4 to enter and exit the vehicle body 1 when the support plate 4 is raised or lowered is provided through the opening 201. A shielding component 3 is provided in the opening 201, and the opening 201 on the protective shell 2 is shielded by the shielding component 3. The shielding component 3 includes a movable frame 301 and a telescopic curtain 306. When the telescopic curtain 306 is working, the opening 201 is shielded. The movable frame 301 is movably connected in the opening 201, and a telescopic curtain 306 is fixed on one side of the movable frame 301, and the telescopic curtain 306 is arranged on the top of the protective shell 2. The end of the telescopic curtain 306 away from the movable frame 301 is fixed to the top of the protective shell 2. When the movable frame 301 works, it is slidably connected in the opening 201, driving the telescopic curtain 306 to extend and retract, covering and opening the opening 201. An electric push rod 405 is fixed to the top of the vehicle body 1 in the protective shell 2. The electric push rod 405 drives the bottom plate 404 to rise and fall. The telescopic end of the electric push rod 405 is fixed to the bottom plate 404. The top of the bottom plate 404 is symmetrically fixed with springs 403. The tops of the two springs 403 are jointly fixed with a support plate 4. The support plate 4 is set Below the opening 201, a wireless charger 401 is fixed vertically through the support plate 4. When it is necessary to receive a drone, the electric push rod 405 is started, and the electric push rod 405 drives the support plate 4 to rise, driving the support plate 4 to rise above the opening 201. When the drone falls on the support plate 4, the weight of the drone presses down the spring sheet 403, which is set on the wireless charger 401. Wireless charging is performed through the wireless charger 401. A solar panel 204 is fixed in the protective shell 2 below the glass plate 203, and the solar panel 204 generates electricity after receiving sunlight.

[0027] Specifically, a skylight window 101 is opened on the top of the vehicle body 1 , and the skylight window 101 is arranged on the outside of the support plate 4 in a top view. When the vehicle body 1 is working, the skylight installation of the vehicle body 1 is provided through the skylight window 101 .

[0028] Furthermore, a sliding bar 202 is symmetrically fixed on the top of the protective shell 2 with a center line parallel to the long side. The sliding bar 202 is arranged on both sides of the opening 201. When the protective shell 2 is working, it is movably connected to the sliding frame 305 through the sliding bar 202.

[0029] Furthermore, a storage battery 205 is fixed to the bottom of the solar panel 204 , and the solar panel 204 is electrically connected to the storage battery 205 . After the solar panel 204 generates electricity, the electricity is stored in the storage battery 205 .

[0030] The operation process of this embodiment is as follows: during operation, when the vehicle body 1 is in motion, the protective shell 2 is driven to move. When the vehicle body 1 moves to a sunny place, the sunlight passes through the glass plate 203 on the top of the protective shell 2 and is transmitted to the solar panel 204. After the solar panel 204 generates electricity, the electric energy is transmitted to the battery 205, and the electricity is stored in the battery 205. The battery 205 transmits the electricity to the wireless charger 401 to wirelessly charge the drone. Specific embodiment 2

[0031] See also Figure 1-6 On the basis of the specific embodiment 1, the shielding assembly 3 further includes a connecting rope 302, a fixed pulley 303, an electric roller 304 and a sliding frame 305. Two electric rollers 304 are rotatably connected to the inner wall of the protective shell 2 below the opening 201. The output ends of the two electric rollers 304 are respectively fixedly connected to the inner wall of the protective shell 2. Two fixed pulleys 303 are fixed on the two electric rollers 304. Two connecting ropes 302 are fixed on the movable frame 301. The two ends of the two connecting ropes 302 are respectively placed on both sides of the movable frame 301. The two fixed pulleys 303 are arranged below the position where the connecting ropes 302 are connected on the movable frame 301 in a top-down perspective. The same connecting rope 302 is wound around the fixed pulley 303 at the same position of the two electric rollers 304, and the two short sides of the top of the movable frame 301 are fixed with sliding frames 305, and the sliding frames 305 are movably connected to the outside of the sliding bar 202. When the shielding component 3 is working, the electric roller 304 drives the fixed pulley 303 to rotate when it rotates, and the fixed pulley 303 drives the connecting rope 302 thereon to move when it rotates, and the movable frame 301 is driven to move through the connecting rope 302. After the movable frame 301 is pushed, the telescopic curtain 306 is pushed to be telescoped, and the sliding frame 305 is slidably connected to the sliding bar 202 to cooperate to limit the telescopic curtain 306 when it is telescoped.

[0032] Specifically, the top of the wireless charger 401 is flush with the top of the support plate 4, a push switch 402 is fixed in the center of the bottom of the wireless charger 401, the bottom of the push switch 402 is flush with the top of the bottom plate 404, the battery 205 is electrically connected to the wireless charger 401, and when the wireless charger 401 is working, when the drone falls on the support plate 4, the weight borne by the support plate 4 increases, driving the reed 403 to press down, so that after the push switch 402 is pressed down, the wireless charger 401 is started to charge the drone supported on the support plate 4.

[0033] The operation process of this embodiment is as follows: during operation, when it is necessary to receive the UAV, the electric push rod 405 is started, and the electric roller 304 is started to rotate at the same time, driving the fixed pulley 303 to rotate. During the rotation of the fixed pulley 303, the movable frame 301 is driven to move, so that the movable frame 301 drives the sliding frame 305 to move on the sliding bar 202 on the protective shell 2, so that the telescopic curtain 306 shrinks and the opening 201 on the protective shell 2 is opened. After the opening 201 is opened, the electric push rod 405 is started, and the bottom plate 404 is driven to rise by the electric push rod 405 until the support plate 4 rises above the opening 201, and then the UAV is landed. When the UAV lands on the support plate 4, the push rod 405 is pressed. The support plate 4 and the reed 403 press the push switch 402 on the wireless charger 401, and the wireless charger 401 starts charging the drone. At the same time, the support plate 4 is driven to descend through the electric push rod 405 until the drone enters the protective shell 2, and then the electric roller 304 is started to reverse, driving the movable frame 301 to move to the contact glass plate 203, completing the shielding effect of the telescopic curtain 306 on the drone. When the drone is released, the electric roller 304 is started to rotate again, and the telescopic curtain 306 is folded to open the opening 201, and the drone is released. After the drone leaves, under the rebound effect of the reed 403, the push switch 402 is released, and the power supply of the wireless charger 401 is stopped.

[0034] In the description of this specification, the description with reference to the terms "one embodiment", "example", "specific example", etc. means that the specific features, structures, materials or characteristics described in conjunction with the embodiment or example are included in at least one embodiment or example of the utility model. In this specification, the schematic representation of the above terms does not necessarily refer to the same embodiment or example. Moreover, the specific features, structures, materials or characteristics described can be combined in any one or more embodiments or examples in a suitable manner.

[0035] The preferred embodiments of the utility model disclosed above are only used to help explain the utility model. The preferred embodiments do not describe all the details in detail, nor do they limit the utility model to the specific implementation methods described. Obviously, many modifications and changes can be made according to the content of this specification. This specification selects and specifically describes these embodiments in order to better explain the principles and practical applications of the utility model, so that technicians in the relevant technical field can well understand and use the utility model. The utility model is limited only by the claims and their full scope and equivalents.

Claims

1. A synthetic combat emergency command vehicle, comprising a vehicle body (1), a protective shell (2), a shielding component (3) and a support plate (4), characterized in that: A protective shell (2) is fixed on the top of the vehicle body (1); a glass plate (203) is fixed through the top of the protective shell (2); the glass plate (203) is arranged at a short side of the top of the vehicle body (1); an opening (201) is provided on the top of the vehicle body (1) along the transverse center line; a shielding component (3) is arranged in the opening (201); the shielding component (3) comprises a movable frame (301) and a telescopic curtain (306); the movable frame (301) is movably connected in the opening (201); a telescopic curtain (306) is fixed on one side of the movable frame (301); and the telescopic curtain (306) is arranged on the top of the protective shell (2); One end of the telescopic curtain (306) away from the sliding frame (305) is fixed to the top of the protective shell (2); an electric push rod (405) is fixed to the top of the vehicle body (1) in the protective shell (2); a bottom plate (404) is fixed to the telescopic end of the electric push rod (405); spring leaves (403) are symmetrically fixed to the top of the bottom plate (404); a support plate (4) is fixed to the tops of the two spring leaves (403); the support plate (4) is arranged below the opening (201); a wireless charger (401) is fixed vertically through the support plate (4); and a solar panel (204) is fixed to the protective shell (2) below the glass plate (203).

2. The synthetic combat emergency command vehicle according to claim 1, characterized in that: The top of the vehicle body (1) is provided with a skylight window (101), and the skylight window (101) is arranged outside the support plate (4) in a top-down perspective.

3. The synthetic combat emergency command vehicle according to claim 1, characterized in that: A sliding bar (202) is symmetrically fixed to the top of the protective shell (2) along a center line parallel to the long side, and the sliding bar (202) is arranged on both sides of the opening (201).

4. The synthetic combat emergency command vehicle according to claim 1, characterized in that: A storage battery (205) is fixed to the bottom of the solar panel (204), and the solar panel (204) is electrically connected to the storage battery (205).

5. The synthetic combat emergency command vehicle according to claim 3 is characterized by: The shielding assembly (3) further comprises a connecting rope (302), a fixed pulley (303), an electric roller (304) and a sliding frame (305); two electric rollers (304) are rotatably connected to the inner wall of the protective shell (2) below the opening (201); output ends of the two electric rollers (304) are respectively fixedly connected to the inner wall of the protective shell (2); two fixed pulleys (303) are fixed to the two electric rollers (304); and two connecting ropes (302) are fixed to the movable frame (301). The two ends of the two connecting ropes (302) are respectively placed on both sides of the movable frame (301); the two fixed pulleys (303) are arranged below the position of the connecting rope (302) on the movable frame (301) in a top view; the same connecting rope (302) is wound around the fixed pulleys (303) at the same position of the two electric rollers (304); and sliding frames (305) are fixed at the two short sides of the top of the movable frame (301); the sliding frames (305) are movably connected to the outside of the sliding bar (202).

6. The synthetic combat emergency command vehicle according to claim 4, characterized in that: The top of the wireless charger (401) is flush with the top of the support plate (4), a push switch (402) is fixed at the center of the bottom of the wireless charger (401), the bottom of the push switch (402) is flush with the top of the bottom plate (404), and the storage battery (205) is electrically connected to the wireless charger (401).

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