CN111420330A - Electronic unmanned aerial vehicle fire control command car - Google Patents
Electronic unmanned aerial vehicle fire control command car Download PDFInfo
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- CN111420330A CN111420330A CN202010282366.8A CN202010282366A CN111420330A CN 111420330 A CN111420330 A CN 111420330A CN 202010282366 A CN202010282366 A CN 202010282366A CN 111420330 A CN111420330 A CN 111420330A
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- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62C—FIRE-FIGHTING
- A62C27/00—Fire-fighting land vehicles
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60P—VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS
- B60P3/00—Vehicles adapted to transport, to carry or to comprise special loads or objects
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60P—VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS
- B60P3/00—Vehicles adapted to transport, to carry or to comprise special loads or objects
- B60P3/06—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles
- B60P3/11—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles for carrying aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/007—Helicopter portable landing pads
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- Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
Abstract
The invention discloses an electric unmanned aerial vehicle fire-fighting command vehicle, which comprises a fire-fighting vehicle body, wherein an unmanned aerial vehicle take-off platform mechanism is also arranged on the fire-fighting vehicle body, a hand-held water cannon is arranged, so that under the condition that a fire-firing floor is lower and a road is not blocked and is convenient to be close to the floor, the fire-firing floor is extinguished by using the hand-held water cannon, the fire-fighting unmanned aerial vehicle is not needed, the selectivity of a fire-fighting mode is increased, when the fire-fighting unmanned aerial vehicle needs to take off, a driving motor rotates to drive a gear which is arranged on the output end of the driving motor and is meshed and connected with a rack welded on a cabin cover to rotate, when the driving motor rotates forwards, the gear pushes the rack out towards the side surface of the fire-fighting vehicle body, when the driving motor rotates backwards, the gear pulls the rack back towards the inner side of, when the cabin cover is closed, the telescopic end of the pneumatic cylinder pulls back the push rod to pull back the take-off platform.
Description
Technical Field
The invention relates to the technical field of fire fighting equipment, in particular to an electric unmanned aerial vehicle fire-fighting command vehicle.
Background
The fire truck is one of the most main rescue devices for accident rescue at present, is especially widely applied to rescue sites such as fire disasters, high altitudes and the like, can be applied to other emergency rescue purposes by most fire departments in China, and can be used for transporting fire technical personnel to the rescue sites as transportation work and carrying various equipment tools required by rescue tasks. Modern fire trucks are usually equipped with steel ladders, water guns, portable fire extinguishers, self-contained respirators, protective clothing, breaking and dismantling tools, first-aid tools and the like, and some fire extinguishing devices can also carry large fire extinguishing equipment such as water tanks, water pumps, foam fire extinguishing devices and the like. The appearance of the fire fighting truck in most areas is red, and the appearance of part of special fire fighting trucks is also the same, and the top of the fire fighting truck is usually provided with a warning bell, a warning lamp and an explosion lamp. Common fire fighting vehicle types include water tank fire fighting vehicles, foam fire fighting vehicles, aerial ladder fire fighting vehicles, and the like.
The multifunctional fire fighting truck disclosed in CN201810786352.2 comprises three major parts, namely a fire fighting truck head, a fire fighting truck body and fire fighting wheels, wherein the fire fighting truck head is a double-row cab, an electric winch is arranged in the middle of the front end of the fire fighting truck head and used for providing traction force for slope rescue, and a fire fighting alarm lamp is mounted at the top of the fire fighting truck head; the fire fighting vehicle comprises six fire fighting wheels, a fire fighting vehicle head is borne by vehicle head wheels, a fire fighting vehicle body is borne by vehicle body front wheels and vehicle body rear wheels, and the fire fighting vehicle has good flexible maneuvering performance, but cannot reach the site in time in urban districts under the condition that roads are narrow or blocked by disorderly parked vehicles, and meanwhile, the existing residential floors are high, so that the fire fighting vehicle cannot effectively carry out fire fighting work on high floors.
Although current fire control unmanned aerial vehicle can put out a fire to the high-rise, nevertheless need widen smooth place when taking off, take off the condition and receive the restriction, also inconvenient transportation to the scene simultaneously.
Aiming at the problems, the invention provides an electric unmanned aerial vehicle fire-fighting command vehicle.
Disclosure of Invention
The invention aims to provide an electric unmanned aerial vehicle fire-fighting command vehicle which comprises a fire-fighting vehicle body, wherein an unmanned aerial vehicle take-off platform mechanism is further mounted on the fire-fighting vehicle body, and an unmanned aerial vehicle take-off platform is arranged, so that the fire-fighting unmanned aerial vehicle can take off conveniently, the fire-fighting unmanned aerial vehicle can extinguish fire conveniently at high floors, and meanwhile, even if a road is blocked, the fire-fighting unmanned aerial vehicle can be controlled to arrive at the scene to extinguish the fire, so that the problems in.
In order to achieve the purpose, the invention provides the following technical scheme: an electric unmanned aerial vehicle fire control command vehicle comprises a fire control vehicle body, wherein an unmanned aerial vehicle take-off platform mechanism is further mounted on the fire control vehicle body, the vehicle body of the fire control vehicle body is provided with a water storage tank, a pump chamber, an equipment chamber and a handheld water cannon, the water storage tank is elastically connected with a chassis frame of the vehicle body and is arranged in the middle of the vehicle body, the pump chamber is arranged at the front end of the vehicle body, the equipment chamber is arranged at the rear end of the vehicle body, and the handheld water cannon is movably mounted on the upper portion;
the unmanned aerial vehicle take-off platform mechanism is provided with an opening and closing cabin cover assembly and a take-off platform assembly, the opening and closing cabin cover assembly is arranged in two groups, the opening and closing cabin cover assembly is movably mounted on the take-off platform assembly, the take-off platform assembly is fixedly welded on the upper end face of a water storage tank and comprises a fixed welding groove seat, guide rail groove strips, a take-off platform and a push-pull device, the fixed welding groove seats are fixedly welded on the upper end face of the water storage tank, the guide rail groove strips are arranged in two groups, the guide rail groove strips are fixedly welded in grooves of the fixed welding groove seats, the take-off platform is movably mounted on the guide rail groove strips, and the push-pull device is fixedly mounted in grooves of the fixed welding groove seats and fixedly.
Preferably, hide the water pitcher and hold a jar structure for the cuboid van-type, and be the component that high-quality carbon steel material made to be provided with division board, business turn over water pipe, overflow pipe and spring shock attenuation post, division board fixed welding is in the inside of hiding the water pitcher, business turn over water pipe fixed welding is in the side of hiding the water pitcher to with hide water pitcher through connection, the overflow pipe is L type structure, fixed the setting is in the side of hiding the water pitcher, one end setting is in the inside of hiding the water pitcher, one end setting is in the outside of hiding the water pitcher, the spring shock attenuation post sets up four groups, four groups spring shock attenuation post fixed mounting hide the lower terminal surface of water.
Preferably, the dividing plate is of a cross-shaped structure and is provided with communication holes, the dividing plate of the cross-shaped structure divides the water storage tank into nine water storage chambers, and the nine water storage chambers are communicated through the communication holes.
Preferably, the pump chamber and the handheld water cannon are both connected with the water storage tank through seamless steel pipes.
Preferably, the cabin cover assembly comprises a cabin cover and an opening and closing driving device, the cabin cover is movably arranged on two sides of the upper end of the fixed welding groove seat, and the opening and closing driving device is fixedly arranged on two sides of the upper end of the fixed welding groove seat and connected with the cabin cover.
Preferably, the cabin cover is of a half-box cover type structure and is provided with a connecting and reinforcing bottom frame, a movable connecting clamping groove and a rack, the connecting and reinforcing bottom frame is fixedly arranged on two sides of the lower end of the cabin cover, the movable connecting clamping groove is formed in the lower end face of the connecting and reinforcing bottom frame, and the rack is fixedly welded on the upper end face of the connecting and reinforcing bottom frame.
Preferably, the opening and closing driving device comprises a driving motor, a support frame and a gear, the support frame is fixedly welded on the driving motor, the driving motor is fixedly installed at one end of two sides of the fixed welding groove seat through the support frame, and the gear is fixedly installed at the output end of the driving motor and is meshed with the rack.
Preferably, the fixed welding slot seat is provided with a cabin cover connecting platform, a mounting threaded hole and a clamping block, the cabin cover connecting platform is fixedly arranged on two sides of the fixed welding slot seat, the mounting threaded hole is formed in one end of the cabin cover connecting platform, and the clamping block is fixedly welded at two ends of the cabin cover connecting platform and matched with the movable connecting clamping groove.
Preferably, the platform of taking off is provided with unmanned aerial vehicle and places the board, the connecting plate, the rectangle notch, baffle and joint strip, unmanned aerial vehicle places the fixed welding connecting plate of one end of board, the rectangle notch is seted up on unmanned aerial vehicle places board and connecting plate, the fixed welding of baffle is at the other end that unmanned aerial vehicle placed the board, and length and width respectively with the groove width and the degree of depth phase-match of fixed welding groove seat, joint strip fixed welding is at the lower terminal surface of connecting plate, and match with the groove of guide rail groove strip piece.
Preferably, the push-pull device is provided with a pneumatic cylinder, a push rod, a supporting hole block and a welding head, the pneumatic cylinder is fixedly installed in a groove of the fixed welding groove seat, the push rod is fixedly connected with the telescopic end of the pneumatic cylinder, the supporting hole block is fixedly installed in the groove of the fixed welding groove seat and sleeved on the push rod, and the welding head is fixedly installed at one end of the push rod and fixedly welded on one side of the connecting plate.
Compared with the prior art, the invention has the following beneficial effects:
1. according to the electric unmanned aerial vehicle fire-fighting command vehicle, the pump chamber and the handheld water cannons are connected with the water-storing tank through the seamless steel pipes, and the handheld water cannons are arranged, so that fire is extinguished on the fire-firing floor by using the handheld water cannons under the condition that the fire-firing floor is low and a road is not blocked, so that the floor is convenient to approach, a fire-fighting unmanned aerial vehicle is not needed, and the selectivity of a fire-fighting mode is increased.
2. According to the electric unmanned aerial vehicle fire-fighting command vehicle, the water storage tank is mounted on the chassis frame of the vehicle body through the four groups of spring shock-absorbing columns, so that even if the vehicle shakes in the running process, the vibration received by the water storage tank can be buffered and absorbed through the spring shock-absorbing columns, and the shaking degree of water in the water storage tank is reduced.
3. According to the electric unmanned aerial vehicle fire-fighting command vehicle, the dividing plate is of the cross-shaped structure and is provided with the communication holes, the dividing plate of the cross-shaped structure divides the water storage tank into nine water storage chambers, the nine water storage chambers are communicated through the communication holes, according to the principle that the larger the volume of water is, the larger the shaking degree of water is, the dividing plate of the cross-shaped structure divides the water storage tank into nine water storage chambers, the large-volume water storage tank is divided into nine small-volume water storage chambers, and the shaking degree of water is effectively reduced.
4. According to the electric unmanned aerial vehicle fire-fighting command vehicle, the cabin cover is clamped with the clamping blocks welded at two ends of the cabin cover connecting table through the movably-connected clamping grooves formed in the lower end face of the connecting reinforcing bottom frame, and is meshed and connected with the racks through the gears and the racks, and the racks are pressed, so that the cabin cover can be movably mounted on the fixed welding groove seats.
5. According to the electric unmanned aerial vehicle fire-fighting command vehicle, when the cabin cover is opened, the telescopic end of the pneumatic cylinder pushes the push rod to push out the take-off platform, so that a wide and flat platform is provided for the fire-fighting unmanned aerial vehicle, the take-off platform is high above the ground, the take-off height is provided, the safety is higher, personnel cannot be injured, and when the cabin cover is closed, the telescopic end of the pneumatic cylinder pulls back the push rod to pull back the take-off platform.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a schematic view of the top cut-away internal structure of the water storing tank of the present invention;
FIG. 3 is a schematic view of the nacelle cover configuration of the present invention;
FIG. 4 is an enlarged view taken at A in FIG. 3 according to the present invention;
FIG. 5 is a schematic structural diagram of an opening/closing driving device according to the present invention;
FIG. 6 is a schematic structural view of a takeoff platform assembly of the present invention;
FIG. 7 is a structural schematic view of a takeoff platform of the present invention;
figure 8 is a schematic view of the push-pull device of the present invention.
In the figure: 1. a fire fighting truck body; 11. a water storing tank; 111. a partition plate; 1111. a communicating hole; 112. a water inlet pipe and a water outlet pipe; 113. an overflow pipe; 114. a spring shock post; 12. a pump chamber; 13. an equipment room; 14. a water cannon is held by hand; 2. an unmanned aerial vehicle takeoff platform mechanism; 21. an opening and closing cabin cover assembly; 211. a nacelle cover; 2111. connecting the reinforcing bottom frame; 2112. the clamping groove is movably connected; 2113. a rack; 212. an opening and closing drive device; 2121. a drive motor; 2122. a support frame; 2123. a gear; 22. a takeoff platform assembly; 221. fixedly welding the groove seat; 2211. a cabin cover connection table; 2212. installing a threaded hole; 2213. a clamping block; 222. a guide rail channel bar block; 223. a takeoff platform; 2231. placing a board for the unmanned aerial vehicle; 2232. a connecting plate; 2233. a rectangular notch; 2234. a baffle plate; 2235. connecting the clamping strips; 224. a push-pull device; 2241. a pneumatic cylinder; 2242. a push rod; 2243. a support hole block; 2244. and (5) welding a head.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
The first embodiment is as follows:
referring to fig. 1-2, an electric unmanned aerial vehicle fire control command vehicle, including a fire-fighting vehicle body 1, the vehicle body of the fire-fighting vehicle body 1 is provided with a water storage tank 11, a pump chamber 12, an equipment chamber 13 and a hand-held water cannon 14, the water storage tank 11 is elastically connected with a vehicle chassis frame and is disposed in the middle of the vehicle body, the pump chamber 12 is disposed at the front end of the vehicle body, the equipment chamber 13 is disposed at the rear end of the vehicle body, the hand-held water cannon 14 is movably mounted at the upper portion of the front end of the vehicle body, the pump chamber 12 and the hand-held water cannon 14 are both connected with the water storage tank 11 through seamless steel pipes, the hand-held water cannon 14 is disposed at a firing floor, a road is not blocked and is conveniently close to a floor, the fire is extinguished by using the hand-held water cannon 14, a fire-fighting unmanned aerial vehicle is not required, selectivity of a fire-extinguishing mode is increased, the water storage tank 11 is a cuboid box-type water storage tank structure and is a member made of high-quality carbon steel, and is disposed at a partition plate 111, the partition plate is disposed with overflow pipes 113 and welded to a shock-absorbing water storage tank 11, the shock-absorbing cylinder 114, the shock-absorbing cylinder is disposed at the side of a shock-absorbing cylinder 11, the shock-absorbing cylinder structure, the shock-absorbing cylinder 11 is disposed at the shock-absorbing cylinder 11, the shock-absorbing cylinder 11, the shock-absorbing cylinder is disposed at the shock-absorbing cylinder 11, the shock-absorbing cylinder 11, the shock-absorbing cylinder is disposed at the shock-absorbing cylinder, the shock-absorbing cylinder 11, the shock.
Example two:
referring to fig. 3-6, an electric unmanned aerial vehicle fire-fighting command vehicle, an unmanned aerial vehicle take-off platform mechanism 2 is further installed on a fire-fighting vehicle body 1, the unmanned aerial vehicle take-off platform mechanism 2 is provided with an opening and closing cabin cover assembly 21 and a take-off platform assembly 22, the opening and closing cabin cover assemblies 21 are arranged in two groups, the two groups of opening and closing cabin cover assemblies 21 are movably installed on the take-off platform assembly 22, the opening and closing cabin cover assembly 21 comprises a cabin cover 211 and an opening and closing driving device 212, the cabin cover 211 is movably installed on two sides of the upper end of a fixed welding groove seat 221, the opening and closing driving device 212 is fixedly installed on two sides of the upper end of the fixed welding groove seat 221 and connected with the cabin cover 211, the cabin cover 211 is of a half-box cover type structure and is provided with a connecting reinforcing bottom frame 2111, a movable connecting clamping groove 2112 and a rack 2113, the connecting reinforcing bottom frame 2111 is fixedly arranged on two sides of the lower, the rack 2113 is fixedly welded on the upper end face of the connection reinforcing bottom frame 2111, the cabin cover 211 is clamped with the clamping blocks 2213 welded on both ends of the cabin cover connection table 2211 through the movably-connected clamping groove 2112 arranged on the lower end face of the connection reinforcing bottom frame 2111, and is engaged with the rack 2113 through the gear 2123 and presses the rack 2113, so that the cabin cover 211 can be movably mounted on the fixed welding groove seat 221, the opening and closing driving device 212 comprises a driving motor 2121, a supporting frame 2122 and a gear 2123, the supporting frame 2122 is fixedly welded on the driving motor 2121, the driving motor 2121 is fixedly mounted on one end of both sides of the fixed welding groove seat 221 through the supporting frame 2122, the gear 2123 is fixedly mounted on the output end of the driving motor 2121 and is engaged with the rack 2113, when the fire-fighting unmanned aerial vehicle needs to take off, the driving motor 2121 rotates to drive the gear 2123 mounted on the output end of the driving motor 2121 and engaged with the rack 2113 welded, when the driving motor 2121 rotates forward, the gear 2123 pushes the rack 2113 out to the side of the fire-fighting vehicle body 1, the cabin cover 211 is opened, and when the driving motor 2121 rotates backward, the gear 2123 pulls the rack 2113 back to the inside of the fire-fighting vehicle body 1, and the cabin cover 211 is closed.
Example three:
referring to fig. 6-8, a fire control command vehicle for an electric unmanned aerial vehicle, a takeoff platform assembly 22 is fixedly welded on the upper end surface of a water storage tank 11, and includes a fixed welding slot seat 221, a guide rail slot block 222, a takeoff platform 223 and a push-pull device 224, the fixed welding slot seat 221 is fixedly welded on the upper end surface of the water storage tank 11, two sets of guide rail slot blocks 222 are provided, the two sets of guide rail slot blocks 222 are fixedly welded in the groove of the fixed welding slot seat 221, the takeoff platform 223 is movably mounted on the guide rail slot block 222, the push-pull device 224 is fixedly mounted in the groove of the fixed welding slot seat 221 and fixedly connected with the takeoff platform 223, the fixed welding slot seat 221 is provided with a cabin cover connecting platform 2211, a mounting threaded hole 2212 and a clamping block 2213, the cabin cover connecting platform 2211 is fixedly arranged on two sides of the fixed welding slot seat 221, the mounting threaded hole 2212 is arranged at one end of the cabin cover connecting platform 2211, a support bracket 2122 is conveniently and fixedly, the clamping blocks 2213 are fixedly welded at two ends of the cabin cover connecting platform 2211 and matched with the movable connecting clamping grooves 2112, the clamping blocks 2213 are connected with the movable connecting clamping grooves 2112 in a clamping mode, so that the effect of limiting the cabin cover 211 is achieved, the cabin cover 211 is more stable when being opened and closed, the take-off platform 223 is provided with an unmanned aerial vehicle placing plate 2231, a connecting plate 2232, a rectangular notch 2233, a baffle 2234 and a connecting clamping strip 2235, one end of the unmanned aerial vehicle placing plate 2231 is fixedly welded with the connecting plate 2232, the rectangular notch 2233 is arranged on the unmanned aerial vehicle placing plate 2231 and the connecting plate 2232, the weight of the baffle 2234 and the connecting plate 2232 is reduced, meanwhile, draining is facilitated, the baffle 2234 is fixedly welded at the other end of the unmanned aerial vehicle placing plate 2231, the length and the width are respectively matched with the groove width and the depth of the fixed welding groove seat 221, so that when the cabin cover 211 is closed and the take, the notch of the fixed welding slot seat 221 can be blocked by the baffle 2234, the connecting clamping strip 2235 is fixedly welded on the lower end face of the connecting plate 2232 and matched with the slot of the guide rail slot block 222, the connecting clamping strip 2235 is connected with the guide rail slot block 222 in a clamping manner, so that the support of the take-off platform 223 is firmer, the push-pull device 224 is provided with a pneumatic cylinder 2241, a push rod 2242, a support hole block 2243 and a welding head 2244, the pneumatic cylinder 2241 is fixedly installed in the slot of the fixed welding slot seat 221, the push rod 2242 is fixedly connected with the telescopic end of the pneumatic cylinder 2241, the support hole block 2243 is fixedly installed in the slot of the fixed welding slot seat 221 and is sleeved on the push rod 2242, the welding head 2244 is fixedly installed at one end of the push rod 2242 and is fixedly welded on one side of the connecting plate 2232, when the cabin cover 211 is opened, the telescopic end of the pneumatic cylinder 2241 pushes the push rod 224, and take-off platform 223 is high off the ground, provides the height of taking off, and safer, can not injure personnel, and when cabin cover 211 closed, the flexible end of pneumatic cylinder 2241 draws back push rod 2242, draws back take-off platform 223.
In summary, the following steps: the invention provides an electric unmanned aerial vehicle fire-fighting command vehicle, which comprises a fire-fighting vehicle body 1, wherein an unmanned aerial vehicle takeoff platform mechanism 2 is also installed on the fire-fighting vehicle body 1, a pump chamber 12 and a handheld water cannon 14 are both connected with a water storage tank 11 through seamless steel pipes, and the handheld water cannon 14 is arranged, so that under the condition that the fire-firing floor is lower and a road is not blocked and is convenient to approach the floor, the fire-firing floor is extinguished through the handheld water cannon 14, a fire-fighting unmanned aerial vehicle is not needed, and the selectivity of a fire-fighting mode is increased; the water storage tank 11 is arranged on a chassis frame of a vehicle body through four groups of spring shock absorption columns 114, so that even if the vehicle shakes in the running process, the vibration received by the water storage tank 11 can be buffered and absorbed through the spring shock absorption columns 114, and the shaking degree of the water in the water storage tank is reduced; the dividing plate 111 is of a cross-shaped structure and is provided with the communicating hole 1111, the dividing plate 111 of the cross-shaped structure divides the water storage tank 11 into nine water storage chambers, the nine water storage chambers are communicated through the communicating hole 1111, according to the principle that the shaking degree of water is larger when the volume is larger, the dividing plate 111 of the cross-shaped structure divides the water storage tank 11 into nine water storage chambers, the water storage tank 11 with large volume is divided into nine water storage chambers with small volume, and the shaking degree of water is effectively reduced; the cabin cover 211 is clamped with clamping blocks 2213 welded at two ends of a cabin cover connecting platform 2211 through a movably-connected clamping groove 2112 formed in the lower end face of a connecting reinforcing bottom frame 2111, is meshed with a rack 2113 through a gear 2123 and presses the rack 2113, so that the cabin cover 211 can be movably mounted on a fixed welding groove seat 221; when cabin cover 211 is opened, pneumatic cylinder 2241's flexible end promotes push rod 2242, will take off platform 223 and release, provides wide and level platform for fire control unmanned aerial vehicle, and takes off platform 223 height from the ground, provides the height of taking off, and safer, can not injure personnel, when cabin cover 211 closes, pneumatic cylinder 2241's flexible end pull back push rod 2242, will take off platform 223 and pull back.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (10)
1. The utility model provides an electronic unmanned aerial vehicle fire control command car, includes fire control automobile body (1), has still installed unmanned aerial vehicle take-off platform mechanism (2) on fire control automobile body (1), its characterized in that: the fire fighting truck comprises a fire fighting truck body (1), wherein a water storage tank (11), a pump chamber (12), an equipment chamber (13) and a handheld water cannon (14) are arranged on the truck body, the water storage tank (11) is elastically connected with a chassis frame of the truck body and is arranged in the middle of the truck body, the pump chamber (12) is arranged at the front end of the truck body, the equipment chamber (13) is arranged at the rear end of the truck body, and the handheld water cannon (14) is movably arranged on the upper part of the front end of the truck;
the unmanned aerial vehicle take-off platform mechanism (2) is provided with an opening and closing cabin cover assembly (21) and a take-off platform assembly (22), the opening and closing cabin cover assembly (21) is provided with two groups, the two groups of opening and closing cabin cover assemblies (21) are movably arranged on the take-off platform assembly (22), the take-off platform assembly (22) is fixedly welded on the upper end face of the water storage tank (11) and comprises a fixed welding groove seat (221), a guide rail groove strip block (222), a take-off platform (223) and a push-pull device (224), the fixed welding groove seat (221) is fixedly welded on the upper end face of the water storage tank (11), the guide rail groove strip block (222) is provided with two groups, the two groups of guide rail groove strip blocks (222) are fixedly welded in a groove of the fixed welding groove seat (221), the take-off platform (223) is movably arranged on the guide rail groove strip block (222), the push-pull device (224) is fixedly arranged, and is fixedly connected with a take-off platform (223).
2. The electric unmanned aerial vehicle fire-fighting command vehicle is characterized in that the water storage tank (11) is of a rectangular box type tank containing structure and is made of high-quality carbon steel, a partition plate (111), a water inlet and outlet pipe (112), an overflow pipe (113) and spring shock-absorbing columns (114) are arranged, the partition plate (111) is fixedly welded in the water storage tank (11), the water inlet and outlet pipe (112) is fixedly welded on the side face of the water storage tank (11) and is in through connection with the water storage tank (11), the overflow pipe (113) is of an L type structure and is fixedly arranged on the side face of the water storage tank (11), one end of the overflow pipe is arranged in the water storage tank (11), one end of the overflow pipe is arranged on the outer portion of the water storage tank (11), four groups of the spring shock-absorbing columns (114) are arranged on the lower end face of the water storage tank (11) and are fixedly welded on a vehicle body chassis frame.
3. The electric unmanned aerial vehicle fire control command car of claim 1, wherein: the partition plate (111) is of a cross-shaped structure and is provided with a communicating hole (1111), the water storage tank (11) is divided into nine water storage chambers by the partition plate (111) of the cross-shaped structure, and the nine water storage chambers are communicated through the communicating hole (1111).
4. The electric unmanned aerial vehicle fire control command car of claim 1, wherein: the pump chamber (12) and the hand-held water cannon (14) are both connected with the water-hiding tank (11) through seamless steel pipes.
5. The electric unmanned aerial vehicle fire control command car of claim 1, wherein: the opening and closing cabin cover assembly (21) comprises a cabin cover (211) and an opening and closing driving device (212), wherein the cabin cover (211) is movably arranged on two sides of the upper end of a fixed welding groove seat (221), and the opening and closing driving device (212) is fixedly arranged on two sides of the upper end of the fixed welding groove seat (221) and is connected with the cabin cover (211).
6. The electric unmanned aerial vehicle fire control command car of claim 5, wherein: the cabin cover (211) is of a half-box cover type structure and is provided with a connection reinforcing bottom frame (2111), a movable connection clamping groove (2112) and a rack (2113), the connection reinforcing bottom frame (2111) is fixedly arranged on two sides of the lower end of the cabin cover (211), the movable connection clamping groove (2112) is formed in the lower end face of the connection reinforcing bottom frame (2111), and the rack (2113) is fixedly welded on the upper end face of the connection reinforcing bottom frame (2111).
7. The electric unmanned aerial vehicle fire control command car of claim 5, wherein: the opening and closing driving device (212) comprises a driving motor (2121), a supporting frame (2122) and a gear (2123), the supporting frame (2122) is fixedly welded on the driving motor (2121), the driving motor (2121) is fixedly installed at one end of two sides of the fixed welding groove seat (221) through the supporting frame (2122), and the gear (2123) is fixedly installed at the output end of the driving motor (2121) and is meshed with the rack (2113).
8. The electric unmanned aerial vehicle fire control command car of claim 1, wherein: the fixed welding groove seat (221) is provided with an engine room cover connecting platform (2211), mounting threaded holes (2212) and clamping blocks (2213), the engine room cover connecting platform (2211) is fixedly arranged on two sides of the fixed welding groove seat (221), the mounting threaded holes (2212) are formed in one end of the engine room cover connecting platform (2211), and the clamping blocks (2213) are fixedly welded at two ends of the engine room cover connecting platform (2211) and matched with the movable connecting clamping grooves (2112).
9. The electric unmanned aerial vehicle fire control command car of claim 1, wherein: take-off platform (223) is provided with unmanned aerial vehicle and places board (2231), connecting plate (2232), rectangle notch (2233), baffle (2234) and hitch clevis strip (2235), unmanned aerial vehicle places fixed welding connecting plate (2232) of one end of board (2231), set up on unmanned aerial vehicle places board (2231) and connecting plate (2232) rectangle notch (2233), baffle (2234) fixed welding is at the other end that unmanned aerial vehicle placed board (2231), and length and width respectively with the groove width and the degree of depth phase-match of fixed welding groove seat (221), hitch clevis strip (2235) fixed welding is at the lower terminal surface of connecting plate (2232), and match with the groove of guide rail groove strip piece (222).
10. The electric unmanned aerial vehicle fire control command car of claim 1, wherein: push-and-pull device (224) are provided with pneumatic cylinder (2241), push rod (2242), support hole piece (2243) and soldered connection (2244), pneumatic cylinder (2241) fixed mounting is at the inslot of fixed welding groove seat (221), the flexible fixed connection of push rod (2242) and pneumatic cylinder (2241), support hole piece (2243) fixed mounting is at the inslot of fixed welding groove seat (221), and the suit is on push rod (2242), soldered connection (2244) fixed mounting is in the one end of push rod (2242), and fixed welding is in one side of connecting plate (2232).
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| CN202010282366.8A CN111420330A (en) | 2020-04-12 | 2020-04-12 | Electronic unmanned aerial vehicle fire control command car |
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| CN202010282366.8A CN111420330A (en) | 2020-04-12 | 2020-04-12 | Electronic unmanned aerial vehicle fire control command car |
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Application publication date: 20200717 |