CN111803838A - Fire-fighting rescue container - Google Patents

Fire-fighting rescue container Download PDF

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Publication number
CN111803838A
CN111803838A CN202010706700.8A CN202010706700A CN111803838A CN 111803838 A CN111803838 A CN 111803838A CN 202010706700 A CN202010706700 A CN 202010706700A CN 111803838 A CN111803838 A CN 111803838A
Authority
CN
China
Prior art keywords
crank arm
fire
fighting
container
box body
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN202010706700.8A
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Chinese (zh)
Inventor
吴正洪
张代兵
向绍华
杨志生
吴刚
伍泽全
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Changsha Yunzhihang Technology Co ltd
Original Assignee
Changsha Yunzhihang Technology Co ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Changsha Yunzhihang Technology Co ltd filed Critical Changsha Yunzhihang Technology Co ltd
Priority to CN202010706700.8A priority Critical patent/CN111803838A/en
Publication of CN111803838A publication Critical patent/CN111803838A/en
Pending legal-status Critical Current

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    • AHUMAN NECESSITIES
    • A62LIFE-SAVING; FIRE-FIGHTING
    • A62CFIRE-FIGHTING
    • A62C27/00Fire-fighting land vehicles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60PVEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS
    • B60P3/00Vehicles adapted to transport, to carry or to comprise special loads or objects
    • B60P3/06Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles
    • B60P3/11Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles for carrying aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND 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
    • B64F1/00Ground or aircraft-carrier-deck installations
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND 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
    • B64F1/00Ground or aircraft-carrier-deck installations
    • B64F1/22Ground or aircraft-carrier-deck installations installed for handling aircraft
    • B64F1/222Ground or aircraft-carrier-deck installations installed for handling aircraft for storing aircraft, e.g. in hangars
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U80/00Transport or storage specially adapted for UAVs
    • B64U80/70Transport or storage specially adapted for UAVs in containers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U80/00Transport or storage specially adapted for UAVs
    • B64U80/80Transport or storage specially adapted for UAVs by vehicles
    • B64U80/86Land vehicles

Abstract

The invention discloses a fire-fighting rescue container, which belongs to the technical field of high-altitude fire fighting and is used for solving the technical problem of single application scene of the existing fire-fighting rescue equipment. The invention has the advantages of simple structure, good maneuverability, convenient carrying and transportation, flexible and quick fire rescue and the like.

Description

Fire-fighting rescue container
Technical Field
The invention mainly relates to the technical field of fire fighting, in particular to a fire-fighting rescue container.
Background
Along with the development of the world economy, the number of urban high-rise and super high-rise buildings is increasing, and once a fire disaster happens to a high-rise building with dozens of meters or even hundreds of meters, the fire-fighting problem can be met. At present traditional fire-fighting equipment such as high-pressure squirt, fire control aerial ladder, high altitude unmanned aerial vehicle all have as follows not enoughly:
(1) the traditional high-pressure water gun is difficult to reach more than 80 meters for fire extinguishing and fire rescue due to the water pressure, the structural weight of the aerial ladder and other reasons, and the existing aerial ladder fire truck is limited by the smooth degree of the area and the street, the fire fighting truck cannot arrive at a fire scene in the first time under many conditions; moreover, fire fighting is mainly carried out by firemen who are directly close to the fire scene, so that high danger is generated and unnecessary casualties are even caused sometimes;
(2) in the face of high-rise fire fighting, a plurality of fire trucks are sometimes required to perform combined operation, the preparation time is long, aerial ladders are adopted to perform high-rise rescue, and the aerial ladders are unfolded to have a slow process, so that the rescue response is slow;
(3) for the high-altitude unmanned aerial vehicle, in view of the performance parameters of the current battery, the unmanned aerial vehicle carries the load and the self weight required by fire extinguishment, the operation time length is limited, the load of fire extinguishment is less, the air operation time is short, and the air and the ground need to be reciprocated for many times; if the carried load is more, the air operation time is short, so the fire rescue unmanned aerial vehicle powered by the battery cannot carry out high-rise fire rescue operation for a long time under a large load, and the precious time of fire rescue is delayed;
(4) in the face of complex fire rescue situations, the traditional fire fighting mode is difficult to meet the diversified and configurable fire fighting requirements of window breaking, large-flow water spraying, dry powder spraying, foam spraying and the like;
(5) due to the limitation of the operation height, the traditional fire fighting means is difficult to provide emergency rescue equipment (such as gas masks, fire blankets, strong light flashlights, interphones and the like) for people trapped at high floors and in urgent need of rescue;
(6) the single-machine operation of the existing fire-fighting unmanned aerial vehicle can complete the fire-fighting operations such as dry powder spraying fire extinguishing, water spraying and the like, and the function of a fire-fighting rescue system is not fully established.
At present, the technology of adopting the mooring unmanned aerial vehicle to carry out fire fighting is adopted, but because the fire fighting equipment is fixed on a fire fighting vehicle, the appropriate fire fighting equipment can not be selected according to the actual situation on site, so that the application scene is single, and the arrangement of the fire fighting equipment is messy, and the maintenance and management of the fire fighting equipment are inconvenient.
Disclosure of Invention
The technical problem to be solved by the invention is as follows: aiming at the technical problems in the prior art, the invention provides a fire-fighting rescue container which is good in mobility, flexible in configuration and wide in application scene.
In order to solve the technical problems, the technical scheme provided by the invention is as follows:
the utility model provides a fire control rescue container of putting out a fire, includes box, aerial operation subsystem and ground guarantee subsystem, the box is upper cavity and lower floor's cavity respectively including two cavitys of arranging from top to bottom, aerial operation subsystem arrange in the upper cavity, ground guarantee subsystem arrange in the cavity of lower floor.
As a further improvement of the above technical solution:
the box body forms an open-close type structure on two sides of the upper layer cavity; the opening-closing structure comprises wing doors positioned on two sides of the partition board, one side of each wing door is hinged with the box body, and an opening-closing driving piece used for driving the corresponding wing door to open and close is arranged on each wing door; when the opening and closing driving piece drives the wing doors to be unfolded, the wing doors on the two sides are used for expanding a take-off and landing platform of the mooring unmanned aerial vehicle; when the driving piece drives the wing doors to fold, the wing doors on two sides fold each other to protect the mooring unmanned aerial vehicle.
Vertical telescopic components are folded at two sides of the box body and used for lifting the box body so as to facilitate the transfer of a trailer; the vertical telescopic assembly comprises a cross rod and a telescopic vertical rod, one end of the cross rod is transmounted on the box body, and the telescopic vertical rod is fixed at the other end of the cross rod; and the top of the telescopic vertical rod is provided with a mandril for supporting the unfolded wing door.
Jacks are formed in two sides of the bottom of the box body and used for allowing fork rods of a forklift to be inserted into the jacks for carrying; and the box body is provided with a hoisting assembly for hoisting operation.
And a position conversion assembly is arranged in the box body and is used for converting the position of the tethered unmanned aerial vehicle of the aerial work subsystem.
The position conversion assembly comprises a crank arm assembly, a first rotating mechanism, a second rotating mechanism and a lifting platform for mooring the unmanned aerial vehicle to take off and land, one end of the crank arm assembly is rotatably installed in the box body through the first rotating mechanism, and the other end of the crank arm assembly is rotatably connected with the lifting platform through the second rotating mechanism; the first rotating mechanism drives the crank arm assembly to rotate between an extending state and a retracting state, and the second rotating mechanism drives the lifting platform to rotate, so that the lifting platform is in a horizontal state when the crank arm assembly rotates.
The crank arm assembly comprises a first crank arm and a second crank arm, one end of the first crank arm is connected with the first rotating mechanism, the other end of the first crank arm is rotatably connected with one end of the second crank arm, and the other end of the second crank arm is connected with the second rotating mechanism; and a telescopic piece is arranged between the first crank arm and the second crank arm.
The first rotating mechanism comprises a first swinging cylinder and a first connecting plate, the first swinging cylinder is fixed in the box body, and the output end of the first swinging cylinder is connected with one end of the crank arm assembly through the first connecting plate; the first swinging cylinder is provided with a first position detection piece for detecting the rotation angle of the first swinging cylinder; the second rotating mechanism comprises a second swinging cylinder and a second connecting plate, the second swinging cylinder is fixed at the other end of the crank arm assembly, and the output end of the second swinging cylinder is connected with the lifting platform through the second connecting plate; and a second position detection piece is arranged on the second swinging cylinder and used for detecting the rotation angle of the second swinging cylinder.
First rotation mechanism is including rotating seat, pivot, gear, rack, slide and telescoping cylinder, it is fixed in to rotate the seat on the box, the pivot fastening is in on the crank arm subassembly and rotate install in rotate on the seat, the gear install in one side or both sides of pivot, rack slidable mounting in on the slide and with gear engagement, the flexible end of telescoping cylinder with the one end of rack links to each other, is used for the drive the rack is in slide on the slide.
The ground support subsystem comprises a fire extinguishing agent supply unit, a power supply unit and a pipeline winding and unwinding unit; the power supply unit is connected with the mooring unmanned aerial vehicle through a mooring cable and used for providing a power supply for the mooring unmanned aerial vehicle; the fire extinguishing agent supply unit is connected with the fire extinguishing unit through a supply pipe and is used for supplying fire extinguishing agent to the fire extinguishing unit; the pipeline reeling and unreeling unit is used for reeling and unreeling the mooring cable or/and the supply pipe; the power supply unit, the pipeline collecting and releasing unit and the fire extinguishing agent supply unit are sequentially arranged along the length direction of the lower cavity.
Compared with the prior art, the invention has the advantages that:
(1) according to the fire-fighting rescue container, the aerial operation subsystem and the ground support subsystem are integrated in the box body to form a container type structure, and are physically separated from various special fire trucks, so that the container can be mounted on the special fire trucks, can be independently placed on the ground or a large-size bearing platform, and can also be placed on general transport vehicles such as flat cars, and the container is convenient to mount, fix, transport and the like.
(2) According to the container for fire-fighting, fire-fighting and rescue, the aerial operation subsystem and the ground support subsystem in the container body can adopt various flexible configurations and modularized settings according to different requirements, so that the container is more favorable for popularization and deep popularization of fire-fighting and rescue equipment, and solves the contradiction between the demand number and insufficient equipment of the fire-fighting and rescue equipment, thereby effectively improving the efficiency and success rate of fire hazard disposal, and expanding a more rapid and safe high-altitude fire-fighting, fire-fighting and rescue means for high-rise buildings, key areas and dangerous areas.
(3) The container type structure is adopted, so that the container type container is low in price and quick in execution speed compared with professional fire-fighting equipment, is convenient to configure at key positions of areas with high risk of fire hazards and key areas, realizes allocation of resident or dynamic positions, can finish quick transfer around a fire range at the first time in the initial stage of fire danger, and can realize cooperative operation among a plurality of containers in the area to carry out fire-fighting rescue; effectively solve the problem that the fire disaster is developed for self rescue in the golden time. Certainly, the aerial operation subsystem and the ground support subsystem in the box body can realize unattended fire situation, triggering in distress, man-machine combination and rapid fire extinguishing and rescue treatment through an automatic logic sequence, a sensor and a controller.
(4) Jacks are formed in two sides of the bottom of the box body and used for allowing fork rods of a forklift to be inserted for carrying; in addition, the box body is provided with a hoisting component (such as a lifting lug) which is convenient for hoisting operation; wherein be equipped with the railing that is used for the climbing on the tail-gate, the maintenance personal of being convenient for etc. climbs the platform that falls and maintains operations such as personnel carry out the maintenance to mooring.
(5) According to the invention, the first rotating mechanism is matched with the second rotating mechanism, so that linkage is formed between the lifting platform and the crank arm assembly, and further switching of the mooring unmanned aerial vehicle on the lifting platform between the box body and the ground position is realized, so that operations of boxing, ground maintenance, transferring and the like of the mooring unmanned aerial vehicle are facilitated, and meanwhile, the lifting platform can be ensured to be always in a horizontal state in the switching process, so that the safety and stability of the mooring unmanned aerial vehicle on the lifting platform are ensured; the whole structure is simple, the position conversion is flexible, safe and reliable.
(6) According to the invention, the crank arm assemblies are arranged into multiple sections, the telescopic pieces are additionally arranged in the middle of the crank arm assemblies, and the positions of the crank arms are changed through the telescopic pieces, so that the automatic switching of the tethered unmanned aerial vehicle between different positions is realized, such as the switching between a boxing position (a box body is positioned on a vehicle or on the ground) and the ground, between the boxing position and a trailer position (the trailer position is higher than the ground), or between the ground and the trailer position, and the like, thereby realizing the seamless butt joint between the operations of boxing, ground maintenance, trailer transfer and the like of the tethered unmanned aerial vehicle; the structure is simple, the operation is simple and convenient, and the realization is easy.
(7) According to the invention, the fire extinguishing agent supply unit, the power supply unit and the pipeline retraction unit are arranged in the carriage, so that the rapid movement of each unit and the mooring unmanned aerial vehicle can be realized, the timeliness of fire fighting and rescue is ensured, and the functions of each unit in the box body are complete; each part has reasonable function division, compact integral structure and convenient maintenance.
(8) The invention is provided with wing doors which are arranged on two sides of a lifting platform in a rotating way and are in a split shape, and when the wing doors are unfolded, the wing doors and the lifting platform form a lifting and maintaining platform together; when the wing door folds, it is whole with the container of box constitution to tie unmanned aerial vehicle, is convenient for transport, simple structure and easy and simple to handle.
Drawings
Fig. 1 is a front view structural view (flap door closed) of the present invention in an embodiment.
Fig. 2 is a side view structural diagram (flap door closed) of the present invention in an embodiment.
Fig. 3 is a perspective view of the present invention (flap door closed).
Fig. 4 is a front view structural view (flap door deployed) of the present invention in an embodiment.
Fig. 5 is a side view structural view (flap door deployed) of the present invention in an embodiment.
Fig. 6 is a perspective view showing the structure of the present invention (flap door open).
Fig. 7 is a top view structural view (flap door open) of the present invention in an embodiment.
Fig. 8 is a front view structural view (on a vehicle) of the present invention in an embodiment.
Fig. 9 is a side view structural view (on a vehicle) of the present invention in an embodiment.
Fig. 10 is a perspective view showing the structure of the present invention (on a vehicle).
Fig. 11 is a perspective view of the vertical retraction assembly of the present invention in a collapsed position.
Fig. 12 is a perspective view of the vertical retraction assembly of the present invention in an open position.
Fig. 13 is a perspective view showing the structure of the telescopic stem of the vertical telescopic assembly of the present invention in an extended state.
Fig. 14 is a perspective view illustrating a configuration of a lift pin supporting a wing door of the vertical telescopic assembly according to the present invention.
Fig. 15 is a perspective view of the position switching unit according to the embodiment of the present invention.
Fig. 16 is a perspective view of another embodiment of the position switch assembly of the present invention.
Fig. 17 is a second perspective view of the position switch assembly according to another embodiment of the present invention.
FIG. 18 is a diagram of an embodiment of the present invention in a specific application.
The reference numbers in the figures denote:
1. a box body; 101. an upper cavity; 102. a lower cavity; 103. a flap door; 104. a switching drive member; 1041. a connecting rod; 1042. a pull rod; 1043. a drive member; 105. a vertical telescopic assembly; 1051. a cross bar; 1052. a telescopic vertical rod; 1053. a top rod; 106. a jack; 107. hoisting the assembly; 1071. lifting lugs; 108. a tailgate; 1081. a railing; 2. an aerial work subsystem; 201. mooring the unmanned aerial vehicle; 3. a ground support subsystem; 301. a fire extinguishing agent supply unit; 3011. a fire water tank; 3012. a water pump; 302. a power supply unit; 3021. a generator; 303. a pipeline deploying and retracting unit; 3031. a pipeline winch; 304. a power supply control box; 305. a hydraulic station; 4. a position conversion assembly; 401. a crank arm assembly; 4011. a Z-shaped crank arm; 4012. a first crank arm; 4013. a second crank arm; 402. a first rotating mechanism; 4021. a first swing cylinder; 4022. a first connecting plate; 4023. a rotating seat; 4024. a rotating shaft; 4025. a gear; 4026. a rack; 4027. a slide base; 4028. a telescopic cylinder; 403. a second rotating mechanism; 4031. a second swing cylinder; 4032. a second connecting plate; 404. a landing platform; 405. a telescoping member; 5. mooring the cable; 6. a supply tube.
Detailed Description
The invention is further described below with reference to the figures and the specific embodiments of the description.
As shown in fig. 1 to 7, the fire-fighting rescue container of the embodiment includes a container type container body 1, an aerial work subsystem 2 and a ground support subsystem 3, wherein a lifting platform 404 is provided in the container body 1, the lifting platform 404 divides the container body 1 into two cavities arranged up and down, which are an upper cavity 101 and a lower cavity 102, respectively, the aerial work subsystem 2 is arranged in the upper cavity 101, and the ground support subsystem 3 is arranged in the lower cavity 102. The fire-fighting rescue container of the invention forms a container type structure by integrating the aerial operation subsystem 2 and the ground support subsystem 3 in the container body 1, thereby having the following advantages:
1. due to the fact that the container type structure is adopted, the container type fire fighting truck can be physically separated from various special fire fighting trucks, not only can be installed on the special fire fighting trucks, but also can be independently placed on the ground or a platform with large size bearing capacity, and can also be placed on general transport vehicles such as flat cars, and therefore installation, fixing and transportation are facilitated.
2. The aerial operation subsystem 2 and the ground support subsystem 3 in the box body 1 can adopt various flexible configurations and modularized settings according to different requirements, are more favorable for popularization and deep popularization of fire-fighting and fire-fighting rescue equipment, and solve the contradiction between the requirement number and insufficient equipment of the fire-fighting equipment, thereby effectively improving the efficiency and success rate of fire hazard disposal, and expanding the more rapid and safe high-altitude fire-fighting and fire-fighting rescue means for fire-fighting and fire-fighting in high-rise buildings, key areas and dangerous areas.
3. Due to the adoption of a container type structure, compared with professional fire-fighting equipment, the container type fire-fighting equipment is low in price and quick in execution speed, and is convenient to configure in key positions of high-risk areas and key areas with hidden fire hazards, resident or dynamic position allocation is realized, quick transfer can be completed around a fire range in the first time at the initial stage of fire danger, cooperative operation among a plurality of containers in the area can be realized, and fire-fighting rescue can be carried out; effectively solve the problem that the fire disaster is developed for self rescue in the golden time. Certainly, the aerial work subsystem 2 and the ground support subsystem 3 in the box body 1 can also realize unattended fire, triggering in distress and man-machine combination through an automatic logic sequence, a sensor and a controller, and quickly process the tasks of fire extinguishing and rescue.
As shown in fig. 5 and 6, in the present embodiment, the box 1 forms an open-close structure on both sides of the upper cavity 101 to facilitate the take-off and landing of the tethered drone 201 of the aerial work subsystem 2. The opening-closing structure comprises wing doors 103 positioned on two sides of an upper-layer cavity 101, one side of each wing door 103 is hinged with the lower parts of two sides of the box body 1, and an opening-closing driving piece 104 used for driving the corresponding wing door 103 to open and close is arranged on each wing door 103; when the opening and closing driving piece 104 drives the wing doors 103 to be unfolded, the wing doors 103 on the two sides are used for expanding a lifting platform of the mooring unmanned aerial vehicle 201, so that the lifting safety of the mooring unmanned aerial vehicle 201 is further improved, and meanwhile, the unfolded wing doors 103 can also serve as a maintenance platform, so that the maintenance operation is facilitated; when the driving piece 104 that opens and shuts drives the wing door 103 and fold, the wing door 103 of both sides folds each other in order to protect mooring unmanned aerial vehicle 201, and the operation of casing promptly is convenient for work such as subsequent saving, transportation. Specifically, as shown in fig. 17, the opening and closing driving member 104 includes a connecting rod 1041, a pull rod 1042 and a driving member 1043, one end of the connecting rod 1041 is hinged to the wing door 103, the other end of the connecting rod 1041 is hinged to one end of the pull rod 1042, and the other end of the pull rod 1042 is connected to the driving member 1043 (such as a telescopic cylinder, etc.); the tension rod 1042 is extended and contracted by the telescopic cylinder, so that the link 1041 is pulled by the tension rod 1042 to open and close the wing door 103. The opening-closing type structure is simple in overall structure, simple and convenient to operate and easy to achieve.
As shown in fig. 1, in the embodiment, two sides of the bottom of the box 1 are provided with insertion holes 106 for inserting the fork rods of the forklift for carrying. In addition, the box body 1 is provided with a hoisting component 107 for hoisting operation. Specifically, as shown in fig. 17, the hoisting assembly 107 includes lifting lugs 1071 at four corner positions of the box body 1. As shown in fig. 2, a rear door 108 is further provided at the rear end of the cabinet 1, and one side of the rear door 108 is hinged to the cabinet 1 and the other side is fastened to the cabinet 1 by a fastening assembly. The tail gate 108 can be opened and closed around one side of the hinge to realize opening or closing; wherein be equipped with the railing 1081 that is used for the climbing on the tail-gate 108, the maintenance personal of being convenient for etc. climbs the platform 404 that falls and maintains etc. operation to the personnel of staying nothing. The arrangement of the structure can carry or transport the box body 1 quickly.
In this embodiment, as shown in fig. 11-14, the box 1 is folded on both sides with vertical telescopic assemblies 105 for lifting the box 1 for transferring the trailer. Specifically, the vertical telescopic assembly 105 comprises a cross bar 1051 and a telescopic vertical bar 1052, one end of the cross bar 1051 is rotatably mounted on the box body 1 through a swing cylinder, and the telescopic vertical bar 1052 is fixed at the other end of the cross bar 1051; the top of the vertical telescopic rod 1052 is provided with a top rod 1053 for supporting the unfolded wing door 103. Preferably, two vertical telescopic assemblies 105 are provided on each side of the cabinet 1, and one end of the crossbar 1051 is engaged in the folded position of the cabinet 1 by rotation of the tilt cylinder when not in use, as shown in fig. 11. When the telescopic vertical rod 1052 needs to be used, the cross rod 1051 is firstly rotated by 90 degrees through the swing cylinder pendulum, and at the moment, the telescopic vertical rod 1052 is in an unextended state, as shown in fig. 12; then flexible montant 1052 extends to carry out the lifting with box 1, as shown in fig. 13, the vehicle then can move back the carriage to box 1 below this moment, and the decline of rethread flexible montant 1052 steadily puts box 1 to the carriage on, thereby is convenient for transport whole box 1. Of course, the transfer of the box 1 from the carriage to the ground can also be achieved by the above-described procedure. In addition, under the state that above-mentioned horizontal pole 1051 is opened, the ejector pin 1053 can support the wing door 103 that opens, guarantees the stationarity of wing door 103 to the security that the maintenance personal maintained mooring unmanned aerial vehicle 201 on wing door 103, as shown in fig. 14. The whole vertical telescopic assembly 105 is simple in structure, simple and convenient to operate and rich in functions, and not only can the box body 1 be converted between the ground position and the carriage position, but also the wing door 103 can be supported and protected.
As shown in fig. 15 to 17, in the present embodiment, a position conversion assembly 4 is disposed in the box 1, and is used for performing position conversion on the tethered drone 201 of the aerial work subsystem 2, such as conversion from inside the box 1 to the ground, or conversion from the ground to inside the box 1. Specifically, the position conversion assembly 4 includes a crank arm assembly 401, a first rotating mechanism 402, a second rotating mechanism 403, and a landing platform 404 for the mooring unmanned aerial vehicle 201 to take off and land, one end of the crank arm assembly 401 is rotatably mounted in the box body 1 through the first rotating mechanism 402, and the other end of the crank arm assembly 401 is rotatably connected with the landing platform 404 through the second rotating mechanism 403; the first rotation mechanism 402 rotates the crank arm assembly 401 between the extended state and the retracted state, and the second rotation mechanism 403 rotates the landing platform 404 so that the landing platform 404 is horizontal when the crank arm assembly 401 rotates. In particular, the crank arm assembly 401 comprises a Z-shaped crank arm, wherein the Z-shaped crank arm 4011 is in an extended state with the landing platform 404 in a ground position; when the Z-shaped crank arm 4011 is in a retracted state, the lifting platform 404 is positioned in the box body 1; through the cooperation of above-mentioned first slewing mechanism 402 and second slewing mechanism 403 for take off and land platform 404 and form the linkage between the crank arm subassembly 401, and then realize the switching between box 1 and the ground position on the platform 404 that takes off and land, be convenient for mooring unmanned aerial vehicle 201's vanning, work such as ground maintenance transportation, simultaneously can guarantee to take off and land platform 404 and be in the horizontality all the time at the in-process that switches, thereby guarantee to mooring unmanned aerial vehicle 201 the safety and stability on the platform 404 that takes off and land. Of course, the tethered drone 201 is fastened to the landing platform 404 by corresponding fastening assemblies, and the corresponding fastening assemblies may employ mounts such as hydraulic push rods to secure the fixed landing gear of the tethered drone 201. The whole structure is simple, the operation is simple and convenient, and the realization is easy.
As shown in fig. 15, in this embodiment, the first rotating mechanism 402 includes a rotating seat 4023, a rotating shaft 4024, a gear 4025, a rack 4026, a sliding seat 4027, and a telescopic cylinder 4028, the rotating seat 4023 is fixed in the housing 1, the rotating shaft 4024 passes through and is fastened to the Z-shaped curved arm 4011, wherein the rotating shaft 4024 is rotatably installed on the rotating seat 4023, the two gears 4025 are fixedly installed on both sides of the rotating shaft 4024, a bottom surface of the rack 4026 is slidably installed on the sliding seat 4027, a top surface of the rack 4026 is engaged with the gear 4025, and a telescopic end of the telescopic cylinder 4028 is connected to one end of the rack 4026 for driving the rack 4026 to slide on the sliding seat 4027, and the gear 4025 is driven to rotate by linear motion of the rack 4026, so that the rotating shaft 4024 rotates and the Z-shaped curved arm 4011 rotates, thereby enabling the Z-shaped curved arm 4011 to rotate between an. Of course, in other embodiments, the first rotating mechanism 402 may also directly use the first swing cylinder 4021 (e.g. a spiral hydraulic swing cylinder), and the first swing cylinder 4021 is fixed in the container, wherein the swing end of the first swing cylinder 4021 is connected to one end of the Z-shaped curved arm 4011 through the first mounting plate. When the swing is performed, the first swing cylinder 4021 swings, and the Z-shaped crank arm 4011 on the first connection plate 4022 is rotated between the extended state and the retracted state. In addition, a first position detecting element (e.g., a position sensor, not shown in the figure) is disposed on the first swing cylinder 4021, and is used for detecting a rotation angle of the first swing cylinder 4021, so as to monitor the rotation angle and ensure safety and reliability of rotation.
As shown in fig. 15, in the present embodiment, the second rotating mechanism 403 includes a second swing cylinder 4031 (e.g., a spiral hydraulic swing cylinder) and a second connecting plate 4032, the second swing cylinder 4031 is fixed to the other end of the crank arm assembly 401, and the output end of the second swing cylinder 4031 is connected to the landing platform 404 through the second connecting plate 4032. Wherein, a second position detecting element (such as a position sensor, not shown in the figure) is arranged on the second swinging cylinder 4031, and is used for detecting the rotation angle of the second swinging cylinder 4031 to realize the monitoring of the rotation angle; an inclination sensor (not shown) is also provided on the landing platform 404 for detecting the inclination between the landing platform 404 and the horizontal plane. In the process of swinging the Z-shaped crank arm 4011, the inclination angle between the landing platform 404 and the horizontal plane changes, and by detecting the inclination angle value between the landing platform 404 and the horizontal plane, when the inclination angle value exceeds a certain range (such as +/-5 degrees), the corresponding second swinging cylinder 4031 is controlled to swing at a corresponding angle in response, so that the landing platform 404 is always in a horizontal state in the swinging process of the Z-shaped crank arm 4011, and the safety of the unmanned aerial vehicle 201 tethered to the landing platform 404 is ensured. Of course, in other embodiments, the swing of the second swing cylinder 4031 may be adjusted according to the rotation angle of the first swing cylinder 4021. When the Z-shaped crank arm 4011 rotates, the inclination angle between the landing platform 404 and the horizontal plane can be obtained through the rotation angle of the Z-shaped crank arm 4011 and the known bending angle of the Z-shaped crank arm 4011, so that the inclination value of the landing platform 404 can be obtained through the rotation angle of the first swing cylinder 4021 detected by the first position detector, and the rotation adjustment of the second swing cylinder 4031 can be realized, that is, the rotation of the second swing cylinder 4031 is performed according to the rotation angle of the first swing cylinder 4021.
In another embodiment, as shown in fig. 16 and 17, the crank arm assembly 401 is composed of multiple crank arms, and specifically includes a first crank arm 4012 and a second crank arm 4013, one end of the first crank arm 4012 is connected to the first rotating mechanism 402, the other end of the first crank arm 4012 is rotatably connected to one end of the second crank arm 4013, and the other end of the second crank arm 4013 is connected to the second rotating mechanism 403; a telescopic part 405 is arranged between the first crank arm 4012 and the second crank arm 4013. The telescopic part 405 may be a telescopic oil cylinder, a telescopic air cylinder, a telescopic electric cylinder, or other telescopic mechanisms. Specifically, above-mentioned crank arm subassembly 401 sets up the structure that the extensible member 405 was add to multistage and centre, can be applicable to the switching between the different positions, like the switching between vanning position and the ground, also can realize vanning position and trailer position (trailer position is higher than ground), if when the trailer position, can make the second crank arm 4013 stretch out forward through the extension of extensible member 405 to adapt to the trailer position and be convenient for transport the processing such as to mooring unmanned aerial vehicle 201 on the landing platform 404. Above-mentioned position conversion subassembly 4, set crank arm subassembly 401 to the multistage and the centre adds extensible member 405, make the position between each crank arm change through the flexible of extensible member 405, realize the automatic switch-over of mooring unmanned aerial vehicle 201 between different positions, like packing position (the container is located on ground or vehicle) and ground, packing position and trailer position (trailer position is higher than ground), or the switch-over between ground and the trailer position etc. to realize mooring unmanned aerial vehicle 201 vanning, ground maintenance, the seamless butt joint between the work such as trailer transport; the structure is simple, the operation is simple and convenient, and the realization is easy.
As shown in fig. 4 and 7, in this embodiment, the ground support subsystem 3 is configured to provide various supports for the tethered drone 201, and specifically includes a fire extinguishing agent supply unit 301, a power supply unit 302, and a pipeline deploying and retracting unit 303, where the power supply unit 302 is configured to provide a power supply to the tethered drone 201 through the tethered cable 5; the fire extinguishing agent supply unit 301 is used for supplying fire extinguishing agent to the tethered drone 201 through the supply pipe 6; the line retraction unit 303 is used for retracting the mooring cable 5 and/or the supply pipe 6. Above-mentioned ground support subsystem 3 will put out fire agent supply unit 301, power supply unit 302 and pipeline and receive and release unit 303 and install in the lower floor cavity 102 of box 1, can realize each unit and the quick travel of mooring unmanned aerial vehicle 201, guarantee the promptness of fire control fire extinguishing rescue, each unit is multiple functional in the box 1, and the use of collocation mooring unmanned aerial vehicle realizes the function integration of rescue and fire control.
As shown in fig. 4 and 7, the fire extinguishing agent supply unit 301 includes a fire water tank 3011 and a water pump 3012, the water pump 3012 has an inlet connected to the fire water tank 3011 and an outlet connected to the supply pipe 6; of course, the water pump 3012 may be directly connected to a water source of a hydrant outside the tank 1. The power supply unit 302 comprises a generator 3021 and a storage battery, the generator 3021 and the storage battery are both connected with the mooring cable 5, and power is generated by the generator 3021 and then converted to provide power for the mooring unmanned aerial vehicle 201. The pipeline reeling and unreeling unit 303 comprises a pipeline winch 3031, a pipeline on the pipeline winch 3031 is connected with the mooring unmanned aerial vehicle 201 through a hole on the landing platform 404, when the mooring unmanned aerial vehicle 201 flies at high altitude, the pipeline winch 3031 realizes reeling and releasing of a water pipe and a cable according to the flying height of the mooring unmanned aerial vehicle 201, the normal length of the water pipe and the cable is ensured, and overlong knotting or winding with other obstacles is avoided. In addition, the controller of the whole fire-fighting and rescue system realizes the taking-off and landing operation of the tethered unmanned aerial vehicle 201, and adjusts the posture and position of the tethered unmanned aerial vehicle 201 and corresponding rescue and fire-fighting operations according to the fire situation image information and the like shot by the tethered unmanned aerial vehicle 201; of course, the controller can be fixed in the cab, and the controller can be taken out of the cab for operation and control through an extension line or a wireless communication mode.
As shown in fig. 4 and 7, in the present embodiment, the power supply unit 302, the pipeline housing unit 303, and the fire extinguishing agent supply unit 301 are sequentially arranged along the length direction of the lower chamber 102. Through the spatial position arrangement of each unit, on the premise of ensuring the running stability of the vehicle, the vehicle-mounted intelligent control system has reasonable functional partitions, compact integral structure and convenient maintenance. In addition, the two sides of the box body 1 are provided with independent box doors, so that the maintenance and the like are convenient; the electric rolling door is adopted as the door, the opening and closing are simple and convenient, the electric rolling door does not occupy the space on two sides of the carriage, the electric rolling door is suitable for the operation area with narrow space, and meanwhile, the electric rolling door is convenient for operators to carry out fire-fighting and fire-fighting rescue operation. In addition, a power control box 304 is arranged between the power supply unit 302 and the pipeline deploying and retracting unit 303, and is used for converting the three-phase alternating current output by the generator 3021 into matched power supply output according to the power supply requirements of each device. In addition, a hydraulic station 305 is arranged at the tail part of the lower cavity 102, and a hydraulic system and a circuit are provided for comprehensively ensuring the opening and closing of the wing door 103, the action of the position conversion assembly 4, the loosening and clamping of the landing gear and the like.
The above is only a preferred embodiment of the present invention, and the protection scope of the present invention is not limited to the above-mentioned embodiments, and all technical solutions belonging to the idea of the present invention belong to the protection scope of the present invention. It should be noted that modifications and embellishments within the scope of the invention may be made by those skilled in the art without departing from the principle of the invention.

Claims (10)

1. The utility model provides a fire control rescue container of putting out a fire, its characterized in that includes box (1), aerial operation subsystem (2) and ground guarantee subsystem (3), box (1) is upper cavity (101) and lower floor's cavity (102) respectively including two cavitys of arranging from top to bottom, aerial operation subsystem (2) arrange in upper cavity (101), ground guarantee subsystem (3) arrange in lower floor's cavity (102).
2. A fire fighting and rescue container as defined in claim 1, characterized in that the box body (1) forms an open-close structure on both sides of the upper cavity (101); the opening and closing structure comprises wing doors (103) positioned on two sides of the partition board, one side of each wing door (103) is hinged with the box body (1), and an opening and closing driving piece (104) used for driving the corresponding wing door (103) to open and close is arranged on each wing door (103); when the opening and closing driving piece (104) drives the wing doors (103) to be unfolded, the wing doors (103) on two sides are used for expanding a take-off and landing platform of the mooring unmanned aerial vehicle (201); when opening and shutting driving piece (104) drive wing door (103) fold, wing door (103) of both sides fold each other and protect mooring unmanned aerial vehicle (201).
3. A fire fighting and rescue container as defined in claim 2, characterized in that the box (1) is folded on both sides with vertical telescopic assemblies (105) for lifting the box (1) for the transfer of a trailer; the vertical telescopic assembly (105) comprises a cross rod (1051) and a telescopic vertical rod (1052), one end of the cross rod (1051) is transmounted on the box body (1), and the telescopic vertical rod (1052) is fixed at the other end of the cross rod (1051); the top of the telescopic vertical rod (1052) is provided with a mandril (1053) for supporting the unfolded wing door (103).
4. A fire-fighting rescue container as claimed in any one of claims 1 to 3, wherein the bottom of the container body (1) is provided with jacks (106) at both sides for insertion of the fork rod of a forklift for carrying; and a hoisting assembly (107) is arranged on the box body (1) and is used for hoisting operation.
5. A fire fighting and rescue container as in any of claims 1 to 3, characterized by a position conversion assembly (4) disposed in the container body (1) for converting the position of the tethered drone (201) of the aerial work subsystem (2).
6. A fire fighting and rescue container as defined in claim 5, wherein the position conversion assembly (4) comprises a crank arm assembly (401), a first rotating mechanism (402), a second rotating mechanism (403) and a landing platform (404) for the mooring unmanned aerial vehicle (201) to take off and land, one end of the crank arm assembly (401) is rotatably mounted in the box body (1) through the first rotating mechanism (402), and the other end of the crank arm assembly (401) is rotatably connected with the landing platform (404) through the second rotating mechanism (403); the first rotating mechanism (402) drives the crank arm assembly (401) to rotate between an extended state and a retracted state, and the second rotating mechanism (403) drives the landing platform (404) to rotate, so that the landing platform (404) is in a horizontal state when the crank arm assembly (401) rotates.
7. A firefighting rescue container as claimed in claim 6 characterized in that the crank arm assembly (401) comprises a first crank arm (4012) and a second crank arm (4013), one end of the first crank arm (4012) being connected to the first turning mechanism (402), the other end of the first crank arm (4012) being connected in rotation to one end of the second crank arm (4013), the other end of the second crank arm (4013) being connected to the second turning mechanism (403); and a telescopic piece (405) is arranged between the first crank arm (4012) and the second crank arm (4013).
8. A fire fighting and rescue container as defined in claim 7, characterized in that the first rotation mechanism (402) comprises a first swing cylinder (4021) and a first connection plate (4022), the first swing cylinder (4021) is fixed in the box body (1), the output end of the first swing cylinder (4021) is connected to one end of the crank arm assembly (401) through the first connection plate (4022); the first swing cylinder (4021) is provided with a first position detection piece for detecting the rotation angle of the first swing cylinder (4021); the second rotating mechanism (403) comprises a second swinging cylinder (4031) and a second connecting plate (4032), the second swinging cylinder (4031) is fixed at the other end of the crank arm assembly (401), and the output end of the second swinging cylinder (4031) is connected with the lifting platform (404) through the second connecting plate (4032); the second swing cylinder (4031) is provided with a second position detection piece for detecting the rotation angle of the second swing cylinder (4031).
9. A fire fighting and rescue container as defined in claim 8, wherein the first rotation mechanism (402) comprises a rotation base (4023), a rotation shaft (4024), a gear (4025), a rack (4026), a sliding base (4027) and a telescoping cylinder (4028), the rotation base (4023) is fixed on the box body (1), the rotation shaft (4024) is fastened on the crank arm assembly (401) and rotatably mounted on the rotation base (4023), the gear (4025) is mounted on one side or both sides of the rotation shaft (4024), the rack (4026) is slidably mounted on the sliding base (4027) and engaged with the gear (4025), and the telescoping end of the telescoping cylinder (4028) is connected with one end of the rack (4026) for driving the rack (4026) to slide on the sliding base (4027).
10. A firefighting rescue container as claimed in any one of claims 1 to 3 wherein the ground support subsystem (3) comprises a fire extinguishing agent supply unit (301), a power supply unit (302) and a pipeline deploying and retracting unit (303); the power supply unit (302) is connected with the tethered unmanned aerial vehicle (201) through a tethered cable (5) and is used for providing power supply for the tethered unmanned aerial vehicle (201); the fire extinguishing agent supply unit (301) is connected with the fire extinguishing unit through a supply pipe (6) and is used for supplying fire extinguishing agent to the fire extinguishing unit; the pipeline reeling and unreeling unit (303) is used for reeling and unreeling the mooring cable (5) or/and the supply pipe (6); the power supply unit (302), the pipeline collecting and releasing unit (303) and the fire extinguishing agent supply unit (301) are sequentially arranged along the length direction of the lower-layer cavity (102).
CN202010706700.8A 2020-07-21 2020-07-21 Fire-fighting rescue container Pending CN111803838A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202010706700.8A CN111803838A (en) 2020-07-21 2020-07-21 Fire-fighting rescue container

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202010706700.8A CN111803838A (en) 2020-07-21 2020-07-21 Fire-fighting rescue container

Publications (1)

Publication Number Publication Date
CN111803838A true CN111803838A (en) 2020-10-23

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN202010706700.8A Pending CN111803838A (en) 2020-07-21 2020-07-21 Fire-fighting rescue container

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Country Link
CN (1) CN111803838A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP4101694A1 (en) * 2021-06-07 2022-12-14 Shanghai Autoflight Co., Ltd. A uav take-off and landing platform
EP4101759A1 (en) * 2021-06-07 2022-12-14 Shanghai Autoflight Co., Ltd. A uav transport box
EP4223650A1 (en) * 2022-02-07 2023-08-09 Shanghai Autoflight Co., Ltd. Transport vehicle and an unmanned aerial vehicle

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP4101694A1 (en) * 2021-06-07 2022-12-14 Shanghai Autoflight Co., Ltd. A uav take-off and landing platform
EP4101759A1 (en) * 2021-06-07 2022-12-14 Shanghai Autoflight Co., Ltd. A uav transport box
US20220396421A1 (en) * 2021-06-07 2022-12-15 Shanghai Autoflight Co., Ltd. UAV Transport Box
US11814241B2 (en) * 2021-06-07 2023-11-14 Shanghai Autoflight Co., Ltd. UAV transport box
EP4223650A1 (en) * 2022-02-07 2023-08-09 Shanghai Autoflight Co., Ltd. Transport vehicle and an unmanned aerial vehicle

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