CN115158692B - Airport aircraft refueling system - Google Patents
Airport aircraft refueling system Download PDFInfo
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- CN115158692B CN115158692B CN202210883578.0A CN202210883578A CN115158692B CN 115158692 B CN115158692 B CN 115158692B CN 202210883578 A CN202210883578 A CN 202210883578A CN 115158692 B CN115158692 B CN 115158692B
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- side wall
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- 229910000831 Steel Inorganic materials 0.000 claims abstract description 59
- 239000010959 steel Substances 0.000 claims abstract description 59
- 238000007665 sagging Methods 0.000 claims description 12
- 210000001503 joint Anatomy 0.000 claims description 9
- 239000000945 filler Substances 0.000 claims description 8
- 238000000926 separation method Methods 0.000 claims description 8
- 230000000694 effects Effects 0.000 claims description 7
- 239000000463 material Substances 0.000 claims description 6
- 238000005086 pumping Methods 0.000 claims description 6
- 229910001220 stainless steel Inorganic materials 0.000 claims description 3
- 239000010935 stainless steel Substances 0.000 claims description 3
- 239000003921 oil Substances 0.000 description 151
- 230000000149 penetrating effect Effects 0.000 description 10
- 239000000446 fuel Substances 0.000 description 9
- 238000005461 lubrication Methods 0.000 description 5
- 239000010742 number 1 fuel oil Substances 0.000 description 5
- 239000000428 dust Substances 0.000 description 4
- 230000003137 locomotive effect Effects 0.000 description 4
- 241000357293 Leptobrama muelleri Species 0.000 description 2
- 238000007599 discharging Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000003032 molecular docking Methods 0.000 description 2
- 239000010865 sewage Substances 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000003031 feeding effect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Classifications
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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
- B64F1/28—Liquid-handling installations specially adapted for fuelling stationary aircraft
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Loading And Unloading Of Fuel Tanks Or Ships (AREA)
- Pipeline Systems (AREA)
Abstract
The invention discloses an aircraft oiling intelligent terminal with 4G encrypted communication, which belongs to the technical field of oiling, wherein a fixed assembly mechanism is arranged on divergent angle steel, a dragging oiling pipe assembly is also arranged on divergent angle steel, a single-chip microcomputer system is arranged on an oiling warehouse, the single-chip microcomputer system registers the oil quantity and the oiling times of each oiling, and a maintenance program is arranged in a server and is used for lifting a prompt to be raised through the oiling quantity and the oiling times. When the device is used, the electric button is pressed when the oil gun heads start to supply oil, the central processing unit sends a signal to the oil pump, the oil pump starts to supply oil, if the oil pump simultaneously receives the pulse signals of N oil gun heads, the oil pump oil supply flow is also improved by N times, and the oil gun heads are put into the underground cavity together with the towing hose after the oil is added.
Description
Technical Field
The invention relates to the technical field of oiling, in particular to an airport aircraft oiling system.
Background
With the development of industrial technology, modern aviation technology is developed more and more perfectly, an airplane stopped at an airport needs to be refueled, the former refueled mode is to use a tank truck, the tank truck runs to the position of the airplane to carry out refueled operation, a locomotive device is needed to be used in the operation, the locomotive device occupies large space, a scratch phenomenon is easy to occur when the locomotive runs, the refueled operation is time-consuming and labor-consuming, and when a manager wants open and see data, a clerk is needed to sort on-site refueled information to be checked;
Secondly, the volume of the oil tank in the airport is too large, and too much aircraft fuel is stored in one oil tank, so that the aircraft fuel has a certain danger, the oil tank truck needs to remove the oil from the oil tank after each oil adding, and the oil tank truck frequently enters and exits in a gate of the oil tank, so that the cost of transporting the oil is increased.
Disclosure of Invention
The invention aims to overcome the defects of the prior art, and provides an airport plane refueling system, when the airport plane refueling system is used, a button is pressed when a refueling gun head starts to supply oil, a central processing unit sends a signal to an oil pump, the oil pump starts to supply oil, if the oil pump simultaneously receives pulse signals of N refueling gun heads, the flow rate of the oil pump for supplying oil is also increased by N times, the refueling gun heads are placed into a subsurface cavity together with a towing hose after the oil is added, and an operation space is saved in a refueling mode of an underground pipeline.
In order to solve the problems, the invention provides the following technical scheme: the utility model provides an airport aircraft refueling system, includes diverges the angle steel, diverges the angle steel and is provided with a plurality of altogether to divergent mutual parallel arrangement between the angle steel, be provided with fixed equipment mechanism on the angle steel diverges, and still be provided with on the angle steel diverges and drag oil filler pipe subassembly, one side of diverging the angle steel is provided with long-range oil feeding unit, and long-range oil feeding unit is connected to on the oil supply storehouse, be provided with singlechip system on the oil supply storehouse.
Further, fixed equipment mechanism includes the bearing turn-ups, and the bearing turn-ups is provided with a plurality of around the support on the lateral wall that the angle steel was diverged to the back of the bearing turn-ups, encircles the top of support and is provided with mounting flange, and mounting flange passes through expansion bolts and building fixed connection, the angle steel that diverges is in the underground tank.
Further, the underground groove is a rectangular cavity under the airport concrete ground, and a wire groove opening is arranged between the rectangular cavity under the airport concrete ground and the ground surface.
Further, pull the oil filler pipe subassembly and include the navigation car, one side of navigation car is provided with four slide wheels, and slide wheel's material is stainless steel material, and slide wheel passes through the lateral wall swivelling joint of thin pole and navigation car, and the top of navigation car is provided with tortuous turn-ups, is provided with two lubricated rings on the tortuous turn-ups, and the inboard activity of lubricated ring is alternated and is dragged the line hose, drags the top of line hose and is provided with the nozzle.
Further, one side of the divergence angle steel back to the bearing flanging is provided with a sagging flanging, the sagging flanging is bent downwards, one side of the divergence angle steel back to the bearing flanging is inclined downwards, and the side wall of the sagging flanging buckled column sliding wheel is provided with a sagging flanging.
Further, the remote oil supply assembly comprises a divergent pipeline, the divergent pipeline is connected with an oil supply port of the towing hose, a three-way pipeline is arranged at the other port of the divergent pipeline, the three-way pipelines are connected in series through a plurality of interlink pipelines, and a pressure sensor is arranged at the inner side of each interlink pipeline.
Further, the oil supply warehouse comprises an oil warehouse frame, a plurality of horizontal and vertical separation plates are arranged in the middle of the oil warehouse frame, the plurality of separation plates are staggered transversely and vertically to form a containing cavity, an oil storage tank is arranged in the containing cavity, a butt joint valve is arranged at the opening of the oil storage tank, and a movable oil pumping mechanism is arranged on one side of the oil warehouse frame.
Further, the movable oil pumping mechanism comprises a lifting rocker, the lifting rocker is arranged on the vertical lifting assembly, two movable guide rods are arranged on the side wall of the lifting rocker, a positioning sliding block is slidably arranged on the movable guide rods, a traversing plate block is arranged on the side wall of the positioning sliding block, an electric push rod is arranged on the side wall of the traversing plate block and fixedly connected with the side wall of the traversing plate block through an arch bridge bracket, an penetrating steel pipe is arranged at the output end of the electric push rod, one side of the penetrating steel pipe is communicated with an oil conveying hose, the other port of the oil conveying hose is communicated with an oil pump, the oil pump is communicated with a port of a connecting link pipeline, the oil conveying hose is of a type with a built-in spiral spring, penetrating wire grooves matched with the penetrating steel pipe are formed in the lifting rocker, a propelling shaft seat is further arranged on the side wall of the lifting rocker, a propelling motor is arranged on the side wall of the propelling shaft seat, a threaded rod is arranged at the output end of the propelling motor, and a nut block sleeved on the threaded rod is arranged on the side wall of the traversing plate block.
Further, vertical lift subassembly includes two vertical guide rails, vertical guide rail fixes on the lateral wall of oil depot frame, slidable mounting has vertical slider on the vertical guide rail, be provided with the lift plate on the lateral wall of vertical slider, the end of lift wane is fixed on the lateral wall of lift plate, the upper and lower both ends of vertical guide rail all are provided with the end plate, fixed mounting has the carrier bar on the lateral wall of end plate, the carrier roller is installed in one side rotation of carrier bar, connect through carrier belt between the carrier roller, the lateral wall and the carrier belt fixed connection of lift plate, one of them carrier roller is installed on elevator motor's output, elevator motor fixes on the lateral wall of carrier bar.
Further, the singlechip system includes central processing unit, and central processing unit connects a plurality of oil supply pulse button, and the oil supply pulse button is provided with the nozzle tip on, presses the button when nozzle tip begins to need the oil feeding, and central processing unit gives the oil pump and sends the signal, and the oil pump begins to use the oil feeding, if the oil pump received the pulse signal of N nozzle tips simultaneously, the flow of oil pump oil feeding also improves N times, and nozzle tip is put into the underground cavity together with dragging hose one after adding oil.
The invention has the beneficial effects that:
Firstly, the device is when using, the button is pressed down when the nozzle tip begins to need the fuel feeding, central processing unit gives the oil pump and sends the signal, the oil pump begins to use the fuel feeding, if the oil pump receives the pulse signal of N nozzle tips simultaneously, the flow of oil pump fuel feeding also improves N times, nozzle tip is put in the underground cavity together with dragging hose one after adding the oil, the operating space has been saved to the mode that underground pipeline refuels, compare in prior art's mode of refueling, former locomotive refuels the mode and need use the tank car to remove the oil tank car to remove the place of oil removal material transport to the shut down in the oil warehouse, this kind of tank car transportation mode not only occupies a large amount of spaces, and transportation cost has also become high.
Secondly, the device is at the oil storage tank of a position of the first counter-rotation of plate of crossing in the in-process of fuel feeding, electric putter drives the interlude steel pipe and stretches out and connect with the butt joint valve switch-on, the oil pump begins to draw the oil of the oil storage tank inside, after a oil storage tank is dried, lift plate and lift wane are along vertical guide rail height-adjusting, the plate of crossing is along movable guide arm adjustment position, and then the plate of crossing can reach the position of all oil storage tanks, realized convenient oil feeding's effect, compare in prior art's oil feeding mode, the easy too big of an oil depot in the past oil feeding mode, this just has certain danger, and oil depot feed-back and unloading operation are troublesome yet, the oil storage tank divide into the monolithic piece, conveniently carry in the middle of the division board, it is also convenient to transport, and if one of them oil storage tank goes wrong can not influence other oil storage tanks.
Thirdly, the aerocar slides on diverging angle steel through the pulley, and the aircraft is after stopping steadily, and manual taking out the nozzle tip and inject the tank filler hole of aircraft, and the aerocar is manual dragging at diverging angle steel's the coasting, has certain flexibility to the interlink pipeline of each is inside all to have pressure sensor, and when oil conveying system was stopped up, each pressure sensor can carry data for the computer, interlink pipeline was established ties, and then first site appears pressureless pressure sensor and is the site of jam, has realized convenient inquiry fault point's effect.
Drawings
The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the invention and do not constitute a limitation on the invention. In the drawings:
FIG. 1 is a schematic diagram of the present invention in elevation.
Fig. 2 is a schematic view of the divergent angle of the present invention.
Fig. 3 is a schematic view of a divergent angle of the present invention at a second view angle.
Fig. 4 is a schematic view of a boat truck according to the present invention.
Fig. 5 is a schematic view of the oil depot frame of the present invention.
Fig. 6 is a schematic view of a threaded rod according to the present invention.
Fig. 7 is a schematic view of the lift rocker of the present invention.
Fig. 8 is a schematic view of an electric putter according to the present invention.
Reference numerals illustrate:
Link pipe 1, divergent pipe 2, tee pipe 3, divergent angle 4, surround bracket 401, mounting flange 402, towing hose 403, load bearing flange 404, drooping flange 405, fuel nozzle 5, boat 6, runner 601, wand 602, tortuous flange 603, lubrication ring 604, reservoir frame 7, gap plate 701, reservoir 702, docking valve 703, vertical rail 8, vertical slider 801, lifting plate 802, tip plate 803, carrier axle seat 804, carrier roller 805, carrier belt 806, lift motor 807, lifting rocker 9, movable guide bar 901, positioning slider 902, traversing plate 903, arch bridge bracket 904, propulsion axle seat 905, propulsion motor 906, threaded rod 907, electric push rod 908, interpenetration steel tube 909, oil delivery hose 910, interpenetration wire slot 10.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the technical solutions of the present invention will be clearly and completely described below with reference to specific embodiments of the present invention and corresponding drawings. It will be apparent that the described embodiments are only some, but not all, embodiments of the invention. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
The following describes in detail the technical solutions provided by the embodiments of the present invention with reference to the accompanying drawings.
Referring to an airport aircraft refueling system shown in fig. 1,2,3,4, 5, 6, 7 and 8, including diverging angle steel 4, diverging angle steel 4 is provided with a plurality of altogether to arrange mutually parallel between the angle steel 4 diverges, be provided with fixed equipment mechanism on diverging angle steel 4, and further be provided with on diverging angle steel 4 and drag the oil filler pipe subassembly, one side of diverging angle steel 4 is provided with long-range oil supply unit, and long-range oil supply unit is connected to the oil supply storehouse, be provided with singlechip system on the oil supply storehouse, the aircraft is stable in the prescription position of airport after, and manual will drag the oil filler pipe subassembly and take out to inject in the oil filler hole of aircraft, and long-range oil supply unit begins to draw the oil of the oil supply storehouse inside and refuels in the oil tank of aircraft.
The fixed equipment mechanism includes bearing turn-ups 404, and bearing turn-ups 404 and divergent angle steel 4 mutually perpendicular, and is provided with a plurality of around support 401 on the lateral wall that the angle steel 4 was diverged in the bearing turn-ups 404 dorsad, and the top of surrounding support 401 is provided with mounting flange 402, and mounting flange 402 passes through expansion bolts and building fixed connection, divergent angle steel 4 is in the underground tank, surrounds support 401 and mounting flange 402 and fixes on the building, and then diverges angle steel 4 just can be in overhead state, drags the oil filler pipe subassembly and can slide along diverged angle steel 4 conveniently, has realized the effect of convenient installation and dismounting device for the device is in the position of damage, and it is more convenient to maintain.
The underground tank is a rectangular cavity of airport concrete ground, a slot opening is arranged between the rectangular cavity of the airport concrete ground and the ground surface, a divergent angle steel 4 and a pipeline for feeding are arranged in an underground position, the oil adding pipeline penetrates out of the slot opening to the upper side of the ground for oiling operation, the hub of the airplane can be expanded from the slot opening, the operation of the airplane is not affected, the space of the airport is not occupied by the tank truck, and the movable space of the airplane is enlarged.
The towing and oiling pipe assembly comprises an aerocar 6, four sliding wheels 601 are arranged on one side of the aerocar 6, the sliding wheels 601 are made of stainless steel materials, the sliding wheels 601 are rotationally connected with the side wall of the aerocar 6 through thin rods 602, a zigzag flanging 603 is arranged at the top end of the aerocar 6, two lubrication rings 604 are arranged on the zigzag flanging 603, a towing hose 403 is movably inserted into the inner side of the lubrication rings 604, an oiling gun head 5 is arranged at the top end of the towing hose 403, the aerocar 6 can slide along the divergent angle steel 4 to adjust the position, the oiling gun head 5 is dragged upwards until the position of an airplane oiling port, the towing hose 403 slides in the two lubrication rings 604, and the position where the airplane is parked every time is not fixed, so that the movable aerocar 6 is convenient to butt joint the oiling port of the airplane.
The angle steel 4 diverges be provided with the sagging turn-ups 405 on one side of back to the bearing turn-ups 404, sagging turn-ups 405 crookedly down, the angle steel 4 diverges the one side slope of back to the bearing turn-ups 404 down, and the turn-ups of sagging turn-ups 405 detain the lateral wall of post slide wheel 601, diverges angle steel 4 and inclines towards the below, this just lets the dust that diverges angle steel 4 top fall down of being convenient for, uses the watering lorry to strike the device in the airport when the clearance, and the water is mingled with the dust and is flowed down from the position of sagging turn-ups 405, and sewage is collected in the sewer and is carried out final treatment.
The remote oil supply assembly comprises a divergent pipeline 2, the divergent pipeline 2 is connected with an oil supply port of a towing hose 403, a three-way pipeline 3 is arranged at the other port of the divergent pipeline 2, the three-way pipelines 3 are connected in series through a plurality of connecting pipelines 1, each connecting pipeline 1 is internally provided with a pressure sensor, each connecting pipeline is internally provided with a pressure sensor, when an oil transportation system is blocked, each pressure sensor can transmit data to a computer, the connecting pipelines are connected in series, and then the pressure sensor with no pressure at a first position is a blocked position, so that the effect of conveniently inquiring fault points is realized.
The oil supply warehouse comprises an oil warehouse frame 7, a plurality of horizontal and vertical separation plates 701 are arranged in the middle of the oil warehouse frame 7, the plurality of separation plates 701 are staggered transversely and vertically to form a containing cavity, an oil storage tank 702 is arranged in the containing cavity, a butt joint valve 703 is arranged at the opening of the oil storage tank 702, a movable oil pumping mechanism is arranged on one side of the oil warehouse frame 7, fuel of an airplane is stored in a plurality of small vessels, compared with the storage mode of the prior art, the capacity of the past airplane oil warehouse is large, the airplane oil warehouse is also troublesome in certain danger, the oil warehouse feeding and discharging operation is troublesome, the oil storage tank 702 is divided into blocks, the oil storage tank 702 is conveniently carried to the middle of the separation plates 701, and the transportation is convenient, and if one of the oil storage tanks 702 is problematic, the other oil storage tanks 702 cannot be influenced.
The movable oil pumping mechanism comprises a lifting rocker 9, the lifting rocker 9 is arranged on a vertical lifting assembly, two movable guide rods 901 are arranged on the side wall of the lifting rocker 9, a positioning sliding block 902 is slidably arranged on the movable guide rods 901, a traversing plate 903 is arranged on the side wall of the positioning sliding block 902, an electric push rod 908 is arranged on the side wall of the traversing plate 903, the electric push rod 908 is fixedly connected with the side wall of the traversing plate 903 through an arch bridge bracket 904, an penetrating steel pipe 909 is arranged at the output end of the electric push rod 908, one side of the penetrating steel pipe 909 is communicated with an oil delivery hose 910, the other port of the oil delivery hose 910 is communicated with an oil pump, the oil pump is communicated with the port of a link pipeline 1, the oil delivery hose 910 is of a built-in spiral spring type, a penetrating wire slot 10 matched with the penetrating steel pipe 909 is arranged on the lifting rocker 9, the side wall of the lifting rocker 9 is also provided with a pushing shaft seat 905, the side wall of the pushing shaft seat 905 is provided with a pushing motor 906, the output end of the pushing motor 906 is provided with a threaded rod 907, the side wall of the traversing plate 903 is provided with a nut block sleeved on the threaded rod 907, the pushing motor 906 drives the traversing plate 903 to slide along the movable guide rod 901 through the threaded rod 907, the traversing plate 903 can further move to the position of a butt joint valve 703 of a plurality of oil storage tanks 702, the electric push rod 908 drives the penetrating steel pipe 909 to extend out and the butt joint valve 703 to be communicated, the oil pump starts to pump oil in the oil storage tanks 702, and after one oil storage tank 702 is pumped out, the traversing plate 903 moves to the position of the next oil storage tank 702 to pump oil again.
The vertical lifting assembly comprises two vertical guide rails 8, the vertical guide rails 8 are fixed on the side walls of the oil depot frame 7, vertical sliding blocks 801 are slidably mounted on the vertical guide rails 8, lifting plate blocks 802 are arranged on the side walls of the vertical sliding blocks 801, the ends of lifting rocker plates 9 are fixed on the side walls of the lifting plate blocks 802, end plate blocks 803 are arranged at the upper end and the lower end of the vertical guide rails 8, carrier shaft seats 804 are fixedly mounted on the side walls of the end plate blocks 803, carrier rollers 805 are rotatably mounted on one side of the carrier shaft seats 804, the carrier rollers 805 are connected through carrier belts 806, the side walls of the lifting plate blocks 802 are fixedly connected with the carrier belts 806, one carrier roller 805 is mounted on the output end of a lifting motor 807, the lifting motor 807 is fixed on the side walls of the carrier shaft seats 804, the lifting motor 807 drives the carrier belts 806 to operate through the carrier rollers 805, and the lifting plate blocks 802 and the lifting rocker plates 9 can lift along with the carrier belts 806, and further traverse 903 to oil reservoirs 702 with the height of each layer.
The singlechip system comprises a central processor, the central processor is connected with a plurality of oil supply pulse buttons, the oil supply pulse buttons are arranged on the oil gun heads 5, the buttons are pressed down when the oil gun heads 5 start to supply oil, the central processor sends out signals to the oil pump, the oil pump starts to supply oil, if the oil pump simultaneously receives pulse signals of the N oil gun heads 5, the oil pump oil supply flow is increased by N times, and the oil gun heads 5 are put into the underground cavity together with the towing hose 403 after oil is added.
Finally, after the aircraft is stabilized at the formulated position of the airport, the dragging oil filling pipe assembly is manually taken out to be inserted into the oil filling port of the aircraft, the remote oil supply assembly starts to extract oil in the oil supply warehouse to fill the oil in the oil tank of the aircraft, the surrounding support 401 and the mounting flange 402 are fixed on the building, further the divergent angle steel 4 can be in an overhead state, the dragging oil filling pipe assembly can conveniently slide along the divergent angle steel 4, the effect of convenient installation and disassembly of the device is realized, the device is more convenient to maintain at a damaged position, the divergent angle steel 4 and a feeding pipeline are positioned in an underground position, the oil filling pipeline penetrates out from the opening of the wire groove to the upper part of the ground for oiling operation, the hub of the aircraft can be expanded from the opening of the wire groove, the operation of the aircraft is not influenced, the space of the airport is not occupied by the tank truck, and the movable space of the aircraft is enlarged, the aerocar 6 can reciprocally slide along the divergent angle steel 4 to adjust the position, the oiling gun head 5 is dragged upwards until the position of the oiling port of the airplane, the dragging hose 403 slides in the two lubrication rings 604, the position where the airplane is parked each time is not fixed, the movable aerocar 6 is convenient for docking the oiling port of the airplane, the divergent angle steel 4 inclines downwards, the dust at the top end of the divergent angle steel 4 is convenient to fall down, the device is impacted by the sprinkler at the airport during cleaning, the water is mixed with the dust to flow down from the position of the sagging flange 405, sewage is collected into a sewer for final treatment, when the oil conveying system is blocked, each pressure sensor can transmit data to a computer, the interlinking pipelines are connected in series, the pressure sensor at the first position is the blocking position, the effect of conveniently inquiring the fault point is realized, the fuel of the aircraft is stored in a plurality of small vessels, compared with the prior art, the prior aircraft oil depot has larger capacity, the operation of feeding and discharging the oil depot is troublesome, the oil depot is divided into single blocks, the oil depot is conveniently transported to the middle of the separation plate 701, the transportation is convenient, and if one oil depot 702 is problematic, the other oil depot 702 is not influenced, the propulsion motor 906 drives the traversing plate 903 to slide along the movable guide rod 901 through the threaded rod 907, the traversing plate 903 can move to the position of the butt joint valve 703 of a plurality of oil depots 702, the electric push rod 908 drives the penetrating steel pipe 909 to extend out and the butt joint valve 703 to be communicated, the oil pump starts to extract the oil in the oil depot 702, after one oil depot 702 is pumped out, the traversing plate 903 moves to the position of the next oil depot 702 again, the lifting motor 807 drives the carrying belt 806 to operate through the carrying roller 805, the lifting plate 903 and the lifting plate 903 can lift along with the carrying belt 806, and the traversing plate 903 can reach the oil depot 702 at each layer of height.
The foregoing description is only a preferred embodiment of the present invention, and is not intended to limit the technical scope of the present invention, so any minor modifications, equivalent changes and modifications made to the above embodiments according to the technical principles of the present invention are still within the scope of the technical solutions of the present invention.
Claims (5)
1. An airport aircraft fueling system, characterized by: comprises a plurality of divergent angle steels (4), the divergent angle steels (4) are provided with a plurality of divergent angle steels (4) and are arranged in parallel, a fixed assembly mechanism is arranged on the divergent angle steels (4), a dragging oil filling pipe assembly is also arranged on the divergent angle steels (4), one side of the divergent angle steels (4) is provided with a remote oil supply assembly which is connected to an oil supply warehouse, a singlechip system is arranged on the oil supply warehouse, the fixed assembly mechanism comprises a bearing flanging (404), the bearing flanging (404) and the divergent angle steels (4) are mutually perpendicular, a plurality of encircling brackets (401) are arranged on the side wall of the bearing flanging (404) back to the divergent angle steels (4), The top of surrounding support (401) is provided with mounting flange (402), mounting flange (402) passes through expansion bolts and building fixed connection, divergent angle steel (4) are in the underground tank, drag oil filler pipe subassembly including boat car (6), one side of boat car (6) is provided with four runner wheels (601), the material of runner wheels (601) is stainless steel material, the side wall swivelling joint of runner wheels (601) through thin pole (602) and boat car (6), the top of boat car (6) is provided with tortuous turn-ups (603), be provided with two lubricated rings (604) on tortuous turn-ups (603), the inboard activity of lubricated ring (604) alternates and has and drags flexible pipe (403), The top end of the dragging hose (403) is provided with an oil gun head (5), the remote oil supply assembly comprises a divergent pipeline (2), the divergent pipeline (2) is connected with an oil supply port of the dragging hose (403), the other port of the divergent pipeline (2) is provided with a three-way pipeline (3), the three-way pipelines (3) are connected in series through a plurality of interlink pipelines (1), the inner side of each interlink pipeline (1) is provided with a pressure sensor, the oil supply warehouse comprises an oil warehouse frame (7), the middle of the oil warehouse frame (7) is provided with a plurality of horizontal and vertical separation plates (701), the plurality of separation plates (701) are transversely and vertically staggered to form a containing cavity, An oil storage tank (702) is arranged in the accommodating cavity, a butt joint valve (703) is arranged at the opening of the oil storage tank (702), a movable oil pumping mechanism is arranged on one side of the oil storage frame (7), the movable oil pumping mechanism comprises a lifting rocker (9), the lifting rocker (9) is arranged on a vertical lifting assembly, two movable guide rods (901) are arranged on the side wall of the lifting rocker (9), a positioning slide block (902) is slidably arranged on the movable guide rods (901), a traversing plate block (903) is arranged on the side wall of the positioning slide block (902), an electric push rod (908) is arranged on the side wall of the traversing plate (903), The electric push rod (908) is fixedly connected with the side wall of the traversing plate (903) through the arch bridge bracket (904), an inserting steel pipe (909) is arranged at the output end of the electric push rod (908), one side of the inserting steel pipe (909) is communicated with an oil conveying hose (910), the other port of the oil conveying hose (910) is communicated with an oil pump, the oil pump is communicated with the port of the link pipeline (1), the oil conveying hose (910) is of a built-in spiral spring type, an inserting wire groove (10) matched with the inserting steel pipe (909) is arranged on the lifting rocker (9), a pushing shaft seat (905) is also arranged on the side wall of the lifting rocker (9), A propulsion motor (906) is arranged on the side wall of the propulsion shaft seat (905), a threaded rod (907) is arranged at the output end of the propulsion motor (906), and a nut block sleeved on the threaded rod (907) is arranged on the side wall of the transverse plate (903).
2. An airport aircraft fueling system as set forth in claim 1 wherein: the underground groove is a rectangular cavity below the airport concrete ground, and a wire groove opening is arranged between the rectangular cavity below the airport concrete ground and the ground surface.
3. An airport aircraft fueling system as set forth in claim 1 wherein: one side of diverging angle steel (4) back to bearing turn-ups (404) is provided with sagging turn-ups (405), and sagging turn-ups (405) crooked down, one side slope down of diverging angle steel (4) back to bearing turn-ups (404), and the turn-ups of sagging turn-ups (405) detain the lateral wall of post runner (601).
4. An airport aircraft fueling system as set forth in claim 1 wherein: the vertical lifting assembly comprises two vertical guide rails (8), the vertical guide rails (8) are fixed on the side walls of the oil depot frame (7), vertical sliding blocks (801) are slidably mounted on the vertical guide rails (8), lifting plate blocks (802) are arranged on the side walls of the vertical sliding blocks (801), the ends of lifting rocker plates (9) are fixed on the side walls of the lifting plate blocks (802), end plate blocks (803) are arranged at the upper end and the lower end of the vertical guide rails (8), carrying shaft seats (804) are fixedly mounted on the side walls of the end plate blocks (803), carrying rollers (805) are rotatably mounted on one side of each carrying shaft seat (804), the carrying rollers (805) are connected through carrying belts (806), the side walls of the lifting plate blocks (802) are fixedly connected with the carrying belts (806), one carrying roller (805) is mounted on the output end of a lifting motor (807), and the lifting motor (807) is fixed on the side walls of the carrying shaft seats (804).
5. An airport aircraft fueling system as set forth in claim 1 wherein: the singlechip system comprises a central processor, the central processor is connected with a plurality of oil supply pulse buttons, the oil supply pulse buttons are arranged on oil gun heads (5), the buttons are pressed down when the oil gun heads (5) start to supply oil, the central processor sends out signals to an oil pump, the oil pump starts to supply oil, if the oil pump simultaneously receives pulse signals of the N oil gun heads (5), the oil pump oil supply flow is improved by N times, and the oil gun heads (5) are placed in an underground cavity together with a dragging hose (403) after oil addition.
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| Application Number | Priority Date | Filing Date | Title |
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| CN202210883578.0A CN115158692B (en) | 2022-07-26 | 2022-07-26 | Airport aircraft refueling system |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210883578.0A CN115158692B (en) | 2022-07-26 | 2022-07-26 | Airport aircraft refueling system |
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| CN115158692A CN115158692A (en) | 2022-10-11 |
| CN115158692B true CN115158692B (en) | 2024-06-21 |
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Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113511624A (en) * | 2020-04-10 | 2021-10-19 | 中国石油化工股份有限公司 | Movable suspension type refueling system |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP3633419B2 (en) * | 2000-02-22 | 2005-03-30 | 株式会社タツノ・メカトロニクス | Automatic oiling device |
| US20070051852A1 (en) * | 2004-09-28 | 2007-03-08 | The Boeing Company | Operational ground support system having automated primary servicing |
| CN205366102U (en) * | 2015-08-14 | 2016-07-06 | 周麟璋 | Helidrome oiling system |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113511624A (en) * | 2020-04-10 | 2021-10-19 | 中国石油化工股份有限公司 | Movable suspension type refueling system |
Non-Patent Citations (1)
| Title |
|---|
| 机场恒压加油系统研究与设计;杜文奇;中国优秀硕士学位论文全文数据库 (工程科技Ⅱ辑);20180315;第C031-537页 * |
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