CN210149585U - Special equipment for emergency rescue aviation oil filling - Google Patents
Special equipment for emergency rescue aviation oil filling Download PDFInfo
- Publication number
- CN210149585U CN210149585U CN201920735323.3U CN201920735323U CN210149585U CN 210149585 U CN210149585 U CN 210149585U CN 201920735323 U CN201920735323 U CN 201920735323U CN 210149585 U CN210149585 U CN 210149585U
- Authority
- CN
- China
- Prior art keywords
- aviation
- valve
- communicated
- oil filling
- pipeline
- 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.)
- Active
Links
Images
Landscapes
- Loading And Unloading Of Fuel Tanks Or Ships (AREA)
Abstract
The utility model discloses an emergency rescue aviation oil filling professional equipment relates to aviation oil filling device field, the utility model discloses an aviation oil delivery connects, filtering separator, electronic fuel filler pump and nozzle, still include pressure fuel filler joint and provide the power supply unit of electric energy for electronic fuel filler pump. The aviation oil from the oil transport vehicle is connected with the aviation oil transportation joint through a rubber pipe, then enters the oiling pump, then enters the filtering separator, then enters the flow meter, then enters the oiling reel, then enters the oiling rubber pipe, then enters the oiling gun or the pressure oiling joint (a dead man controller is also arranged during pressure oiling), and then enters the aircraft oil tank. The utility model discloses under can solving current emergency rescue, relief disaster aviation oil guarantee mode effectively, the emergency guarantee's of aviation oil safety risk is big, refuel with high costs scheduling problem.
Description
Technical Field
The utility model relates to a boat oil filling technical field, more specifically relate to an emergent speedily carry out rescue work boat oil filling professional equipment.
Background
In recent years, various natural disasters and geological disasters are increasing, various helicopters are often required to be used for rescue, rescue and other work, and the traditional aviation fuel supply mode has many adverse factors such as high refueling cost and large safety risk. The development of the equipment is specially used for providing aviation oil guarantee for emergency rescue and disaster relief helicopters.
Under the traditional emergency rescue and disaster relief oil aviation support mode, an oil aviation support unit needs 5 vehicles such as a pickup truck, an oil truck, a tank type refueling truck, a crane and a large-scale platform trailer which are moved at one time. Because the tank type fuelling vehicle is a special vehicle for an airport, the tank type fuelling vehicle cannot run on the road, and can only work by using a crane and a large-scale platform trailer to pull to the site and hang down. 5 kinds of vehicles are moved at one time, so that various costs are greatly increased, and meanwhile, large-scale vehicles such as a flat car and a crane run on a rugged road for a long distance, so that the safety risk is great, and once a road accident occurs, the loss amount is huge.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a: under in order to solve current emergency rescue, relief of disaster aviation oil guarantee mode, the safety risk that current aviation oil guarantee mode exists is big, refuel with high costs scheduling problem, the utility model provides an emergency rescue aviation oil filling professional equipment.
The utility model discloses a realize above-mentioned purpose and specifically adopt following technical scheme:
the utility model provides an emergency rescue aviation oil filling professional equipment, aviation oil delivery connects, filtering separator, electronic fuel filler pump and nozzle, still includes pressure fuel filler joint and for the power supply unit that electronic fuel filler pump provided the electric energy. The aviation oil from the oil transportation vehicle is connected with the aviation oil transportation joint through a rubber pipe, then enters the oiling pump, then enters the filtering separator, then enters the flow meter, then enters the oiling reel, then enters the oiling rubber pipe, then enters the oiling gun or the pressure oiling joint, then enters the aircraft oil tank, and a dead man controller is also arranged during pressure oiling.
The working principle is as follows: the device is provided with two refueling modes of pressure refueling and gravity refueling so as to meet the refueling requirements of aircrafts with different aviation fuel refueling modes, and when the pressure refueling control valve is opened, aviation fuel at the outlet of the electric refueling pump is completely discharged from the pressure refueling joint, so that the aircraft needing pressure refueling can be quickly filled with fuel; when the gravity refueling control valve is started, in order to reduce the gravity refueling outlet pressure, the electric refueling pump bypass regulating valve is started, so that part of aviation fuel at the outlet of the electric refueling pump returns to the inlet of the electric refueling pump through the bypass where the regulating valve is located, and the aviation fuel flow speed and flow coming out of the final refueling gun meet the refueling demand of the gravity refueling aircraft. Simultaneously, the small-size, portable aviation oil filling equipment that this patent disclosed compares with traditional tank service truck or sled dress formula filling equipment, has many characteristics such as light in weight, with low costs, only need with ordinary light truck after simply fixing can, after arriving the scene, need not unload, directly be connected with the oil truck through aviation oil delivery joint with the rubber tube, rubber tube one end and aviation oil delivery joint switch-on, the rubber tube other end is connected with the oil-out of oil truck, just can refuel for the aircraft. Under the new guarantee mode, the oil service guarantee unit only need move 2 kinds of vehicles once only, only need promptly the oil truck with transport the vehicle of this equipment can, this equipment has directly replaced the function of crane, large-scale flatbed trailer, tank truck, pick-up car in traditional emergency rescue. The problems of high oiling cost and high safety risk are thoroughly solved.
Preferably, the fuel tank also comprises a filtering separator which can filter aviation fuel discharged by the electric fuel filling pump. The filter separator makes aviation fuel higher in purity when pouring into the aviation equipment into, has further ensured aviation fuel's quality.
Preferably, a differential pressure gauge is arranged between the inlet and the outlet of the filter separator, one end of the differential pressure gauge is communicated with the inlet of the filter separator through a pipeline, and the other end of the differential pressure gauge is communicated with the outlet of the filter separator through a pipeline.
Preferably, the filtering separator is connected with a closed-circuit sampler for collecting aviation fuel at a drain outlet, an inlet and an outlet of the filtering separator, and the closed-circuit sampler is connected with a waste fuel tank capable of collecting the aviation fuel discharged by the closed-circuit sampler.
Preferably, be connected with the larynx of moving away to avoid possible earthquakes on the filter, the one end and the filter export switch-on of larynx of moving away to avoid possible earthquakes, the other end and the import of electronic fuel pump of moving away to avoid possible earthquakes the larynx pass through the pipeline switch-on, move away to avoid possible earthquakes and be provided with the preceding manometer that can measure the aviation fuel pressure in the larynx of moving away to avoid possible earthquakes on the connecting tube of larynx and electronic fuel pump of moving away to avoid possible earthquakes, the exit of electronic fuel pump also is connected with the larynx of moving away to avoid possible.
Preferably, the inlet of the filtering separator is connected with a one-way valve which enables the aviation fuel to be communicated towards the inlet of the filtering separator in a one-way mode, the inlet end of the one-way valve is communicated with the liquid outlet end of the shock absorption throat through a pipeline, and the outlet end of the one-way valve is communicated with the inlet of the filtering separator through a pipeline.
Preferably, the oil gun is connected with an electro-hydraulic valve, one end of the electro-hydraulic valve is communicated with the oil gun through a pipeline, and the other end of the electro-hydraulic valve is communicated with an outlet of the filtering separator through a pipeline.
Preferably, a flow meter and a valve are arranged on a connecting pipeline of the electro-hydraulic valve and the filtering separator, one end of the flow meter is communicated with the electro-hydraulic valve, the other end of the flow meter is communicated with the valve, and the valve is communicated with an outlet of the filtering separator.
Preferably, an electro-hydraulic valve and a flow meter are arranged between the pressure oiling joint and the valve, one end of the electro-hydraulic valve is communicated with the pressure oiling joint through a pipeline, the other end of the electro-hydraulic valve is communicated with the flow meter, and the flow meter is communicated with an outlet of the valve.
Preferably, the device further comprises a refueling reel capable of receiving the pressure refueling joint and an aviation fuel refueling pipe connected to the refueling gun, and a grounding reel for preventing refueling static electricity.
The utility model has the advantages as follows:
1. the device is provided with two refueling modes of pressure refueling and gravity refueling so as to meet the refueling requirements of different aviation fuel refueling modes, and when the pressure refueling control valve is opened, aviation fuel at the outlet of the electric refueling pump is completely discharged from the pressure refueling joint, so that an aircraft needing pressure refueling can be quickly filled with fuel; when the gravity refueling control valve is started, in order to reduce the gravity refueling outlet pressure, the electric refueling pump bypass regulating valve is started, so that part of aviation fuel at the outlet of the electric refueling pump returns to the inlet of the electric refueling pump through the bypass where the regulating valve is located, and the aviation fuel flow speed and flow coming out of the final refueling gun meet the refueling demand of the gravity refueling aircraft.
2. The small-size, portable boat oil filling equipment that this patent discloses compares with traditional tank service truck or sled dress formula filling equipment, has many characteristics such as light in weight, with low costs, only need with ordinary light truck after simply fixed can, after reacing the scene, need not unload, directly pass through quick-operation joint with the oil truck with the rubber tube and be connected, rubber tube one end and quick-operation joint switch-on, the rubber tube other end is connected with the oil-out of oil truck, just can refuel for the helicopter. Under the new guarantee mode, the oil service guarantee unit only need move 2 kinds of vehicles once only, promptly only need oil truck and transport the vehicle of this equipment can, the efficiency of crane, large-scale flatbed trailer, tank truck, pick-up car in traditional emergency rescue has directly been replaced to this equipment. The problems of high oiling cost and high safety risk are thoroughly solved.
3. The filter separator makes aviation fuel higher in purity when pouring into the aviation equipment into, has further ensured aviation fuel's quality.
4. After the power supply device is arranged, aviation fuel oil filling work can be carried out in the field without power setting by the equipment, which is absent in the traditional aviation fuel oil filling equipment, so that the equipment is used for emergency rescue, is convenient to transport and economical and applicable, and the equipment can completely solve the condition of an external power supply if no power facility exists in the field of emergency rescue.
Drawings
FIG. 1 is a schematic diagram of the operation of the present invention;
fig. 2 is a schematic perspective view of the present invention;
fig. 3 is a side view of the present invention;
fig. 4 is a front view of the present invention.
Reference numerals: 1-aviation fuel delivery joint (1), 2-valve (2), 3-prefilter (3), 4-shock-absorbing throat (4), 5-front pressure gauge (5), 6-electric fuel pump (6), 7-one-way valve (7), 8-differential pressure gauge (8), 9-flow meter (9), 10-filtering separator (10), 11-electro-hydraulic valve (11), 12-fuel pipe reel (12), 13-pressure fuel filling joint (13), 14-fuel filling gun (14), 15-exhaust valve (15), 16-safety valve (16), 17-sight glass (17), 18-closed-circuit sampler (18), 19-waste fuel tank (19), 20-regulating valve (20), 21-reset valve (21), 22-generator (22), 23-distribution means (23), 24-electrostatic grounding reels (24), 25-base (25).
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are some, but not all, embodiments of the present invention. The components of embodiments of the present invention, as generally described and illustrated in the figures herein, may be arranged and designed in a wide variety of different configurations.
Thus, the following detailed description of the embodiments of the present invention, presented in the accompanying drawings, is not intended to limit the scope of the invention, as claimed, but is merely representative of selected embodiments of the invention. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts belong to the protection scope of the present invention.
It should be noted that: like reference numbers and letters refer to like items in the following figures, and thus, once an item is defined in one figure, it need not be further defined and explained in subsequent figures. Furthermore, the terms "first," "second," and the like are used merely to distinguish one description from another, and are not to be construed as indicating or implying relative importance.
In the description of the embodiments of the present invention, it should be noted that the terms "inside", "outside", "up", and the like indicate the directions or positional relationships based on the directions or positional relationships shown in the drawings, or the directions or positional relationships that the products of the present invention are conventionally placed when used, and are only for convenience of describing the present invention and simplifying the description, but do not indicate or imply that the device or element to which the term refers must have a specific direction, be constructed and operated in a specific direction, and thus, should not be construed as limiting the present invention.
Example 1
As shown in fig. 1 to 4, the embodiment provides a special emergency rescue aviation fuel filling device, which includes an aviation fuel delivery connector 1, a pre-filter 3, an electric fuel filler pump 6 and a fuel filler gun 14, wherein the aviation fuel delivery connector 1 is communicated with the pre-filter 3 through a pipeline, the pre-filter 3 is communicated with an inlet of the electric fuel filler pump 6 through a pipeline, and an outlet of the electric fuel filler pump 6 is communicated with the fuel filler gun 14 through a pipeline; still include pressure and refuel joint 13 and for the power supply unit that electric tank filler pump 6 provided the electric energy, be connected with valve 2 on the pressure refuel joint 13, the one end of valve 2 pressure refuel joint 13 passes through the pipeline switch-on, and the other end of valve 2 passes through the pipeline switch-on with the export of electric tank filler pump 6, be connected with governing valve 20 on the electric tank filler pump 6, the pipeline switch-on is passed through with the import of electric tank filler pump 6 to the one end of governing valve 20, and the pipeline switch-on is passed through with the export of electric tank filler pump 6 to the other end of governing valve. The oil gun 14 is communicated with the outlet of the electric oil filling pump 6 through a pipeline, in order to facilitate the oil filling of the switching oil gun 14 and the oil filling of the pressure oil filling joint 13, in the prior art, a valve 2 is arranged on a connecting pipeline between the oil gun 14 and the outlet of the electric oil filling pump 6, one end of the valve 2 connected with the oil gun 14 is communicated with the oil gun 14 through a pipeline, and the other end of the valve 2 connected with the oil gun 14 is communicated with the outlet of the electric oil filling pump 6 through a pipeline.
The power supply device comprises a generator 22 and a power distribution device 23 for applying the electric energy generated by the generator 22 to the electric energy required by the electric gasoline pump 6, after the power supply device is arranged, the device can carry out aviation fuel oil filling work in the field without power setting, which is not available in the traditional aviation fuel oil filling device, so that the device is convenient to transport and economical and applicable to emergency situations, and if no power facility is available on the site of the emergency, the device can completely solve the situation without an external power supply.
Specifically, the electric oiling pump 6 and the power supply device in the equipment are both arranged on the base 25, so that the parts of the device can be integrated, and the device is more convenient and fast in the carrying process.
Because this equipment has set up two kinds of modes of refueling of pressure refueling and gravity refueling, in order to satisfy the refuel demand of the aircraft of different aviation fuel filling modes, close when governing valve 20, the aviation fuel of 6 exports of its electronic fuel filler pump is whole to be discharged from pressure refueling joint 13, let the aircraft that needs pressure refueling can fill up oil fast, when governing valve 20 part is opened, the part aviation fuel of 6 exports of electronic fuel filler pump will get back to 6 entrances of electronic fuel filler pump through governing valve 20 place pipeline, let final fuel filling gun 14 play the aviation fuel velocity and the flow satisfies gravity refueling aircraft and refuels the demand. Simultaneously, the small-size, portable aviation oil filling equipment that this patent disclosed compares with traditional tank service truck or sled dress formula filling equipment, has many characteristics such as light in weight, with low costs, only need with ordinary light truck after simply fixing can, after arriving the scene, need not unload, directly be connected with the oil truck through aviation oil delivery joint 1 with the rubber tube, rubber tube one end and aviation joint 1 switch-on, the rubber tube other end is connected with the oil-out of oil truck, just can refuel for the aircraft. Under the new guarantee mode, the oil supply guarantee unit only needs to move 2 kinds of vehicles once only, namely only needs the oil truck and the vehicle transporting the equipment, and the equipment directly replaces the effects of a crane, a large-scale platform trailer, a tank type refueling truck and a pick-up truck in the traditional emergency rescue. The problems of high oiling cost and high safety risk are thoroughly solved.
Example 2
As shown in fig. 1 to 4, the embodiment provides a special emergency rescue aviation fuel filling device, which includes an aviation fuel delivery connector 1, a pre-filter 3, an electric fuel filler pump 6 and a fuel filler gun 14, wherein the aviation fuel delivery connector 1 is communicated with the pre-filter 3 through a pipeline, the pre-filter 3 is communicated with an inlet of the electric fuel filler pump 6 through a pipeline, and an outlet of the electric fuel filler pump 6 is communicated with the fuel filler gun 14 through a pipeline; still include pressure and refuel joint 13 and for the power supply unit that electric tank filler pump 6 provided the electric energy, be connected with valve 2 on the pressure refuel joint 13, the one end of valve 2 pressure refuel joint 13 passes through the pipeline switch-on, and the other end of valve 2 passes through the pipeline switch-on with the export of electric tank filler pump 6, be connected with governing valve 20 on the electric tank filler pump 6, the pipeline switch-on is passed through with the import of electric tank filler pump 6 to the one end of governing valve 20, and the pipeline switch-on is passed through with the export of electric tank filler pump 6 to the other end of governing valve. The fuel nozzle 14 is connected to the outlet of the electric fuel pump 6 through a pipe, and in order to facilitate switching between the fuel filling of the fuel nozzle 14 and the filling of the pressurized fuel connector 13, in the prior art, a valve 2 is provided on a connection pipe between the fuel nozzle 14 and the outlet of the electric fuel pump 6, one end of the valve 2 connected to the fuel nozzle 14 is connected to the fuel nozzle 14 through a pipe, and the other end of the valve 2 connected to the fuel nozzle 14 is connected to the outlet of the electric fuel pump 6 through a pipe.
The power supply device comprises a generator 22 and a power distribution device 23 for applying the electric energy generated by the generator 22 to the electric energy required by the electric gasoline pump 6, after the power supply device is arranged, the device can carry out aviation fuel oil filling work in the field without power setting, which is not available in the traditional aviation fuel oil filling device, so that the device is convenient to transport and economical and applicable to emergency situations, and if no power facility is available on the site of the emergency, the device can completely solve the situation without an external power supply.
Specifically, electric petrol pump 6 and power supply unit in this equipment all set up on base 25, let the part of this device can integrate, and is more convenient in handling. A filtering separator 10 is also provided which is able to filter the aviation fuel discharged by the electric petrol pump 6. The filter separator 10 enables the purity of the aviation fuel to be higher when the aviation fuel is injected into aviation equipment, and the quality of the aviation fuel is further guaranteed. A differential pressure meter 8 is arranged between the inlet and the outlet of the filter separator 10, one end of the differential pressure meter 8 is communicated with the inlet of the filter separator 10 through a pipeline, and the other end of the differential pressure meter 8 is communicated with the outlet of the filter separator 10 through a pipeline. The filtering separator 10 is connected with a closed-circuit sampler 18 for collecting aviation fuel at a drain outlet, an inlet and an outlet of the filtering separator 10, and the closed-circuit sampler 18 is connected with a waste fuel tank 19 capable of collecting the aviation fuel discharged by the closed-circuit sampler 18. The inlet of the filtering separator 10 is connected with a one-way valve 7 which enables the aviation fuel to be communicated towards the inlet of the filtering separator 10 in a one-way mode, the inlet end of the one-way valve 7 is communicated with the liquid outlet end of the shock absorption throat 4 through a pipeline, and the outlet end of the one-way valve 7 is communicated with the inlet of the filtering separator 10 through a pipeline.
The inlet end of the closed-circuit sampler 18 is communicated with the sewage draining port, the outlet and the inlet of the filtering separator 10 through pipelines respectively, meanwhile, the closed-circuit sampler 18 is communicated with the sewage draining port, the outlet and the inlet of the filtering separator 10 through the valves 2 on connecting pipelines respectively, one end of the reset valve 21 is communicated with the sewage draining port through a pipeline, the other end of the reset valve 21 is communicated with the valves 2 on the connecting pipelines of the closed-circuit sampler 18 and the sewage draining port of the filtering separator 10, the exhaust port of the filtering separator 10 is provided with an exhaust valve 15, the safety valve interface of the filtering separator 10 is provided with a safety valve 16, one end of the safety valve 16 is connected with the filtering separator 10, the other end of the safety valve is provided with a sight glass 17, the sight glass 17 is communicated with.
Example 3
As shown in fig. 1 to 4, the embodiment provides a special emergency rescue aviation fuel filling device, which includes an aviation fuel delivery connector 1, a pre-filter 3, an electric fuel filler pump 6 and a fuel filler gun 14, wherein the aviation fuel delivery connector 1 is communicated with the pre-filter 3 through a pipeline, the pre-filter 3 is communicated with an inlet of the electric fuel filler pump 6 through a pipeline, and an outlet of the electric fuel filler pump 6 is communicated with the fuel filler gun 14 through a pipeline; still include pressure and refuel joint 13 and for the power supply unit that electric tank filler pump 6 provided the electric energy, be connected with valve 2 on the pressure refuel joint 13, the one end of valve 2 pressure refuel joint 13 passes through the pipeline switch-on, and the other end of valve 2 passes through the pipeline switch-on with the export of electric tank filler pump 6, be connected with governing valve 20 on the electric tank filler pump 6, the pipeline switch-on is passed through with the import of electric tank filler pump 6 to the one end of governing valve 20, and the pipeline switch-on is passed through with the export of electric tank filler pump 6 to the other end of governing valve. The oil gun 14 is communicated with the outlet of the electric oil filling pump 6 through a pipeline, in order to facilitate the oil filling of the switching oil gun 14 and the oil filling of the pressure oil filling joint 13, in the prior art, a valve 2 is arranged on a connecting pipeline between the oil gun 14 and the outlet of the electric oil filling pump 6, one end of the valve 2 connected with the oil gun 14 is communicated with the oil gun 14 through a pipeline, and the other end of the valve 2 connected with the oil gun 14 is communicated with the outlet of the electric oil filling pump 6 through a pipeline.
The power supply device comprises a generator 22 and a power distribution device 23 for applying the electric energy generated by the generator 22 to the electric energy required by the electric gasoline pump 6, after the power supply device is arranged, the device can carry out aviation fuel oil filling work in the field without power setting, which is not available in the traditional aviation fuel oil filling device, so that the device is convenient to transport and economical and applicable to emergency situations, and if no power facility is available on the site of the emergency, the device can completely solve the situation without an external power supply.
The one end of throat 4 of moving away to avoid possible earthquakes and the 3 export switch-ons of prefilter, the other end of throat 4 of moving away to avoid possible earthquakes passes through the pipeline switch-on with the import of electronic fuel filler pump 6, be provided with the preceding manometer 5 that can measure the aviation fuel pressure in the throat 4 of moving away to avoid possible earthquakes on the connecting tube of throat 4 of moving away to avoid possible earthquakes and electronic fuel filler pump 6, the exit of electronic fuel filler pump 6 also is connected with throat 4 of moving away to avoid possible earthquakes, the one end of throat 4 of moving away to avoid possible earthquakes and the.
One end of the electro-hydraulic valve 11 is communicated with the oil filling gun 14 through a pipeline, and the other end of the electro-hydraulic valve 11 is communicated with the outlet of the filtering separator 10 through a pipeline. A flow meter 9 and a valve 2 are arranged on a connecting pipeline of the electro-hydraulic valve 11 and the filtering separator 10, one end of the flow meter 9 is communicated with the electro-hydraulic valve 11, the other end of the flow meter 9 is communicated with the valve 2, and the valve 2 is communicated with an outlet of the filtering separator 10.
One end of the electro-hydraulic valve 11 is communicated with the pressure oiling joint 13 through a pipeline, the other end of the electro-hydraulic valve 11 is communicated with the flow meter 9, and the flow meter 9 is communicated with the outlet of the valve 2.
The equipment is also provided with a refueling reel 12 which can accommodate an aviation fuel refueling pipe connected with the pressure refueling joint 13 and the refueling gun 14, and an electrostatic grounding reel 24 for preventing refueling static electricity.
The refuel reel 12, the filter separator 10, the power distribution device 23, the electric refuel pump 6, the ground wire coil 24, the waste oil tank 19, the closed circuit sampler 18 and the generator 22 are all fixedly arranged on a base 25.
Claims (10)
1. The emergency rescue aviation oil filling special equipment comprises an aviation oil delivery joint (1), a prefilter (3) and an electric oil filling pump (6) oil filling gun (14), wherein the aviation oil delivery joint (1) is communicated with the prefilter (3) through a pipeline, the prefilter (3) is communicated with an inlet of the electric oil filling pump (6) through a pipeline, and an outlet of the electric oil filling pump (6) is communicated with the oil filling gun (14) through a pipeline; the method is characterized in that: still include pressure and refuel joint (13) and for the power supply unit that electric gasoline pump (6) provided the electric energy, be connected with valve (2) on pressure refuel joint (13), the one end of valve (2) pressure refuel joint (13) are through the pipeline switch-on, and the other end of valve (2) passes through the pipeline switch-on with the export of electric gasoline pump (6), be connected with governing valve (20) on electric gasoline pump (6), the pipeline switch-on is passed through with the import of electric gasoline pump (6) to the one end of governing valve (20), and the other end of governing valve (20) passes through the pipeline switch-on with the export of electric gasoline pump (6).
2. The special emergency rescue aviation oil filling equipment according to claim 1, characterized in that: the aircraft fuel filter also comprises a filtering separator (10) capable of filtering the aircraft fuel discharged by the electric fuel filling pump (6).
3. The special emergency rescue aviation oil filling equipment according to claim 2, characterized in that: a differential pressure meter (8) is arranged between an inlet and an outlet of the filtering separator (10), one end of the differential pressure meter (8) is communicated with the inlet of the filtering separator (10) through a pipeline, and the other end of the differential pressure meter (8) is communicated with the outlet of the filtering separator (10) through a pipeline.
4. The special emergency rescue aviation oil filling equipment according to claim 2, characterized in that: the aviation fuel oil closed-circuit sampler is characterized in that the filtering separator (10) is connected with a closed-circuit sampler (18) for collecting aviation fuel oil at a drain outlet, an inlet and an outlet of the filtering separator (10), and the closed-circuit sampler (18) is connected with a waste oil tank (19) capable of collecting the aviation fuel oil discharged by the closed-circuit sampler (18).
5. The special emergency rescue aviation oil filling equipment according to claim 2, characterized in that: be connected with throat (4) of moving away to avoid possible earthquakes on prefilter (3), the one end and the filter (3) export switch-on of throat (4) of moving away to avoid possible earthquakes, the other end of throat (4) of moving away to avoid possible earthquakes passes through the pipeline switch-on with the import of electronic fuel filler pump (6), be provided with preceding manometer (5) that can measure the aviation fuel pressure in throat (4) of moving away to avoid possible earthquakes on the connecting tube of throat (4) of moving away to avoid possible earthquakes and electronic fuel filler pump (6), the exit of electronic fuel filler pump (6) also is connected with throat (4) of moving away to avoid possible earthquakes, the one end of throat (4) of moving away to avoid possible earthquakes passes through.
6. The special emergency rescue aviation oil filling equipment according to claim 5, characterized in that: the inlet of the filtering separator (10) is connected with a one-way valve (7) which enables the aviation fuel to be communicated towards the inlet of the filtering separator (10) in a one-way mode, the inlet end of the one-way valve (7) is communicated with the liquid outlet end of the vibrating throat (4) through a pipeline, and the outlet end of the one-way valve (7) is communicated with the inlet of the filtering separator (10) through a pipeline.
7. The special emergency rescue aviation oil filling equipment according to claim 2, characterized in that: the oil gun (14) is connected with an electro-hydraulic valve (11), one end of the electro-hydraulic valve (11) is communicated with the oil gun (14) through a pipeline, and the other end of the electro-hydraulic valve (11) is communicated with an outlet of the filtering separator (10) through a pipeline.
8. The special emergency rescue aviation oil filling equipment according to claim 7, characterized in that: a flow meter (9) and a valve (2) are arranged on a connecting pipeline of the electro-hydraulic valve (11) and the filtering separator (10), one end of the flow meter (9) is communicated with the electro-hydraulic valve (11), the other end of the flow meter (9) is communicated with the valve (2), and the valve (2) is communicated with an outlet of the filtering separator (10).
9. The special emergency rescue aviation oil filling equipment according to claim 2, characterized in that: an electro-hydraulic valve (11) and a flow meter (9) are arranged between the pressure oiling joint (13) and the valve (2), one end of the electro-hydraulic valve (11) is communicated with the pressure oiling joint (13) through a pipeline, the other end of the electro-hydraulic valve (11) is communicated with the flow meter (9), and the flow meter (9) is communicated with an outlet of the valve (2).
10. The special emergency rescue aviation oil filling equipment according to claim 1, characterized in that: the device also comprises an oil filling pipe reel (12) which can accommodate an aviation fuel oil filling pipe connected with the pressure oil filling joint (13) and the oil filling gun (14), and a grounding wire coil (24) which can prevent oil filling static electricity.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920735323.3U CN210149585U (en) | 2019-05-22 | 2019-05-22 | Special equipment for emergency rescue aviation oil filling |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920735323.3U CN210149585U (en) | 2019-05-22 | 2019-05-22 | Special equipment for emergency rescue aviation oil filling |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210149585U true CN210149585U (en) | 2020-03-17 |
Family
ID=69759906
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920735323.3U Active CN210149585U (en) | 2019-05-22 | 2019-05-22 | Special equipment for emergency rescue aviation oil filling |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210149585U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113859342A (en) * | 2021-12-07 | 2021-12-31 | 海丰通航科技有限公司 | Intermediate device for jet fuel transfer |
-
2019
- 2019-05-22 CN CN201920735323.3U patent/CN210149585U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113859342A (en) * | 2021-12-07 | 2021-12-31 | 海丰通航科技有限公司 | Intermediate device for jet fuel transfer |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN208086038U (en) | A kind of large aircraft pot type tank service truck | |
| CN201012647Y (en) | Small-sized fuel oil dispensing vehicle | |
| CN103440962B (en) | Transformer on-line intelligence repairing car and oil supplement method | |
| CN210149585U (en) | Special equipment for emergency rescue aviation oil filling | |
| CN214057913U (en) | Device for oil mixing between airplanes | |
| CN206188377U (en) | A small -size refueling equipment for general aviation | |
| CN105366070B (en) | A kind of aircraft floor lubricating oil pressure refueling device | |
| CN105435400A (en) | Light high-mobility long-distance water supply fire-fighting method and system | |
| CN203681880U (en) | Comprehensive aircraft ground service insurance system | |
| CN103818562B (en) | Airplane ground service integrated support system | |
| CN106364692B (en) | A kind of unmanned plane tank service truck and its working method | |
| CN201002967Y (en) | Jet fuel integration filling device | |
| CN205933200U (en) | Novel integration of on -board helicopter is refueled device | |
| CN213443139U (en) | Portable aviation hydraulic oil filling device | |
| CN105775155A (en) | Gravity refueling type multifunctional integrated aviation oil filling device | |
| CN206969002U (en) | A kind of unpowered multiplex roles refueling device | |
| CN206298340U (en) | A kind of oil pumping system for baby plane pot type tank service truck | |
| CN215516644U (en) | Movable container stores up filling equipment | |
| CN109911238B (en) | Method for refueling seaplane | |
| CN202557383U (en) | Aviation kerosene transfer vehicle | |
| CN210424472U (en) | Infusion system between LNG ship and LNG tank box (or tank car) | |
| CN211731853U (en) | Oil circuit control system of unmanned aerial vehicle oil pumping vehicle for aviation | |
| CN207811250U (en) | One kind can utilize the unpowered refueling device of pipeline pressure | |
| CN112455703B (en) | Device and method for mixing oil between airplanes | |
| CN204029264U (en) | Bulk petroleum railway is unloaded operation analog training device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |