CN110498057A - Polar region helicopter jet fuel fuel loading system peculiar to vessel - Google Patents
Polar region helicopter jet fuel fuel loading system peculiar to vessel Download PDFInfo
- Publication number
- CN110498057A CN110498057A CN201910807435.XA CN201910807435A CN110498057A CN 110498057 A CN110498057 A CN 110498057A CN 201910807435 A CN201910807435 A CN 201910807435A CN 110498057 A CN110498057 A CN 110498057A
- Authority
- CN
- China
- Prior art keywords
- cabin
- oil
- pipe
- valve
- kerosene
- 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
Links
- 239000000446 fuel Substances 0.000 title claims abstract description 51
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims abstract description 50
- 239000003350 kerosene Substances 0.000 claims abstract description 48
- 229910052757 nitrogen Inorganic materials 0.000 claims abstract description 25
- 230000005389 magnetism Effects 0.000 claims description 13
- 238000010438 heat treatment Methods 0.000 claims description 10
- 239000007858 starting material Substances 0.000 claims description 8
- 238000005485 electric heating Methods 0.000 claims description 7
- 238000009413 insulation Methods 0.000 claims description 5
- 239000007789 gas Substances 0.000 claims description 3
- 230000008676 import Effects 0.000 claims description 3
- 238000001914 filtration Methods 0.000 claims 1
- 238000009738 saturating Methods 0.000 claims 1
- 238000009434 installation Methods 0.000 abstract description 6
- 238000013461 design Methods 0.000 abstract description 3
- 239000003921 oil Substances 0.000 description 28
- 108010066057 cabin-1 Proteins 0.000 description 13
- 238000003860 storage Methods 0.000 description 4
- 239000000295 fuel oil Substances 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000011160 research Methods 0.000 description 3
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 2
- 238000004891 communication Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 239000006249 magnetic particle Substances 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 239000001301 oxygen Substances 0.000 description 2
- 229910052760 oxygen Inorganic materials 0.000 description 2
- 230000002093 peripheral effect Effects 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 239000004793 Polystyrene Substances 0.000 description 1
- 238000004220 aggregation Methods 0.000 description 1
- 230000002776 aggregation Effects 0.000 description 1
- WMGSQTMJHBYJMQ-UHFFFAOYSA-N aluminum;magnesium;silicate Chemical compound [Mg+2].[Al+3].[O-][Si]([O-])([O-])[O-] WMGSQTMJHBYJMQ-UHFFFAOYSA-N 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 239000003245 coal Substances 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 238000010891 electric arc Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 239000002828 fuel tank Substances 0.000 description 1
- 229910052736 halogen Inorganic materials 0.000 description 1
- 150000002367 halogens Chemical class 0.000 description 1
- 229920001903 high density polyethylene Polymers 0.000 description 1
- 239000004700 high-density polyethylene Substances 0.000 description 1
- 239000011810 insulating material Substances 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 239000011490 mineral wool Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 description 1
- 229920006389 polyphenyl polymer Polymers 0.000 description 1
- 229920002223 polystyrene Polymers 0.000 description 1
- 238000004321 preservation Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B17/00—Vessels parts, details, or accessories, not otherwise provided for
- B63B17/0027—Tanks for fuel or the like ; Accessories therefor, e.g. tank filler caps
-
- 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
Abstract
The invention discloses a kind of polar region helicopter jet fuel fuel loading systems peculiar to vessel, comprising: boat kerosene cabin；Back-fire relief Ventilated cap, with boat kerosene cabin by flanged joint or threaded connection, the top in boat kerosene cabin is arranged in back-fire relief Ventilated cap；Nitrogen fills inerting unit, is connect with boat kerosene cabin by the first valve and first pipe；Oil-immersed pump is connect with boat kerosene cabin by the second valve and second pipe；Refueling device is connect with oil-immersed pump by third valve and third pipeline；Control device is connect with nitrogen filling inerting unit, the first valve, oil-immersed pump, the second valve, third valve and refueling device.The kerosene cabin outfit nitrogen that navigates fills inerting unit, and oil plant memory capacity is big, and cargo tank is highly-safe.System equipment uses distributing layout design, flexible for installation, is suitble to complicated Ship Structure.
Description
Technical field
The present invention relates to fueling facility technical fields, and in particular to a kind of polar region helicopter jet fuel oiling peculiar to vessel system
System.
Background technique
Polar science investigation is the embodiment of a national overall national strength, is paid much attention to all the time by countries in the world；Pole
Ground scientific surveying ship is the significant capability support carrying out polar science and investigating, and investigates ability and range to expand polar ocean,
Helicopter is commonly equipped on polar science research ship, and in order to increase the job area of helicopter and ensure the activity duration, just
It needs to be equipped with helicopter jet fuel fuel loading system on polar science research ship.
Current integrated fueling facility, including mobile oil storage tank, tank entities, pump unit, refueling device.Mobile oil storage tank
And refueling device is integral device；Tank entities and pump unit are fixed on the same pedestal, constitute an integral device；Storage tank
Unit is connect with pump unit by hose；Pump unit is connect with refueling device by hard tube.It is gone straight up to though the facility can be used for sea
Machine fuel supply, but that there are fuel levels is small, integral installation requirement is high, fueling operation is single, can not adapt to polar region environment etc. asks
Topic, thus it is not used to polar ship helicopter fuel supply.
For this reason, it is necessary to research and develop a oil reserve polar ship that is big, highly-safe, flexible for installation, adapting to polar region condition
Helicopter jet fuel fuel loading system.
Summary of the invention
In view of this, the embodiment of the invention provides a kind of polar region helicopter jet fuel fuel loading system peculiar to vessel, to solve
That there are fuel levels is small, integral installation requirement is high, fueling operation is single, can not adapt to polar region for polar region fueling facility in the prior art
The problem of environment.
The embodiment of the invention provides a kind of polar region helicopter jet fuel fuel loading systems peculiar to vessel, comprising:
Boat kerosene cabin；
Back-fire relief Ventilated cap, with boat kerosene cabin by flanged joint or threaded connection, the upper of boat kerosene cabin is arranged in back-fire relief Ventilated cap
Side；
Nitrogen fills inerting unit, is connect with boat kerosene cabin by the first valve and first pipe；
Oil-immersed pump is connect with boat kerosene cabin by the second valve and second pipe；
Refueling device is connect with oil-immersed pump by third valve and third pipeline；
Control device, with nitrogen filling inerting unit, the first valve, oil-immersed pump, the second valve, third valve and refueling device
Connection.
Optionally, first pipe, second pipe, third pipeline are 316L double-wall pipe.
Optionally, further includes: heating module is laid on first pipe, second pipe, third pipeline external；
Thermal insulation layer is covered on outside heating module.
Optionally, back-fire relief Ventilated cap is electric heating back-fire relief Ventilated cap.
Optionally, refueling device include: filter separator, flow sensor, pressure sensor, the phasmajector that disappears, refuel it is soft
Pipe and reel.
Optionally, further includes: magnetic starter is connect with oil-immersed pump.
Optionally, further includes: display screen and microprocessor, multiple input serial ports and nitrogen the filling inerting dress of microprocessor
It sets, filter separator, flow sensor are connected with the output end of pressure sensor；The output serial ports and display screen of microprocessor
Input terminal connection.
Optionally, kerosene cabin, nitrogen filling inerting unit and oil-immersed pump are navigated in ship lower decks；
Refueling device aboard ship deck, and around helicopter deck；
Magnetic starter and oil-immersed pump are in same cabin；
Display screen and refueling device are in same cabin.
Optionally, further includes: oil return pipe, one terminate at the oil return nozzle of refueling device, and the another of oil return pipe terminates at
The oil return import in boat kerosene cabin.
Optionally, further includes:
Three-way pipeline, first interface and second pipe connects close to the one end in boat kerosene cabin, the second interface of three-way pipeline and
Second pipe is connected close to one end of oil-immersed pump, and the third interface and closed conduct of three-way pipeline pass through flanged joint；
Three-way pipeline is arranged in close to the interface in boat kerosene cabin in soft magnetism disk；There are several through-holes on soft magnetism disk；Soft magnetism circle
The outer diameter of disk is equal to the internal diameter of second pipe；
Permanent magnet is arranged in three-way pipeline closed conduct；
Three electromagnet are circumferentially positioned at outside second pipe corresponding with soft magnetism disk with 120 °.
The embodiment of the present invention the utility model has the advantages that
1, boat kerosene cabin is equipped with nitrogen and fills inerting unit, and oil plant memory capacity is big, and cargo tank is highly-safe.System equipment, which uses, to be divided
Formula layout design is dissipated, it is flexible for installation, it is suitble to complicated Ship Structure.
2, oil pump can local and long-range start-up and shut-down control, ensure that safety and the convenience of operation.
3, boat kerosene cabin uses electric heating Ventilated cap, and pipeline is using 316L double-wall pipe and with heating device, it is ensured that is
System adapts to polar region working environment.
Detailed description of the invention
The features and advantages of the present invention will be more clearly understood by referring to the accompanying drawings, and attached drawing is schematically without that should manage
Solution is carries out any restrictions to the present invention, in the accompanying drawings:
Fig. 1 shows a kind of structure chart of polar region helicopter jet fuel fuel loading system peculiar to vessel in the embodiment of the present invention；
Fig. 2 shows a kind of three-way pipeline knots of polar region helicopter jet fuel fuel loading system peculiar to vessel a kind of in the embodiment of the present invention
Composition；
Fig. 3 shows a kind of another three-way pipeline of polar region helicopter jet fuel fuel loading system peculiar to vessel in the embodiment of the present invention
Structure chart.
Specific embodiment
In order to make the object, technical scheme and advantages of the embodiment of the invention clearer, below in conjunction with the embodiment of the present invention
In attached drawing, technical scheme in the embodiment of the invention is clearly and completely described, it is clear that described embodiment is
A part of the embodiment of the present invention, instead of all the embodiments.Based on the embodiments of the present invention, those skilled in the art are not having
Every other embodiment obtained under the premise of creative work is made, shall fall within the protection scope of the present invention.
The embodiment of the invention provides a kind of polar region helicopter jet fuel fuel loading systems peculiar to vessel, as shown in Figure 1, comprising:
Navigate kerosene cabin 1, back-fire relief Ventilated cap 2, nitrogen filling inerting unit 3, oil-immersed pump 4, refueling device 5 and control device 6, in which: resistance
For fiery Ventilated cap 2 with boat kerosene cabin 1 by flanged joint or threaded connection, the top in boat kerosene cabin 1 is arranged in back-fire relief Ventilated cap 2；
Nitrogen fills inerting unit 3 and is connect with boat kerosene cabin 1 by the first valve and first pipe 101；Oil-immersed pump 4 and boat kerosene cabin
1 is connected by the second valve and second pipe 102；Refueling device 5 and oil-immersed pump 4 pass through third valve and third pipeline
103 connections；Control device 6 and nitrogen fill inerting unit 3, the first valve, oil-immersed pump, the second valve, third valve and add
Oily device connection.
In the present embodiment, boat kerosene cabin 1 is a part of cabin structure, is not necessarily to peripheral hardware oil storage tank.
Control device 6 is computer or other terminals with processing capacity, with each valve by wired or wireless connection,
It controls nitrogen filling inerting system and nitrogen is filled to boat kerosene cabin, the oxygen content navigated in kerosene cabin is made to maintain 5% hereinafter, guaranteeing
The boat safe inerting of kerosene cabin upper gas；And by Local or Remote start-up and shut-down control, can ensure that the safety of operation with
Convenience.6 conventional func of control device is only used in the present embodiment, the start-up and shut-down control to equipment is realized, to control device 6
Model parameter of itself etc. does not specially require, only need to be using control module conventional in the prior art in specific implementation process
It can be realized.
As optional embodiment, first pipe, second pipe, third pipeline are 316L double-wall pipe.
In the present embodiment, 316L double-wall pipe has good pitting corrosion resistant performance, can safety be applied to containing the halogen such as Cl
Plain ionic environment；Hot cracking tendency when welding can be reduced simultaneously.
As optional embodiment, further includes: heating module is laid on first pipe, second pipe, outside third pipeline
Portion；Thermal insulation layer is covered on outside heating module.Pipeline is using 316L double-wall pipe and with heating device, it is ensured that system adapts to
Polar region working environment.
In the present embodiment, HDPE double-wall pipe pipeline may not rupture in -60 DEG C of environment, polar region environment temperature pole
Low, setting heating module makes double-wall pipe temperature be maintained at -60 DEG C or more, ruptures it not, improves use reliability；Thermal insulation layer material
Material selects vacuum heat-insulating plate, aeroge, polyurathamc, extruded polystyrene board, expansion polyphenyl plate, rock wool board or composite aluminium-magnesium-silicate
Heat-insulating material, so as to improve heat preservation and insulation.
As optional embodiment, back-fire relief Ventilated cap 2 is electric heating back-fire relief Ventilated cap.
In the present embodiment, electric heating Ventilated cap is used to adapt to the cold environment of polar region, so that they can work normally.Electricity adds
Thermal resistance fire Ventilated cap maintains the pressure difference of ambient pressure in boat kerosene cabin 1, passes through the inerting inside the positive pressure maintenance in boat kerosene cabin 1
State, while keeping air hole not to be frozen by heating.Kerosene cabin navigate using electric heating Ventilated cap, it is ensured that system adapts to pole
Ground working environment.
As optional embodiment, refueling device 5 includes: filter separator, flow sensor, pressure sensor, disappears
Phasmajector, refueling hose and reel.
In the present embodiment, filter separator is for purifying fuel oil, flow sensor and pressure sensor for measuring combustion
The model parameter of the flow and pressure of oil, flow sensor and pressure sensor does not also specially require, and adopts in the technical program
It is its conventional func and connection type；The phasmajector that disappears is mounted on the export pipeline of filter, with eliminate due to oil liquid with
The mutual friction area of filter element increases and a large amount of electrostatic of aggregation, avoids the occurrence of fire caused by electrostatic spark；Add
Oily hose and reel connect the oil outlet in refueling device, for being connected to the fuel tank of helicopter.
As optional embodiment, further includes: magnetic starter 7 is connect with oil-immersed pump 4.
In the present embodiment, operator carries out start and stop to the oil pump in pump oil unit 4 by operation magnetic starter
Control.
As optional embodiment, further includes: display screen and microprocessor, the multiple input serial ports and nitrogen of microprocessor
Gas filling inerting unit, filter separator, flow sensor are connected with the output end of pressure sensor；The output string of microprocessor
Mouth is connect with the input terminal of display screen.
In the present embodiment, microprocessor for acquire nitrogen filling inerting unit, filter separator, flow sensor and
Pressure sensor state information parameters calculate for example, acquisition nitrogen filling inerting unit releases the flow of nitrogen and release boat kerosene
Nitrogen accounting in cabin and refueling device, to extrapolate oxygen accounting；The filter differential pressure of acquisition filter separator and combustion
Throughput information is expected, to judge whether filter separator works normally；The output of flow sensor is acquired, real time monitoring is refueled
Fuel flow in the process；The bottommost of refueling device is arranged in pressure sensor, for system pressure in signal piping, prevents
Line end superpressure, the fuel oil differential pressure for preventing supply from going straight up to sump are excessive.
Display screen is used to show the information parameter of each sensor in nitrogen filling inerting system and refueling device.Specific real
It applies in example, display screen is touch screen, or in addition configures the input equipments such as keyboard, mouse, and operator passes through touch screen or keyboard
The equipment operations such as mouse magnetic starter carries out start-up and shut-down control to the oil pump in pump oil unit 4.After aircraft flies on high, meeting
Gather some electrostatic, thus by disappear phasmajector before oiling static elimination, avoiding generating electric arc causes to light fuel vapor.
As optional embodiment, kerosene cabin 1 of navigating, nitrogen filling inerting unit 3 and oil-immersed pump are in ship lower decks；It refuels
The aboard ship deck of device 5, and around helicopter deck；Magnetic starter 7 and oil-immersed pump 4 are in same cabin；Display screen with
Refueling device 5 is in same cabin.
In this example it is shown that screen is arranged at deck on the ship with refueling device, convenient for being supervised while refueling
The work of control.
As optional embodiment, further includes: oil return pipe 104, one terminate at the oil return nozzle of refueling device 5, return
Another oil return import for terminating at boat kerosene cabin 1 of oil pipe.
In the present embodiment, the second oil pump is additionally provided among oil return pipe, after helicopter adds oil, by refueling device 5
In remaining oil lead back to boat kerosene cabin 1.In a particular embodiment, due to refueling device aboard ship deck, kerosene cabin is navigated under ship
Deck can make Fuel Remained be back to boat kerosene cabin by gravity.
It further include three-way pipeline, first interface and second pipe as shown in Figures 2 and 3 as optional embodiment
One end connection close to boat kerosene cabin 1, the second interface and second pipe of three-way pipeline are connected close to one end of oil-immersed pump 4, and three
The third interface and closed conduct threaded a pipe pass through flanged joint；Soft magnetism disk 201, setting is in three-way pipeline close to boat kerosene cabin
1 interface；There are several through-holes on soft magnetism disk；The outer diameter of soft magnetism disk is equal to the internal diameter of second pipe；Permanent magnet 202,
It is arranged in three-way pipeline closed conduct；Three electromagnet 203 are circumferentially positioned at corresponding with soft magnetism disk 201 with 120 °
Two pipeline externals.
In the present embodiment, since aviation fuel coal bunker and refueling device are there are difference in height, second pipe needs to carry out bending company
It connects.In a particular embodiment, three-way pipeline is 45 ° of connections.Electromagnet 203 is powered, and generates magnetic field, and soft magnetism disk is made to have magnetic
Property, adsorb the magnetic-particle in fuel oil.Electromagnet 203 is cut off the power, and magnetic-particle falls to closed conduct under the effect of gravity
In, then adsorbed by permanent magnet 202.
In a specific embodiment, valve, easy to disassemble and cleaning closing are set in the third interface of three-way pipeline
Pipeline.
As optional embodiment, the first valve, the second valve and third valve are electric expansion valve.
In the present embodiment, electric expansion valve includes motor, gear assembly, valve rod assembly and valve component, wherein valve seat
Component includes valve seat and the valve seat core in valve seat.Valve seat has valve port, connects the first interface of entrance sleeve and connect out
The second interface of mouth adapter tube.Valve seat core by the valve chamber of valve seat be divided into the inner cavity being connected to valve port and with the exocoel around inner cavity,
Wherein, exocoel is connected to entrance sleeve, and inner cavity is connected to discharge connection, and the peripheral wall of valve seat core, which offers, can be connected to inner cavity and outer
The communication port of chamber；To which the on-off of opening and closing the control entrance sleeve and discharge connection of valve port, the opening size of communication port controls
The uninterrupted of oil mass.
From the above mentioned, in the present invention, boat kerosene cabin is equipped with nitrogen and fills inerting unit, and oil plant memory capacity is big, cargo tank peace
Quan Xinggao, meanwhile, system equipment uses distributing layout design, and it is flexible for installation, it is suitble to complicated Ship Structure.Oil pump can be local
And long-range start-up and shut-down control, it ensure that safety and the convenience of operation.Also, kerosene cabin of navigating uses electric heating Ventilated cap, pipeline
Using 316L double-wall pipe and with heating device, it is ensured that system adapts to polar region working environment.
Although being described in conjunction with the accompanying the embodiment of the present invention, those skilled in the art can not depart from the present invention
Spirit and scope in the case where various modifications and variations can be made, such modifications and variations are each fallen within by appended claims institute
Within the scope of restriction.
Claims (10)
1. a kind of polar region helicopter jet fuel fuel loading system peculiar to vessel characterized by comprising
It navigates kerosene cabin (1)；
Back-fire relief Ventilated cap (2), with the boat kerosene cabin (1) by flanged joint or threaded connection, the back-fire relief Ventilated cap (2) is set
It sets in the top of boat kerosene cabin (1)；
Nitrogen fills inerting unit (3), is connect with the boat kerosene cabin (1) by the first valve and first pipe；
Oil-immersed pump (4) is connect with the boat kerosene cabin (1) by the second valve and second pipe；
Refueling device (5) is connect with the oil-immersed pump (4) by third valve and third pipeline；
Control device (6) fills inerting unit (3), first valve, the oil-immersed pump, second valve with the nitrogen
Door, the third valve and refueling device connection.
2. polar region helicopter jet fuel fuel loading system peculiar to vessel according to claim 1, which is characterized in that first pipe
Road, the second pipe, the third pipeline are 316L double-wall pipe.
3. polar region helicopter jet fuel fuel loading system peculiar to vessel according to claim 1, which is characterized in that further include: add
Thermal modules are laid on the first pipe, the second pipe, the third pipeline external；
Thermal insulation layer is covered on outside the heating module.
4. polar region helicopter jet fuel fuel loading system peculiar to vessel according to claim 1, which is characterized in that the back-fire relief is saturating
Gas cap (2) is electric heating back-fire relief Ventilated cap.
5. polar region helicopter jet fuel fuel loading system peculiar to vessel according to claim 1, which is characterized in that the oiling dress
Setting (5) includes: filter separator, flow sensor, pressure sensor, the phasmajector that disappears, refueling hose and reel.
6. polar region helicopter jet fuel fuel loading system peculiar to vessel according to claim 5, which is characterized in that further include: magnetic
Power starter (7) is connect with the oil-immersed pump (4).
7. polar region helicopter jet fuel fuel loading system peculiar to vessel according to claim 6, which is characterized in that further include: it is aobvious
Display screen and microprocessor, multiple input serial ports and the nitrogen of the microprocessor fill inerting unit (3), are separated by filtration
Device, flow sensor are connected with the output end of pressure sensor；The output serial ports of the microprocessor is defeated with the display screen
Enter end connection.
8. polar region helicopter jet fuel fuel loading system peculiar to vessel according to claim 7, which is characterized in that the boat kerosene
Cabin (1), nitrogen filling inerting unit (3) and the oil-immersed pump are in ship lower decks；
The refueling device (5) aboard ship deck, and around helicopter deck；
The magnetic starter (7) and the oil-immersed pump (4) are in same cabin；
The display screen and the refueling device (5) are in same cabin.
9. polar region helicopter jet fuel fuel loading system peculiar to vessel according to claim 1, which is characterized in that further include: it returns
Oil pipe, one terminate at the oil return nozzle of the refueling device (5), and the another of the oil return pipe terminates at the boat kerosene cabin
(1) oil return import.
10. polar region helicopter jet fuel fuel loading system peculiar to vessel according to claim 1, which is characterized in that further include:
Three-way pipeline, first interface are connect with the second pipe close to one end of boat kerosene cabin (1), the tee tube
The second interface in road is connect with the second pipe close to one end of the oil-immersed pump (4), the third interface of the three-way pipeline
Pass through flanged joint with closed conduct；
The interface in the three-way pipeline close to boat kerosene cabin (1) is arranged in soft magnetism disk；If having on the soft magnetism disk
Dry through-hole；The outer diameter of the soft magnetism disk is equal to the internal diameter of the second pipe；
Permanent magnet is arranged in the closed conduct described in the three-way pipeline；
Three electromagnet are circumferentially positioned at outside the second pipe corresponding with the soft magnetism disk with 120 °.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910807435.XA CN110498057A (en) | 2019-08-29 | 2019-08-29 | Polar region helicopter jet fuel fuel loading system peculiar to vessel |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910807435.XA CN110498057A (en) | 2019-08-29 | 2019-08-29 | Polar region helicopter jet fuel fuel loading system peculiar to vessel |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110498057A true CN110498057A (en) | 2019-11-26 |
Family
ID=68590336
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910807435.XA Pending CN110498057A (en) | 2019-08-29 | 2019-08-29 | Polar region helicopter jet fuel fuel loading system peculiar to vessel |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110498057A (en) |
Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20120079337A (en) * | 2011-01-04 | 2012-07-12 | 선보공업주식회사 | A helicopter refuelling system |
| CN202807106U (en) * | 2012-09-12 | 2013-03-20 | 陕西鼓风机集团西安锅炉有限责任公司（西安特种汽车厂） | Fuel supply system of plane refueling vehicle |
| CN205500750U (en) * | 2016-04-15 | 2016-08-24 | 广汉市天舟航空发动机燃料科技有限公司 | General airport tank service truck refueling system with refuel and draw back glossy way |
| CN205933200U (en) * | 2016-07-22 | 2017-02-08 | 中国舰船研究设计中心 | Novel integration of on -board helicopter is refueled device |
| CN206031700U (en) * | 2016-05-18 | 2017-03-22 | 南通江海海洋工程产业研究院有限公司 | Cabin oil fuel tank device of breathing freely |
| CN107572471A (en) * | 2017-08-08 | 2018-01-12 | 航天晨光股份有限公司 | Multi items oil plant pipeline tank service truck and its control method |
| CN207175456U (en) * | 2017-09-15 | 2018-04-03 | 武汉海翼科技有限公司 | A kind of lift helicopter refueling device |
| CN207809808U (en) * | 2018-02-02 | 2018-09-04 | 上海锆卓船舶设计有限公司 | A kind of helicopter oiling relief system and its ocean platform, ship |
| CN207955968U (en) * | 2018-02-02 | 2018-10-12 | 上海锆卓船舶设计有限公司 | A kind of sea ships and light boats fuel loading system and ocean platform |
| CN209096993U (en) * | 2018-10-31 | 2019-07-12 | 兴化市东方船舶设计有限公司 | A kind of fuel system of ship |
| CN210364429U (en) * | 2019-08-29 | 2020-04-21 | 中国极地研究中心(中国极地研究所) | Helicopter jet fuel refueling system for polar region ship |
-
2019
- 2019-08-29 CN CN201910807435.XA patent/CN110498057A/en active Pending
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20120079337A (en) * | 2011-01-04 | 2012-07-12 | 선보공업주식회사 | A helicopter refuelling system |
| CN202807106U (en) * | 2012-09-12 | 2013-03-20 | 陕西鼓风机集团西安锅炉有限责任公司（西安特种汽车厂） | Fuel supply system of plane refueling vehicle |
| CN205500750U (en) * | 2016-04-15 | 2016-08-24 | 广汉市天舟航空发动机燃料科技有限公司 | General airport tank service truck refueling system with refuel and draw back glossy way |
| CN206031700U (en) * | 2016-05-18 | 2017-03-22 | 南通江海海洋工程产业研究院有限公司 | Cabin oil fuel tank device of breathing freely |
| CN205933200U (en) * | 2016-07-22 | 2017-02-08 | 中国舰船研究设计中心 | Novel integration of on -board helicopter is refueled device |
| CN107572471A (en) * | 2017-08-08 | 2018-01-12 | 航天晨光股份有限公司 | Multi items oil plant pipeline tank service truck and its control method |
| CN207175456U (en) * | 2017-09-15 | 2018-04-03 | 武汉海翼科技有限公司 | A kind of lift helicopter refueling device |
| CN207809808U (en) * | 2018-02-02 | 2018-09-04 | 上海锆卓船舶设计有限公司 | A kind of helicopter oiling relief system and its ocean platform, ship |
| CN207955968U (en) * | 2018-02-02 | 2018-10-12 | 上海锆卓船舶设计有限公司 | A kind of sea ships and light boats fuel loading system and ocean platform |
| CN209096993U (en) * | 2018-10-31 | 2019-07-12 | 兴化市东方船舶设计有限公司 | A kind of fuel system of ship |
| CN210364429U (en) * | 2019-08-29 | 2020-04-21 | 中国极地研究中心(中国极地研究所) | Helicopter jet fuel refueling system for polar region ship |
Non-Patent Citations (2)
| Title |
|---|
| 刘亚琴;潘锦平;董茂盛;: "喷气燃料舱安全性设计", 中国舰船研究, no. 01, pages 64 - 66 * |
| 沈权: "破冰船技术及几种破冰方法", 航海技术, pages 258 - 262 * |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US10974955B2 (en) | Mobile distribution station for fluid dispensing | |
| US10633243B2 (en) | Mobile distribution station | |
| US10815118B2 (en) | Mobile distribution station having sensor communication lines routed with hoses | |
| CN203161377U (en) | Gas fuel supply system of marine power plant | |
| CN204254248U (en) | LNG entrucking is prized | |
| CN204227033U (en) | A kind of separated type ice chest being applicable to small liquid rock gas powered ship | |
| CN106081040A (en) | A kind of LNG ship oceangoing ship dynamical system whole updating method | |
| CN210364429U (en) | Helicopter jet fuel refueling system for polar region ship | |
| CN110498057A (en) | Polar region helicopter jet fuel fuel loading system peculiar to vessel | |
| CN103818562B (en) | Airplane ground service integrated support system | |
| CN112879809B (en) | Propellant transfer integrated cabin and propellant filling system | |
| CN109339981A (en) | A kind of pressure charging system of the cold helium of carrier rocket kerosene case | |
| US10384927B2 (en) | Systems and methods for mobile fuel transloading | |
| CN205633733U (en) | Oily double -deck storage tank of many oils integrated form boat | |
| CN205163988U (en) | Multi -functional fire extinguishing systems | |
| CN112023316A (en) | Intelligent water-saving type transformer and reactor fire extinguishing system and fire extinguishing method thereof | |
| CN101628701A (en) | Ship-type movable explosion-proof oiling device | |
| CN206940412U (en) | A kind of refuelling device | |
| CN203382022U (en) | Double explosion-proof skid-mounted refueling device | |
| CN206344970U (en) | A kind of mobile liquid feeding ship | |
| CN105584355A (en) | Oil filler pipe assembly | |
| CN108619635A (en) | Compressed-air foam intelligent fire device for outer floating roof crude oil storage tank | |
| CN103303609A (en) | Dual-explosion-proof skid-mounted refueling device | |
| CN207645077U (en) | Aviation kerosine storage device | |
| CN218371746U (en) | Oiling machine |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination |