CN205933200U - Novel integration of on -board helicopter is refueled device - Google Patents
Novel integration of on -board helicopter is refueled device Download PDFInfo
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- CN205933200U CN205933200U CN201620774910.XU CN201620774910U CN205933200U CN 205933200 U CN205933200 U CN 205933200U CN 201620774910 U CN201620774910 U CN 201620774910U CN 205933200 U CN205933200 U CN 205933200U
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- water separator
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- oil water
- pipeline
- valve
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Abstract
The utility model discloses a novel integration of on -board helicopter is refueled device, comprises a frame, be equipped with the gasoline pump on the frame, oil water separator, the flowmeter, the secondary filter, refuel hose and reel, the input port connection of gasoline pump has first ball valve, the delivery outlet of gasoline pump passes through pipeline and oil water separator's input port connection, oil water separator's oil -out passes through the input port connection of pipeline and flowmeter, the delivery outlet of flowmeter passes through the pipeline and is connected with the one end of secondary filter, the other end of secondary filter through the pipeline with the input port connection of hose refuels, the hose that refuels twines on the reel. The integrated design of shape moulding massing has effectively reduced the occupation space resource requirement, and the overall arrangement is more regular, reasonable, compact, has reduced cabin space requirement, has reduced the equipment fixing interface and has maintained space requirement, has reduced the site operation degree of difficulty, has improved equipment fixing efficiency, and simple to operate promotes the convenience of maintaining, has ensured that the fluid quality satisfies the user demand.
Description
Technical field
The utility model is related to auxiliary system technical field and in particular to a kind of integrated oiling of new ship-borne helicopter
Device.
Background technology
In recent years, with the lifting of ship for civil use functional requirement, carry helicopter or unmanned plane will become ship for civil use
The inevitable choice of the tasks such as implementation environment monitoring, accident rescue, seawater patrol, Maritime Law Enforcement.In order to realize the carrying of helicopter,
A series of guarantees that need to provide including fuel oil for helicopter.At present, mostly carry the ship for civil use of helicopter or unmanned plane
It is provided with and ensures cabin including gas station, cargo tank, power plant bay etc., but because of cabin resource-constrained, oiling guarantee equipment is arranged
Crowded, suitable dress property is poor, constructional difficulties, pipeline setting-out are lack of standardization, human users and safeguard very inconvenient, and pipe interface answers
The manually operated dependence of miscellaneous, valve member is strong, oiling preparation work time length so that gas station's operation and maintenance efficiency are greatly reduced,
The emergent oiling requirements of support of helicopter cannot be met.With the lifting further of ship functional requirement, in view of aggregate resource is limited
Present situation, integrated optimization will become the general trend of following ship development.
(1) for active service ship ship-borne helicopter refueling terminal facility integrated level is not high, space hold is big, aggregate resource is sharp
With inefficient problem, by modularization Integrated design is carried out to integrated fueling facility, effectively reduce aggregate resource demand,
Decrease equipment mounting interface and safeguard space requirement.
(2) on the premise of meeting oiling security function demand, select the high refueling terminal of small volume, reliability as far as possible
Equipment, while reducing Parts Purchasing and product design cycle, reduces later maintenance cost.
(3) on the premise of meeting standard criterion, the module bottom as little as possible of the profile arrangement according to each parts
Seat simultaneously reduces module maximum appearance and size and installing space demand, base design take into full account reveal the collection of fluid, removing or
Reclaim.
(4) require to need that often safeguards setting according to the use of each parts and maintainability from the angle of ergonomics
Standby the same area being placed on base, to reduce the maintenance space requirement of device.
(5) according to pipeline setting-out technological requirement, the pipeline connection mutual to equipment and pipeline fittings is optimized design,
Make pipeline smooth out as far as possible and be easy to valve member to open and close, for reducing resistance loss of pipeline, adopt bend pipe as far as possible, thief hatch is as far as possible
It is easy to sample.
(6) valve member frequently opening and closing is needed to adopt remote-controlled valve, cooperation refueling control case is realized the one-touch of fueling operation and opened
Close, flexible pipe and hard tube are connected by snap joint, reduce personnel's participation and labour intensity.
Content of the invention
The technical problems to be solved in the utility model is, in view of the foregoing defects the prior art has, there is provided Yi Zhongxin
The integrated refueling device of type ship-borne helicopter, forms modularization Integrated design, effectively reduces shared space resources demand, layout
More regular, reasonable, compact, reduce cabin spaces demand, decrease equipment mounting interface and safeguard space requirement, reduce
Site operation difficulty, improves equipment installation effectiveness, easy for installation, and the convenience that lifting is safeguarded is it is ensured that Oil Quality meets
Use demand.
The utility model be employed technical scheme comprise that by solving above-mentioned technical problem：
A kind of integrated refueling device of new ship-borne helicopter, including framework, framework be provided with gasoline pump, oil water separator,
Flowmeter, fine filter, refueling hose and reel, the input port of gasoline pump is connected with the first ball valve, and the delivery outlet of gasoline pump passes through
Pipeline is connected with the input port of oil water separator, and the oil-out of oil water separator is connected with the input port of flowmeter by pipeline,
The delivery outlet of flowmeter is connected with one end of fine filter by pipeline, and the other end of fine filter passes through the defeated of pipeline and refueling hose
Entrance connects, and refueling hose is wound on reel.
Connect technique scheme, between gasoline pump and the first ball valve, be provided with coarse filter.
Connect technique scheme, the connecting pipe between gasoline pump and oil water separator is sequentially provided with check-valves and second
Ball valve.
Connect technique scheme, the output end of check-valves is connected with equilibrated valve, the other end of equilibrated valve and
The input of one ball valve connects.
Connect technique scheme, the bottom of oil water separator and the bottom of fine filter are equipped with bleeder valve, oil water separator
Oil-out be provided with sampling valve.
Connect technique scheme, the upper end of oil water separator is provided with overfall and exhaust outlet, and oil water separator is externally provided with oil
Water collection tank, oil water separator passes through overfall and exhaust outlet is connected with oil gas collection case.
Connect technique scheme, described also include display control device, be provided with magnetic valve between oil water separator and flowmeter, show
Control device is connected with gasoline pump, magnetic valve and flowmeter respectively.
Connect technique scheme, between fine filter and refueling hose, be provided with the phasmajector that disappears.
Connect technique scheme, reel is provided with electro-motor or rotary handle.
Connect technique scheme, the bottom of framework is provided with ramp type oil trap and floss hole.
The utility model has the advantages that：
1st, by being integrated in each part of refueling device on framework, form modularization Integrated design, effectively reduce institute
Take up room resource requirement, and layout is more regular, reasonable, compact, reduces cabin spaces demand, according to the use of each parts
And maintainability requires the equipment needing often to safeguard is placed on the same area of framework, decrease equipment mounting interface and safeguard empty
Between demand, reduce site operation difficulty, improve equipment installation effectiveness, easy for installation, the convenience that lifting is safeguarded, profit divides
From device and fine filter, moisture in fluid and impurity are filtered it is ensured that Oil Quality meets use demand.
2nd, the switch of the rotation of display control device remotely control gasoline pump and magnetic valve, flowmeter passes to aobvious control by counting flow
Device, can set and show in real time total volume read-out by display control device, need the valve member frequently opening and closing to carry out by display control device
Remote pilot, the one-touch keying of fueling operation realized by cooperation refueling control case, and flexible pipe and hard tube are connected by snap joint, fall
Low personnel's participation and labour intensity, are greatly reduced guarantee task difficulty, reduce artificial maloperation, improve operational security and work
Industry efficiency.
Brief description
Fig. 1 is the front view of the integrated refueling device of ship-borne helicopter in the utility model embodiment；
Fig. 2 is the left view of Fig. 1；
Fig. 3 is the top view of Fig. 1；
Fig. 4 is the elevation of the integrated refueling device of ship-borne helicopter in the utility model embodiment；
Fig. 5 is the principle schematic of the integrated refueling device of ship-borne helicopter in the utility model embodiment；
In figure, 1- gasoline pump, 2- framework, 3- refueling hose, 4- oil gas collection case, 5- oil water separator, 6- pressure balance
Valve, 7- oiling outlet(discharge) flange, 8- flowmeter, 9- check-valves, 10- fine filter, 11- coarse filter, 12- first ball valve, 13- second ball
Valve, 14- display control device, 15- disappears phasmajector, 16- bleeder valve, 17- magnetic valve, 18- oil storage tank, 19- pneumatic control valve, and 20- takes
Sample valve, 21- reel.
Specific embodiment
With reference to the accompanying drawings and examples the utility model is described in detail.
With reference to the integrated oiling of new ship-borne helicopter shown in Fig. 1～Fig. 5, in the embodiment that the utility model provides
Device, including framework 2, framework 2 is provided with gasoline pump 1, oil water separator 5, flowmeter 8, fine filter 10, refueling hose 3 and volume
Disk 21, the input port of gasoline pump 1 is connected with the first ball valve 12, and the delivery outlet of gasoline pump 1 passes through the defeated of pipeline and oil water separator 5
Entrance connects, and the oil-out of oil water separator 5 is connected with the input port of flowmeter 8 by pipeline, and the delivery outlet of flowmeter 8 passes through
Pipeline is connected with one end of fine filter 10, and the other end of fine filter 10 is connected with the input port of refueling hose 3 by pipeline, refuels
Flexible pipe 3 is wound on reel 21；Oil water separator 5 and fine filter 10, moisture in fluid and impurity are filtered it is ensured that oil
Liquid quality meets use demand, by being integrated in each part of refueling device on framework 2, forms modularization Integrated design, has
Effect reduces shared space resources demand, and layout is more regular, reasonable, compact, reduces cabin spaces demand, according to each zero
The use of part and maintainability require the equipment needing often to safeguard is placed on the same area of framework 2, decrease equipment installation
Interface and safeguard space requirement, reduces site operation difficulty, improves equipment installation effectiveness, easy for installation, and lifting is safeguarded
Convenience.
Further, the first ball valve 12 was set before gasoline pump 1, is easy to the maintenance of gasoline pump 1, the first ball valve 12 defeated
Entrance is connected with oil storage tank 18 by pipeline, and oil storage tank 18 and its pneumatic control valve 19 (alternatively manual) that is connected with of outlet are
Integrality in order to illustrate fuel loading system is supplemented up, and described integrated refueling device does not include oil storage tank and pneumatic control valve
19.
Further, described gasoline pump 1 is aviation kerosine pump, and the motor of aviation kerosine pump and pump shaft connect shorter, boat
The rated head of empty kerosene pump is more than or equal to 25m, and rated pressure is more than or equal to 0.6MPa.
Further, oil water separator 5 is Horizontal oil-water separator 5, and the design pressure of oil water separator 5 is 1MPa, contains
Water rate is less than or equal to 15ppm.
Further, fine filter 10 is vertical fine filter 10, and the moisture content of fine filter 10 is less than or equal to 5ppm, filtering accuracy
Less than or equal to 0.5 μm.
Further, it is provided with coarse filter 11 between gasoline pump 1 and the first ball valve 12；Before entering gasoline pump 1, setting is thick
Filter 11, it can be avoided that fluid long term storage forms impurity causing to the impeller of gasoline pump 1 to damage, coarse filter 11 is arranged at first
After ball valve 12, it is easy to the maintenance of coarse filter 11.
Further, described coarse filter 11 is y-type filter.
Further, the connecting pipe between gasoline pump 1 and oil water separator 5 is sequentially provided with check-valves 9 and the second ball
Valve 13；Check-valves 9 can avoid fluid to flow backwards the impeller damaging gasoline pump 1.
Further, the output end of check-valves 9 is connected with equilibrated valve 6, and the rated pressure of equilibrated valve 6 is
0.35MPa, the other end be connected with the input of the first ball valve 12.
Further, the bottom of the bottom of oil water separator 5 and fine filter 10 is equipped with bleeder valve 16；Can be to water-oil separating
Impurity in device 5 and fine filter 10 carries out labor cleaning.
Further, the upper end of oil water separator 5 is provided with overfall and exhaust outlet, and oil water separator 5 is externally provided with profit and receives
Header, oil water separator 5 passes through overfall and exhaust outlet is connected with oil gas collection case 4；Avoid fluid or oil gas excessive, bring peace
Full hidden danger.
Further, the oil-out of oil water separator 5 is provided with sampling valve 20, and fluid can be carried out before oiling with sampling chemical examination,
Can fill for helicopter after qualified.
Further, described also include display control device 14, be provided with magnetic valve 17 between oil water separator 5 and flowmeter 8, show
Control device 14 is connected with gasoline pump 1, magnetic valve 17 and flowmeter 8 respectively；Display control device 14 remotely control gasoline pump 1 rotates and electricity
The switch of magnet valve 17, flowmeter 8 passes to display control device 14 by counting flow, can be set by display control device 14 and show in real time
Total volume read-out, needs the valve member frequently opening and closing to be remotely controlled control by display control device 14, cooperation refueling control case is realized refueling
The one-touch keying of operation, flexible pipe and hard tube are connected by snap joint, reduce personnel's participation and labour intensity, are greatly reduced
Ensure task difficulty, reduce artificial maloperation, improve operational security and operating efficiency.
Further, it is provided with pressure sensor, pressure sensor and display control device between equilibrated valve 6 and check-valves 9
14 connections, by force information back to display control device 14.
Further, check-valves 9 is swing check valve 9, and the first ball valve 12 is the manual ball valve of DN50, the second ball valve 13
Manual ball valve for DN40.
Further, it is provided with the phasmajector 15 that disappears between fine filter and refueling hose 3；The phasmajector 15 that disappears can avoid pipeline and oil
The electrostatic accumulation that material dielectric friction, water-oil separating produce.
Further, reel 21 is grounded by cable, control unit can be interlocked to fueling operation grounding design reliability,
To guarantee the safety of fueling operation.
Further, reel 21 is provided with electro-motor or rotary handle, and electro-motor or rotary handle are easy to drive volume
Disk 21 rotates, and can carry out power-assisted folding and unfolding by electro-motor or rotary handle when flexible pipe is heavier；Refueling hose 3 and reel 21 can be tied
Close cabin layout and folding and unfolding convenience requires to select reasonable direction.
Further, the bottom of framework 2 is provided with ramp type oil trap and floss hole, and floss hole is arranged at ramp type oil trap
On；For the fluid collected and flow out when concentrating cleaning because of leakage or overhaul of the equipments, it is to avoid oil gas volatilization and accumulation, bring safety
Hidden danger, on the premise of meeting standard criterion, the module base as little as possible of the profile arrangement according to each parts simultaneously drops
Low module maximum appearance and size and installing space demand, base design takes into full account collection, removing or the recovery revealing fluid.
Further, framework 2 adopts chan frame structure, on the one hand reduces weight, on the other hand adopts and hull between
Bolt interface, is easy to construct.
Further, according to pipeline setting-out technological requirement, the pipeline connection mutual to equipment and pipeline fittings carries out excellent
Change design, make pipeline smooth out as far as possible and be easy to valve member to open and close, for reducing resistance loss of pipeline, adopt bend pipe, sampling as far as possible
Mouth is easy to sample as far as possible.
Further, on the premise of meeting oiling security function demand, select high the adding of small volume, reliability as far as possible
Oily terminal device, while reducing Parts Purchasing and product design cycle, reduces later maintenance cost；Before equipment enters cabin,
Overall pipeline-cleaning can be carried out and encapsulate, it is to avoid impacts to pipeline-cleaning operation for the job site severe environmental conditions,
Ensure that key equipment not in reason main body tube road impurity excessively stream and damage；On the premise of considering above-mentioned factor, pass through
3D modular design, refueling terminal facility is carried out integrated, integrated after refueling device be connected with hull pedestal by bolt,
Easy for installation.Realize the two sides maintenance of equipment by Ergonomics design, convenience is safeguarded in lifting simultaneously.
In sum, this intellectual achievement slave module design angle has carried out effective integration to refueling terminal equipment, full
From the preferably each parts of Miniaturization Design angle on the premise of sufficient oiling security function demand, from ergonomics angle to equipment
Layout carry out appropriate design, as far as possible reduce operation and maintenance face, be easily installed and safeguard.This intellectual achievement has structure letter
Single compact, small volume (maximum appearance and size 1800mm × 1600mm × 1200mm), lightweight, install, use and safeguard more
Easily feature.
Above be only preferred embodiment of the present utility model, certainly the power of the utility model can not be limited with this
Sharp scope, the equivalence changes therefore made according to the utility model claim, still belong to protection domain of the present utility model.
Claims (10)
1. it is characterised in that including framework, framework is provided with gasoline pump, oil to a kind of integrated refueling device of new ship-borne helicopter
Separator, flowmeter, fine filter, refueling hose and reel, the input port of gasoline pump is connected with the first ball valve, gasoline pump defeated
Outlet is connected with the input port of oil water separator by pipeline, and the oil-out of oil water separator passes through the input of pipeline and flowmeter
Mouth connects, and the delivery outlet of flowmeter is connected with one end of fine filter by pipeline, and the other end of fine filter passes through pipeline and oiling
The input port of flexible pipe connects, and refueling hose is wound on reel.
2. the integrated refueling device of new ship-borne helicopter according to claim 1 is it is characterised in that gasoline pump and the first ball
It is provided with coarse filter between valve.
3. the integrated refueling device of new ship-borne helicopter according to claim 1 is it is characterised in that gasoline pump is divided with profit
Check-valves and the second ball valve are sequentially provided with the connecting pipe between device.
4. the integrated refueling device of new ship-borne helicopter according to claim 3 is it is characterised in that the output end of check-valves
It is connected with equilibrated valve, the other end of equilibrated valve is connected with the input of the first ball valve.
5. the integrated refueling device of new ship-borne helicopter according to claim 1 is it is characterised in that the bottom of oil water separator
The bottom of portion and fine filter is equipped with bleeder valve, and the oil-out of oil water separator is provided with sampling valve.
6. the integrated refueling device of new ship-borne helicopter according to claim 1 it is characterised in that oil water separator upper
End is provided with overfall and exhaust outlet, and oil water separator is externally provided with profit collecting box, and oil water separator passes through overfall and exhaust outlet
It is connected with oil gas collection case.
7. the integrated refueling device of new ship-borne helicopter according to claim 1 is it is characterised in that described boat-carrying is gone straight up to
The integrated refueling device of machine also includes display control device, is provided with magnetic valve between oil water separator and flowmeter, display control device respectively with
Gasoline pump, magnetic valve and flowmeter connect.
8. the integrated refueling device of new ship-borne helicopter according to claim 1 it is characterised in that fine filter with refuel soft
It is provided with the phasmajector that disappears between pipe.
9. the integrated refueling device of new ship-borne helicopter according to claim 1 it is characterised in that reel be provided with electronic
Motor or rotary handle.
10. the integrated refueling device of new ship-borne helicopter according to claim 1 is it is characterised in that the bottom of framework sets
There are ramp type oil trap and floss hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620774910.XU CN205933200U (en) | 2016-07-22 | 2016-07-22 | Novel integration of on -board helicopter is refueled device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620774910.XU CN205933200U (en) | 2016-07-22 | 2016-07-22 | Novel integration of on -board helicopter is refueled device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205933200U true CN205933200U (en) | 2017-02-08 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620774910.XU Active CN205933200U (en) | 2016-07-22 | 2016-07-22 | Novel integration of on -board helicopter is refueled device |
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| CN (1) | CN205933200U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110498057A (en) * | 2019-08-29 | 2019-11-26 | 中国极地研究中心(中国极地研究所) | Polar region helicopter jet fuel fuel loading system peculiar to vessel |
| CN110920821A (en) * | 2019-12-06 | 2020-03-27 | 上海船舶研究设计院（中国船舶工业集团公司第六0四研究院） | Helicopter take-off and landing platform and hangar arrangement structure based on rescue boat |
-
2016
- 2016-07-22 CN CN201620774910.XU patent/CN205933200U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110498057A (en) * | 2019-08-29 | 2019-11-26 | 中国极地研究中心(中国极地研究所) | Polar region helicopter jet fuel fuel loading system peculiar to vessel |
| CN110920821A (en) * | 2019-12-06 | 2020-03-27 | 上海船舶研究设计院（中国船舶工业集团公司第六0四研究院） | Helicopter take-off and landing platform and hangar arrangement structure based on rescue boat |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| EE01 | Entry into force of recordation of patent licensing contract | ||
| EE01 | Entry into force of recordation of patent licensing contract |
Assignee: WUHAN HAIYI SCIENCE AND TECHNOLOGY LIMITED COMPANY Assignor: China Ship Research and Design Center Contract record no.: 2019420000019 Denomination of utility model: Novel integration of on -board helicopter is refueled device Granted publication date: 20170208 License type: Common License Record date: 20190513 |