CN101259948A - Aviation pressure oiling joint - Google Patents
Aviation pressure oiling joint Download PDFInfo
- Publication number
- CN101259948A CN101259948A CNA2008100240391A CN200810024039A CN101259948A CN 101259948 A CN101259948 A CN 101259948A CN A2008100240391 A CNA2008100240391 A CN A2008100240391A CN 200810024039 A CN200810024039 A CN 200810024039A CN 101259948 A CN101259948 A CN 101259948A
- Authority
- CN
- China
- Prior art keywords
- valve
- filter screen
- flange
- joint
- connecting rod
- 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.)
- Granted
Links
- 230000008878 coupling Effects 0.000 claims description 33
- 238000010168 coupling process Methods 0.000 claims description 33
- 238000005859 coupling reaction Methods 0.000 claims description 33
- 210000001503 joint Anatomy 0.000 claims description 13
- 229910000831 Steel Inorganic materials 0.000 claims description 7
- 239000000945 filler Substances 0.000 claims description 7
- 239000010959 steel Substances 0.000 claims description 7
- 238000007789 sealing Methods 0.000 abstract description 3
- 239000003381 stabilizer Substances 0.000 abstract 4
- 239000003921 oil Substances 0.000 description 22
- 239000004020 conductor Substances 0.000 description 4
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 210000003811 finger Anatomy 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 239000000295 fuel oil Substances 0.000 description 1
- 239000002828 fuel tank Substances 0.000 description 1
- 210000004247 hand Anatomy 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 238000003032 molecular docking Methods 0.000 description 1
- 210000003205 muscle Anatomy 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 210000003813 thumb Anatomy 0.000 description 1
Images
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- Details Of Valves (AREA)
Abstract
The invention relates to an aviation oil filling equipment technical field, in particular to an aviation pressure oil adding joint, which comprises a joint body, a pressure stabilizer valve, a filter screen seat, a rubber pipe joint and a butting handle; the joint body, the pressure stabilizer valve, the filter screen seat and the rubber pipe joint are connected with each other; the connection structure between the joint body and the pressure stabilizer valve and between the pressure stabilizer valve and the filter screen seat is a rotatable sealing connection structure. The structure of the aviation pressure oil filling joint ensures that the rubber pipe does not drive the whole oil filling joint to rotate when the oil delivery rubber pipe is distorted and enwound, leads the operator to continue to carry out the oil filling operation by holding the handle with a hand without stopping to tidy the rubber pipe by rotating the oil filling joint, saves the physical strength and improves the oil filling efficiency.
Description
Technical field
The present invention relates to aviation bunkering facilities technical field, particularly a kind of aviation pressure oiling joint.
Background technology
Publication number be CN 2383761Y patent disclosure a kind of aviation pressure oiling joint, has fittings body, butt plate, rubber hose coupling, protective device, pressure maintaining valve, handle, valve base, add oil valve, guide frame and electrostatic conductor assembly, butt plate and pressure maintaining valve be separately fixed at fittings body on, the below, the below of pressure maintaining valve is fixedly connected with rubber hose coupling, handle directly is fixed on the fittings body, also be respectively equipped with reducing valve and electrostatic conductor assembly on the fittings body, have the butt plate groove on the butt plate, be provided with the valve base of opening the valve base groove in the fittings body of butt plate below, the valve base upper support has the oil valve of adding.
From top patent and more existing aviation pressure oiling joints; can see original filter screen seat; pressure maintaining valve and joint valve being connected to each other captiveed joint; the aviation pressure oiling joint of this structure; when refueling operation; because the sebific duct of oil transportation usually can be in the distortion reeling condition; at this moment hand-held fueling connection and aircraft add the font bonded assembly time; the sebific duct that distortion is reeled can drive the fueling connection rotation in the hand; the power of this distortion rotation is very big; can't grip fueling connection to both hands greatly; at this moment having to stop just can move on after fueling connection is made sebific duct in order by rotating, and is unfavorable for rapid refueling.
Summary of the invention
In order to overcome above-mentioned deficiency, the invention provides and a kind ofly can realize rapid refueling, easy to operate aviation pressure oiling joint.
The technical solution used in the present invention is: a kind of aviation pressure oiling joint, comprise fittings body, pressure maintaining valve, filter screen seat, rubber hose coupling and butt joint handle, joint valve, pressure maintaining valve, filter screen seat and rubber hose coupling are connected to each other, the butt joint handle is arranged on the fittings body, between fittings body and the pressure maintaining valve, and the connection structure between pressure maintaining valve and the filter screen seat is the rotary seal connection structure.This structure has guaranteed: still very convenient during the operation fueling connection even when the cargo hose distortion is reeled, fueling connection is owing to the distortion coiling of sebific duct rotates in the time of can effectively preventing to refuel.And the configuration flexibility of this two rotation is good, not easy to wear.
Further optimize structure, the rotary seal connection structure comprises fittings body and pressure maintaining valve, and pressure maintaining valve and filter screen seat each other in the raceway on the joint face and seal ring, the raceway steel ball of device interconnect function and in raceway the filling steel ball filler opening and stop up the screw plug of filler opening.
In order to make this fueling connection fueling connection impassabitity turning handle and make fueling connection break away from the font that adds of aircraft when the fueling state, guarantee to refuel safety; After oiling finishes, when adding oil valve and being closed condition, can not open and add oil valve and fuel oil is overflowed because of maloperation.Fittings body of the present invention comprises housing, butt plate, valve base, valve, the valve safety screen, add the oil valve handgrip, eccentric shaft, link rod plate, connecting rod and connecting rod base, butt plate is fixedly mounted on the bottom of valve body, the valve base that rotary support adds oil valve is set in the valve body on butt plate top, valve is arranged in the valve base, has the flange bonded assembly draw-in groove that is used on the aircraft on butt plate and the valve base respectively, the valve safety screen is fixed on the valve base, connecting rod base is fixed in the inner chamber of housing, connecting rod is installed in the connecting rod base, add the oil valve handgrip, eccentric shaft, link rod plate, connecting rod is connected successively with valve base, adding oil valve handgrip control eccentric shaft rotates, eccentric shaft moves up and down in connecting rod base by the link rod plate drivening rod, and connecting rod promotes the valve opening and closing.When non-mated condition, the moving of the end face limiting rod plate of valve safety screen, when mated condition, the side of valve safety screen and move down after link rod plate offset and prevent, prevent from that valve base from rotating to make the fueling connection can't be from breaking away from the font that adds of aircraft.
Connect apace for convenience, or change rubber hose coupling, the connection structure of filter screen seat and rubber hose coupling comprises the flange on the filter screen seat, be enclosed within the limit coil on the filter screen seat, waveform elastic ring and interior flange locked groove and the flange embedded groove of rubber hose coupling that the promotion limit coil moves, has the spacing push rod that can snap in the flange embedded groove on the limit coil, the flange that screws in the flange locked groove by the flange embedded groove connects filter screen seat and rubber hose coupling, embeds the spacing push rod locking rubber hose coupling of flange embedded groove under the pushing and pressing of waveform elastic ring.
The invention has the beneficial effects as follows: the aviation fueling connection of this structure has guaranteed when the cargo hose distortion is reeled, sebific duct can not drive whole fueling connection and rotate, operating personal still can be handed handle and proceed refueling operation, need not stop and put sebific duct in order by the rotation fueling connection, save muscle power, improved oiling efficient.
Description of drawings
The present invention is further described below in conjunction with drawings and Examples.
Fig. 1 is a structural representation of the present invention.
Fig. 2 is the structural representation when valve is in closed condition among the present invention.
Fig. 3 is the structural representation of valve when semi-open state among the present invention.
Among the figure: 1. fittings body, 1-0. housing, 1-1. butt plate, 1-2. valve base, 1-3. valve, 1-4. valve safety screen, 1-5. add the oil valve handgrip, 1-6. eccentric shaft, 1-7. link rod plate, 1-8. connecting rod, 1-9. connecting rod base, 2. pressure maintaining valve, 3. filter screen seat, 3-1. flange, 3-2. limit coil, 3-3. the wave mode elastic ring, the spacing push rod of 3-4., 4. rubber hose coupling, 4-1. the flange locked groove, 4-2. flange embedded groove, 5. butt joint handle, 6. raceway, 7. seal ring, 8. steel ball, 9. filler opening, 10. screw plug, 11. draw-in grooves, 12. sheath, 13. protecting covers, 14. electrostatic conductor assemblies.
The specific embodiment
A kind of aviation pressure oiling joint as shown in Figure 1, comprise fittings body 1, pressure maintaining valve 2, filter screen seat 3, rubber hose coupling 4 and butt joint handle 5, fittings body 1, pressure maintaining valve 2, filter screen seat 3 and rubber hose coupling 4 are connected to each other, butt joint handle 5 is arranged on the fittings body 1, rubber hose coupling 4 is used for being connected with the sebific duct of carrying oil plant, oil plant in the sebific duct enters aviation pressure oiling joint by rubber hose coupling 4, the impurity that oil plant at first filters wherein by filter screen seat 3, enter pressure maintaining valve 2 then, the effect of pressure maintaining valve 2 is to guarantee that the oil pressure in the fuel tank within the limits prescribed when refueling, in case surpass this pressure, pressure maintaining valve 2 cuts off oil transportation channel with SELF CL.Fittings body 1 docks with the oil filling port of aircraft, will send into fuel tanker from the oil plant that pressure maintaining valve 2 is come, and between fittings body 1 and the pressure maintaining valve 2, and the connection structure between pressure maintaining valve 2 and the filter screen seat 3 is the rotatable sealing connection structure.This rotatable sealing connection structure comprises fittings body 1 and pressure maintaining valve 2, and pressure maintaining valve 2 and filter screen seat 3 play the steel ball 8 of interconnect functions in the raceway 6 on the joint face and seal ring 7, the raceway 6 each other and the filler opening 9 of filling steel ball 8 and the screw plug 10 of obstruction filler opening 9 to raceway 6 in.
Fittings body 1 comprises housing 1-0, butt plate 1-1, valve base 1-2, valve 1-3, valve safety screen 1-4, add oil valve handgrip 1-5, eccentric shaft 1-6, link rod plate 1-7, connecting rod 1-8 and connecting rod base 1-9, butt plate 1-1 is fixedly mounted on the bottom of housing 1-0, rotary valve base 1-2 is set in the housing 1-0 on butt plate 1-1 top, valve 1-3 is arranged in the valve base 1-2, valve safety screen 1-4 is fixed on the valve base 1-2, connecting rod base 1-9 is arranged in the inner chamber of housing 1-0, connecting rod 1-8 is installed among the connecting rod base 1-9, adds oil valve handgrip 1-5, eccentric shaft 1-6, link rod plate 1-7, connecting rod 1-8 is connected successively with valve 1-3.
Shown in Fig. 2,3, add oil valve handgrip 1-5 control eccentric shaft 1-6 and rotate, eccentric shaft 1-6 moves up and down in connecting rod base 1-9 by link rod plate 1-7 drivening rod 1-8, and moving up and down of connecting rod 1-8 promotes valve 1-3 opening and closing.
During butt joint, draw-in groove 11 on butt plate 1-1 and the valve base 1-2 is aligned with each other, and during butt joint, the draw-in groove 11 of flange by butt plate 1-1 that adds on the font of aircraft is inserted in the draw-in groove 11 of valve base 1-2, valve base 1-2 and fittings body 1-1 can relatively rotate, and butt plate 1-1 is fixed on the fittings body 1.When gripping butt joint handle 5 these aviation pressure oiling joints of rotation, the draw-in groove 11 of butt plate 1-1 and the draw-in groove 11 of valve base 1-2 stagger mutually, the non-draw-in groove of butt plate 1-1 partly makes the flange that adds on the font of aircraft deviate from, and that realizes fittings body 1 and aircraft adds docking of font.When butt joint was finished, valve safety screen 1-4 removed from original position, and the motion of link rod plate 1-7 is no longer kept out at the top of valve safety screen 1-4, link rod plate 1-7 can free motion, break off with the fingers and thumb and add oil valve handgrip 1-5, add oil valve handgrip 1-5 and drive eccentric shaft 1-6 rotation, open valve 1-3.When aviation pressure oiling joint is in fueling state, valve 1-3 is in and moves down open mode, the link rod plate 1-7 of this moment has blocked the sidepiece of valve safety screen 1-4, because valve safety screen 1-4 and valve base 1-2 fix, valve base 1-2 can't be rotated when fueling state, also just cannot the font that add of this aviation pressure oiling joint and aircraft be broken away from by rotation.Close valve 1-3, link rod plate 1-7 return, disengaging is spacing to the sidepiece of valve safety screen 1-4, rotate aviation pressure oiling joint, valve safety screen 1-4 moves, and when aviation pressure oiling joint and the disengaging of aircraft refuelling seat, the end face of valve safety screen 1-4 blocks link rod plate 1-7 again, realization is to the locking of valve 1-3, and valve 1-3 can't open.
The connection structure of filter screen seat 3 and rubber hose coupling 4 comprises the flange 3-1 on the filter screen seat 3, be enclosed within the limit coil 3-2 that only can move up and down on the filter screen seat 3, wave mode elastic ring 3-3 that promotion limit coil 3-2 moves and flange locked groove 4-1 and the flange embedded groove 4-2 in the rubber hose coupling 4, has the spacing push rod 3-4 that can snap in flange embedded groove 4-2 on the limit coil 3-2, the flange 3-1 that screws in flange locked groove 4-1 by flange embedded groove 4-2 connects filter screen seat 3 and rubber hose coupling 4, embeds the spacing push rod 3-4 locking rubber hose coupling 4 of flange embedded groove 4-2 under the pushing and pressing of wave mode elastic ring 3-3.With the flange 3-1 on the flange embedded groove 4-2 aligning filter screen seat 3 of rubber hose coupling 4, press down rubber hose coupling 4, rubber hose coupling 4 promotes limit coil 3-2 and descends, pressing down the back that puts in place makes flange embed flange locked groove 4-1 by rotation rubber hose coupling 4, continuing the spacing push rod 3-4 of rotation on limit coil 3-2 embeds the flange embedded groove 4-2 of rubber hose coupling 4 and rubber hose coupling 4 is realized locking, depress limit coil 3-2, releasing is spacing to rubber hose coupling 4, rotate rubber hose coupling 4 and from flange embedded groove 4-2, deviate from, promptly realize 3 release of rubber hose coupling 4 and filter screen seat until flange.
This aviation pressure oiling joint also has a series of fender guards and comprises sheath 12, protecting cover 13, electrostatic conductor assembly 14.
Claims (4)
1, a kind of aviation pressure oiling joint, comprise fittings body (1), pressure maintaining valve (2), filter screen seat (3), rubber hose coupling (4) and butt joint handle (5), fittings body (1), pressure maintaining valve (2), filter screen seat (3) and rubber hose coupling (4) are connected to each other, butt joint handle (5) is arranged on the fittings body (1), it is characterized in that: between described fittings body (1) and the pressure maintaining valve (2), and the connection structure between pressure maintaining valve (2) and the filter screen seat (3) is the rotary seal connection structure.
2, aviation pressure oiling joint according to claim 1 is characterized in that: described rotary seal connection structure comprises that fittings body (1) and pressure maintaining valve (2) and pressure maintaining valve (2) and filter screen seat (3) play the steel ball (8) of interconnect function and annotate the filler opening (9) of steel ball (8) and the screw plug (10) of obstruction filler opening (9) to raceway (6) in the raceway (6) on the joint face and seal ring (7), the raceway (6) each other.
3, aviation pressure oiling joint according to claim 1, it is characterized in that: described fittings body (1) comprises housing (1-0), butt plate (1-1), valve base (1-2), valve (1-3), valve safety screen (1-4), add oil valve handgrip (1-5), eccentric shaft (1-6), link rod plate (1-7), connecting rod (1-8) and connecting rod base (1-9), butt plate (1-1) is fixedly mounted on the bottom of housing (1-0), in the housing (1-0) on butt plate (1-1) top rotary valve base (1-2) is set, has the flange bonded assembly draw-in groove (11) that is used on the aircraft on butt plate (1-1) and the valve base (1-2) respectively, valve (1-3) is arranged in the valve base (1-2), valve safety screen (1-4) is fixed on the valve base (1-2), connecting rod base (1-9) is fixed in the inner chamber of housing (1-0), connecting rod (1-8) is installed in the connecting rod base (1-9), add oil valve handgrip (1-5), eccentric shaft (1-6), link rod plate (1-7), connecting rod (1-8) is connected successively with valve (1-3), adding oil valve handgrip (1-5) control eccentric shaft (1-6) rotates, eccentric shaft (1-6) moves up and down in connecting rod base (1-9) by link rod plate (1-7) drivening rod (1-8), and connecting rod (1-8) promotes valve (1-3) opening and closing.
4, aviation pressure oiling joint according to claim 1, it is characterized in that: the connection structure of described filter screen seat (3) and rubber hose coupling (4) comprises the flange (3-1) on the filter screen seat (3), be enclosed within the limit coil (3-2) on the filter screen seat (3), promote mobile wave mode elastic ring (3-3) of limit coil (3-2) and flange locked groove (4-1) and the flange embedded groove (4-2) in the rubber hose coupling (4), has the spacing push rod (3-4) that can snap in flange embedded groove (4-2) on the described limit coil (3-2), the flange (3-1) that screws in flange locked groove (4-1) by flange embedded groove (4-2) connects filter screen seat (3) and rubber hose coupling (4), embeds spacing push rod (3-3) the locking rubber hose coupling (4) of flange embedded groove (4-2) under the pushing and pressing of wave mode elastic ring (3-3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2008100240391A CN101259948B (en) | 2008-04-23 | 2008-04-23 | Aviation pressure oiling joint |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2008100240391A CN101259948B (en) | 2008-04-23 | 2008-04-23 | Aviation pressure oiling joint |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN101259948A true CN101259948A (en) | 2008-09-10 |
| CN101259948B CN101259948B (en) | 2012-07-25 |
Family
ID=39960691
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2008100240391A Expired - Fee Related CN101259948B (en) | 2008-04-23 | 2008-04-23 | Aviation pressure oiling joint |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN101259948B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105366069A (en) * | 2015-11-26 | 2016-03-02 | 中国航空工业集团公司沈阳飞机设计研究所 | Lubricating oil pressure refueling ground mouth |
| CN110900522A (en) * | 2019-12-17 | 2020-03-24 | 华南蓝天航空油料有限公司湖南分公司 | Emergency breaking and dismantling equipment acting on Kate type oil filling connector |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4567924A (en) * | 1983-02-25 | 1986-02-04 | Brown Albert W | Aircraft under-wing fueling nozzle system |
| US5904302A (en) * | 1997-03-21 | 1999-05-18 | Brown; Albert W. | Aircraft fueling nozzle |
| CN2383761Y (en) * | 1999-07-09 | 2000-06-21 | 武进市腾飞航空油料设备配件厂 | Aeronautic pressure oiling joint |
| US6234224B1 (en) * | 2000-03-14 | 2001-05-22 | Robert L. Schultz, Jr. | Aircraft fueling nozzle |
| CN2615050Y (en) * | 2003-03-26 | 2004-05-12 | 郑友松 | Aero-pressure fueling joint |
| CN2626859Y (en) * | 2003-06-24 | 2004-07-21 | 成都思泰航空科技有限责任公司 | Spigot joint for pressure oiling of airplane |
| CN201209119Y (en) * | 2008-04-23 | 2009-03-18 | 朱金兴 | Aeronautic pressure oiling joint |
-
2008
- 2008-04-23 CN CN2008100240391A patent/CN101259948B/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105366069A (en) * | 2015-11-26 | 2016-03-02 | 中国航空工业集团公司沈阳飞机设计研究所 | Lubricating oil pressure refueling ground mouth |
| CN105366069B (en) * | 2015-11-26 | 2019-09-24 | 中国航空工业集团公司沈阳飞机设计研究所 | A kind of lubricating oil pressure oiling ground connects mouth |
| CN110900522A (en) * | 2019-12-17 | 2020-03-24 | 华南蓝天航空油料有限公司湖南分公司 | Emergency breaking and dismantling equipment acting on Kate type oil filling connector |
Also Published As
| Publication number | Publication date |
|---|---|
| CN101259948B (en) | 2012-07-25 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20221028 Address after: Heng Shan Qiao Zhen Rong Hu Cun, Wujin District, Changzhou City, Jiangsu Province Patentee after: Changzhou Lantian Tengfei Aviation Equipment Co.,Ltd. Address before: 213118 Jiangsu province Changzhou City Furong Town Wujin District No. 84 Tanqiao Dai Jia Ba Cun Wei Zhang Patentee before: Zhu Jinxing |
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| TR01 | Transfer of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20120725 |
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| CF01 | Termination of patent right due to non-payment of annual fee |