CN108773498A - The device put is interlocked for fixing gravity oiling rifle and detecting safe parking - Google Patents

The device put is interlocked for fixing gravity oiling rifle and detecting safe parking Download PDF

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Publication number
CN108773498A
CN108773498A CN201810818778.1A CN201810818778A CN108773498A CN 108773498 A CN108773498 A CN 108773498A CN 201810818778 A CN201810818778 A CN 201810818778A CN 108773498 A CN108773498 A CN 108773498A
Authority
CN
China
Prior art keywords
sleeve
sliding axle
gravity oiling
oiling rifle
pressing plate
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
Application number
CN201810818778.1A
Other languages
Chinese (zh)
Inventor
裴相龙
徐世伟
张良
饶丽娜
刘明
李大宝
董智鸿
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
CHINA FAW GROUP SICHUAN SPECIAL AUTOMOBILE Co Ltd
Original Assignee
CHINA FAW GROUP SICHUAN SPECIAL AUTOMOBILE Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by CHINA FAW GROUP SICHUAN SPECIAL AUTOMOBILE Co Ltd filed Critical CHINA FAW GROUP SICHUAN SPECIAL AUTOMOBILE Co Ltd
Priority to CN201810818778.1A priority Critical patent/CN108773498A/en
Publication of CN108773498A publication Critical patent/CN108773498A/en
Pending legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND 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
    • B64F1/00Ground or aircraft-carrier-deck installations
    • B64F1/28Liquid-handling installations specially adapted for fuelling stationary aircraft

Abstract

The invention discloses a kind of devices for fixing gravity oiling rifle and detecting safe parking interlocking point, upper cover and lower cover form gravity oiling rifle sealed cabin by hinge and hasp connection, other component constitutes detection device, wherein lower cover is fixed on sleeve, pressing plate is located in lower cover, and it is fixed on sliding axle upper end, sliding axle can in sleeve lower slider vertically, bulge loop is set on sliding axle, spring wrap is on sliding axle, gravity oiling rifle pushes down pressing plate when being put into sealed cabin, slide glides downward, spring is compressed, pressing plate is unclamped when taking out gravity oiling rifle, sliding axle and pressing plate playback;Sensor is connect with aircraft bowser safety interlock system signal, and test position is the region passed through when cartridge exterior sliding axle is flexible.It is more secured to the fixation of gravity refueling nozzle when the device, and point is interlocked as safe parking, when not releasing interlocking, tank service truck cannot travel, and improve the safety of aircraft refuelling.

Description

The device put is interlocked for fixing gravity oiling rifle and detecting safe parking
Technical field
The present invention relates to aircraft fueling facilities, more particularly it relates to a kind of for fixing gravity oiling rifle and examining Survey the device of safe parking interlocking point.
Background technology
Existing aircraft gravity oiling rifle is partly solid by tying device by being placed directly in control cabinl pulpit after coil-winding It is fixed, it is easy to shake in tank service truck driving process, gravity oiling rifle is caused to damage and be unable to bio-occlusion aircraft refuelling;Meanwhile In the case that aircraft gravity oiling rifle is connect with fuel tanker, if aircraft bowser driver's maloperation driving vehicle, will cause The generation of serious accident.The present invention has well solved the above problem.
Invention content
The present invention overcomes the deficiencies in the prior art, provide a kind of for fixing gravity oiling rifle and detecting safe parking connection Lock point device, with it is expected can solve aircraft gravity oiling rifle fix loosely, aircraft gravity oiling rifle connect with fuel tank when hold The problem of easy maloperation leads to safety accident.
In order to solve the above technical problems, the present invention uses following technical scheme:
A kind of device for fixing gravity oiling rifle and detecting safe parking interlocking point, including upper cover, lower cover, pressing plate, Mounting bracket, sliding axle, sensor and spring, the upper cover and lower cover are connected through the hinge, the opposite another side setting of hinge Hasp forms therebetween sealed cabin, is fastened after gravity oiling rifle is placed on lower lid when upper cover and lower cover snap together Upper cover is to make gravity oiling rifle be fixed;Hole is opened in the middle part of the lower cover, the mounting bracket has sleeve part, described Sleeve tilts, and lower cover is fixed on sleeve upper end, and the sealed cabin is made to tilt;Pressing plate is located in lower cover, and is fixed on sliding axle End, sliding axle are inserted into from the through-hole in the middle part of lower cover in the sleeve, and can in sleeve lower slider vertically, set on sliding axle Bulge loop is set, slides up and down distance for limiting it, spring wrap is on sliding axle and is limited in sleeve, and gravity oiling rifle is put Pressing plate is pushed down when entering in the sealed cabin, sliding glides downward, spring is driven to be compressed by the bulge loop, takes out gravity oiling rifle Shi Songkai pressing plates, spring tension make sliding axle and pressing plate playback;The sensor is fixed in mounting bracket, and and aircraft refuelling Vehicle safety interlock system signal connects, and test position is the region passed through when cartridge exterior sliding axle is flexible.
The device for fixing gravity oiling rifle and detecting safe parking interlocking point, the top and bottom of sleeve Mounting table is respectively set, lower cover is bolted in the mounting table of sleeve upper end, and sensor passes through connecting plate and spiral shell It tethers and is connected in the mounting table of sleeve lower end.
The device for fixing gravity oiling rifle and detecting safe parking interlocking point, the erecting bed of sleeve lower end Support chip is set between face and sleeve and is used to support sleeve.
The device for fixing gravity oiling rifle and detecting safe parking interlocking point, the shape of sealed cabin is circle Cylinder chamber.
The device for fixing gravity oiling rifle and detecting safe parking interlocking point, the internal diameter at the middle part of sleeve Internal diameter more than sleeve both ends makes upper and lower ends in sleeve be respectively formed step, and spring is limited between the step of upper and lower ends.
The device for fixing gravity oiling rifle and detecting safe parking interlocking point, sensor select inductance type Sensor.
The device for fixing gravity oiling rifle and detecting safe parking interlocking point, pressing plate pass through with sliding axle Bolt is fixedly connected.
The device for fixing gravity oiling rifle and detecting safe parking interlocking point, when pressing plate is not slided by pressure When moving axis playbacks, the lower end surface of sliding axle is flushed with sleeve lower face.
The device for fixing gravity oiling rifle and detecting safe parking interlocking point, upper cover and lower cover are using resistance to Oily rubber material is made, and the sealed cabin surface that the two is formed has cyclic annular tapered protrusion.
Compared with prior art, the present invention at least has the advantages that:Aircraft gravity oiling rifle can be played compared with Good fixed function, prevents aircraft gravity oiling rifle from being shaken in tank service truck driving process, and the fixing device is as safety One of interlocking point forms safety interlock system, only when all safety interlocking points are solved with other safety interlocking points in tank service truck When except interlocking, aircraft bowser can just enter transport condition, therefore avoid aircraft gravity oiling rifle and connect with aircraft mailbox In the case of maloperation tank service truck traveling cause serious accident occur situation.
Description of the drawings
Fig. 1 is that the present invention is used to fix gravity oiling rifle and detects the device external structure signal of safe parking interlocking point Figure.
Fig. 2 is that the present invention is used to fix gravity oiling rifle and detects the outer of another side of device of safe parking interlocking point Portion's structural schematic diagram.
Fig. 3 is the A-A sectional views of Fig. 2.
Fig. 4 is that the present invention is used to fix gravity oiling rifle and detects the vertical view of the device of safe parking interlocking point.
Wherein, 1- upper covers, 2- hinges, 3- pressing plates, 4- lower covers, 5- hasps, 6- mounting brackets, 61- sleeves, 62- erecting beds Face, 63- support chips, 7- sliding axles, 8- inductance type transducers, 9- springs, 10- sealed cabins, 11- bulge loops.
Specific implementation mode
In order to make the purpose , technical scheme and advantage of the present invention be clearer, with reference to the accompanying drawings and embodiments, right The present invention is further elaborated.It should be appreciated that the specific embodiments described herein are merely illustrative of the present invention, and It is not used in the restriction present invention.
Fig. 1, Fig. 2 and Fig. 4 show for fix gravity oiling rifle and detect safe parking interlocking point device outside Shape, Fig. 3 are sectional view, show internal structure.What upper cover 1 and lower cover 4 were connected together, it is connected through the hinge, cuts with scissors on one side Hasp 5 is arranged in chain opposite side, facilitates together with being completely fixed upper cover 1 with lower cover 4.Upper cover is actually to be opened on a rectangle The structure that one semicolumn slot is formed, the shape of lower cover is as upper cover, and when the two snaps together, two semicolumn slots are just tied It is combined, forms a cylindrical cavity, both ends are unclosed, and completely open, which is gravity refueling nozzle Sealed cabin 10, upper cover and lower cover are made of oil-resistant rubber material, in order to increase the frictional force with gravity oiling rifle gun barrel, When oil-resistant rubber material sulfidization molding, the sealed cabin surface of upper cover and lower cover has cyclic annular tapered protrusion.Upper cover is opened, by gravity Refueling nozzle is placed on lower lid, then so that upper cover and lower cover is fastened to make gravity oiling rifle be fixed by hasp again.Upper cover and Lower cover is grouped together into the structure of fixed gravity oiling rifle, which is fixed in mounting bracket 6, and mounting bracket 6 includes Sleeve 61 installs end face 62 and support chip 63.
Other than upper cover, lower cover and mounting bracket, the dress put is interlocked for fixing gravity oiling rifle and detecting safe parking Set further includes pressing plate 3, sliding axle 7, inductance type transducer 8 and spring 9.Hole is opened at the middle part of lower cover 4, and the mounting bracket 6 has There are sleeve part, sleeve to tilt, lower cover 4 is fixed on 61 upper end of sleeve, so that sealed cabin 10 is tilted, when being fixed due to gravity oiling rifle Need that there are angles with ground, it is therefore desirable to which sealed cabin tilts and cannot be horizontally disposed with sealed cabin, and if horizontally disposed fixing Its fixed effect of cabin is deteriorated;Pressing plate 3 is located in lower cover 4, and is bolted on 7 upper end of sliding axle, and sliding axle 7 is from lower cover 4 In the through-hole insertion sleeve 61 at middle part, and can in sleeve 61 lower slider vertically, bulge loop 11 is set on sliding axle 7, is used for It limits it and slides up and down distance, spring 9 is wrapped on sliding axle and is limited in sleeve, and the internal diameter at the middle part of sleeve 61 is more than The internal diameter at sleeve both ends makes upper and lower ends in sleeve be respectively formed step, and spring 9 is limited between the step of upper and lower ends, or There is step, spring upper end to be limited by bulge loop 11 for sleeve inner only lower end, and the outer diameter of bulge loop 11 is more than lower cover middle through-hole Diameter by lower cover to be limited.Gravity oiling rifle pushes down pressing plate when being put into the sealed cabin 10, drives sliding axle 7 to downslide Dynamic, spring 9 is compressed by the bulge loop 11, unclamps pressing plate 3 when taking out gravity oiling rifle, spring tension makes sliding axle 7 and pressing plate 3 return Position, when pressing plate 3 not by pressure and sliding axle 7 playback when, the lower end surface of sliding axle 7 is flushed with 61 lower face of sleeve.Inductance type Sensor 8 is fixed in mounting bracket 6, and is connect with aircraft bowser safety interlock system signal, and test position is sleeve The region that slide outside axis passes through when flexible.Mounting table 62 is respectively set in the top and bottom of the sleeve 61, and lower cover 4 passes through Bolt is fixed in the mounting table of 61 upper end of sleeve, and inductance type transducer 8 is by connecting plate and is bolted to sleeve lower end Mounting table on, between the mounting table and sleeve of 61 lower end of sleeve be arranged support chip 63 be used to support sleeve.
Operation principle:
(1) gravity oiling rifle is placed on by suitable angle on pressing plate 3, is closed up in upper cover 1 to lower cover 4, pressing hasp 5, sliding axle axis 7 moves down, and spring 9 is made to be compressed, and sliding axle 7 stretches out 6 lower part of mounting bracket, reaches inductance type transducer 8 Detection zone in, inductance type transducer sends out electric signal, and signal gravity oiling rifle is in place.Tank service truck drives indoor finger at this time Show that lamp extinguishes, in the case where other safety interlocks are in place simultaneously, parking braking interlocking releases, and aircraft bowser can be into Enter transport condition.
(2) upper cover 1 is opened, gravity oiling rifle is lifted, sliding axle 7 moves up under the tension force effect of spring 9, sliding 8 detection zone of inductance type transducer is left in 7 lower end of axis, and inductance type transducer 8 has disengaged from solid without detection signal, signal gravity oiling rifle Fixed point.The indoor indicator light of tank service truck driving at this time is bright, and parking braking interlocking, aircraft bowser cannot enter transport condition.
Although reference be made herein to invention has been described for explanatory embodiment of the invention, however, it is to be understood that ability Field technique personnel can be designed that a lot of other modification and implementations, these modifications and implementations will be fallen in the application public affairs Within the scope and spirit opened.It more specifically, can be to the group of theme combination layout in range disclosed in the present application A variety of variations and modifications are carried out at component and/or layout.In addition to variations and improvements to the component parts and or layout, To those skilled in the art, other purposes also will be apparent.

Claims (9)

1. a kind of device for fixing gravity oiling rifle and detecting safe parking interlocking point, it is characterised in that including upper cover, under Lid, pressing plate, mounting bracket, sliding axle, sensor and spring, the upper cover and lower cover are connected through the hinge, opposite another of hinge Hasp is set on one side, when upper cover and lower cover snap together, forms sealed cabin therebetween, gravity oiling rifle is placed on lower cover Upper cover is fastened after upper to make gravity oiling rifle be fixed;Hole is opened in the middle part of the lower cover, the mounting bracket has sleeve Component, the sleeve tilt, and lower cover is fixed on sleeve upper end, and the sealed cabin is made to tilt;Pressing plate is located in lower cover, and is fixed on Sliding axle upper end, sliding axle are inserted into from the through-hole in the middle part of lower cover in the sleeve, and can in sleeve lower slider vertically, it is sliding Bulge loop is set on moving axis, slides up and down distance for limiting it, spring wrap is on sliding axle and is limited in sleeve, gravity Refueling nozzle pushes down pressing plate when being put into the sealed cabin, and sliding glides downward, spring is driven to be compressed by the bulge loop, takes out weight Pressing plate is unclamped when power refueling nozzle, spring tension makes sliding axle and pressing plate playback;The sensor is fixed in mounting bracket, and with Aircraft bowser safety interlock system signal connects, and test position is the region passed through when cartridge exterior sliding axle is flexible.
2. the device according to claim 1 for fixing gravity oiling rifle and detecting safe parking interlocking point, feature It is that mounting table is respectively set in the top and bottom of the sleeve, lower cover is bolted on the mounting table of sleeve upper end On, sensor is by connecting plate and is bolted in the mounting table of sleeve lower end.
3. the device according to claim 2 for fixing gravity oiling rifle and detecting safe parking interlocking point, feature Setting support chip is used to support sleeve between being the mounting table and sleeve of the sleeve lower end.
4. the device according to claim 1 for fixing gravity oiling rifle and detecting safe parking interlocking point, feature It is that the shape of the sealed cabin is cylindrical cavity.
5. the device according to claim 1 for fixing gravity oiling rifle and detecting safe parking interlocking point, feature It is that the internal diameter at the middle part of the sleeve makes upper and lower ends in sleeve be respectively formed step more than the internal diameter at sleeve both ends, spring is limited Position is between the step of upper and lower ends.
6. the device according to claim 1 for fixing gravity oiling rifle and detecting safe parking interlocking point, feature It is that the sensor selects inductance type transducer.
7. the device according to claim 1 for fixing gravity oiling rifle and detecting safe parking interlocking point, feature It is that the pressing plate is bolted to connection with sliding axle.
8. the device according to claim 1 for fixing gravity oiling rifle and detecting safe parking interlocking point, feature It is that the lower end surface of sliding axle is flushed with sleeve lower face when pressing plate not by pressure and when sliding axle playback.
9. the device according to claim 1 for fixing gravity oiling rifle and detecting safe parking interlocking point, feature It is that the upper cover and lower cover are made of oil-resistant rubber material, the sealed cabin surface that the two is formed has cyclic annular tapered protrusion.
CN201810818778.1A 2018-07-24 2018-07-24 The device put is interlocked for fixing gravity oiling rifle and detecting safe parking Pending CN108773498A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810818778.1A CN108773498A (en) 2018-07-24 2018-07-24 The device put is interlocked for fixing gravity oiling rifle and detecting safe parking

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810818778.1A CN108773498A (en) 2018-07-24 2018-07-24 The device put is interlocked for fixing gravity oiling rifle and detecting safe parking

Publications (1)

Publication Number Publication Date
CN108773498A true CN108773498A (en) 2018-11-09

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CN201810818778.1A Pending CN108773498A (en) 2018-07-24 2018-07-24 The device put is interlocked for fixing gravity oiling rifle and detecting safe parking

Country Status (1)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110963063A (en) * 2019-10-31 2020-04-07 彩虹无人机科技有限公司 Oil gun control device capable of realizing multi-degree-of-freedom movement

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2468899Y (en) * 2001-03-29 2002-01-02 刘玉忠 Safety linkage apparatus for air-port fuelling vehicle
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
JP2011111212A (en) * 2009-11-30 2011-06-09 Yano Special Vehicle Manufacturing Corp Fuel nozzle latching structure of aircraft fuel supplying vehicle
CN202828100U (en) * 2012-09-07 2013-03-27 上海浦东国际机场航空油料有限责任公司 Aircraft fueling device with interaction control of aircraft fueling vehicle fueling joint interlock and deadman
CN204277874U (en) * 2014-12-01 2015-04-22 江西洪都航空工业集团有限责任公司 A kind of mounting and positioning device for oil tank joint nozzle
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
CN205737506U (en) * 2016-05-17 2016-11-30 航天晨光股份有限公司 A kind of oil truck parking interlocked brake system
CN207242067U (en) * 2017-10-11 2018-04-17 威海广泰空港设备股份有限公司 Aircraft gravity oiling rifle fixes self-locking device
CN208616208U (en) * 2018-07-24 2019-03-19 一汽(四川)专用汽车有限公司 The device put is interlocked for fixing gravity oiling rifle and detecting safe parking

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2468899Y (en) * 2001-03-29 2002-01-02 刘玉忠 Safety linkage apparatus for air-port fuelling vehicle
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
JP2011111212A (en) * 2009-11-30 2011-06-09 Yano Special Vehicle Manufacturing Corp Fuel nozzle latching structure of aircraft fuel supplying vehicle
CN202828100U (en) * 2012-09-07 2013-03-27 上海浦东国际机场航空油料有限责任公司 Aircraft fueling device with interaction control of aircraft fueling vehicle fueling joint interlock and deadman
CN204277874U (en) * 2014-12-01 2015-04-22 江西洪都航空工业集团有限责任公司 A kind of mounting and positioning device for oil tank joint nozzle
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
CN205737506U (en) * 2016-05-17 2016-11-30 航天晨光股份有限公司 A kind of oil truck parking interlocked brake system
CN207242067U (en) * 2017-10-11 2018-04-17 威海广泰空港设备股份有限公司 Aircraft gravity oiling rifle fixes self-locking device
CN208616208U (en) * 2018-07-24 2019-03-19 一汽(四川)专用汽车有限公司 The device put is interlocked for fixing gravity oiling rifle and detecting safe parking

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110963063A (en) * 2019-10-31 2020-04-07 彩虹无人机科技有限公司 Oil gun control device capable of realizing multi-degree-of-freedom movement

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