CN108545215A - It is popped one's head in the air by oil and docks detection device - Google Patents
It is popped one's head in the air by oil and docks detection device Download PDFInfo
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- CN108545215A CN108545215A CN201810477148.2A CN201810477148A CN108545215A CN 108545215 A CN108545215 A CN 108545215A CN 201810477148 A CN201810477148 A CN 201810477148A CN 108545215 A CN108545215 A CN 108545215A
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- butt tube
- oil
- fuelling coupling
- air
- head
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- 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
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/60—Testing or inspecting aircraft components or systems
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- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
- Quick-Acting Or Multi-Walled Pipe Joints (AREA)
Abstract
It is popped one's head in the air by oil and docks detection device, including butt tube.Butt tube import has fuelling coupling, and it is circular conical surface that fuelling coupling, which is located on the inside of butt tube import, is equipped with piston on the inside of the circular conical surface of fuelling coupling right side, the circular conical surface fitted seal on the right side of circular conical surface and fuelling coupling on the left of piston.Piston rod right end is stretched by oily adapter Left-side center hole, and clearance fit is hinged by the first split pin.Multiple windows are opened up by oily adapter middle part.Butt tube right end outer surface thread is connected with lower annulus set.Butt tube right end outlet outside is additionally provided with briquetting component, and briquetting component includes briquetting and cone roller.The axle bed of briquetting bottom and docking tube outer surface is hinged.It is hinged with cone roller at the top of briquetting.Lower annulus set is the horn shape being open to the right, and loudspeaker mouth circle is corresponding with briquetting bottom.It is set on the left of fuelling coupling and screws blanking cover component.It is simple in structure, easy to operate, check that the function by oil probe is normally in the air and the pressure of ground refueling is observed in leakproofness, monitoring.
Description
Technical field：
The present invention relates to being popped one's head in dock detection field in the air by oil, detection device is docked more particularly to being popped one's head in the air by oil.
Background technology
Air refuelling technology is of great significance to improving airborne combat efficiency, can be increased by air refuelling winged
Machine voyage and combat radius increase aircraft bullet-loading capacity, extend aircraft airborne period, improve aircraft utilization, reduce aircraft and set out
Quantity, flight refueling capability are direct one for determining fuel-servicing equipment verification complexity and influencing tanker refuelling system effective utilization
Important indicator, but really determine tanker refuelling system effective utilization often refueled aircraft by oily ability.In the air by oil tech
Be mounted on aircraft it is aerial docked with fuel-servicing equipment by oily probe apparatus, in the air by the safety of oily probe apparatus, close
Feng Xing, the normal operation of function are particularly important, it is therefore necessary to being normally detected in the air with leakproofness by the function of oil probe.
Popped one's head in the air by oil dock detection device, it can be achieved that detection in the air by the function of oil probe normally and leakproofness, and monitoring is seen
Examine the function of the pressure of ground refueling.
Invention content：
The object of the present invention is to provide being popped one's head in dock detection device in the air by oil, this equipment, which can be realized, to be checked in the air by oil probe
Function normally and leakproofness, and the pressure of monitoring observation ground refueling function, it is reasonable in design it is advanced, meet a variety of machines
The detection of type provides safety guarantee, practicality easy to operate.
The technical solution adopted is that：
It is popped one's head in the air by oil and docks detection device, including butt tube, fuelling coupling, piston and by oily adapter.
Technical points are：
Butt tube has axially extending bore, left end to have import, right end to have outlet.
The entrance of butt tube is fixed with fuelling coupling, and it is circular conical surface, circle that fuelling coupling, which is located on the inside of the import of butt tube,
Conical surface tip is towards a left side.
Piston is equipped on the inside of circular conical surface on the right side of fuelling coupling, the circular cone on the right side of circular conical surface and fuelling coupling on the left of piston
Face fitted seal.
Piston has piston rod to the right.Piston rod right end is stretched by oily adapter Left-side center hole, and mutual gap is matched
It closes, piston rod right end is equipped with the first split pin, is located in butt tube axially extending bore by oily adapter.
It is to be open to the right by oily adapter, hollow structure, left side tip closing, and opened up by oily adapter middle part surface
Multiple windows.Window has gap with pipe internal surface is docked.
On by oily adapter, it is located at window right side outer cylinder surface and docks inside pipe wall joint dynamic sealing.
Butt tube right end outer surface thread is connected with lower annulus set.
Butt tube right end outlet outside is additionally provided with multigroup briquetting component, and every group of briquetting component includes briquetting and cone roller.
The hole of briquetting bottom is hinged by the axle bed of axis pin and docking tube outer surface.
Hole at the top of briquetting passes through bolted splice with cone roller.
Lower annulus set is the horn shape being open to the right, and loudspeaker mouth circle is corresponding with briquetting bottom.
The outlet of butt tube right end also has by oily blanking cover of popping one's head in, and multiple oilings are fixed on fuelling coupling left end periphery
Connector is raised, and multiple fuelling coupling card slots are also provided in fuelling coupling left end circumferential end surfaces.
Blanking cover component is equipped on the left of fuelling coupling, blanking cover component screws on fuelling coupling.
It the advantage is that：
1, detection that is advanced, meeting different types of machines reasonable in design, provides safety guarantee, practicality easy to operate.
First aviation pressure oiling joint is accessed to be popped one's head in by oil in the air on ground and dock detection device, passes through aviation pressure
Fuelling coupling is engaged docking with the inside and outside convex block and card slot of this equipment, wouldn't pull aviation pressure oiling joint and connect switch.Then
It is docked with being popped one's head in the air by oil, rotates lower annulus, the lower lower annulus of annulus drive covers and briquetting component is in the air by oily probe orientation
It is mobile, make cone roller to inboard movement with one heart, locking is popped one's head in by oil in the air, and docking finishes；Aviation pressure oiling is finally pulled to connect
Head switch makes cutting somebody's hair inside aviation pressure oiling joint push piston, is extruded by oily probe spring switch when in the air certain
After stroke, snap switch is detached with end, is simultaneously open in the air by oil probe oil circuit and this service of connection devices oil circuit.
2, selection is suitable：
The service of connection devices material uses aerolite or titanium alloy material, light-weight, intensity is high.
3, it is used to be docked subject by oil in the air in ground surface simulated training；For check in the air by oil probe function normally with
Leakproofness, the pressure of monitoring observation ground refueling.
Description of the drawings：
Fig. 1 is the sectional view of the present invention（A-A sectional views in Fig. 2）.
Fig. 2 is the front view of the present invention.
Fig. 3 is the sectional view of circle ring device part in the present invention.
Fig. 4 is the front view of circle ring device part in the present invention.
Fig. 5 is the front view of briquetting component part of the present invention.
Fig. 6 is the left view of Fig. 5 of the present invention.
Fig. 7 is the front view of annulus and lower annulus set under the present invention.
Fig. 8 is the B-B sectional views of Fig. 7 of the present invention.
Fig. 9 is sectional view of the present invention by oily adapter component part.
Figure 10 is the front view of blanking cover components of the present invention.
Figure 11 is the C-C sectional views of Figure 10.
Figure 12 is the sectional view of inventive piston part.
Figure 13 is the partial sectional view of blanking cover components.
Figure 14 is the three-dimensional cutaway view of blanking cover components.
Figure 15 is the stereogram of fuelling coupling.
Figure 16 is the stereogram of end cap.
Figure 17 is the front sectional view of blanking cover components.
Figure 18 is the stereogram of the present invention.
Figure 19 be in the air by oil pop one's head in fuel feeding when structural schematic diagram.
Butt tube 1, upper circle ring device 2, briquetting component 3, the second guidance tape 4, by oil probe blanking cover 5,
Fuelling coupling 6, in the air by oil probe 7, by oily adapter component 8, blanking cover component 9, piston 10, limited post the 11, the 3rd 6
Hex bolt 12, the first hexagon-headed bolt 13, axis pin 14, plain washer 15, the second split pin 16, the second O-ring seal 17, first
O-ring seal 18, cross recessed countersunk head sscrew 19, meter connector component 20, briquetting 21, cone roller 22, the second hexagon-headed bolt 23, on
Annulus 24, fixed plate 25, lower annulus cover 26, lower annulus 27, connecting tube 28, are used by oily adapter 29, the first guidance tape 30, piston
Glais ring 31, vulcanized rubber circle 32, end cap 33, the second pin 34, the first pin 35, blanking cover 36, split washer 37, the O-shaped sealing of third
Circle 38, right chamber 40, left chamber 41, blocks 42, meter connector 43, bonded washer 44, the first split pin 45, pressure gauge at compressed spring 39
46, aviation pressure oiling joint 47, annular steps 1-1, fuelling coupling protrusion 6-1, fuelling coupling card slot 6-2, chamfering 6-1-1,
Snap switch 7-1, end 7-2, piston rod 10-1, piston boss 10-2, window 29-1, end cap ontology 33-1, end cap protrusion 33-
2, blanking cover central boss 36-1, the 47-1 that cuts somebody's hair, aviation pressure oiling joint switch 47-2.
Specific implementation mode：
It is popped one's head in the air by oil and docks detection device, including butt tube 1, fuelling coupling 6, piston 10 and by oily adapter 29（Such as Fig. 1
It is shown）.
Butt tube 1 has axially extending bore, left end to have import, right end to have outlet.
The entrance of butt tube 1 is fixed with fuelling coupling 6, and it is circular cone that fuelling coupling 6, which is located on the inside of the import of butt tube 1,
Face, circular conical surface tip is towards a left side.
Piston 10, circular conical surface and 6 right side of fuelling coupling in 10 left side of piston are equipped on the inside of the circular conical surface on 6 right side of fuelling coupling
Circular conical surface fitted seal, be sealed by the first O-ring seal 18.
There is piston rod 10-1 on 10 right side of piston（Cylinder）, have piston boss 10-2, piston boss 10- on piston rod 10-1
2 are located at by the outside of 29 Left-side center hole of oily adapter.
Piston rod 10-1 right ends are stretched by 29 Left-side center hole of oily adapter, can be in piston rod by oily adapter 29
It is slided on 10-1, mutual clearance fit, piston rod 10-1 right ends are equipped with the first split pin 45, and piston rod 10-1 passes through first
Split pin 45 is hinged with by oily adapter 29, and the first split pin 45 prevents piston 10 from falling off from by oily adapter 29, is turned by oil
Connector 29 is located in 1 axially extending bore of butt tube, and the first split pin 45 is located at by oily adapter 29.
It is bell, the hollow structure that is open to the right, left side tip by oily adapter 29（Left end is vertical plectane, to the right
Extend to circular conical surface）Closing, right openings（Round mouth）, and opened up multiple window 29-1 by 29 middle part surface of oily adapter.Window
Mouth 29-1 has gap with 1 inner surface of butt tube.
On by oily adapter 29, it is located at outer cylinder surface and 1 inner wall joint dynamic sealing of butt tube on the right side of window 29-1,
And it is left-to-right successively equipped with the first guidance tape 30, piston Glais ring 31 and the second guidance tape 4.
It is being equipped with vulcanized rubber circle 32 by 29 right openings edge of oily adapter.
1 right end of butt tube outlet outside is equipped with upper circle ring device 2, and upper circle ring device 2 includes upper annulus 24 and multiple fixations
Plate 25（It is three fixed plates 25 in the present embodiment）.Upper annulus 24 and multiple fixed plates 25 are weld assembly, multiple fixed plates 25
Even cloth is circumferentially.
The axis perpendicular of upper annulus 24 and butt tube 1 is fixed on by three fixed plates 25 on circumference outside butt tube 1
Surface.Fixed plate 25 is fixed on 1 outer surface of butt tube by the first hexagon-headed bolt 13.
1 right end outer surface thread of butt tube is connected with lower annulus set 26, and lower annulus set 26 is located at 24 left side of upper annulus.Lower circle
Ring set 26 is the horn shape being open to the right, and loudspeaker mouth circle is corresponding with 21 bottom of briquetting.
1 right end of butt tube outlet outside is additionally provided with multigroup briquetting component 3, and every group of briquetting component 3 includes briquetting 21 and two
Cone roller 22.It is three groups of briquetting components 3 in the present embodiment.3 even cloth of multigroup briquetting component is circumferentially.3 court of multigroup briquetting component
The center of circle is exported to 1 right end of butt tube.
The hole of 21 bottom of briquetting is hinged by the axle bed of 1 outer surface of axis pin 14, the second split pin 16 and butt tube.
The hole at 21 top of briquetting and the cone roller 22 at both ends are hinged with bolt (the second hexagon-headed bolt 23), two cone rollers
22 are located at the both sides of briquetting 21, and 22 tip of cone roller is opposite.
It is inside and outside conical surface contact by oil probe blanking cover 5 and the right end outlet of butt tube 1, the tip of circular conical surface is to the left.
Had a circle necking down by oil probe blanking cover 5, three groups totally six cone rollers 22 it is corresponding with necking down position.
Instantly annulus set 26 is moved to right-hand screw, can push away briquetting 21, and six cone rollers 22 are blocked by oil probe blanking cover 5
Necking down.
Instantly annulus set 26 is moved to left-hand screw, can decontrol briquetting 21, and six cone rollers 22 are decontroled by oil probe blanking cover 5
Necking down, can remove by oil pop one's head in blanking cover 5.
6 left side of fuelling coupling is equipped with blanking cover component 9, and blanking cover component 9 can screw on fuelling coupling 6.
Blanking cover component 9 includes end cap 33, blanking cover 36 and compressed spring 39.
The setting of blanking cover 36 in the round inner groovy in the left side of fuelling coupling 6,36 right side of blanking cover have third O-ring seal 38 with
The round inner groovy inner face sealing in 6 left side of fuelling coupling.
Blanking cover 36 stretch out to the left blanking cover central boss 36-1, discoidal end cap ontology 33-1 centre bore be set in it is stifled
On lid central boss 36-1, the centre bore left-external side of end cap ontology 33-1 is equipped with split washer 37, by split washer 37 end
Lid 33 is kept off on blanking cover 36, and compressed spring 39 is equipped between end cap ontology 33-1 and blanking cover 36.
End cap 33 can horizontally slip on blanking cover central boss 36-1, gap between them cooperation.
39 left end of compressed spring is supported with end cap ontology 33-1 phases, and 39 right end of compressed spring is supported with 36 phase of blanking cover.
The circumferential edges of end cap ontology 33-1 are equipped with multiple end cap protrusion 33-2 of back hook to the right, multiple end cap protrusions
The even cloth of 33-2 is circumferentially.End cap protrusion 33-2 is three in the present embodiment.
Multiple fuelling coupling protrusion 6-1 are fixed on 6 left end periphery of fuelling coupling.The present embodiment is three oilings
Connector protrusion 6-1, even cloth is circumferentially.End cap protrusion 33-2 is corresponding with the fuelling coupling positions protrusion 6-1.
Three end cap left surfaces protrusion 33-2 are fixed end cap 33 with three right surfaces fuelling coupling protrusion 6-1 and refuel
Connector 6.
End cap protrusion 33-2 is parallel with end cap ontology 33-1.
There are one the first pins 35 (interference fit) for the right surface fixations of end cap ontology 33-1.
The left surface of each end cap protrusion 33-2 is respectively and fixedly provided with second pin 34 (interference fit).
The end cap protrusion 33-2 adjacent with the first pin 35 that second pin 34 at left surface is located remotely from the first pin 35
Position.
On other two end cap protrusion 33-2, each fixed second pins 34 of end cap protrusion 33-2, position with it is above-mentioned that
A second pin 34 is identical.As shown in Figure 14,16,17.
When so that end cap protrusion 33-2 being compressed with fuelling coupling protrusion 6-1, the first pin 35 and that adjacent second pin 34
Positioned at the both sides of a fuelling coupling protrusion 6-1, the position of other two the second pin 34 and respectively corresponding fuelling coupling protrusion 6-1
Relative position it is identical as that second pin 34 above-mentioned and corresponding fuelling coupling protrusion 6-1 relative positions.
Multiple fuelling coupling card slot 6-2, multiple fuelling coupling card slot 6- are also provided in 6 left end circumferential end surfaces of fuelling coupling
2 even cloth uniformly interlock in circumferential end surfaces with fuelling coupling protrusion 6-1, and fuelling coupling card slot 6-2 is three in the present embodiment,
It is used when for connecting aviation pressure oiling joint 47.
Blanking cover component 9 installs detailed process：As viewed from the right side of Fig. 1：（As shown in figure 17）
The setting of blanking cover 36 is in the round inner groovy in 6 left side of fuelling coupling.
It presses end cap 33 and compresses compressed spring 39, end cap 33 slides on blanking cover central boss 36-1.
The end cap protrusion 33-2 of clockwise adjacent and the second pin 34 above connect from two oilings on first pin 35 and circumference
It is moved at neutral gear between head protrusion 6-1.Fuelling coupling protrusion 6-1 is also opposite from the neutral gear between end cap protrusion 33-2 to be moved
It is dynamic.
Other two end cap protrusion 33-2 and the second pin 34 respectively above move from corresponding neutral gear.
When three the second pins 34 press to be more than fuelling coupling protrusion 6-1 position, rotate clockwise, three the second pins 34 across
Fuelling coupling protrusion 6-1 is crossed, then looses one's grip and decontrols compressed spring 39, three the second pins 34 to three fuelling coupling protrusion 6-1
Homonymy, for the first pin 35 in the other side of a fuelling coupling protrusion 6-1, end cap protrusion 33-2 compresses fuelling coupling protrusion 6-1,
Blanking cover component 9 is installed on fuelling coupling 6.
End cap 33 is pressed again, is rotated counterclockwise, according to process opposite above, is taken blanking cover component 9.
The right sides fuelling coupling protrusion 6-1 are equipped with chamfering 6-1-1, when being engaged with the parts end cap protrusion 33-2 when in order to rotate
Guiding buffering.（When rotating clockwise, the parts end cap protrusion 33-2 are guided to move from bottom surface to high face）.
1 outside of butt tube is equipped with pressure gauge 46.Pressure gauge 46 is connected to 1 left chamber of butt tube by 29 left side of oily adapter
41。
Butt tube 1 and fuelling coupling 6, are circumferentially fastenedly connected by multiple screws, and multiple third turret head spiral shells are passed through
Bolt 12 fastens.
6 outer surface of fuelling coupling is sealing surface with 1 inner surface of butt tube, is sealed by the second O-ring seal 17.
Lower annulus set 26 is externally provided with lower annulus 27, passes through connecting tube 28（Steel pipe）It is fixed to be set in outside lower annulus set 26.
By oily adapter component 8（Including being oriented to by oily adapter 29, the first guidance tape 30, piston Glais ring 31, second
Band 4 and vulcanized rubber circle 32）It is dynamic sealing matching relationship with butt tube 1, and can be free to move axially in butt tube 1.
Vulcanized rubber circle 32, piston Glais ring 31, two guidance tapes are nested in the corresponding axial trough by oily adapter 29, vulcanization
Rubber ring 32 between snap switch 7-1 for sealing.
1 outer surface of butt tube is fixed with limited post 11, and limited post 11 makees spiral shell with butt tube 1 by cross recessed countersunk head sscrew 19
Line is fastenedly connected, and limited post 11 is located at 26 left side of lower annulus set.
This equipment need to be mounted on a platform when using, and connect with this equipment there are one connecting seat, used round anchor ear
It encases, limited post 11 is for preventing this equipment free play in anchor ear.
The meter connector component 20 of pressure gauge 46（Including blocking 42, meter connector 43 and bonded washer 44, blocks 42 and pass through screw thread
It is screwed with 43 one end of meter connector, bonded washer 44 is sleeved on 43 other end of meter connector, convenient for 43 external screw thread of meter connector and butt tube 1
Fastening and sealing function from when screw thread is installed）.
It is fixed with plain washer 15 by vertical plane on the right side of the Left-side center hole of oily adapter 29.
Left chamber 41 is piston 10 and the region by 29 left side of oily adapter.
Right chamber 40 is the region in the butt tube 1 by 29 right side of oily adapter.
Upper annulus 24 is played to by oil 7 guiding roles of probe, briquetting component 3 is located at 24 inside of upper annulus, prevents from pressing in the air
Block assembly 3 excessively turns up.
It is corresponding with the widest annular steps 1-1 of 1 interior diameter of butt tube by 29 right side of oily adapter.
Operation principle is：
When needing to check in the air by oily probe 7, left side blanking cover component 9 is removed, removes right side by oil probe blanking cover 5.
Shape by oil probe blanking cover 5 is consistent by oil 7 shapes of probe with exterior air, is also had a circle by oil probe 7 in the air
Necking down is similar to bell by 29 interior shape of oily adapter, is that basis is designed by oil 7 shapes of probe in the air.
It is stretched into the air from 1 right chamber 40 of butt tube by oily adapter 29 by oil probe 7, passes through the lower annulus 27 of rotation, lower annulus
Spiral moves set 26 to left and right, and either six cone rollers 22 of compression briquetting 21 drive are decontroled or locking is visited by oil in the air for relieving
First 7.
6 side of fuelling coupling connects aviation pressure oiling joint 47,47 outer cover of aviation pressure oiling joint and end cap 33
Shape is consistent, and manner is also consistent.
Aviation pressure oiling joint switch 47-2 is pulled when work, makes the 47-1 that cuts somebody's hair inside its aviation pressure oiling joint 47
It pushes piston 10 and drives and moved right by oily adapter component 8, squeezed in the air by the spring on oil probe 7 by oily adapter 29
Switch 7-1 makes snap switch 7-1 be detached with end 7-2, until squeeze make snap switch 7-1 compress certain distance after, in the air by
Oil 7 oil circuits of probe are opened, and vulcanized rubber circle 32 seals when to being refueled in the air by oil probe 7 with mouth at snap switch 7-1.
Oil is from left chamber 41, window 29-1, is popped one's head in 7 oil circuits by oil in the air by entering to the right in oily adapter 29, at this time can be with
Whether detection is good by the unobstructed and leakproofness of oil 7 oil circuits of probe in the air.
When fuel cut-off, aviation pressure oiling joint switch 47-2 is pulled first, switch is made to be closed, stop
The 47-1 that cuts somebody's hair inside aviation pressure oiling joint 47 pushes piston 10, is resetted in the air by the snap switch 7-1 in oil probe 7, to
It moves left, and pushes and be moved to the left by oily adapter 29, piston boss 10-2, until being sealed with 6 cone match of fuelling coupling good
It is good.
As can reaching above-mentioned requirements, both can be determined that normally good with leakproofness by the function of oil probe 7 in the air.
If above-mentioned requirements cannot be smoothly completed, judge in the air by oil probe 7 function is abnormal and poor sealing.
Butt tube 1, fuelling coupling 6, piston 10 and be aerolite or titanium alloy by 29 material of oily adapter, this is
Know material.
Claims (10)
1. popped one's head in by oil docks detection device, including butt tube in the air（1）, fuelling coupling（6）, piston（10）With by oily adapter
（29）, it is characterised in that：
Butt tube（1）There are axially extending bore, left end to there is import, right end to have outlet；
Butt tube（1）Entrance be fixed with fuelling coupling（6）, fuelling coupling（6）Positioned at butt tube（1）Import on the inside of for circle
The conical surface, circular conical surface tip is towards a left side；
Fuelling coupling（6）Piston is equipped on the inside of the circular conical surface on right side（10）, piston（10）The circular conical surface and fuelling coupling in left side（6）
The circular conical surface fitted seal on right side；
Piston（10）There is piston rod to the right（10-1）；Piston rod（10-1）Right end is stretched by oily adapter（29）Left-side center
In hole, mutual clearance fit, piston rod（10-1）Right end is equipped with the first split pin（45）, by oily adapter（29）Positioned at pair
It takes over（1）In axially extending bore；
By oily adapter（29）To be open to the right, hollow structure, left side tip closing, and by oily adapter（29）Middle part surface
Open up multiple windows（29-1）；Window（29-1）With butt tube（1）Inner surface has gap；
By oily adapter（29）On, it is located at window（29-1）Right side outer cylinder surface and butt tube（1）Move close in inner wall joint
Envelope.
2. according to claim 1 popped one's head in the air by oil docks detection device, it is characterised in that：
Butt tube（1）Right end outer surface thread is connected with lower annulus set（26）；
Butt tube（1）Right end outlet outside is additionally provided with multigroup briquetting component（3）, every group of briquetting component（3）Including briquetting（21）With
Cone roller（22）；
Briquetting（21）The hole of bottom passes through axis pin（14）And butt tube（1）The axle bed of outer surface is hinged；
Briquetting（21）The hole at top and cone roller（22）Pass through bolted splice；
Lower annulus set（26）For the horn shape being open to the right, loudspeaker mouth circle and briquetting（21）Bottom is corresponding.
3. according to claim 1 popped one's head in the air by oil docks detection device, it is characterised in that：Butt tube（1）Right end has
Outlet also has by oil probe blanking cover（5）.
4. according to claim 1 popped one's head in the air by oil docks detection device, it is characterised in that：Fuelling coupling（6）Left end
Multiple fuelling coupling protrusions are fixed on head periphery（6-1）, fuelling coupling（6）It is also provided in left end circumferential end surfaces multiple
Fuelling coupling card slot（6-2）.
5. according to claim 4 popped one's head in the air by oil docks detection device, it is characterised in that：Fuelling coupling（6）Left side
Equipped with blanking cover component（9）, blanking cover component（9）Screw fuelling coupling（6）On.
6. according to claim 5 popped one's head in the air by oil docks detection device, it is characterised in that：Blanking cover component（9）Including
End cap（33）, blanking cover（36）And compressed spring（39）；
Blanking cover（36）It is arranged in fuelling coupling（6）In the inner groovy of left side；
Blanking cover（36）Blanking cover central boss is stretched out to the left（36-1）, end cap ontology（33-1）Centre bore be set in blanking cover center
Boss（36-1）On, gap between them cooperation, end cap ontology（33-1）Centre bore left-external side be blocked in blanking cover central boss
（36-1）On；
End cap ontology（33-1）And blanking cover（36）Between be equipped with compressed spring（39）；
End cap ontology（33-1）Circumferential edges be equipped with to the right back hook multiple end caps protrusion（33-2）；
Fuelling coupling（6）Multiple fuelling coupling protrusions are fixed on left end periphery（6-1）；
End cap protrusion（33-2）Left surface and corresponding fuelling coupling protrusion（6-1）Right surface is fixed end cap（33）And oiling
Connector（6）.
7. according to claim 6 popped one's head in the air by oil docks detection device, it is characterised in that：End cap ontology（33-1）It is right
There are one the first pins for surface fixation（35）；
Each end cap protrusion（33-2）Left surface be respectively and fixedly provided with one second pin（34）；
With the first pin（35）Adjacent end cap protrusion（33-2）Fixed second pin on left surface（34）It is located remotely from the first pin
（35）Position；
Multiple second pins（34）It is stuck in end cap protrusion（33-2）Side limits, the first pin（35）With the second adjacent pin（34）It is stuck in
Corresponding that end cap protrusion（33-2）Both sides.
8. according to claim 1 popped one's head in the air by oil docks detection device, it is characterised in that：Butt tube（1）Right end goes out
Upper circle ring device is equipped on the outside of mouthful（2）, upper circle ring device（2）Including upper annulus（24）With multiple fixed plates（25）, fixed plate
（25）It is fixed on butt tube（1）On.
9. according to claim 1 popped one's head in the air by oil docks detection device, it is characterised in that：Butt tube（1）, refuel connect
Head（6）, piston（10）With by oily adapter（29）Material is aerolite or titanium alloy.
10. according to claim 1 popped one's head in the air by oil docks detection device, it is characterised in that：Butt tube（1）Left chamber
（41）It is connected with pressure gauge（46）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810477148.2A CN108545215B (en) | 2018-05-18 | 2018-05-18 | Butt joint detection equipment for aerial oil receiving probe |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810477148.2A CN108545215B (en) | 2018-05-18 | 2018-05-18 | Butt joint detection equipment for aerial oil receiving probe |
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| CN108545215A true CN108545215A (en) | 2018-09-18 |
| CN108545215B CN108545215B (en) | 2023-10-03 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111749794A (en) * | 2020-07-08 | 2020-10-09 | 中国航发沈阳发动机研究所 | Lubricating oil pressure filling device |
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| DE520180C (en) * | 1926-11-25 | 1931-03-09 | Donald Hugh Baillie Reynolds L | Sealing testing device for pipe joints |
| KR200301210Y1 (en) * | 2002-10-22 | 2003-01-17 | 안중곤 | Leak tester |
| CN103738502A (en) * | 2013-11-27 | 2014-04-23 | 中国航空工业集团公司西安飞机设计研究所 | Airplane air oil-receiving device ground detecting switching equipment |
| CN105083586A (en) * | 2015-08-12 | 2015-11-25 | 中国航空工业集团公司西安飞机设计研究所 | Device for testing aerial refueling adapter equipment |
| CN208149645U (en) * | 2018-05-18 | 2018-11-27 | 沈阳飞研航空设备有限公司 | It is popped one's head in the air by oil and docks detection device |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE520180C (en) * | 1926-11-25 | 1931-03-09 | Donald Hugh Baillie Reynolds L | Sealing testing device for pipe joints |
| KR200301210Y1 (en) * | 2002-10-22 | 2003-01-17 | 안중곤 | Leak tester |
| CN103738502A (en) * | 2013-11-27 | 2014-04-23 | 中国航空工业集团公司西安飞机设计研究所 | Airplane air oil-receiving device ground detecting switching equipment |
| CN105083586A (en) * | 2015-08-12 | 2015-11-25 | 中国航空工业集团公司西安飞机设计研究所 | Device for testing aerial refueling adapter equipment |
| CN208149645U (en) * | 2018-05-18 | 2018-11-27 | 沈阳飞研航空设备有限公司 | It is popped one's head in the air by oil and docks detection device |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111749794A (en) * | 2020-07-08 | 2020-10-09 | 中国航发沈阳发动机研究所 | Lubricating oil pressure filling device |
| CN111749794B (en) * | 2020-07-08 | 2022-12-20 | 中国航发沈阳发动机研究所 | Lubricating oil pressure filling device |
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| Publication number | Publication date |
|---|---|
| CN108545215B (en) | 2023-10-03 |
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