CN109599003A - A kind of multi-functional training platform for the assembly of aircraft conduit - Google Patents
A kind of multi-functional training platform for the assembly of aircraft conduit Download PDFInfo
- Publication number
- CN109599003A CN109599003A CN201910071526.1A CN201910071526A CN109599003A CN 109599003 A CN109599003 A CN 109599003A CN 201910071526 A CN201910071526 A CN 201910071526A CN 109599003 A CN109599003 A CN 109599003A
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- Prior art keywords
- conduit
- assembly
- table top
- folded plate
- plate
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- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M3/00—Investigating fluid-tightness of structures
- G01M3/02—Investigating fluid-tightness of structures by using fluid or vacuum
- G01M3/26—Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors
- G01M3/28—Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors for pipes, cables or tubes; for pipe joints or seals; for valves ; for welds
- G01M3/2807—Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors for pipes, cables or tubes; for pipe joints or seals; for valves ; for welds for pipes
- G01M3/2815—Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors for pipes, cables or tubes; for pipe joints or seals; for valves ; for welds for pipes using pressure measurements
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- Engineering & Computer Science (AREA)
- Theoretical Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Business, Economics & Management (AREA)
- Educational Administration (AREA)
- Educational Technology (AREA)
- Mutual Connection Of Rods And Tubes (AREA)
- Examining Or Testing Airtightness (AREA)
Abstract
The invention discloses a kind of multi-functional training platforms for the assembly of aircraft conduit, air-tightness detection device including cabinet body and for detecting conduit air-tightness, cabinet body includes frame and the table top that is fixedly mounted on above frame, the top of table top is upper assembly space, the lower section of table top is lower assembly space, support is used for equipped with several in upper assembly space and changes the folded plate of conduit bending angle, it is also provided with several on table top and is used for the via hole that conduit passes through, support is used for equipped with several in lower assembly space and changes the orifice plate of conduit bending angle, the lower portion of cabinet body has been removably installed crossbeam and stringer, the orifice plate is removably mounted on crossbeam or stringer, orifice plate is slidably connected by slide assemblies with the sliding slot being provided on crossbeam and stringer.The present invention is capable of the basic assemble ability of training technique personnel, moreover it is possible to by promoting difficulty come the assemble ability of lift technique personnel, have training efficiency height, the good advantage of result of training.
Description
Technical field
The present invention relates to aircraft conduit assembly field more particularly to a kind of multi-functional trainings for the assembly of aircraft conduit
Platform.
Background technique
With the continuous development of aero-manufacturing technology, manufacture and installation accuracy to aircraft conduit require also to be continuously improved,
The installation quality of aircraft conduit has become one of most important link in modern aircraft manufacture.And due to aircraft and its engine
On conduit it is very much, and require to save conduit as far as possible and be taken up space, it is therefore necessary to by guiding-tube bend at various shape, to avoid
It interferes with each other in a limited space, causes the installation difficulty of aircraft conduit higher.
Interior of aircraft pipeline needs a large amount of skilled engineers to come as the essential a part of aircraft system
At the assembly of interior of aircraft pipeline, reality but faces problem in detail below.
With the rapid development of aircraft industries, interior of aircraft pipeline becomes increasingly complex, and the requirement to technical staff is increasingly
Height, the demand to technical staff are even more to increase, and following contradiction occur: 1, for the stability of aircraft and safety, not having
The technical staff of experience can not go to assemble to scene, on the other hand, in the feelings that not true aircraft or prototype quantity are considerably less
It (is hardly directly trained on prototype) under condition, needs to complete the training mission of the assembly maintenance to aircraft conduit；2, with
Aircraft technology it is higher and higher, the complexity of internal pipeline is also higher and higher, cause technical staff assembly aircraft conduit
When need to possess consummate technology, and assemble training device without molding aircraft conduit in the prior art, can more not fit
Answer the assembly training device of plurality of specifications aircraft catheter models；3, the contradiction of technical staff's scarcity and actual demand.
Summary of the invention
The present invention provides a kind of for the multi-functional of aircraft conduit assembly to solve shortcoming in the prior art
Training station, can training technique personnel basic assemble ability, air-leakage test can carried out at once after the assembly is completed, moreover it is possible to logical
It crosses and promotes the assemble ability that difficulty carrys out lift technique personnel, the personnel's that develop skill is professional, has training efficiency high, training is imitated
The good advantage of fruit.
The present invention adopted the technical scheme that solve the above-mentioned problems, is provided a kind of for the assembly of aircraft conduit
Multi-functional training platform comprising cabinet body and the air-tightness detection device for detecting conduit air-tightness, cabinet body include frame and consolidate
Table top of the Dingan County above frame, the top of table top are upper assembly space, and the lower section of table top is lower assembly space, and upper assembly is empty
In equipped with several for support and change the folded plate of conduit bending angle, offer several mounting holes on table top, it is described
Folded plate has different size and is removably mounted on table top respectively, and the folded plate has different inclinations angle in the horizontal plane
Degree, so that the angle that conduit passes through changes.
Several are also provided on table top for the via hole that conduit passes through, the via hole uniform intervals are arranged and are
Through-hole for support and changes the orifice plate of conduit bending angle equipped with several in lower assembly space, offers first on folded plate
Location hole offers second location hole on orifice plate, connector, connector is separately installed in first positioning hole and second location hole
It is connect with conduit.The lower portion of cabinet body has been removably installed crossbeam and stringer, and crossbeam and stringer pass through angled seat and fastening spiral shell
Bolt links together with frame, in this way, the position of crossbeam and stringer can rapidly adjust at any time according to customer demand, it is convenient fast
It is prompt.The orifice plate is removably mounted on crossbeam or stringer by fastening bolt, and each orifice plate is displayed in the extension of crossbeam length
Different location on direction or stringer length extending direction offers sliding slot on crossbeam and stringer, and the orifice plate passes through sliding
Component is slidably connected with sliding slot.
Preferably, the folded plate includes the first folded plate, the second folded plate, third folded plate and the 4th folded plate, the first folded plate, second
The width of folded plate, third folded plate and the 4th folded plate is sequentially increased.
Preferably, watch window is offered on the table top, the outside of watch window is arranged in mounting hole.At watch window
It is hinged with cover board by hinge, observes assembly situation in lower assembly space convenient for raising cover board, it is also mountable at watch window
Transparent glass window can be observed without raising.
Preferably, the two sides of each via hole symmetrically open up the mounting hole.
Preferably, the slide assemblies include hexagon socket head cap screw and tetragonal nut, and the sliding slot is T shape sliding slot, quadrangle spiral shell
Mother is slidably connected in sliding slot, and hexagon socket head cap screw is protruded into sliding slot and is threadedly coupled with tetragonal nut.
The aluminum profile of different length can be used in the crossbeam and stringer, has on four surfaces of existing aluminum profile and slides
Slot, pipe clamp and orifice plate can be moved on aluminum profile by slide assemblies.
Preferably, several pipe clamps for fixed catheter are additionally provided in lower assembly space, pipe clamp can by slide assemblies
It is releasably mounted on crossbeam or stringer, each pipe clamp is mounted on crossbeam length extending direction or stringer length extending direction
Different location, the pipe clamp include pipe clamp body, and the holding holes of through tube clamp are offered on pipe clamp body, and the two sides of holding holes are symmetrical
Offer bolt hole.
Preferably, the invention also includes the air-tightness detection device for detecting conduit air-tightness, air-tightness detection devices
Including gas source, check valve, pressure regulator valve, switch valve, pressure gauge and relief valve, portable pressure source is can be used in gas source, can also be used
Electric air pump, gas source are connect by pressure supply pipeline with the tube at one end that assembly is completed, and the other end for assembling the conduit of completion blocks,
Check valve, pressure regulator valve, switch valve and pressure gauge are successively set on pressure supply pipeline along gas flow direction, are located on pressure supply pipeline
Position between switch valve and pressure gauge is connected with pressure relief pipe, and relief valve is mounted on pressure relief pipe, pacifies on the table top of cabinet body
Equipped with console, pressure regulator valve, switch valve, pressure gauge and relief valve are installed on console, are provided with below table top for putting
Set the pump box of gas source.
Preferably, filter is connected between gas source and check valve.
Preferably, back plate is installed on rear side of frame, left plate is installed on the left of frame, the right side is installed on the right side of frame
Side plate.
Preferably, the bottom of frame is equipped with castor.Specifically, the bottom four corners of frame are welded with castor connecting board, foot
The steel plate that connecting plate is 10mm thickness is taken turns, castor is mounted on castor connecting board.
By adopting the above technical scheme, the invention has the following advantages that
The technical staff of installation aircraft conduit can not quickly and accurately assemble interior of aircraft before no contact aircraft
Catheter channel.Multi-functional training platform of the invention is exactly one and is used for training technique personnel before being not exposed to aircraft, mentions
The preceding training exercising platform for grasping interior of aircraft catheter channel erectility.
The present invention is easy duplication, solves the problems, such as that unfamiliar technical staff can not remove assembly, Xin Shouwu to scene
The problem of method directly participates in, at the same also solve the disadvantage that can not a large amount of training technique personnel simultaneously, convenient for improving culture technique
The efficiency of personnel cultivates more technical staff.
Upper assembly space and the components (such as folded plate, orifice plate and pipe clamp) of the fixed catheter in lower assembly space can be one
Determine to move in range, as the components of fixed catheter are mobile, catheter position will change, the advantage that be can be with
Training technique personnel assemble the ability of interior of aircraft conduit in different situations.Orifice plate and pipe clamp can pass through slide assemblies respectively
On crossbeam or stringer sliding slot sliding, can Fast transforms orifice plate and pipe clamp position, operate it is convenient.
The present invention display combination different on table top by the folded plate of different size, crossbeam and stringer and frame
The change in location of position adjustment and pipe clamp on crossbeam or stringer is trained to realize that the conduit of different pipeline models assembles,
The training objectives of plurality of specifications aircraft conduit installation requirements can be realized by having reached a training station.
After completing conduit using present invention assembly, it can be used the air-tightness detection device being mounted in the present invention to assembly
The conduit of completion carries out air-leakage test, checks the training effect of assembly in real time, in time, result of training is good for feedback.
To sum up, multi-functional training platform of the invention can assemble the conduit of different pipeline model and different size, can
The basic assemble ability of training technique personnel can carry out air-leakage test at once after the assembly is completed, moreover it is possible to by promoting difficulty
Carry out the assemble ability of lift technique personnel.
Detailed description of the invention
Fig. 1 is the schematic perspective view of the preferred embodiment of the present invention；
Fig. 2 is one of cross-sectional view of Fig. 1；
Fig. 3 is the two of the cross-sectional view of Fig. 1；
Fig. 4 is the three of the cross-sectional view of Fig. 1；
Fig. 5 is the slide assemblies structural schematic diagram of the preferred embodiment of the present invention；
Fig. 6 is the structural schematic diagram of pipe clamp in the present invention；
Fig. 7 is the air circuit connection schematic diagram of the air-tightness detection device in the present invention.
Specific embodiment
As shown in Figures 1 to 7, a kind of multi-functional training platform for the assembly of aircraft conduit of the invention includes cabinet body and use
In the air-tightness detection device of detection conduit air-tightness, cabinet body includes frame 4 and the table top 6 for being fixedly mounted on 4 top of frame, frame
Frame 4 is one a length of 2 meters made of the C-type steel welded steel with different size, and width is 1.2 meters, high-order 0.71 meter of cuboid
Frame.The rear side of frame 4 is equipped with back plate 22, and the left side of frame 4 is equipped with left plate 5, and the right side of frame 4 is equipped with right side plate
16.Back plate 22, left plate 5 and right side plate 16 are welded on frame 4, and back plate 22, left plate 5 and right side plate 16 are 2mm
Thick stainless steel plate.
The bottom of frame 4 is equipped with castor 1, easy to remove.Specifically, the bottom four corners of frame 4 are welded with castor connection
Plate 2, castor connecting board 2 are the steel plate of 10mm thickness, and castor 1 is mounted on castor connecting board 2.Castor 1, which is selected, has service brake can
Self-locking castor is carried out, multi-functional training platform of the invention has both been moved easily, has nor affected on the fixation of multi-functional training platform.
The top of table top 6 is upper assembly space, and the lower section of table top 6 is lower assembly space, is equipped in upper assembly space several
It is a for support and to change the folded plate of conduit bending angle, several mounting holes 13 are offered on table top 6, the folded plate has not
It same specification and is removably mounted on table top 6 respectively, the folded plate displays out different tilt angles in the horizontal plane, by each
Mutual alignment between folded plate changes, and realizes the bending angle for changing conduit.The folded plate is L shape, and the horizontal position of folded plate is logical
It crosses fastening bolt to be mounted on table top 6, first positioning hole 15 is offered on the vertical position of folded plate, is installed in first positioning hole 15
There are connector, connector connecting conduit.The connector is navigation mark part (Aviation Industry standard component), and it is straight that A type can be selected in navigation mark part
Connection for bbreather pipe and its supporting part, the conduit of each diameter correspond to specific A type free flow coupling.
The folded plate includes the first folded plate 10, the second folded plate 9, third folded plate 8 and the 4th folded plate 7, the first folded plate 10, second
The width of folded plate 9, third folded plate 8 and the 4th folded plate 7 is sequentially increased.Mounting hole 13 can be in a row placed equidistant with, the folding of different in width
Plate can choose any two or more than two mounting hole 13 carries out installation fixation, and in the present embodiment, the width of the first folded plate 10 is
100mm, the width of the second folded plate 9 are 150mm, and the width of third folded plate 8 is 200mm, and the width of the 4th folded plate 7 is 300mm.The
One folded plate 10 does not tilt in the horizontal plane, the second folded plate 9, the inclined degree of third folded plate 8 and the 4th folded plate 7 in the horizontal plane according to
Secondary reduction.The bending angle of different size that can change conduit of folded plate, the folded plate of same specification width have not in the horizontal plane
With the bending angle that can equally change conduit when inclined degree, the folded plate of the folded plate of different in width and different inclined degrees forms more
Kind display combination, the different display combination of folded plate make conduit have different bending angles, so as to realize dress
Demand with different conduits.
Watch window is offered on the table top 6, the outside of watch window is arranged in mounting hole 13.Pass through at watch window
Hinge 12 is hinged with cover board 11, convenient for raising the assembly situation under cover board 11 is observed in assembly space, can also pacify at watch window
Transparent glass window is filled, can be observed without raising.
Several are also provided on table top 6 for the via hole 14 that conduit passes through, 14 uniform intervals of the via hole setting
And be through-hole, it is connected to the upper assembly space and lower assembly space of table top 6, the two sides of each via hole 14 symmetrically open up the peace
Hole 13 is filled, setting in this way is the slave peace that conduit can be convenient in order to meet after folded plate configured on table top 6 by mounting hole 13
It is pierced by or draws in the via hole 14 that dress hole 13 is closed on.The conduit of upper assembly space can enter lower assembly by via hole 14
Space, with this come connect up and down assembly space.The meaning of the setting of assembly space up and down of the invention: being that interior of aircraft is certain first
Having conduit is to move towards up and down, in addition, lower assembly space also simulates operator in the narrow work of interior of aircraft and operation ring
Border.
Support is used for equipped with several in lower assembly space and changes the orifice plate 18 of conduit bending angle, and orifice plate 18 is equipped with
Second location hole 19, connector, connector connecting conduit are equipped in second location hole 19, and the connector is navigation mark part (boat
Null industry standard component), A type free flow coupling and its supporting part can be selected in navigation mark part, removably pacifies inside the frame 4 of cabinet body
Equipped with crossbeam 20 and stringer 21, crossbeam 20 and stringer 21 are linked together by angled seat and fastening bolt with frame 4, in this way, horizontal
The position of beam 20 and stringer 21 can rapidly adjust at any time according to customer demand, convenient and efficient.The orifice plate 18 passes through fastening
Bolt is removably mounted on crossbeam 20 or stringer 21.
As shown in figure 5, offering sliding slot 31, the orifice plate along respective length extending direction on crossbeam 20 and stringer 21
18 are slidably connected by slide assemblies with sliding slot 31.The slide assemblies include hexagon socket head cap screw 33 and tetragonal nut 32, described
Sliding slot 31 is T shape sliding slot 31, and tetragonal nut 32 is slidably connected in sliding slot 31, and hexagon socket head cap screw 33 protrudes into sliding slot 31 and with four
Angle nut 32 is threadedly coupled.Using tetragonal nut 32 rather than hex nut, be to be easier to rotate in sliding slot 31 due to hex nut.
The pipe clamp for fixed catheter is additionally provided in lower assembly space, pipe clamp is removably mounted on cross by slide assemblies
On beam 20 or stringer 21, the pipe clamp includes pipe clamp body 41, and the holding holes 42 of through tube clamp are offered on pipe clamp body 41, clamping
The two sides in hole 42 symmetrically offer bolt hole 43.Annular protrusion is equipped in holding holes 42, it is possible to increase frictional force.
In the present embodiment, the crossbeam 20 and stringer 21 can be used the aluminum profile of different length, and four of existing aluminum profile
There is sliding slot 31, pipe clamp and orifice plate 18 can be moved on aluminum profile by slide assemblies, can be according to specific when training on surface
Demand quickly adjusts the position of orifice plate 18 and pipe clamp.Hexagon socket head cap screw 33 passes through orifice plate 18 or pipe clamp and 32 screw thread of tetragonal nut connects
It connects, when adjusting position, unscrews hexagon socket head cap screw 33, it is convenient and efficient.
The invention also includes the air-tightness detection device for detecting conduit air-tightness, air-tightness detection device includes gas source
28, portable pressure source can be used in check valve 30, pressure regulator valve 25, switch valve 26, pressure gauge 24 and relief valve 27, gas source 28,
Electric air pump can be used, gas source 28 is connect by pressure supply pipeline with the tube at one end that assembly is completed, and the another of the conduit of completion is assembled
One end block, check valve 30, pressure regulator valve 25, switch valve 26 and pressure gauge 24 along gas flow direction (in Fig. 7 shown in arrow side
To) be successively set on pressure supply pipeline, filter 29 is connected between gas source 28 and check valve 30.
Position on pressure supply pipeline between switch valve 26 and pressure gauge 24 is connected with pressure relief pipe, and relief valve 27 is installed
On pressure relief pipe, one end of pressure relief pipe is connected on pressure supply pipeline, and the other end of pressure relief pipe is communicated with the atmosphere, cabinet body
Console 23 is installed, console 23 is welded on the upper right corner of table top 6, pressure regulator valve 25, switch valve 26, pressure gauge 24 on table top 6
It is installed on console 23 with relief valve 27, can control the on-off and pressure size of gas circuit, be provided with and be used for below table top 6
The pump box 17 of gas source 28 is placed, pump box 17 is towards the one side closed of interior of the cabinet, and pump box 17 is open towards the side outside cabinet body, pump
Case 17 can not only place portable pressure source, can also place some other tools.
It is different on table top 6 by the folded plate of different size when realizing that different pipeline model conduits assembles training
Display the position of position adjustment and pipe clamp on crossbeam 20 or stringer 21 of combination, crossbeam 20 and stringer 21 with frame 4
Variation to realize, substantially be change for support and change conduit bending angle orifice plate 18 and folded plate on training station
Mutual alignment relation is realized.When realizing the assembly of conduit of different size training, change first positioning hole 15 on folded plate
And on orifice plate 18 second location hole 19 size, corresponding replacement connector, such as A type free flow coupling and its supporting part
Specification.Such flexible setting, plurality of specifications aircraft conduit installation requirements can be realized by having reached a training station
Training objective.
Since the training station is easy duplication, so that asking for assembly can not be gone to scene by solving unfamiliar technical staff
Topic, while also solving the disadvantage that a large amount of training technique personnel to cultivate simultaneously convenient for improving the efficiency of culture technique personnel
More technical staff.
After having assembled conduit using the present invention, the air-tightness detection device being mounted in the present invention can be used to complete assembly
Conduit carry out air-leakage test, check the training effect of assembly in real time, result of training is good.
When detecting air-tightness, pressure supply pipeline and pressure relief pipe are connected, turns on the switch valve 26, closes relief valve 27, starting
Gas source 28 is supplied, and after the completion of gas supply, turns off the switch valve 26, if the conduit poor air-tightness that assembly is completed, pressure gauge 24
Degree cannot keep stabilization, after air-leakage test, opens the relief valve 27 on pressure relief pipe, the gas in conduit is discharged
Into atmosphere.
It is the castor 1, connector (navigation mark part), hexagon socket head cap screw 33, tetragonal nut 32, gas source 28, filter 29, unidirectional
Valve 30, pressure regulator valve 25, switch valve 26, pressure gauge 24 and relief valve 27 are existing conventional equipment, are specifically no longer described in detail.
Above-described embodiment not makes any form of restriction shape of the invention, material, structure etc., all according to this
The technical spirit of invention any simple modification, equivalent change and modification to the above embodiments, belong to the technology of the present invention
The protection scope of scheme.
Claims (10)
1. a kind of multi-functional training platform for the assembly of aircraft conduit, it is characterised in that: including cabinet body and for detecting conduit gas
The air-tightness detection device of close property, cabinet body include frame and the table top that is fixedly mounted on above frame, and the top of table top is upper dress
With space, the lower section of table top is lower assembly space, is equipped with several for support in upper assembly space and changes conduit bending angle
The folded plate of degree, several mounting holes are offered on table top, and the folded plate has different size and is removably mounted at table top respectively
On, each folded plate displays out different tilt angles in the horizontal plane；
Several are also provided on table top for the via hole that conduit passes through, the via hole uniform intervals are arranged and are logical
Hole, the interior orifice plate for being used for support equipped with several and change conduit bending angle of lower assembly space, the lower portion of cabinet body are removable
Crossbeam and stringer are installed with unloading, the orifice plate is removably mounted on crossbeam or stringer, and it is long that each orifice plate is displayed in crossbeam
The different location on extending direction or stringer length extending direction is spent, sliding slot is offered on crossbeam and stringer, the orifice plate is logical
Slide assemblies are crossed to be slidably connected with sliding slot；
First positioning hole is offered on folded plate, and second location hole is offered on orifice plate, is divided in first positioning hole and second location hole
Connector is not installed, connector is connect with conduit.
2. a kind of multi-functional training platform for the assembly of aircraft conduit according to claim 1, it is characterised in that: the folding
Plate includes the first folded plate, the second folded plate, third folded plate and the 4th folded plate, the first folded plate, the second folded plate, third folded plate and four fold
The width of plate is sequentially increased.
3. a kind of multi-functional training platform for the assembly of aircraft conduit according to claim 1, it is characterised in that: described
Watch window is offered on face, the outside of watch window is arranged in mounting hole.
4. a kind of multi-functional training platform for the assembly of aircraft conduit according to claim 1, it is characterised in that: each lead
The two sides of through-hole symmetrically open up the mounting hole.
5. a kind of multi-functional training platform for the assembly of aircraft conduit according to claim 1, it is characterised in that: the cunning
Dynamic component includes hexagon socket head cap screw and tetragonal nut, and the sliding slot is T shape sliding slot, and tetragonal nut is slidably connected in sliding slot, interior
Hex bolts is protruded into sliding slot and is threadedly coupled with tetragonal nut.
6. a kind of multi-functional training platform for the assembly of aircraft conduit according to claim 1 or 5, it is characterised in that: under
Be additionally provided with several pipe clamps for fixed catheter in assembly space, pipe clamp by slide assemblies be removably mounted on crossbeam or
On stringer, each pipe clamp is mounted on the different location on crossbeam length extending direction or stringer length extending direction, the pipe clamp
Including pipe clamp body, the holding holes of through tube clamp are offered on pipe clamp body, the two sides of holding holes symmetrically offer bolt hole.
7. a kind of multi-functional training platform for the assembly of aircraft conduit according to claim 1, it is characterised in that: air-tightness
Detection device includes gas source, check valve, pressure regulator valve, switch valve, pressure gauge and relief valve, and gas source passes through pressure supply pipeline and assembled
At tube at one end connection, assemble the conduit of completion the other end block, check valve, pressure regulator valve, switch valve and pressure gauge are along gas
Body flow direction is successively set on pressure supply pipeline, and the position on pressure supply pipeline between switch valve and pressure gauge, which is connected with, lets out
Pressure pipe road, relief valve are mounted on pressure relief pipe, are equipped with console on the table top of cabinet body, pressure regulator valve, switch valve, pressure gauge and
Relief valve is installed on console, and the pump box for placing gas source is provided with below table top.
8. it is according to claim 7 it is a kind of for aircraft conduit assembly multi-functional training platform, it is characterised in that: gas source with
Filter is connected between check valve.
9. a kind of multi-functional training platform for the assembly of aircraft conduit according to claim 8, it is characterised in that: frame
Rear side is equipped with back plate, and left plate is equipped on the left of frame, is equipped with right side plate on the right side of frame.
10. a kind of multi-functional training platform for the assembly of aircraft conduit according to claim 9, it is characterised in that: frame
Bottom castor is installed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910071526.1A CN109599003B (en) | 2019-01-25 | 2019-01-25 | Multifunctional training table for aircraft duct assembly |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910071526.1A CN109599003B (en) | 2019-01-25 | 2019-01-25 | Multifunctional training table for aircraft duct assembly |
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| CN109599003B CN109599003B (en) | 2023-09-19 |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN110246406A (en) * | 2019-04-29 | 2019-09-17 | 广州飞机维修工程有限公司 | A kind of rack for the simulation of aircraft pipeline construction |
| CN110389036A (en) * | 2019-07-26 | 2019-10-29 | 中国航发沈阳发动机研究所 | Simulate the generic item bank of the true mounting coordinate of aero-engine exterior line |
| CN113470476A (en) * | 2021-08-20 | 2021-10-01 | 沈阳飞机工业（集团）有限公司 | Dynamic simulation training operating platform of airplane control system and using method |
| CN113706954A (en) * | 2021-08-18 | 2021-11-26 | 凌云(宜昌)航空装备工程有限公司 | Integrated aircraft maintenance skill training device |
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| CN110389036A (en) * | 2019-07-26 | 2019-10-29 | 中国航发沈阳发动机研究所 | Simulate the generic item bank of the true mounting coordinate of aero-engine exterior line |
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| CN113706954B (en) * | 2021-08-18 | 2023-02-07 | 凌云(宜昌)航空装备工程有限公司 | Integrated aircraft maintenance skill training device |
| CN113470476A (en) * | 2021-08-20 | 2021-10-01 | 沈阳飞机工业（集团）有限公司 | Dynamic simulation training operating platform of airplane control system and using method |
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| CN109599003B (en) | 2023-09-19 |
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