CN209513667U - A kind of rudder of aircraft ray detection tooling - Google Patents
A kind of rudder of aircraft ray detection tooling Download PDFInfo
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- CN209513667U CN209513667U CN201920101396.7U CN201920101396U CN209513667U CN 209513667 U CN209513667 U CN 209513667U CN 201920101396 U CN201920101396 U CN 201920101396U CN 209513667 U CN209513667 U CN 209513667U
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- rudder
- plate
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- aircraft
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- 238000001514 detection method Methods 0.000 title claims abstract description 21
- 239000007787 solid Substances 0.000 claims description 2
- 238000010586 diagram Methods 0.000 description 4
- 230000005855 radiation Effects 0.000 description 4
- 238000007689 inspection Methods 0.000 description 3
- 238000009434 installation Methods 0.000 description 3
- 230000007246 mechanism Effects 0.000 description 3
- 230000006872 improvement Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000013475 authorization Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
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Abstract
The utility model discloses a kind of rudder of aircraft ray detection toolings, are related to aeronautical product detection technique field, solve can not adjust automatically to the transillumination position of rudder the technical issues of.Technical points include bracket, the fixed frame for being set to frame upper end and the x-ray flaw detector being installed on fixed frame, the upper end of rack is provided with the X for driving fixed frame to slide along fixed frame length direction to sliding assembly, and X is provided with the Y-direction sliding assembly for driving fixed frame to slide along fixed frame width direction on sliding assembly；The utility model have the advantages that can adjust automatically to the transillumination position of rudder.
Description
Technical field
The utility model relates to aeronautical product detection technique fields, more specifically, it relates to which a kind of rudder of aircraft is penetrated
Line detecting tool.
Background technique
A kind of rudder of aircraft ray detection tooling is disclosed in the Chinese patent that Authorization Notice No. is CN205808964U,
Including fixed frame, detection device bracket, ray head, longitudinal sliding motion carrying platform, bottom plate, the lower end of bottom plate is equipped with walking
Wheel, ray head are mounted on the upper end of detection device bracket by fixed frame, and bottom plate is located at the underface of detection device bracket, indulge
The surface of bottom plate is mounted on to sliding carrying platform.
It is similar to above-mentioned detecting tool in the prior art, passes through movable base plate and longitudinal sliding motion carrying platform adjustment side
To the irradiation position of rudder, it is not necessarily to manual handling, greatly improves working efficiency, and the risk for rudder of damaging is effectively reduced；But
In the irradiation position of adjustment direction rudder, it is still necessary to manually go to operate, to ensure that work safety, rudder need to prevent in special
It is carried out in Radiation work room, when being detected, staff needs to leave radiation protection operating room, when repeatedly being projected, work
It needs to enter repeatedly as personnel and exits radiation protection operating room, need to take a substantial amount of time, it is therefore desirable to improve.
Utility model content
Problem in view of the prior art, the purpose of this utility model is to provide a kind of rudder of aircraft ray detection works
Dress, have the advantages that can adjust automatically to the transillumination position of rudder.
To achieve the above object, the utility model provides following technical solution: including bracket, being set to frame upper end
Fixed frame and the x-ray flaw detector being installed on fixed frame, the upper end of the rack are provided with for driving fixed frame along solid
The X of frame length direction sliding is determined to sliding assembly, and the upper end of the rack is provided with for driving fixed frame along fixed frame width
The Y-direction sliding assembly of direction sliding.
By using above-mentioned technical proposal, energy is cooperated to sliding assembly and Y-direction sliding assembly by rack-mounted X
The horizontal position of enough adjust automatically fixed frames, thus reach the operating position for the x-ray flaw detector that adjustment is mounted on fixed frame,
So that x-ray flaw detector is scanned transillumination to each position of rudder when without personnel's operation, work is greatly improved
Efficiency.
The utility model is further arranged to: the X to sliding assembly include the loading plate for being set to frame upper end, two
It is fed through carrying board ends respectively and rack is fixed on the first guide rod of the both ends of rack fixation and cylinder body respectively in both ends
The first cylinder that upper and piston rod is connect with loading plate, the fixed mount setting is in the lower section of loading plate.
By using above-mentioned technical proposal, loading plate can be pushed along the length direction of the first guide rod by the first cylinder
Function mobile, that simple realization pushes fixed frame to slide along fixed frame length direction.
The utility model is further arranged to: the Y-direction sliding assembly include two along rack width direction setting and
Both ends are individually fixed in the second guide rod of carrying board ends, are set to below loading plate and both ends are sheathed on two second respectively
Sliding plate and cylinder body on guide rod are fixed on the second cylinder that on loading plate and piston rod is connect with sliding plate.
By using above-mentioned technical proposal, sliding plate can be pushed to move along the second guide rod by the second cylinder, simply
Realize the function of pushing fixed frame to slide along fixed frame width direction.
The utility model is further arranged to: the fixed frame includes that two pieces is set to below sliding plate to live for banding
The clip at x-ray flaw detector both ends.
By using above-mentioned technical proposal, by clip can by x-ray flaw detector banding below sliding plate to realize X
The detachable installation of ray inspection machine is fixed.
The utility model is further arranged to: being provided with rubber pad on the inner wall of two clips.
By using above-mentioned technical proposal, buffering, liner can be played the role of by rubber pad, so that x-ray inspection
The installation of machine is more stable.
The utility model is further arranged to: being provided with zigzag line in each one side of the rubber pad far from clip inner wall
Road.
By using above-mentioned technical proposal, rubber can be further increased by the zigzag lines being arranged on rubber pad
The bonding strength of pad and x-ray flaw detector, so that the installation of x-ray flaw detector is more stable.
The utility model is further arranged to: being provided with cylinder body on the sliding plate and is fixed on sliding plate upper surface and piston
The third cylinder that bar is arranged straight down is provided with the lifting fixed with the piston rod of third cylinder below the sliding plate
Plate, two clips are both secured on the lower surface of lifter plate.
By using above-mentioned technical proposal, two pieces card can be controlled by the cooperation between third cylinder and lifter plate simultaneously
Hoop drops to low level, and x-ray flaw detector is installed in lower position, then can be by two using third cylinder
It is interfered when part clip is raised to a high position again to prevent x-ray flaw detector mobile with rudder.
The utility model is further arranged to: four ends angle of the lifter plate is provided with telescopic rod, each described flexible
The upper and lower ends of bar are fixed with sliding plate and lifter plate respectively.
By using above-mentioned technical proposal, guiding and stable effect can be played by each telescopic rod, so that lifting
The lifting work of plate is more stable, and shaking is generated when third cylinder being avoided to go up and down x-ray flaw detector.
Compared with prior art, the utility model has the beneficial effects that
(1) x-ray flaw detector is able to drive to the cooperation between sliding assembly, Y-direction sliding assembly and fixed frame by X to exist
It is moved on horizontal plane, so that operating when needing to detect the different location of rudder without staff, greatly improves inspection
Survey efficiency；
(2) by the cooperation of third cylinder and lifter plate x-ray flaw detector is mounted on admittedly in lower position
Determine on frame, installs or removes x-ray flaw detector convenient for staff.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the present embodiment；
Fig. 2 is the structural schematic diagram of the present embodiment fixed frame；
Fig. 3 is structural schematic diagram of the present embodiment X to sliding assembly；
Fig. 4 is the structural schematic diagram of the present embodiment Y-direction sliding assembly.
Appended drawing reference: 1, rack；2, X is to sliding assembly；21, the first guide rod；22, the first cylinder；23, loading plate；
231, support plate；3, Y-direction sliding assembly；31, the second guide rod；32, the second cylinder；33, sliding plate；4, x-ray flaw detector；5,
Fixed frame；51, lifter plate；52, telescopic rod；53, third cylinder；54, clip；55, rubber pad；551, zigzag lines；6, it pushes away
Vehicle；61, plate；62, handle；63, universal wheel；64, foot brake mechanism.
Specific embodiment
With reference to the accompanying drawings and examples, the utility model is described in detail.
A kind of rudder of aircraft ray detection tooling, as shown in Figure 1, including rack 1, the fixation for being set to 1 upper end of rack
Frame 5, the x-ray flaw detector 4 being removably mounted on fixed frame 5 are set in rack 1 for driving fixed frame 5 along cart 6
Length direction sliding X to sliding assembly 2, be set in rack 1 with for drive fixed frame 5 along 6 width direction of cart slide
Y-direction sliding assembly 3 and cart 6 for being placed for rudder；Cart 6 includes horizontally disposed plate 61, more than one piece difference
The universal wheel 63 that is set at each end angle of plate 61 and it is set to handle 62 of the universal wheel 63 wherein on one end, each part is universal
Foot brake mechanism 64 is provided on wheel 63.
Referring to figs. 1 and 2, fixed frame 5 includes being horizontally placed on lifter plate 51 immediately below Y-direction sliding assembly 3, more
Part cylinder body is fixed on the third cylinder 53 that on Y-direction sliding assembly 3 and piston rod is connect with lifter plate 51 vertically, two pieces is fixed respectively
Clip 54 and more than one piece in 51 both ends of lifter plate be respectively arranged at each end angle of lifter plate 51 and upper and lower ends respectively with Y-direction
The telescopic rod 52 that sliding assembly 3 and lifter plate 51 are fixed；Wherein, the both ends of x-ray flaw detector 4 pass through the hoop of two pieces clip 54 respectively
It fastens, and is provided with the rubber for increasing clip 54 Yu 4 bonding strength of x-ray flaw detector in the inner wall of two pieces clip 54
Rubber mat 55 is provided with zigzag lines 551 far from clip 54 in each part rubber pad 55 on one side.
In conjunction with shown in Fig. 1 and Fig. 3, X includes horizontally disposed loading plate 23, two to sliding assembly 2 and is horizontally disposed with and divides
The first guide rod 21 and cylinder body for not being fed through 23 both ends of loading plate are fixed in rack 1 and piston rod is connect with loading plate 23
The first cylinder 22, both ends of the both ends of each first guide rod 21 respectively with rack 1 are fixed.
In conjunction with shown in Fig. 1 and Fig. 4, Y-direction sliding assembly 3 includes that two horizontally disposed and both ends are individually fixed in loading plate 23
Second guide rod 31 at both ends is set to the lower section of loading plate 23 and both ends are sheathed on sliding on two second guide rods 31 respectively
Plate 33 and cylinder body are fixed in rack 1 and piston rod is connect for pushing sliding plate 33 along the second guiding with sliding plate 33
Second cylinder 32 of 31 length direction of bar sliding；Wherein, the cylinder body of the second cylinder 32 is removably mounted in rack 1, the second gas
The piston rod of cylinder 32 is fixed together in such a way that bolt lock is paid with loading plate 23.
Wherein, a piece of support plate 231 being vertically arranged, each second guide rod 31 are respectively and fixedly provided at the both ends of loading plate 23
Both ends it is fixed with two panels support plate 231 respectively, the cylinder body of the second cylinder 32 is installed in wherein a piece of support plate 231.
Wherein, the cylinder body of each part third cylinder 53 and the upper end of each part telescopic rod 52 are both secured on sliding plate 33.
The course of work of the utility model is as follows:
Before work, rudder is lain on cart 6 by staff, then utilizes trailer by rudder push to rack
1 position that is interior and adjusting rudder, finally makes cart 6 keep stopping capable state using foot brake mechanism 64.
When detection, it should be ensured that all staff are away from radiation protection operating room, then control x-ray flaw detector 4 into
Row transillumination, when needing the launching position to rudder to be adjusted, it is only necessary to control X and be slid to sliding assembly 2 and Y-direction
Component 3 pushes fixed frame 5, and structure is simple, convenient to carry out, reduces manual operation process, effectively improves detection efficiency.
The above is only the preferred embodiment of the utility model, and the protection scope of the utility model is not limited merely to
Above-described embodiment, technical solution belonging to the idea of the present invention belong to the protection scope of the utility model.It should refer to
Out, for those skilled in the art, it is without departing from the principle of the utility model it is several improvement and
Retouching, these improvements and modifications also should be regarded as the protection scope of the utility model.
Claims (8)
1. a kind of rudder of aircraft ray detection tooling including bracket, is set to the fixed frame (5) of rack (1) upper end and pacifies
Loaded on the x-ray flaw detector (4) on fixed frame (5), it is characterised in that: the upper end of the rack (1) is provided with solid for driving
X that frame (5) slides along fixed frame (5) length direction is determined to sliding assembly (2), and the X is provided on sliding assembly (2) and is used for
The Y-direction sliding assembly (3) that driving fixed frame (5) slides along fixed frame (5) width direction.
2. a kind of rudder of aircraft ray detection tooling according to claim 1, it is characterised in that: the X is to sliding group
Part (2) include be set to the loading plate (23) of rack (1) upper end, two be fed through loading plate (23) both ends and both ends respectively and distinguish
Fixed the first guide rod (21) and cylinder body are fixed on rack (1) and piston rod and loading plate with the both ends of rack (1)
(23) the first cylinder (22) connected, the fixed frame (5) are set to the lower section of loading plate (23).
3. a kind of rudder of aircraft ray detection tooling according to claim 2, it is characterised in that: the Y-direction sliding group
Part (3) includes the second guiding that the two width direction settings and both ends along rack (1) are individually fixed in loading plate (23) both ends
Bar (31), be set to below loading plate (23) and both ends be sheathed on respectively the sliding plate (33) on two second guide rods (31) with
And cylinder body is fixed on the second cylinder (32) that on loading plate (23) and piston rod is connect with sliding plate (33).
4. a kind of rudder of aircraft ray detection tooling according to claim 3, it is characterised in that: the fixed frame (5)
The clip (54) for living x-ray flaw detector (4) both ends below sliding plate (33) for banding is set to including two pieces.
5. a kind of rudder of aircraft ray detection tooling according to claim 4, it is characterised in that: two clips (54)
Inner wall on be provided with rubber pad (55).
6. a kind of rudder of aircraft ray detection tooling according to claim 5, it is characterised in that: each rubber pad
(55) zigzag lines (551) are provided in the one side far from clip (54) inner wall.
7. a kind of rudder of aircraft ray detection tooling according to claim 4, it is characterised in that: the sliding plate (33)
On be provided with the third cylinder (53) that cylinder body is fixed on sliding plate (33) upper surface and piston rod is arranged straight down, the sliding
The lifter plate (51) fixed with the piston rod of third cylinder (53) is provided with below plate (33), two clips (54) are fixed
In on the lower surface of lifter plate (51).
8. a kind of rudder of aircraft ray detection tooling according to claim 7, it is characterised in that: the lifter plate (51)
Four ends angle be provided with telescopic rod (52), the upper and lower ends of each telescopic rod (52) respectively with sliding plate (33) and lifting
Plate (51) is fixed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920101396.7U CN209513667U (en) | 2019-01-19 | 2019-01-19 | A kind of rudder of aircraft ray detection tooling |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920101396.7U CN209513667U (en) | 2019-01-19 | 2019-01-19 | A kind of rudder of aircraft ray detection tooling |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209513667U true CN209513667U (en) | 2019-10-18 |
Family
ID=68201726
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920101396.7U Expired - Fee Related CN209513667U (en) | 2019-01-19 | 2019-01-19 | A kind of rudder of aircraft ray detection tooling |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209513667U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110702713A (en) * | 2019-10-21 | 2020-01-17 | 国营芜湖机械厂 | Airplane rudder ray detection automatic system |
-
2019
- 2019-01-19 CN CN201920101396.7U patent/CN209513667U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110702713A (en) * | 2019-10-21 | 2020-01-17 | 国营芜湖机械厂 | Airplane rudder ray detection automatic system |
| CN110702713B (en) * | 2019-10-21 | 2022-07-01 | 国营芜湖机械厂 | Airplane rudder ray detection automatic system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20191018 |
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| CF01 | Termination of patent right due to non-payment of annual fee |