CN218726774U - Aircraft wing radiographic inspection transillumination layout adjusting device - Google Patents
Aircraft wing radiographic inspection transillumination layout adjusting device Download PDFInfo
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- CN218726774U CN218726774U CN202222718229.1U CN202222718229U CN218726774U CN 218726774 U CN218726774 U CN 218726774U CN 202222718229 U CN202222718229 U CN 202222718229U CN 218726774 U CN218726774 U CN 218726774U
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- frame
- transillumination
- aircraft wing
- radiographic inspection
- track groove
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Abstract
The utility model discloses an aircraft wing ray detection transillumination overall arrangement adjusting device, this aircraft wing ray detection transillumination overall arrangement adjusting device include: remove the ladder frame and adjust the support, the upper mounting platform department level that removes the ladder frame is provided with the track groove, adjust support sliding connection in on the track groove, and can follow the extending direction in track groove slides, it is provided with the ray source that is used for ray detection to adjust fixedly on the support. The utility model discloses an universal wheel promotes to remove ladder frame adjustment position, to remove the ladder frame and remove the locking location behind the detection site of aircraft wing, according to the detection demand of reality, respectively through the roller train, the triaxial position of the corresponding difference adjustment ray source of stroke accommodate the lead screw and focus accommodate the lead screw to can accomplish normal work of transilluminating respectively to the detection position of difference, compare in current detection mode, both ensured the ray detection time measuring aircraft, equipment, personnel's safety, detection efficiency has been promoted again greatly.
Description
Technical Field
The utility model relates to an aircraft maintenance technical field especially relates to an aircraft wing ray detection transillumination overall arrangement adjusting device.
Background
The method is characterized in that ray detection is carried out on the wings of the airplane, and in the conventional detection process, the conventional common ladder frame is used for placing a ray source and adjusting the focal length to carry out transillumination layout.
However, this method has the following problems: 1. the common ladder frame is not provided with a fixing device, so that a ray source is easy to fall off in actual work, and airplanes and equipment are damaged; 2. the ray detection focal length and the detection area can not be quickly adjusted, and the working efficiency is low.
SUMMERY OF THE UTILITY MODEL
In order to overcome the not enough of relevant product among the prior art, the utility model provides an aircraft wing ray detection transillumination overall arrangement adjusting device.
The utility model provides an aircraft wing ray detection transillumination overall arrangement adjusting device, include: remove the ladder frame and adjust the support, the upper mounting plate department level that removes the ladder frame is provided with the track groove, it is in to adjust support sliding connection on the track groove, and can follow the extending direction in track groove slides, it is provided with the ray source that is used for ray detection to adjust to fix on the support.
The utility model discloses an in some embodiments, adjust the support and include bottom suspension strut, upper bracket and remove the frame, the upper bracket is fixed to be set up the upper end of bottom suspension strut, the inboard of upper bracket is provided with the slide rail, it is in to remove a sliding connection on the slide rail.
In some embodiments of the present invention, the movable frame is provided with a fixing base for fixing the radiation source.
In some embodiments of the present invention, the end of the upper support frame is provided with a limiting plate.
The utility model discloses an in some embodiments, the under bracing frame includes parallel arrangement's upper ledge and underframe, four bights of underframe all are provided with focus adjusting screw perpendicularly, the upper ledge corresponds to focus adjusting screw's position is provided with the sleeve respectively, focus adjusting screw spiro union is in the sleeve that corresponds.
In some embodiments of the present invention, two sets of mounting seats are symmetrically arranged on two sides of the bottom of the upper frame, respectively, a stroke adjusting screw rod is arranged on the two sets of mounting seats, and a hand wheel is fixedly connected to one end of the stroke adjusting screw rod; the bottom of the moving frame is provided with a stroke nut, the stroke nut is in threaded connection with the stroke adjusting screw rod, and the moving frame can be correspondingly driven to move on the upper supporting frame through adjusting the hand wheel.
In some embodiments of the present invention, the lower frame is provided with a roller set at a position corresponding to the track groove, and the roller set is slidably disposed in the track groove.
In some embodiments of the present invention, the lower frame further comprises a fixing screw.
In some embodiments of the present invention, the bottom of the movable ladder rack is provided with a plurality of universal wheels with locking function.
In some embodiments of the present invention, the safety handrail frame is enclosed at the edge of the upper platform of the movable ladder frame.
Compared with the prior art, the utility model discloses there is following advantage:
the embodiment of the utility model provides an aircraft wing radiographic inspection shines overall arrangement adjusting device thoroughly through the universal wheel and promotes to remove ladder frame adjusting position, will remove the ladder frame and remove the locking location behind the detection site of aircraft wing, according to the detection demand of reality, respectively through the roller train, the corresponding triaxial position of adjusting respectively the ray source of stroke accommodate the lead screw and focus accommodate the lead screw, thereby can accomplish normal work of shining thoroughly respectively to the detection position of difference, compare in current detection mode, both ensured the radiographic inspection time measuring aircraft, equipment, personnel's safety, detection efficiency has been promoted again greatly.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings needed to be used in the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art that other drawings can be obtained according to these drawings without creative efforts.
Fig. 1 is a schematic structural view of the perspective layout adjusting device for aircraft wing radiographic inspection according to the present invention;
fig. 2 is a schematic structural view of the adjusting bracket of the present invention.
Description of reference numerals:
1. adjusting the bracket; 2. moving the ladder frame; 3. a track groove; 4. a universal wheel; 5. a safety handrail frame; 10. a lower support frame; 11. an upper support frame; 12. a movable frame; 13. a limiting plate; 14. a fixed seat; 15. a mounting seat; 16. a stroke adjusting screw rod; 17. a focal length adjusting screw rod; 18. a roller set; 19. fixing the screw rod; 20. a slide rail; 21. hand wheel.
Detailed Description
In order to make the technical field person understand the scheme of the present invention better, the following will combine the drawings in the embodiments of the present invention to clearly and completely describe the technical scheme in the embodiments of the present invention. It is to be understood that the embodiments described are merely exemplary of the invention, and that no limitations are intended to the details of construction or design herein shown. The present invention may be embodied in many different forms and is not limited to the embodiments described herein, but rather, these embodiments are provided so that this disclosure will be thorough and complete.
Referring to fig. 1, the aircraft wing radiographic inspection transillumination layout adjusting device comprises a movable ladder frame 2 and an adjusting support 1, a track groove 3 is horizontally arranged at the upper platform of the movable ladder frame 2, the adjusting support 1 is connected to the track groove 3 in a sliding mode and can slide along the extending direction of the track groove 3, a ray source for radiographic inspection is fixedly arranged on the adjusting support 1, and therefore spatial position adjustment of an inspection area is achieved through the adjusting support 1.
Referring to fig. 2, the adjusting bracket 1 includes a lower supporting frame 10, an upper supporting frame 11 and a moving frame 12, the upper supporting frame 11 is fixedly disposed at the upper end of the lower supporting frame 10, a slide rail 20 is disposed at the inner side of the upper supporting frame 11, the moving frame 12 is slidably connected to the slide rail 20, and specifically, the moving frame 12 may be provided with a pulley (not shown) at a side surface corresponding to the slide rail 20, so that the pulley and the slide rail 20 may cooperate (driven by human power or mechanical power) to realize the lateral movement of the moving frame 12.
The movable frame 12 is provided with a fixed seat 14 for fixing the radiation source, and a conventional clamping device or other clamping pieces with the same function can be selected to realize the dismounting of the radiation source.
And a limiting plate 13 is arranged at the end part of the upper support frame 11 and used for limiting the movement stroke range of the movable frame 12.
The lower support frame 10 includes an upper frame and a lower frame which are arranged in parallel, four corners of the lower frame are vertically provided with focal length adjusting screw rods 17, the positions of the upper frame corresponding to the focal length adjusting screw rods 17 are respectively provided with a sleeve, the focal length adjusting screw rods 17 are screwed in the corresponding sleeves, so that the height between the upper frame and the lower frame can be correspondingly adjusted by adjusting the focal length adjusting screw rods 17.
Two groups of mounting seats 15 are symmetrically arranged on two sides of the bottom of the upper frame respectively, a stroke adjusting screw rod 16 penetrates through the two groups of mounting seats 15, and a hand wheel 21 is fixedly connected to one end of the stroke adjusting screw rod 16; the bottom of the moving frame 12 is provided with a travel nut (not shown) which is screwed on the travel adjusting screw rod 16, and the moving frame 12 can be correspondingly driven to move on the upper support frame 11 by adjusting the hand wheel 21.
The lower frame is provided with a roller group 18 corresponding to the position of the track groove 3, and the roller group 18 is slidably arranged in the track groove 3.
Still set up fixing screw 19 on the underframe, through adjusting fixing screw 19 up-and-down motion, fixing screw 19 can peg graft the upper mounting plate relevant position (can be screw, through-hole or kidney slot according to actual need, the utility model discloses do not have the restriction to this) of removal ladder 2 can come spacing fixed the position of adjusting support 1.
The embodiment of the utility model provides an in, the bottom of removing ladder frame 2 is provided with the universal wheel 4 of multiunit area locking function (like adjusting screw etc.), can pass through universal wheel 4 realizes that spatial position removes.
The edge position of the upper platform of the movable ladder frame 2 is surrounded with a safety handrail frame 5 for providing safety protection and support when a worker places a ray source.
The embodiment of the utility model provides an aircraft wing ray detection shines overall arrangement adjusting device thoroughly through universal wheel 4 and promotes and remove 2 adjustment position of ladder frame, will remove 2 detection position back locking location that remove the ladder frame to the aircraft wing, according to the detection demand of reality, respectively through roller train 18, stroke accommodate the lead screw 16 and the corresponding triaxial position of adjusting respectively the ray source of focus accommodate the lead screw 17, thereby can accomplish normal work of shining thoroughly respectively to the detection position of difference, compare in current detection mode, both ensured ray detection time measuring aircraft, equipment, personnel's safety, detection efficiency has greatly been promoted again.
Those not described in detail in this specification are within the skill of the art. Although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described in the foregoing detailed description, or equivalent replacements may be made for some of the technical features of the embodiments. All utilize the equivalent structure that the content of the utility model discloses a specification and attached drawing was done, direct or indirect application is in other relevant technical field, all is in the same way the utility model discloses within the patent protection scope.
Claims (10)
1. The utility model provides an aircraft wing radiographic inspection transillumination overall arrangement adjusting device which characterized in that includes: remove ladder frame (2) and adjust support (1), the upper mounting plate department level that removes ladder frame (2) is provided with track groove (3), adjust support (1) sliding connection be in on track groove (3), and can follow the extending direction in track groove (3) slides, it is provided with the ray source that is used for radiographic inspection to adjust to fix on support (1).
2. The aircraft wing radiographic inspection transillumination layout adjustment apparatus of claim 1, wherein: adjust support (1) and include bottom suspension strut (10), top suspension strut (11) and remove frame (12), top suspension strut (11) is fixed to be set up the upper end of bottom suspension strut (10), the inboard of top suspension strut (11) is provided with slide rail (20), it is in to remove frame (12) sliding connection slide rail (20) are last.
3. The aircraft wing radiographic inspection transillumination layout adjustment apparatus of claim 2, wherein: the movable frame (12) is provided with a fixed seat (14) for fixing the ray source.
4. The aircraft wing radiographic inspection transillumination layout adjustment apparatus of claim 2, wherein: and a limiting plate (13) is arranged at the end part of the upper support frame (11).
5. The aircraft wing radiographic inspection transillumination layout adjustment apparatus of claim 2, wherein: the lower support frame (10) comprises an upper frame and a lower frame which are arranged in parallel, four corners of the lower frame are vertically provided with focus adjusting screw rods (17), sleeves are respectively arranged at positions of the upper frame corresponding to the focus adjusting screw rods (17), and the focus adjusting screw rods (17) are in threaded connection in the corresponding sleeves.
6. The aircraft wing radiographic inspection transillumination layout adjustment apparatus of claim 5, wherein: two sides of the bottom of the upper frame are respectively and symmetrically provided with two groups of mounting seats (15), a stroke adjusting screw rod (16) penetrates through the two groups of mounting seats (15), and one end of the stroke adjusting screw rod (16) is fixedly connected with a hand wheel (21); the bottom of the movable frame (12) is provided with a stroke nut which is in threaded connection with the stroke adjusting screw rod (16), and the movable frame (12) can be correspondingly driven to move on the upper support frame (11) through adjusting the hand wheel (21).
7. The aircraft wing radiographic inspection transillumination layout adjustment apparatus of claim 5, wherein: the lower frame is provided with a roller group (18) corresponding to the position of the track groove (3), and the roller group (18) is arranged in the track groove (3) in a sliding manner.
8. The aircraft wing radiographic inspection transillumination layout adjustment apparatus of claim 5, wherein: and a fixing screw rod (19) is also arranged on the lower frame.
9. The aircraft wing radiographic inspection transillumination layout adjustment apparatus of claim 1, wherein: the bottom of the movable ladder frame (2) is provided with a plurality of universal wheels (4) with locking functions.
10. The aircraft wing radiographic inspection transillumination layout adjustment apparatus of claim 1, wherein: the safety handrail frame (5) is arranged around the edge of the upper platform of the movable ladder frame (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222718229.1U CN218726774U (en) | 2022-10-14 | 2022-10-14 | Aircraft wing radiographic inspection transillumination layout adjusting device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222718229.1U CN218726774U (en) | 2022-10-14 | 2022-10-14 | Aircraft wing radiographic inspection transillumination layout adjusting device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218726774U true CN218726774U (en) | 2023-03-24 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222718229.1U Active CN218726774U (en) | 2022-10-14 | 2022-10-14 | Aircraft wing radiographic inspection transillumination layout adjusting device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218726774U (en) |
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2022
- 2022-10-14 CN CN202222718229.1U patent/CN218726774U/en active Active
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