Support device for X-ray detection of narrow welds of an aeroengine case support plate
By designing a support device to adjust the irradiation angle of the aero-engine casing support plate, the problem of invalid detection results in the prior art is solved, and accurate detection of narrow welds on the support plate is achieved, which is suitable for in-situ repair of the air intake casing assembly.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- STATE-OWNED SICHUAN WEST MASCH FACTORY
- Filing Date
- 2023-03-01
- Publication Date
- 2026-05-05
AI Technical Summary
Existing X-ray inspection methods cannot effectively detect narrow weld defects in the support plates of aero-engine intake casing components, and the X-ray head is too large to be directly aimed at the weld for radiographic examination, resulting in invalid inspection results.
Design a support device including a base frame, adjustment components and support fixing structure. The adjustment components adjust the illumination angle of the aircraft engine casing support plate in the horizontal and vertical directions to ensure an effective illumination angle. A mobile trailer and omnidirectional wheel set are used to facilitate movement and stable support.
It enables accurate inspection of narrow welds on aero-engine casing support plates, ensuring the validity and reliability of inspection results. It is particularly suitable for X-ray inspection during in-situ repair of intake casing components.
Smart Images

Figure CN116164200B_ABST
Abstract
Description
Technical Field
[0001] This invention relates to a support device, and more particularly to a support device for X-ray inspection of narrow weld seams in aero-engine casing plates, belonging to the field of aero-engine maintenance and repair process equipment design and manufacturing technology. Background Technology
[0002] The air intake is the flow path through which air is drawn into an aero-engine, and it is one of the "five major components" of an aero-engine. The air intake casing assembly is an important part of the aero-engine air intake. It is located at the front of the engine and mainly includes support plates, adjustable blades, and load-bearing rings. During engine operation, it can introduce a sufficient amount of air into the compressor with minimal flow loss. Therefore, the quality of the air intake casing assembly directly affects the normal operation of all parts of the aero-engine. If, during use, the air intake casing assembly develops faults such as cracked or chipped support plates or detached adjustable blades, it can easily cause serious damage to the engine, leading to a major flight accident with incalculable losses.
[0003] Since the replacement of the intake casing assembly support plate involves in-situ electron beam welding, the quality of the weld needs to be inspected by X-ray in-situ replacement support plate in the intake casing. The weld length should be about 10mm, the width about 1mm, and the thickness about 1.5mm.
[0004] Existing X-ray inspection methods involve placing the inspected part within an effective radiographic field and performing vertical radiographic inspection. However, this approach has several drawbacks: First, the inspection parameters are insufficient to effectively detect weld defects; second, when replacing a narrow weld on the support plate in its original position within the intake casing, the outer ring of the intake casing and other support plates obstruct the weld during vertical radiographic inspection under current conditions; third, the X-ray machine head is too large to be positioned directly above the weld; and fourth, the horizontal and vertical angles of the replacement support plate weld cannot be guaranteed, resulting in ineffective inspection results. Summary of the Invention
[0005] The technical problem to be solved by the present invention is to provide a support device for X-ray inspection of narrow welds on the support plate of an aero-engine casing, which can ensure an effective radiographic angle for the narrow welds of the in-situ replacement support plate and accurately and effectively detect defects in the narrow welds of the in-situ replacement support plate.
[0006] The technical solution adopted to solve the above-mentioned technical problems is: a support device for X-ray inspection of narrow weld seams of aero-engine casing plates, the support device including a base frame, an adjustment component and a support fixing structure, the support fixing structure being arranged on the base frame; during the X-ray inspection of narrow weld seams of aero-engine casing plates, the irradiation angle of the aero-engine casing plate fixed on the support fixing structure in the horizontal and / or vertical directions is adjusted to a specified position by the adjustment component.
[0007] Furthermore, the support device also includes a mobile trailer, on which the base frame is arranged.
[0008] A preferred embodiment of the above solution is that the mobile trailer includes a frame, a mop, and a set of casters, the mop being fixedly mounted on the frame, the set of casters being fixedly mounted on the bottom of the frame, and the base frame being arranged on the frame.
[0009] Furthermore, the base frame includes a base frame, a bogie, and a support frame. The support frame is fixed to the base frame via the bogie. The base frame is detachably fixed to the mobile trailer. The support fixing structure is supported on the support frame with the cooperation of the adjustment assembly.
[0010] In a preferred embodiment of the above scheme, the bogie includes a right-angled truncated cone and an adjusting connector. The adjusting connector is arranged on the side of the top of the right-angled truncated cone with adjustable rotation angle. The bogie is connected to the base frame through the bottom of the right-angled truncated cone, and the support frame is detachably connected to the adjusting connector.
[0011] Furthermore, the supporting and fixing structure is a casing fixing wheel, the aircraft engine casing support plate is arranged on the free end of the casing fixing wheel, and the other end of the casing fixing wheel is arranged on the support frame in an adjustable manner via the adjustment component for horizontal and / or vertical illumination angles.
[0012] In a preferred embodiment of the above scheme, the adjustment assembly includes at least a horizontal illumination angle adjustment device and a vertical angle adjustment device, and the casing fixing wheel is arranged on the support frame through the horizontal illumination angle adjustment device and the vertical angle adjustment device.
[0013] Furthermore, the adjustment assembly also includes an effective illumination angle infrared locator, which is arranged on the housing fixing wheel.
[0014] In a preferred embodiment of the above scheme, a connecting frame is also connected to the lower part of the receiver fixing wheel, the receiver fixing wheel is movably connected to the support frame through the connecting frame, and the horizontal transmission angle adjustment device and the vertical angle adjustment device lock the receiver fixing wheel through the connecting frame.
[0015] The beneficial effects of this invention are as follows: The technical solution provided in this application sets up a support device including a base frame, an adjustment component, and a support fixing structure, and arranges the support fixing structure on the base frame; then, during the X-ray inspection of the narrow weld seam of the aero-engine casing support plate, the irradiation angle of the aero-engine casing support plate fixed on the support fixing structure in the horizontal and / or vertical directions is adjusted to a specified position by the adjustment component. Since the aero-engine casing support plate fixed to the support fixing structure can be adjusted by the adjustment component during the X-ray inspection of the narrow weld seam of the aero-engine casing support plate, the effective irradiation angle of the narrow weld seam of the in-situ replacement support plate of the intake casing can be ensured, achieving the purpose of accurately and effectively detecting defects in the narrow weld seam of the in-situ replacement support plate, and thus judging whether there are welding defects such as incomplete fusion affecting the quality of the intake casing assembly. The repair weld seam of the aero-engine casing support plate inspected using the support device of this application has a high accuracy rate and is easy to operate, making it particularly suitable for X-ray inspection during the in-situ repair of the intake casing assembly support plate. Attached Figure Description
[0016] Figure 1 This is a front view of the support device for X-ray inspection of narrow weld seams in aero-engine casing plates according to the present invention.
[0017] Figure 2 for Figure 1 Side view.
[0018] The components in the diagram are labeled as follows: 1. Base frame; 2. Adjustment assembly; 3. Support and fixing structure; 4. Mobile trailer; 5. Frame; 6. Mop; 7. Universal wheel set; 8. Base frame; 9. Bogie; 10. Support frame; 11. Right-angle cone body; 12. Adjustment connector; 13. Horizontal illumination angle adjustment device; 14. Vertical angle adjustment device; 15. Effective illumination angle infrared locator; 16. Connecting frame. Detailed Implementation
[0019] like Figure 1 , Figure 2The diagram illustrates a support device for X-ray inspection of narrow weld seams in aero-engine casing support plates, provided by this invention. This device ensures an effective radiographic angle for narrow weld seams during in-situ replacement of air intake casing support plates and accurately detects defects in these weld seams. The support device includes a base frame 1, an adjustment assembly 2, and a support fixing structure 3, with the support fixing structure 3 positioned on the base frame 1. During X-ray inspection of narrow weld seams in aero-engine casing support plates, the radiographic angle of the aero-engine casing support plate, fixed to the support fixing structure 3, in the horizontal and / or vertical directions is adjusted to a predetermined position using the adjustment assembly 2. The technical solution provided in this application involves setting up a support device including a base frame, an adjustment assembly, and a support fixing structure, and arranging the support fixing structure on the base frame. Then, during X-ray inspection of narrow weld seams in aero-engine casing support plates, the radiographic angle of the aero-engine casing support plate, fixed to the support fixing structure, in the horizontal and / or vertical directions is adjusted to a predetermined position using the adjustment assembly. Because the narrow weld seam of the aero-engine casing support plate can be adjusted and fixed to the support structure via an adjustment component during X-ray inspection, the effective radiographic angle of the narrow weld seam of the in-situ replacement support plate of the intake casing can be ensured. This achieves the goal of accurately and effectively detecting defects in the narrow weld seam of the in-situ replacement support plate, and further, it can be used to assess whether there are welding defects such as incomplete fusion affecting the quality of the intake casing assembly. The support device of this application provides high accuracy and simple operation for inspecting the repair weld seam of the aero-engine casing support plate, making it particularly suitable for X-ray inspection during the in-situ repair of the intake casing assembly support plate.
[0020] In light of actual production conditions, to facilitate the reversible movement of the support device described in this application, the support device further includes a mobile trailer 4, on which the base frame 1 is arranged. Preferably, the mobile trailer 4 includes a frame 5, a mop handle 6, and a set of casters 7. The mop handle 6 is fixed to the frame 5, the set of casters 7 is fixed to the bottom of the frame 5, and the base frame 1 is arranged on the frame 5. Furthermore, to ensure the stability of the support and to simplify the structure of each component, facilitating manufacturing and subsequent use, the base frame 1 includes a base frame 8, a bogie 9, and a support frame 10. The support frame 10 is fixed to the base frame 8 via the bogie 9. The base frame 8 is detachably fixed to the mobile trailer 4, and the support fixing structure 3 is supported on the support frame 10 with the cooperation of the adjusting component 2. At this time, the bogie 9 includes a right-angled frustum 11 and an adjusting connector 12. The adjusting connector 12 is arranged on the side of the top of the right-angled frustum 11 with adjustable rotation angle. The bogie 9 is connected to the base frame 8 through the bottom of the right-angled frustum 11. The support frame 10 is detachably connected to the adjusting connector 12. The support fixing structure 3 is a casing fixing wheel. The aircraft engine casing support plate is arranged on the free end of the casing fixing wheel. The other end of the casing fixing wheel is arranged on the support frame 10 with adjustable horizontal and / or vertical illumination angles via the adjusting assembly 2.
[0021] Meanwhile, for convenient horizontal and / or vertical angle adjustment, the adjustment assembly 2 described in this application includes at least a horizontal illumination angle adjustment device 13 and a vertical angle adjustment device 14. The housing fixing wheel is arranged on the support 10 frame via the horizontal illumination angle adjustment device 13 and the vertical angle adjustment device 14. The adjustment assembly 2 also includes an effective illumination angle infrared locator 15, which is arranged on the housing fixing wheel. For ease of connection and adjustment, a connecting frame 16 is also connected to the lower part of the housing fixing wheel. The housing fixing wheel is movably connected to the support frame 10 via the connecting frame 16, and the horizontal illumination angle adjustment device 13 and the vertical angle adjustment device 14 lock the housing fixing wheel via the connecting frame 16.
[0022] In summary, using the support device provided in this application for X-ray inspection of narrow welds in aero-engine casing plates has the following advantages:
[0023] ① The fixed wheel of the transillumination device can effectively fix the casing and rotate 360°, and can effectively cover the weld seam of the intake casing support plate that needs to be inspected;
[0024] ② By using an infrared positioner for the illumination angle, casters, vertical angle adjustment device for the narrow weld seam of the support plate, and horizontal illumination angle adjustment device for the narrow weld seam of the support plate, the vertical and horizontal illumination angles and positions of the intake casing support plate weld seam can be adjusted to achieve the correct illumination angle and avoid missed detections.
[0025] ③ By adopting the inspection parameters of the intake casing support plate with a unique structure for this type of aircraft, weld defects are effectively detected, ensuring the effectiveness of the inspection of narrow welds on the casing support plate with this structure.
[0026] ④ The casters can adjust the intake casing and the support plate to be inspected at any position in the radiographic field.
[0027] Example 1
[0028] The above technical solutions of this application will be further illustrated below through specific embodiments:
[0029] The special X-ray inspection device for the narrow weld seam of the in-situ support plate of the intake casing consists of a casing fixing wheel, a vertical angle adjustment device for the narrow weld seam of the support plate, a horizontal radiographic angle adjustment device for the narrow weld seam of the support plate, an effective radiographic angle infrared locator, a casing support frame (3), and casters. During inspection, the inner ring of the casing is fixed on the fixing wheel of the radiographic device, and the casing is placed in the effective X-ray radiographic area along with the radiographic device. The vertical and horizontal radiographic angles and the radiographic position are adjusted using the radiographic angle infrared locator, casters, vertical angle adjustment device for the narrow weld seam of the support plate, and horizontal radiographic angle adjustment device for the narrow weld seam of the support plate. Various inspection process parameters (number of radiographic exposures, tube voltage, tube current, radiographic time, image quality meter sensitivity, etc.) are set to realize the X-ray inspection of the narrow weld seam of the in-situ support plate of the intake casing. The casing fixing wheel is a 360° rotating wheel with 8 balance holes and casing mounting holes.
Claims
1. A support device for X-ray inspection of narrow weld seams in aircraft engine casing plates, characterized in that: The support device includes a base frame (1), an adjustment assembly (2), and a support fixing structure (3), wherein the support fixing structure (3) is arranged on the base frame (1); during the X-ray inspection of the narrow weld seam of the aero-engine casing plate, the irradiation angle of the aero-engine casing plate fixed on the support fixing structure (3) in the horizontal and / or vertical directions is adjusted to the specified position by the adjustment assembly (2). The base frame (1) includes a base frame (8), a bogie (9), and a support frame (10). The support frame (10) is fixed to the base frame (8) via the bogie (9). The support fixing structure (3) is supported on the support frame (10) with the cooperation of the adjustment assembly (2). The supporting and fixing structure (3) is a casing fixing wheel, and the aircraft engine casing support plate is arranged on the free end of the casing fixing wheel. The other end of the casing fixing wheel is arranged on the support frame (10) through the adjustment component (2) for adjustable horizontal and / or vertical illumination angles. The adjustment assembly (2) includes at least a horizontal illumination angle adjustment device (13) and a vertical angle adjustment device (14), and the casing fixing wheel is arranged on the support frame (10) through the horizontal illumination angle adjustment device (13) and the vertical angle adjustment device (14).
2. The support device for X-ray inspection of narrow weld seams in aero-engine casing plates according to claim 1, characterized in that: The support device also includes a mobile trailer (4), on which the base frame (1) is arranged.
3. The support device for X-ray inspection of narrow weld seams in aero-engine casing plates according to claim 2, characterized in that: The mobile trailer (4) includes a frame (5), a mop (6) and a set of casters (7). The mop (6) is fixed on the frame (5), the set of casters (7) is fixed on the bottom of the frame (5), and the base frame (1) is arranged on the frame (5).
4. The support device for X-ray inspection of narrow weld seams in aero-engine casing plates according to claim 2 or 3, characterized in that: The base frame (8) is detachably fixed to the mobile trailer (4).
5. The support device for X-ray inspection of narrow weld seams in aero-engine casing plates according to claim 4, characterized in that: The bogie (9) includes a right-angled truncated cone (11) and an adjusting connector (12). The adjusting connector (12) is arranged on the side of the top of the right-angled truncated cone (11) with adjustable rotation angle. The bogie (9) is connected to the base frame (8) through the bottom of the right-angled truncated cone (11). The support frame (10) is detachably connected to the adjusting connector (12).
6. The support device for X-ray inspection of narrow weld seams in aero-engine casing plates according to claim 1, characterized in that: The adjustment assembly (2) further includes an effective transmission angle infrared locator (15), which is arranged on the housing fixing wheel.
7. The support device for X-ray inspection of narrow weld seams in aero-engine casing plates according to claim 1, characterized in that: A connecting frame (16) is also connected to the lower part of the housing fixing wheel. The housing fixing wheel is movably connected to the support frame (10) through the connecting frame (16). The horizontal transmission angle adjustment device (13) and the vertical angle adjustment device (14) lock the housing fixing wheel through the connecting frame (16).
Citation Information
Patent Citations
Tooling trolley for radiographic detection of casing part of aeroengine
CN105882698A
Case clamping device for nondestructive test
CN204630912U