Search

CN-116164200-B - Supporting device for X-ray detection of narrow weld joint of aero-engine casing support plate

CN116164200BCN 116164200 BCN116164200 BCN 116164200BCN-116164200-B

Abstract

The invention discloses a supporting device, in particular discloses a supporting device for X-ray detection of narrow welding seams of a support plate of an aero-engine box, and belongs to the technical field of design and manufacture of aero-engine maintenance process equipment. The support device for X-ray detection of the narrow welding line of the support plate of the aero-engine case can ensure that the effective transillumination angle of the narrow welding line of the support plate is replaced in situ by the air inlet case, and accurately and effectively detect the defect of the narrow welding line of the support plate in situ. The supporting device comprises a base frame, an adjusting component and a supporting and fixing structure, wherein the supporting and fixing structure is arranged on the base frame, and in the process of detecting the narrow weld X-rays of the aero-engine box support plate, the irradiation angle of the aero-engine box support plate fixedly arranged on the supporting and fixing structure in the horizontal and/or vertical directions is adjusted to a specified position through the adjusting component.

Inventors

  • LI JIANPING
  • HUANG PING
  • LUO KUILIN
  • HUANG XUANMIN
  • LI QI
  • LIU ZHU
  • ZHENG JIE
  • WANG JIEYU
  • YUAN ZIWEI

Assignees

  • 国营川西机器厂

Dates

Publication Date
20260505
Application Date
20230301

Claims (7)

  1. 1. The supporting device for the narrow welding line X-ray detection of the aero-engine box support plate is characterized by comprising a base frame (1), an adjusting component (2) and a supporting and fixing structure (3), wherein the supporting and fixing structure (3) is arranged on the base frame (1), in the process of the narrow welding line X-ray detection of the aero-engine box support plate, the irradiation angle of the aero-engine box support plate fixedly arranged on the supporting and fixing structure (3) in the horizontal and/or vertical direction is adjusted to a specified position through the adjusting component (2), The base frame (1) comprises a base frame (8), a bogie (9) and a supporting frame (10), the supporting frame (10) is fixedly arranged on the base frame (8) through the bogie (9), the supporting and fixing structure (3) is supported on the supporting frame (10) under the cooperation of the adjusting component (2), The supporting and fixing structure (3) is a casing fixed wheel disc, the aeroengine casing support plate is arranged on the free end of the casing fixed wheel disc, the other end of the casing fixed wheel disc is arranged on the supporting frame (10) through the adjusting component (2) with adjustable horizontal irradiation angle and/or vertical irradiation angle, The adjusting assembly (2) at least comprises a horizontal transillumination angle adjusting device (13) and a vertical angle adjusting device (14), and the casing fixing wheel disc is arranged on the supporting frame (10) through the horizontal transillumination angle adjusting device (13) and the vertical angle adjusting device (14).
  2. 2. The support device for narrow-bead X-ray detection of an aircraft engine case support plate according to claim 1, further comprising a mobile trailer (4), wherein the base frame (1) is arranged on the mobile trailer (4).
  3. 3. The supporting device for detecting narrow weld X-rays of an aeroengine casing support plate according to claim 2, wherein the mobile trailer (4) comprises a frame (5), a mop (6) and a universal wheel set (7), the mop (6) is fixedly arranged on the frame (5), the universal wheel set (7) is fixedly arranged at the bottom of the frame (5), and the base frame (1) is arranged on the frame (5).
  4. 4. A support device for aeroengine case support plate narrow weld X-ray detection according to claim 2 or 3, characterized in that the chassis (8) is detachably fixed to the mobile trailer (4).
  5. 5. The supporting device for detecting narrow weld X-rays of an aeroengine casing support plate according to claim 4, wherein the bogie (9) comprises a right-angle frustum body (11) and an adjusting connecting body (12), the adjusting connecting body (12) is arranged on the side face of the top of the right-angle frustum body (11) in an adjustable angle mode, the bogie (9) is connected with the underframe (8) through the bottom of the right-angle frustum body (11), and the supporting frame (10) is detachably connected with the adjusting connecting body (12).
  6. 6. The supporting device for detecting narrow weld X-rays of an aero-engine casing support plate according to claim 1, wherein the adjusting assembly (2) further comprises an effective transillumination angle infrared positioner (15), and the effective transillumination angle infrared positioner (15) is arranged on the casing fixing wheel disc.
  7. 7. The supporting device for detecting narrow weld X-rays of an aeroengine casing support plate according to claim 1, wherein a connecting frame (16) is further connected to the lower portion of a casing fixing wheel disc, the casing fixing wheel disc is movably connected with a supporting frame (10) through the connecting frame (16), and the horizontal transillumination angle adjusting device (13) and the vertical angle adjusting device (14) lock the casing fixing wheel disc through the connecting frame (16).

Description

Supporting device for X-ray detection of narrow weld joint of aero-engine casing support plate Technical Field The invention relates to a supporting device, in particular to a supporting device for X-ray detection of a narrow weld joint of a support plate of an aero-engine box, and belongs to the technical field of design and manufacture of aero-engine maintenance process equipment. Background The air inlet channel is a channel for sucking air of the aero-engine, and belongs to one of five parts of the aero-engine. The air inlet casing component is an important component of an air inlet channel of an aeroengine, and mainly comprises a support plate, adjustable blades and a bearing ring at the forefront end of the aeroengine. Therefore, the quality of the air inlet casing assembly is directly related to the normal operation of all parts of the aeroengine, and if the air inlet casing assembly has faults such as crack and block falling of a support plate, falling of an adjustable blade and the like in the use process, the engine is easily damaged seriously, and further, grade flight accidents are caused, so that the loss is immeasurable. Because the repair of the replacement support plate of the air inlet casing assembly is to perform in-situ electron beam welding, the quality of the welding seam is detected by the X-ray of the replacement support plate of the air inlet casing assembly, the length of the welding seam is detected to be about 10mm, the width is about 1mm, and the thickness is about 1.5 mm. The existing X-ray detection method is to place the detection part of the detected part in an effective transillumination field and detect the part vertically. The technical scheme includes that firstly, welding line defects cannot be effectively detected through detection parameters, secondly, when an air inlet casing is in situ and the existing condition is perpendicular to transillumination, an outer ring of the air inlet casing and other support plates shield welding lines of the support plates to be detected and replaced, thirdly, an X-ray machine head is large in size and cannot be placed right above the welding lines to transilluminate, and fourthly, angles of the welding lines of the support plates in the horizontal direction and the vertical direction cannot be ensured, effective transillumination angles cannot be ensured, and detection results are invalid. Disclosure of Invention The technical problem to be solved by the invention is to provide the support device for the X-ray detection of the narrow welding line of the support plate of the aeroengine case, which can ensure the effective transillumination angle of the narrow welding line of the support plate of the in-situ replacement support plate of the air inlet case, and accurately and effectively detect the defect of the narrow welding line of the support plate of the in-situ replacement support plate. The technical scheme is that the supporting device for the narrow welding line X-ray detection of the aero-engine box support plate comprises a base frame, an adjusting component and a supporting and fixing structure, wherein the supporting and fixing structure is arranged on the base frame, and in the process of the narrow welding line X-ray detection of the aero-engine box support plate, the irradiation angle of the aero-engine box support plate fixedly arranged on the supporting and fixing structure in the horizontal and/or vertical direction is adjusted to a specified position through the adjusting component. Further, the supporting device further comprises a mobile trailer, and the base frame is arranged on the mobile trailer. The preferable mode of the scheme is that the mobile trailer comprises a frame, a mop and a universal wheel set, wherein the mop is fixedly arranged on the frame, the universal wheel set is fixedly arranged at the bottom of the frame, and the base frame is arranged on the frame. Further, the base frame comprises a bottom frame, a bogie and a supporting frame, wherein the supporting frame is fixedly arranged on the bottom frame through the bogie, the bottom frame is detachably fixed on the mobile trailer, and the supporting and fixing structure is supported on the supporting frame under the cooperation of the adjusting component. The preferred mode of above-mentioned scheme is, the bogie include right angle frustum body and adjustment connector, the adjustable side of arranging at right angle frustum body top of adjustment connector corner, the bogie pass through the bottom and the chassis connection of right angle frustum body, the support frame with adjustment connector detachable be connected. Further, the supporting and fixing structure is a casing fixing wheel disc, the aeroengine casing support plate is arranged at the free end of the casing fixing wheel disc, and the other end of the casing fixing wheel disc is arranged on the supporting frame through the adjusting component in an adjustable mode of horizontal irr