CN218674852U - Magnetic powder inspection device for aircraft parts - Google Patents
Magnetic powder inspection device for aircraft parts Download PDFInfo
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- CN218674852U CN218674852U CN202222966116.3U CN202222966116U CN218674852U CN 218674852 U CN218674852 U CN 218674852U CN 202222966116 U CN202222966116 U CN 202222966116U CN 218674852 U CN218674852 U CN 218674852U
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- grip slipper
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
- Y02P70/10—Greenhouse gas [GHG] capture, material saving, heat recovery or other energy efficient measures, e.g. motor control, characterised by manufacturing processes, e.g. for rolling metal or metal working
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Abstract
The utility model relates to a magnetic particle inspection device for aircraft spare part relates to check out test set technical field, for solving the clamping in-process and presss from both sides easily and hinder the possibility that detects personnel, and it includes the organism, be provided with on the organism and detect the platform, it is provided with the fixture who is used for fixed spare part to detect bench, fixture includes first grip slipper, second grip slipper and is used for driving the drive assembly that the second grip slipper removed, first grip slipper and second grip slipper set up along the length direction who detects the platform, all be provided with the carousel on first grip slipper and the second grip slipper, it has seted up the reserve tank to detect bench, be provided with the mounting panel that supplies spare part to place in the reserve tank, the mounting panel bottom is provided with the support, one side that the mounting panel was kept away from to the support is provided with and drives actuating cylinder, it sets up in the reserve tank to drive actuating cylinder, still be provided with on the organism and spray the mechanism. The application has the effect of improving the safety of the detection equipment.
Description
Technical Field
The application relates to the technical field of detection equipment, in particular to a magnetic powder inspection device for aircraft parts.
Background
The magnetic particle inspection is a method for observing defects by using magnetic particles as a display medium, and the inspection method is divided into a wet method and a dry method according to the type of the magnetic particle medium applied during magnetization; inspection methods are classified into a continuous method and a residual magnetism method according to the time for applying magnetic powder to a workpiece.
After a ferromagnetic material workpiece is magnetized, due to the existence of discontinuity, magnetic lines of force on the surface and near the surface of the workpiece are subjected to local distortion to generate a leakage magnetic field, magnetic powder applied on the surface of the workpiece is adsorbed, and visible magnetic marks are formed under proper illumination, so that the position, size, shape and severity of the discontinuity are displayed, namely magnetic powder inspection or magnetic powder flaw detection, and the method belongs to one of five conventional methods for nondestructive inspection.
When an airplane needs to be repaired or repaired, the airframe structure and accessories need to be inspected, wherein crack detection of various parts is an important task, such as: the undercarriage parts, the hub connecting bolt, the engine suspension point bolt, the welding part and other ferromagnetic material parts can be subjected to flaw detection in a magnetic powder detection mode.
Before the detection of the existing detection equipment, a workpiece is held by a detection person to clamp a part to be detected, the detection person may be accidentally clamped in the clamping process, and the clamping process has certain potential safety hazards, so that the potential safety hazards are to be improved.
SUMMERY OF THE UTILITY MODEL
In order to solve the possibility that a detection worker is easily damaged by clamping in the clamping process, the application provides a magnetic powder flaw detection device for aircraft parts.
The application provides a magnetic particle inspection device for aircraft spare part adopts following technical scheme:
the utility model provides an aircraft is magnetic particle inspection device for spare part, includes the organism, be provided with on the organism and examine test table, it is provided with the fixture who is used for fixed spare part to examine test table, fixture includes first grip slipper, second grip slipper and is used for driving the drive assembly that the second grip slipper removed, first grip slipper and second grip slipper set up along the length direction who examines test table, all be provided with the carousel on first grip slipper and the second grip slipper, it has seted up the reservation groove on the test table to examine, be provided with the mounting panel that supplies spare part to place in the reservation groove, the mounting panel bottom is provided with the support, one side that the mounting panel was kept away from to the support is provided with drives actuating cylinder, it sets up in the reservation groove to drive actuating cylinder, still be provided with on the organism and spray the mechanism.
Before the existing detection equipment detects, a workpiece is held by a detection person to clamp a part to be detected, the detection person may be accidentally clamped in the clamping process, and certain potential safety hazards exist in the clamping process; by adopting the technical scheme, the part to be detected is placed on the mounting plate, the driving assembly is started, the driving assembly drives the second clamping seat to move towards one side of the first clamping seat until the parts are clamped by the turntables on the first clamping seat and the second clamping seat, the driving cylinder drives the mounting plate to move downwards at the moment, the spraying mechanism sprays the part, and the turntables drive the part to rotate, so that the surface of the part is uniformly sprayed; through the arrangement of the detection table, the preformed groove, the mounting plate, the support and the driving cylinder, the driving cylinder drives the mounting plate to lift, so that the position of the part is adjusted, the first clamping seat and the second clamping seat are fixed conveniently, the driving cylinder drives the mounting plate to descend into the preformed groove, the possibility of collision in the process that the turntable drives the part to rotate is reduced, and the part is effectively protected; meanwhile, no hand-held part is needed in the clamping process, the possibility of clamping injury of detection personnel is reduced, and the overall safety of the equipment is improved.
Optionally, drive assembly is including rotating the lead screw, rotating the motor and the track that slides, it rotates to connect in the reservation tank to rotate the lead screw, it sets up along examining test table length direction to rotate the lead screw, the output of rotating the motor is connected on rotating the lead screw, second grip slipper threaded connection is on rotating the lead screw, the track that slides sets up along the length direction of organism, the second grip slipper connection that slides is on the track that slides.
By adopting the technical scheme, the driving assembly consists of the rotating lead screw, the rotating motor and the sliding track, when a part to be detected is fixed, the rotating motor works, the rotating motor drives the rotating lead screw to rotate synchronously, the second clamping seat is in threaded connection with the rotating lead screw, the second clamping seat is connected to the sliding track in a sliding manner, and the second clamping seat gradually approaches to the first clamping seat until the part is clamped between the first clamping seat and the second clamping seat; through rotating the lead screw, rotating motor and the orbital setting that slides, help realizing the fixed to spare part, and the second grip slipper removes steadily.
Optionally, the spraying mechanism comprises a spraying box, a plurality of spraying branch pipes and a spraying pump for pumping out magnetic suspension in the spraying box, the spraying box is arranged on the outer wall of the machine body, one end of each spraying branch pipe is communicated with the spraying box, and the other end of each spraying branch pipe is arranged towards one side of the detection platform.
By adopting the technical scheme, the spraying mechanism consists of a spraying box, a plurality of spraying branch pipes and a spraying pump; after the part to be detected is clamped and fixed, the spraying pump starts to work, the spraying pump extracts the magnetic suspension in the spraying box, and the magnetic suspension is sprayed out of the plurality of spraying branch pipes to the part to be detected; through the setting of spraying branch pipe, a plurality of spraying branch pipes and spray pump, the setting of many spraying branch pipes helps improving the effect of spraying, sprays more comprehensively.
Optionally, a collecting pipe is arranged on the detection table, one end of the collecting pipe is communicated with the reserved groove, the other end of the collecting pipe is communicated with the spray box, and a collecting pump used for pumping out magnetic suspension is arranged on the collecting pipe.
By adopting the technical scheme, the bus pipe is arranged on the detection platform, and two ends of the bus pipe are respectively communicated with the interior of the reserved groove and the interior of the spraying box; after the detection of the parts is finished, starting a flow converging pump, and recycling the magnetic suspension collected in the reserved tank into a spraying box through a flow converging pipe by the flow converging pump; through the setting of collecting pipe and confluence pump, help realizing recycling to magnetic suspension, reduce the extravagant possibility of magnetic suspension, reduced the detection cost simultaneously.
Optionally, a baffle for shielding splashing of the magnetic suspension is arranged on the machine body, and the baffle is arranged at one end of the detection table.
By adopting the technical scheme, the machine body is provided with the baffle; through the setting of baffle, help realizing blockking the magnetic suspension who splashes, reduce the magnetic suspension and splash the possibility of polluting operational environment, improved the clean degree of detection ring border.
Optionally, a detection lamp for observing the surface condition of the component is arranged on the machine body.
By adopting the technical scheme, the machine body is provided with the detection lamp; through the setting of detecting lamp, be convenient for observe the magnetism trace on the spare part, observation effect is good, influences observation effect's possibility when reducing the observation because detection environment is dim.
Optionally, the machine body is provided with a support rod along the length direction, the support rod is arranged above the detection table, the support rod is wound with a hinge, the top of the detection lamp is provided with two support rings, one end of the hinge is connected to one of the support rings, and the other end of the hinge is connected to the other support ring.
By adopting the technical scheme, the machine body is provided with the supporting rod, and the supporting rod is wound with the hinge; through the setting of hinge, support rings and bracing piece, help realizing the installation to the detection lamp, stimulate the detection lamp simultaneously for the hinge slides on the bracing piece, thereby realizes the regulation of detection lamp position, is convenient for realize searchlighting the change of position, further improves the observation effect.
In summary, the present application includes at least one of the following beneficial technical effects:
1. through the arrangement of the detection table, the preformed groove, the mounting plate, the support and the driving cylinder, the driving cylinder drives the mounting plate to lift, so that the position of the part is adjusted, the first clamping seat and the second clamping seat are fixed conveniently, the driving cylinder drives the mounting plate to descend into the preformed groove, the possibility of collision in the process that the turntable drives the part to rotate is reduced, and the part is effectively protected; meanwhile, no hand-held part is needed in the clamping process, the possibility of clamping injury of detection personnel is reduced, and the overall safety of the equipment is improved;
2. through the arrangement of the spraying branch pipes, the plurality of spraying branch pipes and the spraying pump, the arrangement of the plurality of spraying branch pipes is beneficial to improving the spraying effect, and the spraying is more comprehensive;
3. through the setting of detecting lamp, be convenient for observe the magnetism trace on the spare part, observation effect is good, influences observation effect's possibility when reducing the observation because detection environment is dim.
Drawings
Fig. 1 is a schematic structural diagram of a magnetic particle inspection device for aircraft parts in an embodiment of the present application.
Fig. 2 is a sectional view of a clamping mechanism structure according to an embodiment of the present application.
Fig. 3 is a sectional view for embodying the structure of the spray mechanism in the embodiment of the present application.
Description of reference numerals: 1. a body; 2. a detection table; 21. reserving a groove; 3. a clamping mechanism; 31. a first clamping seat; 32. a second clamping seat; 33. a drive assembly; 331. rotating the screw rod; 332. rotating the motor; 333. a sliding track; 4. a turntable; 5. mounting a plate; 51. a support; 52. a driving cylinder; 6. a spraying mechanism; 61. a spray box; 62. spraying and pipe dividing; 63. a spray pump; 7. a collector pipe; 71. a converging pump; 8. a baffle plate; 9. a detection lamp; 91. supporting a lifting ring; 92. a hinge; 10. a support rod.
Detailed Description
The present application is described in further detail below with reference to figures 1-3.
The embodiment of the application discloses magnetic particle inspection device for aircraft parts. Referring to fig. 1 and 2, magnetic particle inspection device for aircraft spare part includes organism 1, installs the test table 2 that is used for spare part to detect on the organism 1, has seted up the reservation groove 21 on the test table 2, and the reservation groove 21 is seted up along the direction of height who detects table 2, installs fixture 3 on the test table 2, and fixture 3 is used for the fixed spare part that waits to detect, installs on the organism 1 and sprays mechanism 6.
Referring to fig. 2, the clamping mechanism 3 includes a first clamping seat 31, a second clamping seat 32 and a driving component 33, the first clamping seat 31 and the second clamping seat 32 are disposed along a length direction of the detection table 2, the first clamping seat 31 is welded and fixed on the detection table 2, the driving component 33 includes a rotating lead screw 331, a rotating motor 332 and a sliding rail 333, the rotating lead screw 331 is disposed along the length direction of the detection table 2, the rotating lead screw 331 is rotatably connected in the reserved slot 21, the rotating motor 332 is installed in the reserved slot 21, an output end of the rotating motor 332 is welded and fixed on an end portion of the rotating lead screw 331, in this embodiment, the rotating motor 332 can rotate in a forward and reverse direction, the second clamping seat 32 is in threaded connection with the rotating lead screw 331, the sliding rail 333 is installed on the machine body 1, and the second clamping seat 32 is slidably connected on the sliding rail 333 to limit a possibility that the rotating lead screw 331 drives the second clamping seat 32 to rotate.
Referring to fig. 2, the first clamping seat 31 and the second clamping seat 32 are both provided with a rotating plate 4, and in this embodiment, rotating members for controlling the rotation of the rotating plate 4 are disposed inside the first clamping seat 31 and the second clamping seat 32.
Referring to fig. 2 and 3, a driving cylinder 52 is installed on the detection table 2, the driving cylinder 52 is welded and fixed on the bottom wall of the preformed groove 21, the driving cylinder 52 is vertically arranged in the preformed groove 21, a support 51 is welded and fixed at the output end of the driving cylinder 52, and a mounting plate 5 is integrally formed at one end, away from the driving cylinder 52, of the support 51, wherein the mounting plate 5 is used for placing parts to be detected in the embodiment.
Referring to fig. 3, spraying mechanism 6 is used for spraying magnetic suspension on waiting to detect the spare part, spraying mechanism 6 includes spray box 61, a plurality of sprays are in charge of 62 and spray pump 63, spray box 61 sets up on organism 1 outer wall, the magnetic suspension is equipped with in spray box 61, a plurality of one end intercommunication that sprays in charge of 62 are on spray box 61, the 2 orientation settings of platform are examined to the spray end orientation of a plurality of sprays in charge of 62, spray pump 63 installs on a plurality of sprays in charge of 62, be used for taking out the magnetic suspension in spray box 61, many sprays in charge of 62 and be used for having improved the spraying effect, it is more comprehensive to spray.
Referring to fig. 3, the spray tank 61 is communicated with a collecting pipe 7, one end of the collecting pipe 7, which is far away from the spray tank 61, is communicated with the reserved tank 21, and a collecting pump 71 is installed on the collecting pipe 7, so as to recycle the magnetic suspension accumulated in the reserved tank 21, reduce the possibility of magnetic suspension waste, and reduce the detection cost.
Referring to fig. 3, one end of the detection table 2 is welded and fixed with a baffle 8, and the baffle 8 in the embodiment is shielded at the opening end of the detection table 2 and used for blocking the splashed magnetic suspension, so that the possibility that the magnetic suspension splashes to pollute the working environment is reduced, and the cleanliness of the detection environment is improved.
Referring to fig. 2 and 3, install the detection lamp 9 on the organism 1, the detection lamp 9 is located and examines test table 2 top, detection lamp 9 is used for observing spare part surface condition in this embodiment, install bracing piece 10 on the organism 1, bracing piece 10 sets up along the length direction who examines test table 2, around being equipped with hinge 92 on the bracing piece 10, two rings 91 that support are installed at the top of detection lamp 9, fixed connection is on two rings 91 that support respectively at the both ends of hinge 92, the quantity of hinge 92 is two sets of in this embodiment, be used for observing the magnetic trace on the spare part, the observation effect is good, influence the possibility of observation effect when reducing the observation because the measuring environment is dim.
The implementation principle of the magnetic powder inspection device for the airplane parts in the embodiment of the application is as follows: before detection, a part to be detected is placed on the mounting plate 5, the rotating motor 332 is started, the rotating screw 331 rotates, the second clamping seat 32 slides on the sliding rail 333, the second clamping seat 32 gradually approaches one side of the first clamping seat 31 until the two rotary tables 4 abut against the part, the rotating motor 332 stops rotating, the driving cylinder 52 drives the mounting plate 5 to move downwards, meanwhile, the spraying pump 63 starts to work, the spraying branch pipe 62 sprays magnetic suspension in the spraying box 61 onto the part to be detected, the rotary tables 4 drive the part to rotate, so that the part is uniformly sprayed, finally, a magnetization reaction is carried out, and a detector observes magnetic marks on the surface of the part through the detection lamp 9 so as to detect the part; through the arrangement of the detection table 2, the reserved groove 21, the mounting plate 5, the support 51 and the driving cylinder 52, the driving cylinder 52 drives the mounting plate 5 to ascend and descend, so that the position of the part is adjusted, the first clamping seat 31 and the second clamping seat 32 are fixed conveniently, the driving cylinder 52 drives the mounting plate 5 to descend into the reserved groove 21, the possibility of collision in the process that the turntable 4 drives the part to rotate is reduced, and the part is effectively protected; meanwhile, no hand-held part is needed in the clamping process, the possibility of clamping injury of detection personnel is reduced, and the overall safety of the equipment is improved.
The above embodiments are preferred embodiments of the present application, and the protection scope of the present application is not limited by the above embodiments, so: all equivalent changes made according to the structure, shape and principle of the present application shall be covered by the protection scope of the present application.
Claims (7)
1. The utility model provides an aircraft is magnetic particle inspection device for spare part which characterized in that: including organism (1), be provided with on organism (1) and examine test table (2), examine and be provided with fixture (3) that are used for fixed spare part on test table (2), fixture (3) include first grip slipper (31), second grip slipper (32) and are used for driving drive assembly (33) that second grip slipper (32) removed, length direction along examining test table (2) sets up first grip slipper (31) and second grip slipper (32), all be provided with carousel (4) on first grip slipper (31) and second grip slipper (32), reserve groove (21) have been seted up on examining test table (2), be provided with mounting panel (5) that supply spare part to place in reserve groove (21), mounting panel (5) bottom is provided with support (51), one side that mounting panel (5) were kept away from in support (51) is provided with drive actuating cylinder (52), drive actuating cylinder (52) set up in reserve groove (21), still be provided with on organism (1) and spray mechanism (6).
2. The magnetic particle inspection device for the aircraft parts according to claim 1, characterized in that: drive assembly (33) are including rotating lead screw (331), rotating motor (332) and track (333) that slides, it connects in preformed groove (21) to rotate lead screw (331), it sets up along examining test table (2) length direction to rotate lead screw (331), the output of rotating motor (332) is connected on rotating lead screw (331), second holder (32) threaded connection is on rotating lead screw (331), the length direction setting of organism (1) is followed to track (333) that slides, second holder (32) slide and connect on track (333) that slides.
3. The magnetic particle inspection device for the aircraft parts according to claim 1, wherein: spray mechanism (6) including spraying case (61), a plurality of spray and be used for taking out spray pump (63) that spray the interior magnetic suspension of case (61), spray case (61) and set up on organism (1) outer wall, the one end intercommunication that sprays and manage (62) is on spraying case (61), the other end orientation that sprays and manage (62) detects platform (2) one side and sets up.
4. The magnetic particle inspection device for the aircraft parts according to claim 3, characterized in that: detect and be provided with collector pipe (7) on platform (2), the one end intercommunication of collector pipe (7) is in reservation groove (21), the other end of collector pipe (7) with spray tank (61) and be linked together, be provided with on collector pipe (7) and be used for taking out magnetic suspension converge pump (71).
5. The magnetic particle inspection device for the aircraft parts according to claim 1, characterized in that: the machine body (1) is provided with a baffle (8) used for shielding splashing of the magnetic suspension, and the baffle (8) is arranged at one end of the detection table (2).
6. The magnetic particle inspection device for the aircraft parts according to claim 1, characterized in that: and a detection lamp (9) for observing the surface condition of the part is arranged on the machine body (1).
7. The magnetic particle inspection device for the aircraft parts according to claim 6, wherein: organism (1) is provided with bracing piece (10) along length direction, bracing piece (10) set up in examining test table (2) top, around being equipped with hinge (92) on bracing piece (10), the top of detecting lamp (9) is provided with two and supports rings (91), the one end of hinge (92) is connected one of it supports on rings (91), the other end of hinge (92) is connected another support rings (91).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222966116.3U CN218674852U (en) | 2022-11-08 | 2022-11-08 | Magnetic powder inspection device for aircraft parts |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222966116.3U CN218674852U (en) | 2022-11-08 | 2022-11-08 | Magnetic powder inspection device for aircraft parts |
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| Publication Number | Publication Date |
|---|---|
| CN218674852U true CN218674852U (en) | 2023-03-21 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222966116.3U Active CN218674852U (en) | 2022-11-08 | 2022-11-08 | Magnetic powder inspection device for aircraft parts |
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| CN (1) | CN218674852U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116754633A (en) * | 2023-08-17 | 2023-09-15 | 深圳市鑫泽峰科技有限公司 | Stamping hardware surface defect detection device |
-
2022
- 2022-11-08 CN CN202222966116.3U patent/CN218674852U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116754633A (en) * | 2023-08-17 | 2023-09-15 | 深圳市鑫泽峰科技有限公司 | Stamping hardware surface defect detection device |
| CN116754633B (en) * | 2023-08-17 | 2023-10-13 | 深圳市鑫泽峰科技有限公司 | Stamping hardware surface defect detection device |
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