CN115931597B - A quick detection device for aviation cable detects - Google Patents
A quick detection device for aviation cable detects Download PDFInfo
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- CN115931597B CN115931597B CN202310220389.XA CN202310220389A CN115931597B CN 115931597 B CN115931597 B CN 115931597B CN 202310220389 A CN202310220389 A CN 202310220389A CN 115931597 B CN115931597 B CN 115931597B
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Abstract
The invention discloses a rapid detection device for aviation cable detection, and belongs to the technical field of cable detection. Including the support frame, still include: the wire tightening wheel is rotationally connected to the surface of the support frame; the support column is fixedly connected to the surface of the support frame, the outer wall of the support column is fixedly connected with a fixing plate, and a first chute is formed in the surface of the fixing plate; the sliding strip is connected in the first sliding groove in a sliding way, an arc-shaped plate is fixedly connected to the surface of the sliding strip, and the arc-shaped plate is circumferentially arrayed with the support column as the center; the fixed connection is in the actuating mechanism on support frame surface, actuating mechanism is used for driving the draw runner and removes in first spout, makes the carousel rotate through handheld handle to adjust the circular internal diameter that each arc board encloses, this device need not the dismouting and changes, can realize adjusting aviation cable's deflection of bending, easy operation, convenient to use.
Description
Technical Field
The invention relates to the technical field of cable detection, in particular to a rapid detection device for aviation cable detection.
Background
The wire and cable are used to transmit electrical (magnetic) energy, information and wire products for electromagnetic energy conversion. The broad sense of electric wire and cable is also simply referred to as cable, and the narrow sense of cable is referred to as insulated cable, which can be defined as: an aggregate consisting of; one or more insulated cores, and the respective coatings, total protective layers and outer protective layers that they may have, may also have additional uninsulated conductors.
The aviation cable is a cable for aerospace, before the aviation cable is used, a user needs to detect the aviation cable, so that accidents in the using process are avoided, and when the bending deflection of the cable is verified and detected, the bending deflection of the aviation cable is often detected by replacing rotating supporting wheels with different diameters by the aviation cable detection device in the prior art.
In the detection method in the prior art, the bending deflection of the aviation cable needs to be adjusted every time, and the aviation cable needs to be disassembled, assembled and replaced, so that the process is complicated, and therefore, the aviation cable needs to be improved.
Disclosure of Invention
The invention aims to solve the problem that the process is complicated because the bending deflection of an aviation cable needs to be adjusted every time in the detection mode in the prior art, and provides a rapid detection device for aviation cable detection.
In order to achieve the above purpose, the present invention adopts the following technical scheme:
a quick detection device for aviation cable detects, includes the support frame, still includes: the wire tightening wheel is rotationally connected to the surface of the support frame; the support column is fixedly connected to the surface of the support frame, the outer wall of the support column is fixedly connected with a fixing plate, and a first chute is formed in the surface of the fixing plate; the sliding strip is connected in the first sliding groove in a sliding way, an arc-shaped plate is fixedly connected to the surface of the sliding strip, and the arc-shaped plate is circumferentially arrayed with the support column as the center; the driving mechanism is fixedly connected to the surface of the supporting frame and is used for driving the sliding strip to move in the first sliding groove.
In order to facilitate the movement of the drive slide, preferably, the drive mechanism comprises: the rotary pipe is rotatably connected to the surface of the support frame, the outer wall of the rotary pipe is fixedly connected with a rotary table, and a second chute is formed in the surface of the rotary table; the sliding column is fixedly connected to the surface of the sliding strip, a third sliding groove is formed in the surface of the fixing plate, and the sliding column is slidably connected in the third sliding groove and the second sliding groove; the rotary rack comprises a support frame, a first rotary rod, a handle and a first chain, wherein the first rotary rod is rotatably connected to the surface of the support frame, the handle is fixedly connected to the outer wall of the first rotary rod, and the first chain is connected between the first rotary rod and a rotary pipe in a transmission mode.
In order to reduce the abrasion between the support column and the rotating tube, further, the support column and the rotating tube are coaxial, and the inner diameter of the rotating tube is larger than the outer diameter of the support column.
In order to prevent the aviation cable from being separated from the arc-shaped plate in the process of adjusting the disturbance angle, preferably, the outer wall of the arc-shaped plate is symmetrically and fixedly connected with a first limiting plate.
To facilitate the detection of the coiled aerial cable, it preferably further comprises: the motor is fixedly connected to the surface of the support frame, the output end of the motor is fixedly connected with a first rotating column, and the first rotating column is rotationally connected with the support frame; the first rotary column is connected to the surface of the support frame in a rotating way, clamping grooves are formed in the surfaces of the first rotary column and the second rotary column, nuts are connected to the outer walls of the first rotary column and the second rotary column in a threaded mode, and a second chain is connected between the first rotary column and the second rotary column in a transmission mode; the second bull stick that sets up first bull stick surface, the surface of second bull stick is provided with the third bull stick, the equal fixedly connected with winding roller of outer wall of second bull stick and third bull stick, wherein, the one end fixedly connected with locating bar of second bull stick and third bull stick, locating bar and draw-in groove mutually match, the outer wall of second bull stick and third bull stick is provided with the external screw thread, the external screw thread mutually matches with the nut.
In order to prevent the aviation cable from being separated from the winding roller, further, the outer wall of the winding roller is symmetrically and fixedly connected with a second limiting plate.
In order to facilitate electrical detection of the aviation cable, further, the method further comprises: the surface of the connecting plate is fixedly connected with a circuit box, and the surface of the circuit box is fixedly connected with a first electrode column and a second electrode column; the positioning pipes are symmetrically and fixedly connected to the surface of the circuit box, the positioning pipes correspond to the first electrode columns and the second electrode columns one by one, and the first electrode columns and the second electrode columns are positioned in the corresponding positioning pipes; the through holes are formed in the surface of the second limiting plate, and the clamping mechanism is arranged on the surface of the second limiting plate.
In order to facilitate the fixing of the aerial cable, still further, the clamping mechanism comprises: the fourth sliding groove is formed in the surface of the second limiting plate, a sliding block is connected in a sliding manner in the fourth sliding groove, and a second clamping block is fixedly connected to the surface of the sliding block; the first clamping block is fixedly connected to the surface of the second limiting plate; the threaded rod is rotationally connected to the surface of the first clamping block, the threaded rod is in threaded connection with the second clamping block, and one end of the threaded rod is fixedly connected with a knob.
In order to improve the stability of the second clamping block, further, the sliding block is of a T shape, and the side walls of the first clamping block and the second clamping block are fixedly connected with protrusions.
In order to facilitate the detection of the heating fault of the cable, further, the surface of the supporting frame is fixedly connected with an infrared detector.
Compared with the prior art, the invention provides a rapid detection device for detecting aviation cables, which has the following beneficial effects:
1. this a quick detection device for aviation cable detects, when needing the adjustment to aviation cable's deflection of bending, handheld handle makes the carousel rotate, and the carousel drives the slide column and slides in the second spout, and the slide column drives the draw runner and slides in the third spout, and the draw runner drives the arc and removes to adjust the circular internal diameter that each arc encloses, this device need not the dismouting and changes, can realize adjusting aviation cable's deflection of bending, easy operation, convenient to use.
2. This a quick detection device for aviation cable detects, through with the location strip joint in the draw-in groove, rotatory nut will second bull stick and first revolving post between, fixed connection between third bull stick and the second revolving post, start motor drive line roller rotates to conveniently according to the circular shape external diameter's that the arc encloses size real-time mobile cable, improved work efficiency, simultaneously, under the linking effect of external screw thread, nut, location strip, draw-in groove, make things convenient for the fixed and dismantlement of two tight line wheels.
3. This a quick detection device for aviation cable detects before carrying out the electrical property detection, pass the through-hole with the extension end of cable, with the extension end and first electrode post, the contact of second electrode post of cable, rotatory knob makes the second clamp splice be close to first clamp splice, thereby the convenience is with the cable centre gripping between first clamp splice and second clamp splice, and then the extension end of fixed cable, because the extension end of cable is located the locating tube, can prevent the poor contact between cable and first electrode post, the second electrode post, the accuracy of cable electrical property testing result has been improved.
4. This a quick detection device for aviation cable detects carries out the electrical property detection in advance, at the in-process of electrical property detection, carries out the fault detection that generates heat to aviation cable, then, makes the extension end and the circuit box separation of cable, and finally, carries out the deflection detection of bending to aviation cable, and this device can carry out the electrical property simultaneously and detects, generates heat and detects, the detection of disturbance degree, has improved detection efficiency, avoids using multiple detection device to detect the cable, has reduced detection cost, simultaneously, has improved detection efficiency.
Drawings
Fig. 1 is a schematic structural diagram of a rapid detection device for detecting an aviation cable according to the present invention;
fig. 2 is a schematic structural diagram of a driving mechanism in a rapid detection device for detecting an aviation cable according to the present invention;
fig. 3 is a schematic diagram of a part of a rapid detection device for detecting an aviation cable according to the present invention;
fig. 4 is an enlarged schematic diagram of a structure at a in fig. 3 of a rapid detection device for detecting an aviation cable according to the present invention;
fig. 5 is a schematic diagram of a winding roller structure in a rapid detection device for detecting an aviation cable according to the present invention;
fig. 6 is a schematic structural diagram of a clamping mechanism in a rapid detection device for detecting an aviation cable according to the present invention;
fig. 7 is an enlarged schematic view of the structure at B in fig. 6 of a rapid detection device for detecting an aviation cable according to the present invention;
fig. 8 is a schematic diagram of a part of a rapid detection device for detecting an aviation cable according to the present invention.
In the figure: 1. a support frame; 101. a wire tightening wheel; 102. a support column; 103. a fixing plate; 104. a slide bar; 105. an arc-shaped plate; 106. a first chute; 2. a first rotating lever; 201. a handle; 202. a rotary pipe; 203. a turntable; 204. a second chute; 205. a spool; 206. a third chute; 207. a first chain; 208. a first limiting plate; 3. a motor; 301. a first swivel post; 302. a second rotating rod; 303. a wire winding roller; 304. a positioning strip; 305. a clamping groove; 306. a nut; 307. an external thread; 308. a second chain; 4. a second swivel post; 401. a third rotating rod; 402. a second clamping block; 403. a second limiting plate; 404. a through hole; 405. a fourth chute; 406. a slide block; 407. a threaded rod; 408. a first clamping block; 5. a splice plate; 501. a circuit box; 502. a first electrode column; 503. a second electrode column; 504. a protrusion; 505. a positioning tube; 506. a knob; 507. an infrared detector.
Detailed Description
The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments.
In the description of the present invention, it should be understood that the terms "upper," "lower," "front," "rear," "left," "right," "top," "bottom," "inner," "outer," and the like indicate or are based on the orientation or positional relationship shown in the drawings, merely to facilitate description of the present invention and to simplify the description, and do not indicate or imply that the devices or elements referred to must have a specific orientation, be configured and operated in a specific orientation, and thus should not be construed as limiting the present invention.
Example 1:
referring to fig. 1 to 3, a rapid detection device for detecting an aviation cable comprises a support frame 1, and further comprises: the wire tightening wheel 101 is rotatably connected to the surface of the support frame 1; the support column 102 is fixedly connected to the surface of the support frame 1, the outer wall of the support column 102 is fixedly connected with the fixing plate 103, and a first chute 106 is formed in the surface of the fixing plate 103; the sliding strips 104 are slidably connected in the first sliding grooves 106, the surfaces of the sliding strips 104 are fixedly connected with arc-shaped plates 105, the arc-shaped plates 105 are circumferentially arrayed by taking the supporting columns 102 as the center, and the number of the arc-shaped plates 105 is 3-5; the driving mechanism is fixedly connected to the surface of the support frame 1, and is used for driving the sliding strip 104 to move in the first sliding groove 106.
Referring to fig. 1 and 3, the number of the take-up pulley 101 is four, and the fixing plate 103 is located between two of the take-up pulleys 101.
Referring to fig. 1-3, the drive mechanism includes: the rotating pipe 202 is rotatably connected to the surface of the support frame 1, the outer wall of the rotating pipe 202 is fixedly connected with the rotating disk 203, and a second chute 204 is formed in the surface of the rotating disk 203; the sliding column 205 is fixedly connected to the surface of the sliding strip 104, a third sliding groove 206 is formed in the surface of the fixed plate 103, and the sliding column 205 is slidably connected in the third sliding groove 206 and the second sliding groove 204; the first rotating rod 2 is rotatably connected to the surface of the supporting frame 1, and a handle 201 is fixedly connected to the outer wall of the first rotating rod 2.
It should be noted that, referring to fig. 2-3, the first sprocket is fixedly connected to the outer walls of the first rotating rod 2 and the rotating tube 202, and a first chain 207 is connected between adjacent first sprockets.
When the bending deflection of the aviation cable needs to be adjusted, the first rotating rod 2 is rotated by the handheld handle 201, the rotating tube 202 is driven to rotate by the first rotating rod 2, the rotating tube 202 drives the rotating disc 203 to rotate, the rotating disc 203 drives the sliding column 205 to slide in the second sliding groove 204, the sliding column 205 drives the sliding strip 104 to slide in the third sliding groove 206, the sliding strip 104 drives the arc plates 105 to move, and accordingly the circular inner diameter enclosed by the arc plates 105 is adjusted.
To reduce wear between support post 102 and rotor tube 202, referring to FIG. 3, support post 102 is coaxial with rotor tube 202, and the inner diameter of rotor tube 202 is greater than the outer diameter of support post 102.
In order to prevent the aviation cable from separating from the arc plate 105 in the process of adjusting the disturbance angle, referring to fig. 1-3, the outer wall of the arc plate 105 is symmetrically and fixedly connected with a first limiting plate 208.
Example 2:
referring to fig. 1-5, substantially the same as example 1, further, embodiments of the aerial cable to enhance test spooling were added.
Because the cable for aviation is longer, if lean on the measuring staff to remove the cable alone, realize the deflection detection of bending everywhere to the cable, detection efficiency is lower, consequently, this a quick detection device for aviation cable detects still includes: the motor 3 is fixedly connected to the surface of the support frame 1, the output end of the motor 3 is fixedly connected with a first rotating column 301, and the first rotating column 301 is rotationally connected with the support frame 1; the second rotating column 4 is rotatably connected to the surface of the supporting frame 1, clamping grooves 305 are formed in the surfaces of the first rotating column 301 and the second rotating column 4, and nuts 306 are connected to the outer walls of the first rotating column 301 and the second rotating column 4 in a threaded mode; the second bull stick 302 of setting on first bull stick 301 surface, the surface of second bull stick 4 is provided with third bull stick 401, the equal fixedly connected with wire winding roller 303 of outer wall of second bull stick 302 and third bull stick 401, wherein, the one end fixedly connected with location strip 304 of second bull stick 302 and third bull stick 401, location strip 304 and draw-in groove 305 mutual match, the outer wall of second bull stick 302 and third bull stick 401 is provided with external screw thread 307, external screw thread 307 and nut 306 mutual match, namely threaded connection.
In this embodiment, the outer walls of the first rotating post 301 and the second rotating post 4 are fixedly connected with second sprockets, and a second chain 308 is in transmission connection between adjacent second sprockets.
When the wire winding device is used, the locating bar 304 is aligned with the clamping groove 305, the locating bar 304 is clamped in the clamping groove 305, the rotating nut 306 fixedly connects the second rotating rod 302 with the first rotating rod 301 and the third rotating rod 401 with the second rotating rod 4, a cable is wound on one wire winding roller 303, the extending end of the cable is sequentially fixed on the other wire winding roller 303 through the wire tightening wheel 101, the arc-shaped plate 105 and the wire tightening wheel 101, the motor 3 is started to drive the first rotating rod 301 to rotate, the first rotating rod 301 drives the second rotating rod 302 to rotate, meanwhile, under the action of the second chain 308, the first rotating rod 301 drives the second rotating rod 4 to rotate, the second rotating rod 4 drives the third rotating rod 401 to rotate, and the third rotating rod 401 and the second rotating rod 302 drive the wire winding roller 303 to rotate, so that the cable can be conveniently moved in real time according to the size of the circular outer diameter surrounded by the arc-shaped plate 105, the working efficiency is improved, and simultaneously, under the connection effect of the external threads 307, the nut 306, the locating bar 304 and the clamping groove, the two wire tightening wheels 101 are conveniently fixed and detached.
In order to prevent the aviation cable from being separated from the winding roller 303, the outer wall of the winding roller 303 is symmetrically and fixedly connected with a second limiting plate 403.
Example 3:
referring to fig. 3-8, substantially the same as example 2, further, embodiments for electrical testing of an aerial cable have been added.
Because the cables applied to aviation all need to be electrically detected before being used, referring to fig. 3-8, the rapid detection device for aviation cable detection further comprises: the connecting plate 5 is fixedly connected to the surface of one of the wire winding rollers 303, the surface of the connecting plate 5 is fixedly connected with the circuit box 501, and the surface of the circuit box 501 is fixedly connected with the first electrode column 502 and the second electrode column 503; the positioning pipes 505 are symmetrically and fixedly connected to the surface of the circuit box 501, the positioning pipes 505 correspond to the first electrode columns 502 and the second electrode columns 503 one by one, and the first electrode columns 502 and the second electrode columns 503 are positioned in the corresponding positioning pipes 505; through holes 404 formed in the surface of the second limiting plate 403, and a clamping mechanism is arranged on the surface of the second limiting plate 403.
Referring to fig. 7, the clamping mechanism includes: a fourth sliding groove 405 formed on the surface of the second limiting plate 403, a sliding block 406 is connected in a sliding manner in the fourth sliding groove 405, and a second clamping block 402 is fixedly connected on the surface of the sliding block 406; a first clamping block 408 fixedly connected to the surface of the second limiting plate 403; the threaded rod 407 connected to the surface of the first clamping block 408 is rotated, the threaded rod 407 is in threaded connection with the second clamping block 402, and one end of the threaded rod 407 is fixedly connected with a knob 506.
It should be noted that the through hole 404 is located between the first clamping block 408 and the second clamping block 402.
Before electrical detection, the extending end of the cable passes through the through hole 404, one extending end of the cable is in contact with the first electrode column 502, the other extending end of the cable is in contact with the second electrode column 503, the threaded rod 407 is rotated by the rotating knob 506, the threaded rod 407 drives the second clamping block 402 to be close to the first clamping block 408, and the sliding block 406 can only slide in the fourth sliding groove 405, so that the moving range of the second clamping block 402 is limited, the cable is conveniently clamped between the first clamping block 408 and the second clamping block 402, the extending end of the cable is further fixed, and poor contact between the cable and the first electrode column 502 and the second electrode column 503 can be prevented due to the fact that the extending end of the cable is positioned in the positioning tube 505, and the electrical detection result of the cable is affected.
The slider 406 is T-shaped, and can prevent the second clamping block 402 from deflecting during the movement of the second clamping block 402, thereby improving the stability of the second clamping block 402.
Since the sidewalls of the first and second clamping blocks 408 and 402 are fixedly coupled with the protrusions 504 during clamping of the cable.
Example 4:
referring to fig. 1, substantially the same as example 3, further, a specific embodiment of detecting a heat generation failure of the cable is added.
The heating fault is a common fault of the cable, and if the heating fault occurs in the aviation cable, a safety accident is easily caused, so that in order to conveniently detect the heating fault of the aviation cable, the surface of the support frame 1 is fixedly connected with an infrared detector 507.
The electrical property detection is firstly carried out, the heating fault detection is carried out on the aviation cable in the electrical property detection process, then, the extending end of the cable is separated from the circuit box 501, and finally, the bending deflection detection is carried out on the aviation cable.
The foregoing is only a preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art who is skilled in the art to which the present invention pertains should make equivalent substitutions or modifications according to the technical scheme and the inventive concept disclosed herein, and should be covered by the scope of the present invention.
Claims (7)
1. The utility model provides a quick detection device for aviation cable detects, includes support frame (1), its characterized in that still includes:
a wire tightening wheel (101) rotatably connected to the surface of the support frame (1);
the support column (102) is fixedly connected to the surface of the support frame (1), the outer wall of the support column (102) is fixedly connected with the fixing plate (103), and a first chute (106) is formed in the surface of the fixing plate (103);
the sliding strip (104) is connected in the first sliding groove (106) in a sliding way, an arc-shaped plate (105) is fixedly connected to the surface of the sliding strip (104), and the arc-shaped plate (105) is circumferentially arrayed by taking the supporting column (102) as the center;
the driving mechanism is fixedly connected to the surface of the supporting frame (1) and is used for driving the sliding bar (104) to move in the first sliding groove (106);
further comprises: the motor (3) is fixedly connected to the surface of the support frame (1), the output end of the motor (3) is fixedly connected with a first rotating column (301), and the first rotating column (301) is rotationally connected with the support frame (1);
the second rotating column (4) is rotatably connected to the surface of the supporting frame (1), clamping grooves (305) are formed in the surfaces of the first rotating column (301) and the second rotating column (4), nuts (306) are connected to the outer walls of the first rotating column (301) and the second rotating column (4) in a threaded mode, and a second chain (308) is connected between the first rotating column (301) and the second rotating column (4);
the second rotating rod (302) is arranged on the surface of the first rotating column (301), a third rotating rod (401) is arranged on the surface of the second rotating column (4), the outer walls of the second rotating rod (302) and the third rotating rod (401) are fixedly connected with a winding roller (303),
one end of the second rotating rod (302) and one end of the third rotating rod (401) are fixedly connected with a locating bar (304), the locating bar (304) is matched with the clamping groove (305), external threads (307) are arranged on the outer walls of the second rotating rod (302) and the third rotating rod (401), and the external threads (307) are matched with the nuts (306);
the outer wall of the winding roller (303) is symmetrically and fixedly connected with a second limiting plate (403);
further comprises: the connecting plate (5) is fixedly connected to the surface of one winding roller (303), a circuit box (501) is fixedly connected to the surface of the connecting plate (5), and a first electrode column (502) and a second electrode column (503) are fixedly connected to the surface of the circuit box (501);
the positioning pipes (505) are symmetrically and fixedly connected to the surface of the circuit box (501), the positioning pipes (505) are in one-to-one correspondence with the first electrode columns (502) and the second electrode columns (503), and the first electrode columns (502) and the second electrode columns (503) are positioned in the corresponding positioning pipes (505);
and a through hole (404) formed in the surface of the second limiting plate (403), wherein a clamping mechanism is arranged on the surface of the second limiting plate (403).
2. A rapid inspection device for the inspection of an aircraft cable according to claim 1, wherein the drive mechanism comprises:
the rotary pipe (202) is rotatably connected to the surface of the support frame (1), a rotary table (203) is fixedly connected to the outer wall of the rotary pipe (202), and a second chute (204) is formed in the surface of the rotary table (203);
the sliding column (205) is fixedly connected to the surface of the sliding strip (104), a third sliding groove (206) is formed in the surface of the fixed plate (103), and the sliding column (205) is slidably connected in the third sliding groove (206) and the second sliding groove (204);
the rotary support comprises a support frame (1), and is characterized in that a first rotary rod (2) is rotatably connected to the surface of the support frame (1), a handle (201) is fixedly connected to the outer wall of the first rotary rod (2), and a first chain (207) is connected between the first rotary rod (2) and a rotary pipe (202) in a transmission mode.
3. A rapid detection device for aerial cable detection according to claim 2, characterized in that the support column (102) is coaxial with a swivel tube (202), the swivel tube (202) having an inner diameter larger than the outer diameter of the support column (102).
4. The rapid detection device for aviation cable detection according to claim 1, characterized in that the outer wall of the arc-shaped plate (105) is symmetrically and fixedly connected with a first limiting plate (208).
5. A rapid inspection device for the inspection of an aircraft cable according to claim 1, wherein the clamping mechanism comprises:
a fourth sliding groove (405) formed in the surface of the second limiting plate (403), wherein a sliding block (406) is connected in a sliding manner in the fourth sliding groove (405), and a second clamping block (402) is fixedly connected to the surface of the sliding block (406);
the first clamping block (408) is fixedly connected to the surface of the second limiting plate (403);
the threaded rod (407) is rotatably connected to the surface of the first clamping block (408), the threaded rod (407) is in threaded connection with the second clamping block (402), and one end of the threaded rod (407) is fixedly connected with a knob (506).
6. The rapid detection device for detecting an aviation cable according to claim 5, wherein the slider (406) is T-shaped, and the side walls of the first clamping block (408) and the second clamping block (402) are fixedly connected with protrusions (504).
7. The rapid detection device for detecting aviation cables according to claim 1, characterized in that the surface of the support frame (1) is fixedly connected with an infrared detector (507).
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| CN202310220389.XA CN115931597B (en) | 2023-03-09 | 2023-03-09 | A quick detection device for aviation cable detects |
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| CN202310220389.XA CN115931597B (en) | 2023-03-09 | 2023-03-09 | A quick detection device for aviation cable detects |
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| CN118090094A (en) * | 2024-04-25 | 2024-05-28 | 四川新蓉电缆有限责任公司 | Detection device for aviation cable |
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