CN115931597A - A quick detection device for aviation cable detects - Google Patents
A quick detection device for aviation cable detects Download PDFInfo
- Publication number
- CN115931597A CN115931597A CN202310220389.XA CN202310220389A CN115931597A CN 115931597 A CN115931597 A CN 115931597A CN 202310220389 A CN202310220389 A CN 202310220389A CN 115931597 A CN115931597 A CN 115931597A
- Authority
- CN
- China
- Prior art keywords
- fixedly connected
- column
- sliding
- rotating
- support frame
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Images
Landscapes
- Geophysics And Detection Of Objects (AREA)
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 rotatably connected to the surface of the support frame; the supporting column is fixedly connected to the surface of the supporting frame, the outer wall of the supporting column is fixedly connected with a fixing plate, and the surface of the fixing plate is provided with a first sliding chute; the sliding strip is connected in the first sliding groove in a sliding mode, an arc-shaped plate is fixedly connected to the surface of the sliding strip, and the arc-shaped plate is arranged in a circumferential array by taking a supporting column as the center; 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 encloses, this device need not the dismouting and changes, can realize adjusting the amount of deflection of bending of aviation cable, 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 is used for transmitting electric (magnetic) energy, information and wire products for realizing electromagnetic energy conversion. A wire cable in a broad sense, also referred to as a cable for short, refers to an insulated cable, which can be defined as: an aggregate consisting of; one or more insulated wire cores, and their respective possible coatings, total protective layers and outer jackets, the cable may also have additional conductors without insulation.
The aviation cable is a cable for aerospace, and before the aviation cable is used, a user needs to detect the cable so as to avoid accidents in the using process.
The detection mode in the prior art needs to be disassembled, assembled and replaced when the bending deflection of the aviation cable needs to be adjusted every time, so that the process is complicated, and the aviation cable needs to be improved.
Disclosure of Invention
The invention aims to solve the problem that in the detection mode in the prior art, the aviation cable needs to be disassembled, assembled and replaced every time the bending deflection of the aviation cable needs to be adjusted, so that the process is complicated, and the rapid detection device for aviation cable detection is provided.
In order to achieve the purpose, the invention adopts the following technical scheme:
the utility model provides a quick detection device for aviation cable detects, includes the support frame, still includes: the wire tightening wheel is rotatably connected to the surface of the support frame; the supporting column is fixedly connected to the surface of the supporting frame, the outer wall of the supporting column is fixedly connected with a fixing plate, and the surface of the fixing plate is provided with a first sliding chute; the sliding strip is connected in the first sliding groove in a sliding mode, an arc-shaped plate is fixedly connected to the surface of the sliding strip, and the arc-shaped plate is arranged in a circumferential array by taking a supporting column as the center; the driving mechanism is fixedly connected to the surface of the support frame and used for driving the sliding strip to move in the first sliding groove.
In order to facilitate driving the slide bar to move, preferably, the driving mechanism includes: the rotating pipe is rotatably connected to the surface of the support frame, the outer wall of the rotating pipe is fixedly connected with a rotating disc, and a second sliding groove is formed in the surface of the rotating disc; 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 connected in the third sliding groove and the second sliding groove in a sliding mode; rotate to be connected the first bull stick on support frame surface, the outer wall fixedly connected with handle of first bull stick, the transmission is connected with first chain between first bull stick and the bull pipe.
In order to reduce the abrasion between the supporting column and the rotating pipe, further, the supporting column is coaxial with the rotating pipe, and the inner diameter of the rotating pipe is larger than the outer diameter of the supporting column.
In order to prevent that the aviation cable breaks away from the arc at the in-process of adjusting the degree of disturbance angle, preferably, the outer wall symmetry fixedly connected with first limiting plate of arc.
In order to facilitate the detection of the coiled aviation cable, it is preferable that the method 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 rotatably connected with the support frame; the second rotary column is rotatably connected to the surface of the support frame, 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 setting is in the second bull stick on first bull stick surface, the surface of second bull stick is provided with the third bull stick, the equal fixedly connected with winding roll of outer wall of second bull stick and third bull stick, wherein, the one end fixedly connected with location strip of second bull stick and third bull stick, location strip and draw-in groove match each other, the outer wall of second bull stick and third bull stick is provided with the external screw thread, the external screw thread matches each other with the nut.
In order to prevent the aviation cable from separating from the winding roll, a second limiting plate is symmetrically and fixedly connected to the outer wall of the winding roll.
In order to facilitate the electrical detection of the aviation cable, further, the method further comprises: the connecting plate is fixedly connected to the surface of one of the winding rollers, a circuit box is fixedly connected to the surface of the connecting plate, and a first electrode column and a second electrode column are fixedly connected to the surface of the circuit box; the positioning tubes are symmetrically and fixedly connected to the surface of the circuit box, the positioning tubes correspond to the first electrode columns and the second electrode columns one to one, and the first electrode columns and the second electrode columns are located in the corresponding positioning tubes; the through hole is 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 aircraft cable, furthermore, the clamping mechanism comprises: a fourth sliding groove formed in the surface of the second limiting plate, a sliding block is connected in the fourth sliding groove in a sliding manner, 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 connected to the surface of the first clamping block in a rotating mode, the threaded rod is in threaded connection with the second clamping block, and a knob is fixedly connected to one end of the threaded rod.
In order to improve the stability of the second clamping block, furthermore, the sliding block is T-shaped, and the side walls of the first clamping block and the second clamping block are fixedly connected with protrusions.
In order to facilitate detection of the heating fault of the cable, furthermore, an infrared detector is fixedly connected to the surface of the support frame.
Compared with the prior art, the invention provides a rapid detection device for aviation cable detection, which has the following beneficial effects:
1. this a quick detection device for aviation cable detects, when the amount of deflection of bending of aviation cable is adjusted to needs, handheld handle makes the carousel rotate, the carousel drives the traveller and slides in the second spout, the traveller drives the draw runner and slides in the third spout, the draw runner drives the arc and removes, thereby adjust the circular internal diameter that each arc encloses, this device need not the dismouting and changes, can realize adjusting the amount of deflection of bending of aviation cable, and is easy operation, high durability and convenient use.
2. This a quick detection device for aviation cable detects, through with the location strip joint in the draw-in groove, swivel nut is with between second bull stick and the first bull stick, fixed connection between third bull stick and the second bull stick, the starter motor drive winding roll rotates, thereby the convenience is according to the big or small real-time mobile cable of the circular shape external diameter that the arc encloses, and the work efficiency is improved, and simultaneously, at the external screw thread, the nut, the location strip, under the linking effect of draw-in groove, make things convenient for the fixed of two tights and dismantle.
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 the first electrode post of cable, the contact of second electrode post, rotatory knob makes the second clamp splice be close to first clamp splice, thereby conveniently 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 registration arm, can prevent cable and first electrode post, contact failure between 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 electrical property detection earlier, at the in-process that electrical property detected, to aviation cable fault detection that generates heat, then, makes the extension end and the circuit box separation of cable, and finally, the amount of deflection that bends to aviation cable detects, and this device can carry out electrical property detection simultaneously, generate heat and detect, the degree of deflection detects, has improved detection efficiency, avoids using multiple detection device to detect the cable, has reduced the detection cost, simultaneously, has improved detection efficiency.
Drawings
Fig. 1 is a schematic structural diagram of a rapid detection device for aviation cable detection according to the present invention;
FIG. 2 is a schematic structural diagram of a driving mechanism in a rapid detection device for aviation cable detection according to the present invention;
FIG. 3 is a schematic view of a part of the structure of a rapid detection device for aviation cable detection according to the present invention;
fig. 4 is an enlarged schematic view of a structure at a in fig. 3 of the rapid detection device for aviation cable detection according to the present invention;
fig. 5 is a schematic structural diagram of a winding roll in a rapid detection device for aviation cable detection according to the present invention;
FIG. 6 is a schematic structural diagram of a clamping mechanism in a rapid detection device for aviation cable detection according to the present invention;
fig. 7 is an enlarged schematic view of a structure at B in fig. 6 of the rapid detection device for aviation cable detection according to the present invention;
fig. 8 is a schematic partial structural diagram of a rapid detection device for aviation cable detection 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. rotating the pipe; 203. a turntable; 204. a second chute; 205. a traveler; 206. a third chute; 207. a first chain; 208. a first limit plate; 3. a motor; 301. a first rotating column; 302. a second rotating rod; 303. a winding roll; 304. a positioning bar; 305. a card slot; 306. a nut; 307. an external thread; 308. a second chain; 4. a second rotary column; 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 slider; 407. a threaded rod; 408. a first clamping block; 5. a connector tile; 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 technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments.
In the description of the present invention, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, are merely for convenience in describing the present invention and simplifying the description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention.
Example 1
Referring to fig. 1-3, a quick detection device for aviation cable detection includes a support frame 1, and further includes: a wire tightening wheel 101 which is rotatably connected to the surface of the support frame 1; the supporting column 102 is fixedly connected to the surface of the supporting frame 1, the outer wall of the supporting column 102 is fixedly connected with a fixing plate 103, and the surface of the fixing plate 103 is provided with a first sliding groove 106; the sliding strip 104 is connected in the first sliding groove 106 in a sliding mode, the surface of the sliding strip 104 is fixedly connected with arc-shaped plates 105, the arc-shaped plates 105 are arranged in a circumferential array by taking the supporting column 102 as the center, and the number of the arc-shaped plates 105 is 3-5; and the driving mechanism is fixedly connected to the surface of the support frame 1 and is used for driving the slide bar 104 to move in the first sliding groove 106.
Referring to fig. 1 and 3, the number of the take-up pulleys 101 is four, and the fixed plate 103 is located between two of the take-up pulleys 101.
Referring to fig. 1 to 3, the driving 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 a rotating disc 203, and the surface of the rotating disc 203 is provided with a second sliding chute 204; a sliding column 205 fixedly connected to the surface of the sliding strip 104, a third sliding groove 206 is formed on the surface of the fixing plate 103, and the sliding column 205 is connected in the third sliding groove 206 and the second sliding groove 204 in a sliding manner; rotate the first bull stick 2 of connecting on support frame 1 surface, the outer wall fixedly connected with handle 201 of first bull stick 2.
It should be added that, referring to fig. 2 to fig. 3, the first rotating rod 2 and the outer wall of the rotating tube 202 are both fixedly connected with first chain wheels, and a first chain 207 is connected between adjacent first chain wheels in a transmission manner.
When the bending deflection of aviation cable needs to be adjusted, the handle 201 is held to enable the first rotating rod 2 to rotate, the first rotating rod 2 drives the rotating pipe 202 to rotate, the rotating pipe 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-shaped plates 105 to move, thereby adjusting the circular inner diameter formed by the arc-shaped plates 105 in a surrounding mode, the device does not need to be disassembled and assembled for replacement, the bending deflection of aviation cable can be adjusted, the operation is simple, and the use is convenient.
To reduce wear between the support post 102 and the rotating tube 202, and referring to fig. 3, the support post 102 is coaxial with the rotating tube 202, with the inner diameter of the rotating tube 202 being greater than the outer diameter of the support post 102.
In order to prevent the aviation cable from being separated from the arc-shaped plate 105 in the process of adjusting the deflection angle, referring to fig. 1 to 3, a first limiting plate 208 is symmetrically and fixedly connected to the outer wall of the arc-shaped plate 105.
Example 2
Referring to fig. 1-5, essentially the same as in example 1, further, embodiments are added to enhance the detection of coiled aircraft cables.
Because the cable for the aviation is longer, if singly lean on the measurement personnel to remove the cable, realize the flexibility of bending everywhere to the cable and detect, 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 rotatably connected with the support frame 1; the second rotary column 4 is rotatably connected to the surface of the support frame 1, clamping grooves 305 are formed in the surfaces of the first rotary column 301 and the second rotary column 4, and nuts 306 are connected to the outer walls of the first rotary column 301 and the second rotary column 4 in a threaded mode; the setting is at second bull stick 302 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 winding roll 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 match each other, the outer wall of second bull stick 302 and third bull stick 401 is provided with external screw thread 307, external screw thread 307 matches each other with nut 306, that is to say threaded connection.
In this embodiment, the outer walls of the first rotary column 301 and the second rotary column 4 are both fixedly connected with second chain wheels, and a second chain 308 is connected between the adjacent second chain wheels in a transmission manner.
When the cable tightening device is used, the positioning strip 304 is aligned to the clamping groove 305, the positioning strip 304 is clamped in the clamping groove 305, the rotating nut 306 fixedly connects the second rotating rod 302 and the first rotating column 301, the third rotating rod 401 and the second rotating column 4, a cable is wound on one winding roller 303, the extending end of the cable sequentially passes through the wire tightening wheel 101, the arc-shaped plate 105 and the wire tightening wheel 101 and is fixed on the other winding roller 303, the starting motor 3 drives the first rotating column 301 to rotate, the first rotating column 301 drives the second rotating rod 302 to rotate, meanwhile, under the action of the second chain 308, the first rotating column 301 drives the second rotating column 4 to rotate, the second rotating column 4 drives the third rotating rod 401 to rotate, the third rotating rod 401 and the second rotating rod 302 drive the winding roller 303 to rotate, so that the cable can be conveniently moved in real time according to the size of the outer diameter of the circle surrounded by the arc-shaped plate 105, the working efficiency is improved, and meanwhile, under the linking action of the outer thread 307, the nut 306, the positioning strip 304 and the clamping groove 305, the wire tightening wheel 101 can be conveniently detached.
In order to prevent the aviation cable from being separated from the winding roller 303, a second limiting plate 403 is symmetrically and fixedly connected to the outer wall of the winding roller 303.
Example 3
Referring to fig. 3-8, substantially the same as example 2, further, a specific embodiment for electrical inspection of the aircraft cable is added.
Since the cable applied to aviation needs to be electrically detected before use, referring to fig. 3 to 8, the rapid detection device for aviation cable detection further includes: the connecting plate 5 is fixedly connected to the surface of one of the winding rollers 303, the surface of the connecting plate 5 is fixedly connected with a circuit box 501, and the surface of the circuit box 501 is fixedly connected with a first electrode column 502 and a second electrode column 503; the positioning tubes 505 are symmetrically and fixedly connected to the surface of the circuit box 501, the positioning tubes 505 correspond to the first electrode posts 502 and the second electrode posts 503 one by one, and the first electrode posts 502 and the second electrode posts 503 are positioned in the corresponding positioning tubes 505; a through hole 404 formed in the surface of the second limiting plate 403, and a clamping mechanism is provided on the surface of the second limiting plate 403.
Referring to fig. 7, the chucking mechanism includes: a fourth sliding chute 405 formed in the surface of the second limiting plate 403, wherein a sliding block 406 is slidably connected in the fourth sliding chute 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 limit 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 the knob 506.
It should be added that the through hole 404 is located between the first clamping block 408 and the second clamping block 402.
Before electrical detection is carried out, the extending end of the cable penetrates 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 rotary knob 506 is rotated to enable the threaded rod 407 to rotate, 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 can be conveniently clamped between the first clamping block 408 and the second clamping block 402, the extending end of the cable is further fixed, and the extending end of the cable is located in the positioning tube 505, so that poor contact between the cable and the first electrode column 502 and the second electrode column 503 can be prevented, and the electrical detection result of the cable is influenced.
The slider 406 is T-shaped, which prevents 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 protrusions 504 are fixedly attached to the sidewalls of the first clamping block 408 and the second clamping block 402 during the process of clamping the cable.
Example 4
Referring to fig. 1, substantially the same as in example 3, further, a specific embodiment of detecting a heat failure of a cable is added.
The fault that generates heat is the common trouble of cable, and if the fault that generates heat appears in the air cable, then causes the incident easily, consequently, for the convenient fault that generates heat that detects the air cable, the surperficial fixedly connected with infrared ray detection machine 507 of support frame 1.
Carry out electrical property earlier and detect, at electrical property detection's in-process, carry out the fault detection that generates heat to the aviation cable, then, make the extension end of cable and circuit box 501 separation, finally, the amount of deflection that bends to the aviation cable detects, and this device can carry out electrical property detection simultaneously, generate heat and detect, the degree of deflection detects, has improved detection efficiency, avoids using multiple detection device to detect the cable, has reduced the detection cost, simultaneously, has improved detection efficiency.
The above description is only for the preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art should be considered to be within the technical scope of the present invention, and the technical solutions and the inventive concepts of the present invention are equivalent to or changed within the technical scope of the present invention.
Claims (10)
1. The utility model provides a quick detection device for aviation cable detects, includes support frame (1), its characterized in that still includes:
the wire tightening wheel (101) is rotatably connected to the surface of the support frame (1);
the supporting column (102) is fixedly connected to the surface of the supporting frame (1), the outer wall of the supporting column (102) is fixedly connected with a fixing plate (103), and a first sliding groove (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 mode, an arc-shaped plate (105) is fixedly connected to the surface of the sliding strip (104), and the arc-shaped plate (105) is arranged in a circumferential array with a supporting column (102) as the center;
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).
2. A rapid detection device for aircraft cable detection according to claim 1, wherein the drive mechanism comprises:
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 a rotating disc (203), and a second sliding groove (204) is formed in the surface of the rotating disc (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 fixing plate (103), and the sliding column (205) is connected in the third sliding groove (206) and the second sliding groove (204) in a sliding mode;
rotate to be connected first bull stick (2) on support frame (1) surface, the outer wall fixedly connected with handle (201) of first bull stick (2), the transmission is connected with first chain (207) between first bull stick (2) and commentaries on classics pipe (202).
3. The rapid detection device for aviation cable detection according to claim 2, wherein the support column (102) is coaxial with the rotating pipe (202), and the inner diameter of the rotating pipe (202) is larger than the outer diameter of the support column (102).
4. The rapid detection device for the aviation cable detection according to claim 1, wherein the outer wall of the arc-shaped plate (105) is symmetrically and fixedly connected with a first limiting plate (208).
5. The rapid detection device for aviation cable detection as recited in claim 1, further comprising:
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 rotatably connected with the support frame (1);
the second rotary column (4) is rotatably connected to the surface of the support frame (1), clamping grooves (305) are formed in the surfaces of the first rotary column (301) and the second rotary column (4), nuts (306) are connected to the outer walls of the first rotary column (301) and the second rotary column (4) in a threaded mode, and a second chain (308) is connected between the first rotary column (301) and the second rotary column (4);
a second rotating rod (302) arranged on the surface of the first rotating column (301), a third rotating rod (401) 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 roll (303),
one end of each of the second rotating rod (302) and the third rotating rod (401) is fixedly connected with a positioning strip (304), the positioning strips (304) are matched with the clamping grooves (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 nuts (306).
6. The rapid detection device for aviation cable detection according to claim 5, wherein the outer wall of the winding roller (303) is symmetrically and fixedly connected with a second limiting plate (403).
7. The rapid detection device for aviation cable detection as recited in claim 6, further comprising:
the connecting plate (5) is fixedly connected to the surface of one of the wire winding rollers (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 tubes (505) are symmetrically and fixedly connected to the surface of the circuit box (501), the positioning tubes (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 located in the corresponding positioning tubes (505);
the clamping device comprises a through hole (404) formed in the surface of a second limiting plate (403), and a clamping mechanism is arranged on the surface of the second limiting plate (403).
8. A rapid detection device for aerial cable detection according to claim 7, wherein the clamping mechanism comprises:
a fourth sliding chute (405) formed in the surface of the second limiting plate (403), wherein a sliding block (406) is connected in the fourth sliding chute (405) in a sliding manner, 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 connected to the surface of the first clamping block (408) in a rotating mode, the threaded rod (407) is in threaded connection with the second clamping block (402), and a knob (506) is fixedly connected to one end of the threaded rod (407).
9. The rapid detection device for aviation cable detection according to claim 8, wherein the sliding block (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).
10. The rapid detection device for aviation cable detection according to claim 8, wherein an infrared detector (507) is fixedly connected to the surface of the support frame (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310220389.XA CN115931597B (en) | 2023-03-09 | 2023-03-09 | A quick detection device for aviation cable detects |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310220389.XA CN115931597B (en) | 2023-03-09 | 2023-03-09 | A quick detection device for aviation cable detects |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN115931597A true CN115931597A (en) | 2023-04-07 |
| CN115931597B CN115931597B (en) | 2023-06-09 |
Family
ID=85835768
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202310220389.XA Active CN115931597B (en) | 2023-03-09 | 2023-03-09 | A quick detection device for aviation cable detects |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN115931597B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
Citations (27)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5945594A (en) * | 1998-10-14 | 1999-08-31 | Meritor Light Vehicle Systems-France | Method and apparatus for the electrochemical inspection of galvanized cable and method and apparatus for predicting the corrosion life of galvanized cable undergoing mechanical fatigue |
| US20050241409A1 (en) * | 2004-04-30 | 2005-11-03 | Taylor Geoffrey L | Normal force gradient/shear force sensors and method of measuring internal biological tissue stress |
| CN106706410A (en) * | 2016-11-09 | 2017-05-24 | 中国电力科学研究院 | Aluminum alloy strip lock-armo cable flexibility test device and aluminum alloy strip lock-armo cable flexibility test method |
| JP2018147803A (en) * | 2017-03-08 | 2018-09-20 | 住友電気工業株式会社 | Production method of cable, inspection method of cable and cable appearance inspection device |
| CN209247655U (en) * | 2018-11-02 | 2019-08-13 | 深圳通源电线电缆有限公司 | A kind of cable detecting device |
| WO2020073581A1 (en) * | 2018-10-10 | 2020-04-16 | 中国矿业大学 | Device and method for testing bearing property of mining annular steel wire rope |
| CN210487464U (en) * | 2019-08-27 | 2020-05-08 | 重庆市永晟电线电缆有限公司 | Cable breakage-proof detection device |
| CN212432841U (en) * | 2020-04-20 | 2021-01-29 | 中国石油天然气集团有限公司 | Coiling performance detection testing machine for reinforced plastic composite continuous pipe |
| CN212621855U (en) * | 2020-10-10 | 2021-02-26 | 宁波依本立流体装备制造有限公司 | Cable service life detector |
| CN213302407U (en) * | 2020-08-27 | 2021-05-28 | 苏州联升电线电缆有限公司 | Cable performance detection equipment |
| CN214472437U (en) * | 2021-03-04 | 2021-10-22 | 江苏灵跃电子科技有限公司 | Detection device for aviation cable |
| CN214503120U (en) * | 2021-01-28 | 2021-10-26 | 南昌航空大学 | Detection device for aviation cable |
| CN214539289U (en) * | 2020-12-01 | 2021-10-29 | 开化晶芯电子有限公司 | Detection apparatus based on silicon chip finished product |
| CN214951170U (en) * | 2021-06-25 | 2021-11-30 | 两山工程技术(武汉)有限公司 | A spheroid scanner for water supply pipe structure detects |
| CN113753671A (en) * | 2021-09-17 | 2021-12-07 | 上海临玥科技有限公司 | Communication cable length detection device and detection method thereof |
| CN114002215A (en) * | 2021-10-19 | 2022-02-01 | 江苏依卡维电子科技有限公司 | Cable joint specification online real-time detection system based on cable joint production line |
| CN114083510A (en) * | 2021-12-03 | 2022-02-25 | 上海交通大学 | Variable angle, tunnel inspection robot of diameter |
| CN216512064U (en) * | 2021-12-27 | 2022-05-13 | 中钢集团郑州金属制品研究院股份有限公司 | Take-up reel capable of automatically adjusting take-up diameter |
| CN114486482A (en) * | 2020-11-12 | 2022-05-13 | 无锡市天成线缆有限公司 | Strength detection device and detection method for armored cable production |
| CN216594846U (en) * | 2021-12-24 | 2022-05-24 | 深圳市兴达通电线电缆有限公司 | Cable wire product detection mechanism |
| CN217542912U (en) * | 2022-04-27 | 2022-10-04 | 陕西维百思特航空科技有限公司 | Aviation cable detects uses quick check out test set |
| CN217577773U (en) * | 2022-04-11 | 2022-10-14 | 徐州市银铃新能源科技有限公司 | Automatic winding device for vehicle wire harness |
| CN115303881A (en) * | 2022-06-28 | 2022-11-08 | 杭州青云新材料股份有限公司 | Preparation system based on low-stress fine-denier spandex filaments and detection method thereof |
| CN115326562A (en) * | 2022-08-09 | 2022-11-11 | 国网河北省电力有限公司电力科学研究院 | Overhead insulated wire tensile test device |
| CN115406677A (en) * | 2022-08-16 | 2022-11-29 | 卢寅颖 | Automobile shock absorber performance detection device and detection method |
| CN115528605A (en) * | 2022-10-11 | 2022-12-27 | 王欢 | Electric power construction line tightening system and line tightening method |
| CN115864098A (en) * | 2022-12-22 | 2023-03-28 | 陈亚杰 | High-altitude wiring device and method for power detection |
-
2023
- 2023-03-09 CN CN202310220389.XA patent/CN115931597B/en active Active
Patent Citations (27)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5945594A (en) * | 1998-10-14 | 1999-08-31 | Meritor Light Vehicle Systems-France | Method and apparatus for the electrochemical inspection of galvanized cable and method and apparatus for predicting the corrosion life of galvanized cable undergoing mechanical fatigue |
| US20050241409A1 (en) * | 2004-04-30 | 2005-11-03 | Taylor Geoffrey L | Normal force gradient/shear force sensors and method of measuring internal biological tissue stress |
| CN106706410A (en) * | 2016-11-09 | 2017-05-24 | 中国电力科学研究院 | Aluminum alloy strip lock-armo cable flexibility test device and aluminum alloy strip lock-armo cable flexibility test method |
| JP2018147803A (en) * | 2017-03-08 | 2018-09-20 | 住友電気工業株式会社 | Production method of cable, inspection method of cable and cable appearance inspection device |
| WO2020073581A1 (en) * | 2018-10-10 | 2020-04-16 | 中国矿业大学 | Device and method for testing bearing property of mining annular steel wire rope |
| CN209247655U (en) * | 2018-11-02 | 2019-08-13 | 深圳通源电线电缆有限公司 | A kind of cable detecting device |
| CN210487464U (en) * | 2019-08-27 | 2020-05-08 | 重庆市永晟电线电缆有限公司 | Cable breakage-proof detection device |
| CN212432841U (en) * | 2020-04-20 | 2021-01-29 | 中国石油天然气集团有限公司 | Coiling performance detection testing machine for reinforced plastic composite continuous pipe |
| CN213302407U (en) * | 2020-08-27 | 2021-05-28 | 苏州联升电线电缆有限公司 | Cable performance detection equipment |
| CN212621855U (en) * | 2020-10-10 | 2021-02-26 | 宁波依本立流体装备制造有限公司 | Cable service life detector |
| CN114486482A (en) * | 2020-11-12 | 2022-05-13 | 无锡市天成线缆有限公司 | Strength detection device and detection method for armored cable production |
| CN214539289U (en) * | 2020-12-01 | 2021-10-29 | 开化晶芯电子有限公司 | Detection apparatus based on silicon chip finished product |
| CN214503120U (en) * | 2021-01-28 | 2021-10-26 | 南昌航空大学 | Detection device for aviation cable |
| CN214472437U (en) * | 2021-03-04 | 2021-10-22 | 江苏灵跃电子科技有限公司 | Detection device for aviation cable |
| CN214951170U (en) * | 2021-06-25 | 2021-11-30 | 两山工程技术(武汉)有限公司 | A spheroid scanner for water supply pipe structure detects |
| CN113753671A (en) * | 2021-09-17 | 2021-12-07 | 上海临玥科技有限公司 | Communication cable length detection device and detection method thereof |
| CN114002215A (en) * | 2021-10-19 | 2022-02-01 | 江苏依卡维电子科技有限公司 | Cable joint specification online real-time detection system based on cable joint production line |
| CN114083510A (en) * | 2021-12-03 | 2022-02-25 | 上海交通大学 | Variable angle, tunnel inspection robot of diameter |
| CN216594846U (en) * | 2021-12-24 | 2022-05-24 | 深圳市兴达通电线电缆有限公司 | Cable wire product detection mechanism |
| CN216512064U (en) * | 2021-12-27 | 2022-05-13 | 中钢集团郑州金属制品研究院股份有限公司 | Take-up reel capable of automatically adjusting take-up diameter |
| CN217577773U (en) * | 2022-04-11 | 2022-10-14 | 徐州市银铃新能源科技有限公司 | Automatic winding device for vehicle wire harness |
| CN217542912U (en) * | 2022-04-27 | 2022-10-04 | 陕西维百思特航空科技有限公司 | Aviation cable detects uses quick check out test set |
| CN115303881A (en) * | 2022-06-28 | 2022-11-08 | 杭州青云新材料股份有限公司 | Preparation system based on low-stress fine-denier spandex filaments and detection method thereof |
| CN115326562A (en) * | 2022-08-09 | 2022-11-11 | 国网河北省电力有限公司电力科学研究院 | Overhead insulated wire tensile test device |
| CN115406677A (en) * | 2022-08-16 | 2022-11-29 | 卢寅颖 | Automobile shock absorber performance detection device and detection method |
| CN115528605A (en) * | 2022-10-11 | 2022-12-27 | 王欢 | Electric power construction line tightening system and line tightening method |
| CN115864098A (en) * | 2022-12-22 | 2023-03-28 | 陈亚杰 | High-altitude wiring device and method for power detection |
Non-Patent Citations (3)
| Title |
|---|
| HEINRICH B 等: "Current rating of multi-core cable", 《IEEE TRANSAC-TIONS ON INDUSTRY APPLICATIONS》 * |
| 王作天;吕思璐;田开顺;: "航空整机电缆检测系统集成设计", 计算机测量与控制 * |
| 罗云林;吴林;: "航空多芯电缆检测系统设计", 控制工程 * |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
Also Published As
| Publication number | Publication date |
|---|---|
| CN115931597B (en) | 2023-06-09 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN114558815B (en) | Robot and control method thereof | |
| CN115931597A (en) | A quick detection device for aviation cable detects | |
| CN111442972A (en) | Stretch-proofing performance detection device for cable processing | |
| CN218903097U (en) | Wire drawing device for producing cables | |
| CN206269951U (en) | The tension force measuring device of wire in transformer coil | |
| CN107449791A (en) | A kind of the cannot-harm-detection device and its method of carbon fibre composite wire plug | |
| CN210051786U (en) | Lightning arrester live-line detection test device | |
| CN112834372A (en) | Terminal detection machine | |
| CN218470415U (en) | Be applied to verifying attachment of electronic product constant voltage | |
| CN214418571U (en) | Positioning fixture for cable tension detection | |
| CN115825157A (en) | Device convenient for detecting air holes of enameled wires of transformer | |
| CN214749514U (en) | Terminal detection machine | |
| CN220787658U (en) | Winding device with winding roller easy to replace | |
| CN116337885A (en) | Transformer comprehensive detection device based on visual detection | |
| CN209052226U (en) | Drawing cable clamping device and drawing cable equipment | |
| CN114200270A (en) | Cable welding inspection device | |
| CN118226182B (en) | Fault matching detection device for power distribution network | |
| CN221351018U (en) | Superfine special enameled wire anti-breaking detection device | |
| CN221929872U (en) | Multifunctional optical fiber fault test equipment | |
| CN220961809U (en) | Cable insulation detection device | |
| CN220960951U (en) | Cable tension detection device | |
| CN220872505U (en) | High-voltage cable detection device | |
| CN211945700U (en) | High-precision electric wire intercepting device for electric power | |
| CN220399119U (en) | Dual-phase steel channel performance test equipment | |
| CN215894789U (en) | Electric reactor electrical performance testing device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |