CN109817390B - General aircraft wing pencil wiring arrangement - Google Patents
General aircraft wing pencil wiring arrangement Download PDFInfo
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- CN109817390B CN109817390B CN201910241866.4A CN201910241866A CN109817390B CN 109817390 B CN109817390 B CN 109817390B CN 201910241866 A CN201910241866 A CN 201910241866A CN 109817390 B CN109817390 B CN 109817390B
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Abstract
The invention discloses a universal aircraft wing wire harness wiring device which comprises a rack, a wiring board arranged on the rack, a plurality of wire clamps arranged on the wiring board and used for clamping wires, a graduated scale and a plurality of marking pieces arranged on the wiring board and used for determining the end position of the wires, wherein the marking pieces are respectively aligned with one graduated position on the graduated scale. According to the wing wire harness wiring device of the general airplane, the mark piece is arranged on the wiring board and matched with the graduated scale, so that the length of each wire can be accurately and quickly determined, and the manufacturing efficiency of the wing wire harness can be improved.
Description
Technical Field
The invention belongs to the technical field of general aviation auxiliary equipment, and particularly relates to a general airplane wing wire harness wiring device.
Background
In the field of current general aviation avionics manufacturing, the manufacturing of aircraft wire harnesses mainly comprises wing wire harnesses, fuselage wire harnesses, audio wire harnesses, avionics wire harnesses, instrument board wire harnesses and the like, and compared with other wire harnesses, the wing wire harnesses are longer, the longest length is 5.1 meters, and the lengths are different. In the production and manufacturing process of the wing wire harness, the situations of mistaken shearing, short shearing and the like of the wire are easily caused, so that the resource waste is caused, the material cost is increased, the working hours are delayed, and the production efficiency is reduced. Therefore, cutting with a tape measure is not the best method.
Meanwhile, after each wire is cut as required, the length of the wire is classified, length identification is made, then different male pins or female pins are pressed and connected, and then different connectors are inserted. The operation process is characterized in that the identification work of the conducting wire is repeated when each set of wing wire harness is manufactured, and the operation mode is low in production efficiency.
On the other hand, when the wing wire harness is manufactured, the wire harness is very easy to twist due to the fact that the wire harness is long and large in number, product quality is affected, and manufacturing difficulty is increased.
Therefore, in summary, in the manufacturing process of the general aviation wire harness, the traditional manufacturing process has the defects of low production efficiency, poor quality stability, high manufacturing difficulty and the like.
Disclosure of Invention
The present invention is directed to solving at least one of the problems of the prior art. Therefore, the invention provides a universal aircraft wing wire harness wiring device, and aims to improve the manufacturing efficiency of a wing wire harness.
In order to achieve the purpose, the invention adopts the technical scheme that: general aircraft wing pencil wiring arrangement, including the frame, set up the wiring board in the frame, set up on the wiring board and be used for the fastener of centre gripping wire, scale and set up on the wiring board and be used for confirming the mark piece of wire tip position, the fastener sets up a plurality ofly, and the mark piece sets up a plurality ofly, and each mark piece aligns with a scale position on the scale respectively.
The wiring board is obliquely arranged on the frame.
All wire clamps on the wiring board are arranged in matrix M rows and N columns.
All the mark pieces are sequentially arranged on the wiring board along the length direction of the wiring board, and the length direction of the wiring board is the horizontal direction.
The graduated scale is arranged on the wiring board, the graduated scale is positioned at the bottom of the wiring board, the length direction of the graduated scale is parallel to the length direction of the wiring board, and the mark piece extends towards the upper part of the graduated scale.
The mark piece is connected with the wiring board in a detachable mode.
The mark piece is connected with the wiring board in an adhesive mode.
The mark piece is the sticky tape and is colored sticky tape.
The wiring board sets up two and two wiring boards and is arranged in the V-arrangement, and the frame is located between two wiring boards.
The wiring board is made of an insulating material.
According to the wing wire harness wiring device of the general airplane, the mark piece is arranged on the wiring board and matched with the graduated scale, so that the length of each wire can be accurately and quickly determined, and the manufacturing efficiency of the wing wire harness can be improved.
Drawings
The description includes the following figures, the contents shown are respectively:
FIG. 1 is a schematic structural diagram of a universal aircraft wing harness routing device in accordance with the present invention;
FIG. 2 is a schematic view of the structure of the wire clamp;
FIG. 3 is a cross-sectional view of the castor;
FIG. 4 is a schematic structural view of a stent;
labeled as: 1. a graduated scale; 2. a wiring board; 3. a marker; 4. a universal caster; 401. a roller body; 402. a support leg; 403. mounting a plate; 404. a limiting plate; 405. an upper bearing; 406. a lower bearing; 407. fastening screws; 408. a nut; 5. a frame; 6. a directional wheel; 7. and (4) wire clamping.
Detailed Description
The following detailed description of the embodiments of the present invention will be given with reference to the accompanying drawings for a purpose of helping those skilled in the art to more fully, accurately and deeply understand the concept and technical solution of the present invention and to facilitate its implementation.
As shown in figure 1, the invention provides a universal aircraft wing wire harness wiring device which comprises a frame 5, a wiring board 2 arranged on the frame 5, a wire clamp 7 arranged on the wiring board 2 and used for clamping a wire, a graduated scale 1 and a marking piece 3 arranged on the wiring board 2 and used for determining the end position of the wire, wherein the wire clamp 7 is arranged in a plurality, the marking piece 3 is arranged in a plurality, and each marking piece 3 is respectively aligned with one graduated position on the graduated scale 1.
Specifically, as shown in fig. 1, the frame 5 has a frame structure, the frame 5 has a certain length, a certain width and a certain height, the width direction of the frame 5 is parallel to a first direction, the length direction of the frame 5 is parallel to a second direction, both the first direction and the second direction are horizontal, and the first direction and the second direction are perpendicular. The wiring board 2 is a rectangular flat plate, the wiring board 2 has a certain length and width, and the length direction of the wiring board 2 is parallel to the second direction. All the wire clamps 7 on the wiring board 2 are arranged in a matrix M-row and N-column manner, all the wire clamps 7 in the same row are sequentially arranged along the length direction of the wiring board 2, all the wire clamps 7 in the same column are sequentially arranged along the width direction of the wiring board 2, and all the wire clamps 7 are positioned on the same side of the wiring board 2. When the wiring operation is performed, the wires are laid in a preset path, the wires sequentially pass through the wire clamps 7 positioned on the preset path, and the wire clamps 7 clamp the wires so that the wires can be fixed.
As shown in fig. 1, preferably, the wiring board 2 is disposed obliquely on the rack 5, so as to facilitate the operation of a wiring person, an included angle is formed between the width direction of the wiring board 2 and the first direction, the included angle is an acute angle, an included angle is formed between the width direction of the wiring board 2 and the vertical direction, the included angle is also an acute angle, and the scale 1, the marking member 3 and the wire clamp 7 are all located on the same side of the wiring board 2.
Because aircraft wing pencil comprises a plurality of wires, plug connector and a total joint, the wire has a first end and a second end, first end and second end be the relative both ends on the wire length direction, the first end and the same total joint of all wires are connected, the second end of each wire is connected with a plug connector respectively, operating personnel is when carrying out the wiring operation, place the first end of all wires in same position department, be connected with same total joint, then lay each wire according to the route that predetermines respectively. The lengths of all the wires are different in size, therefore, the plurality of mark pieces 3 are arranged on the wiring board 2, and each mark piece 3 is used for determining the position of the second end of at least one wire respectively, so that an operator can quickly and accurately determine the length of the wire according to the position of the mark piece 3 during wiring operation and cut off the redundant part of the wire, the situations that the wire is mistakenly cut and cut short in the manufacturing process of the wing wire harness and the like can be reduced, errors in work are reduced, the wire does not need to be marked in length in advance, and the manufacturing efficiency of the wing wire harness is improved. As shown in fig. 1, all the markers 3 are arranged on the wiring board 2 in order along the longitudinal direction of the wiring board 2, the longitudinal direction of the wiring board 2 being the horizontal direction. The marker 3 has a length, the length direction of the marker 3 is parallel to the width direction of the wiring board 2, the marker 3 extends in the width direction of the wiring board 2 and the marker 3 extends to the upper end of the wiring board 2, so that the marking range of the marker 3 is wide. The scale 1 is provided on the wiring board 2, the scale 1 is located at the bottom of the wiring board 2 and the length direction of the scale 1 is parallel to the length direction of the wiring board 2, the mark members 3 extend toward the upper side of the scale 1, and the scale 1 is located below all the mark members 3. The scale 1 is fixedly connected with the wiring board 2, the scale 1 is arranged at the lower end of the wiring board 2, the length of the scale 1 is the same as that of the wiring board 2, and two ends of the scale 1 in the length direction are aligned with two ends of the wiring board 2 in the length direction. Scale mark is made for using length unit as the standard among the prior art to scale 1, measure the ruler of object length, scale mark and the scale that corresponds are carved with on the scale 1, the scale mark distributes along scale 1's length direction, the lower extreme of each mark piece 3 aligns with a scale position on the scale 1 respectively, the scale size that each scale position corresponds is different, just so make the end position that the scale position on the scale 1 can correspond the wire, make the wiring personnel can the accurate length of confirming the wire, it is directly perceived, efficiency and accuracy are high.
The mark piece 3 is detachably connected with the wiring board 2, so that the mark piece 3 is convenient to detach and the position of the mark piece 3 is convenient to replace. When the wing wire harnesses with different lengths need to be manufactured or the marker 3 is damaged, the marker 3 can be detached from the wiring board 2, and then the position of the marker 3 can be changed or a new marker 3 can be changed. Preferably, the marker 3 and the wiring board 2 are connected in an adhesive manner, so that the operation is convenient and simple, and the efficiency is high. The thickness of the marking member 3 is small so as not to affect the laying of the wires, and the marking member 3 is preferably an adhesive tape so that the marking member 3 is directly stuck on the surface of the wiring board 2 facing the wiring person when the marking member 3 is mounted. The marking member 3 is also a colored tape, the color of the marking member 3 is different from the color of the wiring board 2, and the color of the marking member 3 may be blue, yellow, red, or the like.
Preferably, the wiring board 2 is made of an insulating material, such as a rubber-based insulating material or a plastic-based material.
As shown in fig. 1, in the present embodiment, two wiring boards 2 are provided and two wiring boards 2 are arranged in a V-shape, and a chassis 5 is located between the two wiring boards 2. The two wiring boards 2 are symmetrically arranged, the vertical distance between the lower ends of the two wiring boards 2 is larger than the vertical distance between the upper ends of the two wiring boards 2, the two wiring boards 2 are respectively provided with the wire clamp 7, the graduated scale 1 and the mark pieces 3, and the number and/or the positions of the mark pieces 3 on the two wiring boards 2 can be set to be different so as to be suitable for manufacturing wing wire harnesses with different lengths and structures.
As shown in fig. 1 and 2, the wire clamp 7 is substantially U-shaped, the wire clamp 7 has a clamping groove for a wire to be inserted therein, the wire clamp 7 has a certain length, one end of the wire clamp 7 in the length direction has an opening for the wire to pass therethrough, the opening communicates with the clamping groove, the other end of the wire clamp 7 in the length direction is fixedly connected to the wiring board 2, the width of the opening in the wire clamp 7 is smaller than the width of the clamping groove, the width of the opening in the wire clamp 7 is smaller than the diameter of the wire, and the wire can be inserted into the clamping groove through the opening in the wire clamp 7 or can be extracted from the clamping groove. The wire clamp 7 has certain elastic performance, the wire clamp 7 can generate certain elastic deformation, and when a lead passes through the opening of the wire clamp 7, the width of the opening of the wire clamp 7 can be slightly increased, so that the lead can pass through; after the wire passes through the opening, the wire clamp 7 is restored to a state of minimum width under the action of self elasticity.
As shown in fig. 1, the universal aircraft wing harness routing device of the invention further comprises a directional wheel 6 and a universal caster 4 which are arranged on the frame 5, wherein at least two directional wheels 6 and at least two universal casters 4 are respectively arranged. Directional wheel 6 and universal caster 4 set up in the bottom of frame 5, and directional wheel 6 and universal caster 4 install on frame 5, provide the supporting role to frame 5. The directional wheel 6 is a roller device which can roll only in a specific direction, namely, can only move forwards and backwards, and cannot turn. The construction of the orienting wheel 6 is as known to the person skilled in the art and will not be described in further detail here. All the directive wheels 6 are on the same straight line parallel to the first direction, and all the caster wheels 4 are also on the same straight line parallel to the first direction.
As shown in fig. 3 and 4, the caster 4 includes a bracket and a roller body 401 rotatably connected to the bracket, the roller body 401 is a cylinder, the roller body 401 is rotatably connected to the bracket through a rotating shaft, an axis of the rotating shaft is located in a horizontal plane, a shaft hole for the rotating shaft to pass through is formed in a center of the roller body 401, the roller body 401 and the rotating shaft are coaxially disposed, an outer circumferential surface of the roller body 401 is used for contacting with the ground, and when the frame 5 moves, the roller body 401 rolls along the ground. The bottom fixed connection of support and frame 5 and the support passes through the bolt and installs the bottom in frame 5, the support includes the landing leg 402 of two relative settings, limiting plate 404 with two landing leg 402 fixed connection, be located the mounting panel 403 of limiting plate 404 top, fastening screw 407, nut 408, upper bearing 405 and lower bearing 406, mounting panel 403 is connected with frame 5 through the bolt, the upper end and the limiting plate 404 fixed connection of landing leg 402, the lower extreme of landing leg 402 is equipped with the through-hole that lets the pivot pass, gyro wheel body 401 is located between two landing legs 402, gyro wheel body 401 is installed on two landing legs 402 through the pivot, gyro wheel body 401 is and is located the below of limiting plate 404. The mounting plate 403 is screwed to the fastening screw 407, and the mounting plate 403 has a female screw hole at the center thereof through which the fastening screw 407 passes, and the female screw hole is a through hole provided in the mounting plate 403 so as to pass through in the plate thickness direction, and the axis of the female screw hole is located in a vertical plane. The center of the limiting plate 404 has a through hole for passing the fastening screw 407 therethrough, and the through hole is a circular hole and is coaxial with the internal threaded hole of the mounting plate 403. The upper bearing 405 is sandwiched between the mounting plate 403 and the stopper plate 404, and the upper bearing 405 is a thrust ball bearing to receive an axial load. The top of limiting plate 404 has the last holding chamber that holds upper bearing 405, goes up the holding chamber and is circular cavity and goes up the holding chamber and begin the inside extension formation of downward orientation limiting plate 404 from the top surface of limiting plate 404, and the diameter of going up the holding chamber is the same with the external diameter size of upper bearing 405, and upper bearing 405 is difficult to drop. Fastening screw 407 is hexagonal head screw, and fastening screw 407 is hexagonal head and screw portion including the hexagonal head that is connected, and hexagonal head is the hexagon structure, and screw portion is the shaft-like structure that the surface is equipped with the external screw thread, and the one end of screw portion is in the center department and hexagonal head fixed connection of hexagonal head, and screw portion inserts the internal thread hole on mounting panel 403 after passing the through-hole on the limiting plate 404 in, and screw portion and mounting panel 403 are threaded connection. The lower bearing 406 is sleeved on the screw portion of the fastening screw 407, the lower bearing 406 is sandwiched between the limiting plate 404 and the hexagonal head of the fastening screw 407, and the lower bearing 406 is a thrust ball bearing to bear an axial load. The bottom of limiting plate 404 has the lower holding chamber that holds lower bearing 406, lower holding chamber is circular cavity and lower holding chamber and begins upwards to extend towards the inside of limiting plate 404 from the bottom surface of limiting plate 404 and form, the external diameter of lower bearing 406 is less than the external diameter of upper bearing 405, the internal diameter of lower bearing 406 is less than the diameter of the circumscribed circle of the hexagonal head of fastening screw 407, the diameter in lower holding chamber is the same with the external diameter size of lower bearing 406, lower bearing 406 is difficult to drop, high reliability, make the bearing capacity of universal caster 4 stronger. The hexagonal head of the fastening screw 407 is located above the roller body 401, the outer diameter of the lower bearing 406 is larger than the diameter of a through hole formed in the limit plate 404 and allowing the screw to pass through, and a gap is formed between the mounting plate 403 and the limit plate 404, so that the limit plate 404 can rotate relative to the mounting plate 403, and the steering of the roller body 401 is realized. The upper bearing 405, the lower bearing 406 and the fastening screw 407 are coaxially arranged, the fastening screw 407 being located at a middle position of the two legs 402. The top surface of the mounting plate 403 is provided with a groove for accommodating the nut 408, the groove is a circular groove, the nut 408 is sleeved on the screw portion of the fastening screw 407, the nut 408 is in threaded connection with the screw portion, and the nut 408 is in welded connection with the screw portion. After the fastening screw 407 and the nut 408 are screwed and fixed, the nut 408 and the fastening screw 407 are welded together, the nut 408 and the fastening screw 407 are relatively fixed, and the fastening screw 407 and the nut 408 clamp the limit plate 404, the upper bearing 405, the limit plate 404 and the lower bearing 406 to form an integral structure; and the mounting plate 403 is in threaded connection with the fastening screw 407, and the nut 408 is matched to form an effect similar to that of a double nut, meanwhile, the nut 408 and the fastening screw 407 are welded and fixed, the nut 408 can not rotate any more, the loosening of the screw and the nut 408 to cause the falling of related parts is prevented, a safe fixing effect is provided, and the universal caster 4 can provide stable movement and realize the steering of the equipment when the equipment moves.
As shown in fig. 1, in the present embodiment, two directional wheels 6 and two casters 4 are disposed, the two directional wheels 6 and the two casters 4 are distributed in a rectangular shape, and each directional wheel 6 and one caster 4 are located on the same straight line parallel to the second direction.
The invention is described above with reference to the accompanying drawings. It is to be understood that the specific implementations of the invention are not limited in this respect. Various insubstantial improvements are made by adopting the method conception and the technical scheme of the invention; the present invention is not limited to the above embodiments, and can be modified in various ways.
Claims (10)
1. General aircraft wing pencil wiring arrangement, its characterized in that: the wire clamp is arranged on the wiring board, the wire clamp is used for clamping a wire, the graduated scale is arranged on the wiring board, and the mark piece is arranged on the wiring board and used for determining the end position of the wire;
all the mark pieces are sequentially arranged on the wiring board along the length direction of the wiring board, and the length direction of the wiring board is the horizontal direction; the graduated scale is arranged on the wiring board, the graduated scale is positioned at the bottom of the wiring board, the length direction of the graduated scale is parallel to the length direction of the wiring board, the length direction of the marking piece is parallel to the width direction of the wiring board, the marking piece extends towards the upper part of the graduated scale, the marking piece and the wiring board are detachably connected, and the position of the marking piece can be changed;
all wire clamps on the wiring board are arranged in a matrix M-row N-column mode, the marking piece is connected with the wiring board in an adhesive mode, and the color of the marking piece is different from that of the wiring board;
the aircraft wing wiring harness comprises a plurality of wires, plug connectors and a main joint, wherein each wire is provided with a first end part and a second end part, the first end parts and the second end parts are opposite ends in the length direction of the wire, the first end parts of all the wires are connected with the same main joint, and the second end parts of all the wires are respectively connected with one plug connector;
when an operator performs wiring operation, the first end parts of all the wires are arranged at the same position and connected with the same main joint, then the wires are laid according to a preset path respectively, the wires sequentially pass through the wire clamps on the preset path, the wire clamps clamp the wires, each marking piece is used for determining the position of at least one second end part of one wire respectively, and the operator can determine the length of the wires according to the positions of the marking pieces and cut off the redundant parts of the wires during the wiring operation.
2. The universal aircraft wing harness routing device of claim 1, wherein: the wiring board is obliquely arranged on the frame.
3. The universal aircraft wing harness routing device of claim 1, wherein: the flag extends in the width direction of the wiring board and the flag extends to the upper end of the wiring board.
4. A universal aircraft wing harness routing device according to any one of claims 1 to 3, wherein: the mark piece is the sticky tape and is colored sticky tape.
5. The universal aircraft wing harness routing device of claim 4, wherein: the color of the marker is blue, yellow or red.
6. A universal aircraft wing harness routing device according to any one of claims 1 to 3, wherein: the fastener is U type structure, and the fastener has the draw-in groove that lets the wire embedding, and the fastener has certain length, and the one end on the length direction of fastener has the opening that lets the wire pass through, this opening and draw-in groove intercommunication, the other end and the wiring board fixed connection on the length direction of fastener, and the width of the open-ended on the fastener is less than the width of draw-in groove, and the width of the open-ended on the fastener is less than the diameter of wire.
7. A universal aircraft wing harness routing device according to any one of claims 1 to 3, wherein: the wiring boards are provided in two and two in a V-shaped arrangement, the chassis is located between the two wiring boards, and the number and/or positions of the markers on the two wiring boards are set to be different.
8. A universal aircraft wing harness routing device according to any one of claims 1 to 3, wherein: the wiring board is made of an insulating material.
9. The universal aircraft wing harness routing device of claim 8, wherein: the wiring board is made of rubber insulating materials or plastic materials.
10. A universal aircraft wing harness routing device according to any one of claims 1 to 3, wherein: the universal caster comprises a support and a roller body rotationally connected with the support, the support comprises two opposite support legs, a limiting plate fixedly connected with the two support legs, an installation plate positioned above the limiting plate, a fastening screw, a nut, an upper bearing and a lower bearing, the installation plate is connected with the rack through a bolt, and the roller body is positioned between the two support legs; the mounting plate and the fastening screw are in threaded connection, the upper bearing is clamped between the mounting plate and the limiting plate, the upper bearing is a thrust ball bearing, the fastening screw is a hexagonal head screw and comprises a hexagonal head portion and a screw portion which are connected, the lower bearing sleeve is arranged on the screw portion of the fastening screw, the lower bearing is clamped between the hexagonal head portion of the limiting plate and the hexagonal head portion of the fastening screw, the lower bearing is the thrust ball bearing, the hexagonal head portion of the fastening screw is located above the roller body, and the nut sleeve is arranged on the screw portion of the fastening screw and is in welded connection with the screw portion.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910241866.4A CN109817390B (en) | 2019-03-28 | 2019-03-28 | General aircraft wing pencil wiring arrangement |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910241866.4A CN109817390B (en) | 2019-03-28 | 2019-03-28 | General aircraft wing pencil wiring arrangement |
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| CN109817390A CN109817390A (en) | 2019-05-28 |
| CN109817390B true CN109817390B (en) | 2021-04-02 |
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| CN201910241866.4A Active CN109817390B (en) | 2019-03-28 | 2019-03-28 | General aircraft wing pencil wiring arrangement |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN113363861A (en) * | 2021-05-10 | 2021-09-07 | 中航西安飞机工业集团股份有限公司 | High-precision planar liquid crystal display wiring equipment and wiring method |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE202014002053U1 (en) * | 2014-03-11 | 2014-04-08 | Gt Elektrotechnische Produkte Gmbh | House connection socket |
| CN107134357A (en) * | 2017-06-26 | 2017-09-05 | 国网河南省电力公司濮阳供电公司 | A kind of bench type transformer lead wire platform for making |
| CN207977160U (en) * | 2018-03-23 | 2018-10-16 | 青岛川古电子有限公司 | Tie up glue harness assembly or fitting table |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102419145B (en) * | 2011-12-20 | 2013-06-05 | 山东电力集团公司滨州供电公司 | Hole pitch positioning device for copper row and wire clamp |
| CN205247988U (en) * | 2015-12-29 | 2016-05-18 | 天津长城精益汽车零部件有限公司 | Wiring arrangement is used in pencil processing |
| CN207353765U (en) * | 2017-09-20 | 2018-05-11 | 南京好世通电气有限公司 | A kind of automotive wire bundle connecton layout |
| CN208068091U (en) * | 2018-03-14 | 2018-11-09 | 中电科芜湖钻石飞机制造有限公司 | Aircraft harness crimping tool fixing device |
| CN208070048U (en) * | 2018-04-11 | 2018-11-09 | 中电科芜湖钻石飞机制造有限公司 | Aircraft harness wiring plate supporting device |
-
2019
- 2019-03-28 CN CN201910241866.4A patent/CN109817390B/en active Active
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE202014002053U1 (en) * | 2014-03-11 | 2014-04-08 | Gt Elektrotechnische Produkte Gmbh | House connection socket |
| CN107134357A (en) * | 2017-06-26 | 2017-09-05 | 国网河南省电力公司濮阳供电公司 | A kind of bench type transformer lead wire platform for making |
| CN207977160U (en) * | 2018-03-23 | 2018-10-16 | 青岛川古电子有限公司 | Tie up glue harness assembly or fitting table |
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