CN207559466U - A kind of aircraft self routing cable clamp - Google Patents

A kind of aircraft self routing cable clamp Download PDF

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Publication number
CN207559466U
CN207559466U CN201721854975.6U CN201721854975U CN207559466U CN 207559466 U CN207559466 U CN 207559466U CN 201721854975 U CN201721854975 U CN 201721854975U CN 207559466 U CN207559466 U CN 207559466U
Authority
CN
China
Prior art keywords
shaped folder
folder plate
pressed pole
cable
guide rod
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.)
Expired - Fee Related
Application number
CN201721854975.6U
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Chinese (zh)
Inventor
田密
曾伟
曾伟一
贺银平
罗辉
孙强
王攀
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Chengdu Aeronautic Polytechnic
Original Assignee
Chengdu Aeronautic Polytechnic
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Chengdu Aeronautic Polytechnic filed Critical Chengdu Aeronautic Polytechnic
Priority to CN201721854975.6U priority Critical patent/CN207559466U/en
Application granted granted Critical
Publication of CN207559466U publication Critical patent/CN207559466U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model is related to a kind of aircraft self routing cable clamps, including motion control device, U-shaped folder plate blanking device, cable wire-clamping device and pedestal, motion control device is connected respectively with U-shaped folder plate blanking device and cable wire-clamping device, pedestal is equipped with cable wire-clamping device and supporting block, cable wire-clamping device is equipped with the top setting U-shaped folder plate blanking device of support plate, supporting block and support plate.The utility model can automatic clamping cable, can largely save the time, polylith U-shaped folder plate can clamp one group of inhomogeneity, the different cable of diameter.

Description

A kind of aircraft self routing cable clamp
Technical field
The utility model is related to aircraft self routing fields, and in particular to a kind of aircraft self routing cable clamp.
Background technology
Cable has special and consequence aboard, and dosage is big, wide in variety, working environment is complex, with The raising of aeroplane performance requirement, the dosage of cable also incrementally increase.In the environment of current intelligence manufacture, and current aircraft life In production. art, a large amount of cable layings still rely on manual routing.But traditional manual routing's mode not only takes more, work Efficiency is low, it is impossible to realize that conducting wire is quickly laid, and manually participate in wiring, easily malfunction when cable run is more.
But self routing is presently, there are many difficult points, such as the classification of similar conducting wire is tied up, the clamp of inhomogeneity conducting wire bundle How bundle, conducting wire both ends accurately correspond to, and how number of cable etc. is accurately laid when cable is more.Present wiring unit focuses mostly on Solve the problems, such as that conducting wire both ends accurately correspond to, but the classification of similar conducting wire is tied up, the clamp of inhomogeneity conducting wire is tied up, wiring efficiency And wiring number is also to be solved the problems such as accurately controlling.
Utility model content
The technical problem to be solved by the utility model is to provide a kind of aircraft self routing cable clamps, solve winged The problem of cable clamp takes in machine self routing.
The technical solution that the utility model solves above-mentioned technical problem is as follows:A kind of aircraft self routing cable clamp, It is characterised in that it includes motion control device, U-shaped folder plate blanking device, cable wire-clamping device and pedestal, the motion control dress It puts and is connected respectively with U-shaped folder plate blanking device and cable wire-clamping device, the pedestal is equipped with cable wire-clamping device and supporting block, The cable wire-clamping device is equipped with the top setting U-shaped folder plate blanking device of support plate, the supporting block and support plate.
Based on the above technical solution, the utility model can also do following improvement.
Further, the motion control device includes free gear, lateral down-pressed pole and longitudinal down-pressed pole, the work Moving gear is connected by rack with the longitudinal down-pressed pole being vertically arranged, and the longitudinal direction down-pressed pole is equipped with lateral down-pressed pole, described Lower platen is equipped at the separate longitudinal down-pressed pole in lateral down-pressed pole bottom.
Further, the U-shaped folder plate blanking device includes upper shell, is equipped with and is located at below lower platen in the upper shell U-shaped folder plate rest area, the U-shaped folder plate rest area bottom, which is equipped with, can make the narrow slit that U-shaped folder plate passes through, and the U-shaped folder plate is placed Area is connected by the first guide rod with the inner wall of upper shell, and first guide rod is equipped with the first spring.
Further, the cable wire-clamping device includes lower housing, is equipped with the second guide rod in the lower housing, and described second Guide rod is connected with longitudinal down-pressed pole, is equipped with baffle, second spring, push plate, lock-switch, wedge shape on second guide rod successively Lock, cable mounting table, third spring and fixed baffle.
Further, the narrow slit of the U-shaped folder plate rest area bottom is located between push plate and wedge shape lock.
Further, fixed gear is equipped between supporting block longitudinal direction down-pressed pole and the second guide rod.
The beneficial effects of the utility model are:In the utility model, free gear rotation drives longitudinal down-pressed pole downward Movement, lateral down-pressed pole linkage, lower platen press to the U-shaped folder plate placed in upper shell between push plate and wedge shape lock, Longitudinal down-pressed pole, which moves downward, pushes the second guide rod to move right, and second spring pushes the right side of U-shaped folder plate value wedge shape lock And lock, two blocks of U-shaped folder plates can clamp single line cable, the utility model can automatic clamping cable, can largely save the time, polylith U-shaped folder plate can clamp one group of inhomogeneity, the different cable of diameter.
Description of the drawings
Fig. 1 is the utility model structure chart.
In attached drawing, parts list represented by the reference numerals are as follows:
1st, longitudinal down-pressed pole, 2, lateral down-pressed pole, the 3, first guide rod, 4, baffle, the 5, first spring, 6, U-shaped folder plate puts Put area, 7, wedge shape lock, 8, third spring, 9, fixed baffle, the 10, second guide rod, 11, pedestal, 12, lock-switch, 13, push away Plate, 14, support plate, 15, second spring, 16, fixed gear, 17, supporting block, 18, rack, 19, free gear, 20, cable puts Put platform, 21, lower platen, 22, upper shell, 23, lower housing.
Specific embodiment
The principle and feature of the utility model are described below in conjunction with attached drawing, example is served only for explaining this practicality It is novel, it is not intended to limit the scope of the utility model.
As shown in Figure 1, a kind of aircraft self routing cable clamp, fills including motion control device, the blanking of U-shaped folder plate Put, cable wire-clamping device and pedestal 11, motion control device are connected respectively with U-shaped folder plate blanking device and cable wire-clamping device, Pedestal 11 is equipped with cable wire-clamping device and supporting block 17, and cable wire-clamping device is equipped with support plate 14, supporting block 17 and support The top setting U-shaped folder plate blanking device of plate 14.
In the utility model embodiment, motion control device includes free gear 19, lateral down-pressed pole 2 and longitudinal direction and pushes Bar 1, free gear 19 are connected by rack 18 with the longitudinal down-pressed pole 1 being vertically arranged, and longitudinal down-pressed pole 1, which is equipped with, laterally to be pushed Bar 2, lateral 2 bottom of down-pressed pole are equipped with lower platen 21 far from longitudinal 1 side of down-pressed pole.
In the utility model embodiment, U-shaped folder plate blanking device includes upper shell 22, and position is equipped in the upper shell 22 In the U-shaped folder plate rest area 6 of 21 lower section of lower platen, 6 bottom of U-shaped folder plate rest area, which is equipped with, can make the narrow slit that U-shaped folder plate passes through, U Type clamping plate rest area 6 is connected by the first guide rod 3 with the inner wall of upper shell 22, and the first guide rod 3 is equipped with the first spring 5.
In the utility model embodiment, cable wire-clamping device includes lower housing 23, and being equipped with second in lower housing 23 is oriented to Bar 10, the second guide rod 10 are connected with longitudinal down-pressed pole 1, are equipped with baffle 4 on the second guide rod 10 successively, second spring 15, push away Plate 13, lock-switch 12, wedge shape lock 7, cable mounting table 20, third spring 8 and fixed baffle 9.
In the utility model embodiment, the narrow slit of 6 bottom of U-shaped folder plate rest area be located at push plate 13 and wedge shape lock 7 it Between.
Fixed gear 16 is equipped in the utility model embodiment, between longitudinal 1 and second guide rod 10 of down-pressed pole.
The specific work process of the utility model is:Free gear 19 drives longitudinal down-pressed pole 1 to transport downwards by rack 18 Dynamic, the pushing of longitudinal down-pressed pole 1 can drive the pushing of lateral down-pressed pole 2 and lower platen 21, and fixed gear 16 pushes second to be oriented to Bar 10 moves right, and lateral down-pressed pole 2 makes lower platen 21 push the U-shaped folder plate in upper shell 22, is fallen to down by narrow slit Between push plate 13 and wedge shape lock 7 in housing 23, meanwhile, the motive force of fixed gear 16 is acted in push plate 13, push plate 13 U-shaped folder plate is pushed to the right, because shackle designs are lozenges, U-shaped folder plate easily passes through wedge shape lock 7 to the right side of wedge shape lock 7 Side, U-shaped folder plate clamp cable on cable mounting table 20, and the third spring 8 on 7 right side of wedge shape lock is in impaction state, therefore U Type clamping plate can be also clamped in this position.Free gear 19 is moved to negative direction, as longitudinal down-pressed pole 1 lifts, wedge-lock State before button 7 is restored to, and U-shaped folder plate is prevented to left movement.Continue to repeat above movement, be wanted until clamp number reaches It asks, completes all clamp work, open lock-switch 12 when clamp finishes and take out cable.
The above is only the preferred embodiment of the present invention, is not intended to limit the utility model, all in this practicality Within novel spirit and principle, any modification, equivalent replacement, improvement and so on should be included in the guarantor of the utility model Within the scope of shield.

Claims (6)

1. a kind of aircraft self routing cable clamp, which is characterized in that including motion control device, U-shaped folder plate blanking device, Cable wire-clamping device and pedestal (11), the motion control device respectively with U-shaped folder plate blanking device and cable wire-clamping device phase Even, the pedestal (11) is equipped with cable wire-clamping device and supporting block (17), and the cable wire-clamping device is equipped with support plate (14), the top of the supporting block (17) and support plate (14) setting U-shaped folder plate blanking device.
2. aircraft self routing cable clamp according to claim 1, which is characterized in that the motion control device packet Free gear (19), lateral down-pressed pole (2) and longitudinal down-pressed pole (1) are included, the free gear (19) is by rack (18) with erecting The longitudinal down-pressed pole (1) directly set is connected, and the longitudinal direction down-pressed pole (1) is equipped with lateral down-pressed pole (2), the transverse direction down-pressed pole (2) bottom is equipped with lower platen (21) far from longitudinal down-pressed pole (1) side.
3. aircraft self routing cable clamp according to claim 2, which is characterized in that the U-shaped folder plate blanking dress It puts including upper shell (22), the upper shell (22) is interior to be equipped with the U-shaped folder plate rest area (6) being located at below lower platen (21), institute It states U-shaped folder plate rest area (6) bottom and is equipped with the narrow slit that can pass through U-shaped folder plate, the U-shaped folder plate rest area (6) passes through first Guide rod (3) is connected with the inner wall of upper shell (22), and first guide rod (3) is equipped with the first spring (5).
4. aircraft self routing cable clamp according to claim 3, which is characterized in that the cable wire-clamping device packet Lower housing (23) is included, the second guide rod (10) is equipped in the lower housing (23), second guide rod (10) pushes with longitudinal direction Bar (1) is connected, and is equipped with baffle (4), second spring (15), push plate (13), lock-switch on second guide rod (10) successively (12), wedge shape lock (7), cable mounting table (20), third spring (8) and fixed baffle (9).
5. aircraft self routing cable clamp according to claim 4, which is characterized in that the U-shaped folder plate rest area (6) narrow slit of bottom is located between push plate (13) and wedge shape lock (7).
6. aircraft self routing cable clamp according to claim 4, which is characterized in that the longitudinal direction down-pressed pole (1) Fixed gear (16) is equipped between the second guide rod (10).
CN201721854975.6U 2017-12-26 2017-12-26 A kind of aircraft self routing cable clamp Expired - Fee Related CN207559466U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201721854975.6U CN207559466U (en) 2017-12-26 2017-12-26 A kind of aircraft self routing cable clamp

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201721854975.6U CN207559466U (en) 2017-12-26 2017-12-26 A kind of aircraft self routing cable clamp

Publications (1)

Publication Number Publication Date
CN207559466U true CN207559466U (en) 2018-06-29

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201721854975.6U Expired - Fee Related CN207559466U (en) 2017-12-26 2017-12-26 A kind of aircraft self routing cable clamp

Country Status (1)

Country Link
CN (1) CN207559466U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110054035A (en) * 2019-03-01 2019-07-26 泉州市在梦里信息科技有限公司 A kind of electric power overhaul take-up using the two-way neat de-sludging of typesetting beam
CN110729679A (en) * 2019-10-23 2020-01-24 哈尔滨学院 Electric is combined material cable intelligent stand for tubular well

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110054035A (en) * 2019-03-01 2019-07-26 泉州市在梦里信息科技有限公司 A kind of electric power overhaul take-up using the two-way neat de-sludging of typesetting beam
CN110054035B (en) * 2019-03-01 2020-09-29 广东电网有限责任公司肇庆供电局 Adopt two-way composing to restraint even descaling's electric power to overhaul and use take-up
CN110729679A (en) * 2019-10-23 2020-01-24 哈尔滨学院 Electric is combined material cable intelligent stand for tubular well
CN110729679B (en) * 2019-10-23 2020-06-19 哈尔滨学院 Electric is combined material cable intelligent stand for tubular well

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Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20180629

Termination date: 20191226

CF01 Termination of patent right due to non-payment of annual fee