CN103884594A - Horizontal thin wire harness tension detector - Google Patents
Horizontal thin wire harness tension detector Download PDFInfo
- Publication number
- CN103884594A CN103884594A CN201410147290.2A CN201410147290A CN103884594A CN 103884594 A CN103884594 A CN 103884594A CN 201410147290 A CN201410147290 A CN 201410147290A CN 103884594 A CN103884594 A CN 103884594A
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- China
- Prior art keywords
- wire harness
- wire
- connection terminal
- servo motor
- compact heap
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Abstract
The invention discloses a horizontal thin wire harness tension detector. The horizontal thin wire harness tension detector consists of a control panel (1), a wiring terminal clamping mold (2), a lead compression block (4), a lead compression seat (5), a wire harness (6), a guide chute (7), a transverse drive servo motor (11), a detector body (12) and a wiring terminal rotation drive servo motor (13). The horizontal thin wire harness tension detector is characterized in that the wiring terminal end of the wire harness (6) is fixed in a clamping groove of the wiring terminal clamping mold (2), and the wire harness (7) is pulled to reach the detection force value required by the control panel (1). According to the invention, an operator fixes the wiring terminal end of the wire harness on the wiring terminal clamping device according to the diameter of the wire harness, fixes the lead end of the wire harness in the lead clamping device, and controls the detection force so as to determine the wire harness automatically; the horizontal thin wire harness tension detector can effectively guarantee the quality of a thin wire harness lead, and is especially suitable for detection on a vehicle-mounted control circuit with high reliability requirement.
Description
Technical field
The present invention relates to a kind of strength of joint pick-up unit to the more tiny harness connecting terminal of wire diameter, be particularly suitable for the detection of the operation circuit to vehicle-mounted different-diameter.
Background technology
Along with social development, people more and more pay close attention to for the safety event in life now.The safety of for example automobile, automobile is all vehicle-mounted computer control mostly now, and vehicle-mounted computer is equivalent to the brain of vehicle, and communication just need to be carried out by each wire harness, and the nerve that wire harness is equivalent to human body is the same, and it is very fearful that wire harness breaks down.Wire harness generally breaks down most all in the junction of two lines, and this just requires to be connected closely reliably between the connection terminal of wire harness and wire.Connection terminal was all the connection tight ness rating of feeling both by workman's feel after being connected with wire in the past, artificial feeling can be along with personnel's degree of fatigue changes, this just causes the quality of product very unstable, for the use in wire harness future hides some dangers for.Automobile all requires light weight words now, and wire harness is more and more thinner, manually in the time detecting with hand, may overexert, and wire is broken in insulation course, occurs that in use electric conductivity declines and the self-burning of vehicle phenomenon of appearance.
Summary of the invention
For above deficiency, the object of the present invention is to provide a kind of pulling force of horizontal fine rule bundle to detect machine, be the detection at the laggard row wire of production moulding and connection terminal strength of joint to tiny wire harness, be particularly suitable for the detection of the vehicle-mounted control circuit higher to reliability requirement.
Technical scheme of the present invention is achieved in the following ways: a kind of pulling force of horizontal fine rule bundle detects machine, by control panel, connection terminal clamping mould, wire compact heap, wire pressed seat, wire harness, guide chute, traversing driving servo motor, fuselage and connection terminal rotarily actuate servo motor composition, connection terminal clamping mould and connection terminal rotarily actuate servo motor and are fixed on fuselage, wire compact heap and wire pressed seat can slide in the guide chute of fuselage, in control panel, be set with detection power value, it is characterized in that: the connection terminal end of described wire harness is fixed in the draw-in groove of connection terminal clamping mould, the conductor part of wire harness is compressed by wire compact heap and wire pressed seat, drive servo motor by ball-screw will drive wire compact heap and wire pressed seat traversing, pull wire harness to reach the required detection power value of control panel.
The conductor clamping device that the traversing drive wire of actuator movement compact heap, wire pressed seat, the wire lock-screw that described driving servo motor driven is made up of ball axle sleeve, ball-screw, shaft coupling forms moves, thereby pull wire harness, out of service in the time detecting that outputting power reaches the value of setting in control panel.
Described connection terminal clamping mould can be rotated under connection terminal rotarilys actuate the driving of servo motor, can detect wire harness and be subject to force intensity in the time that distortion is stressed.
The present invention, operative employee only need be according to beam diameter, the connection terminal end of wire harness is fixed on connection terminal gripping mechanism, the conductor wire end of wire harness is fixed in conductor clamping device, control detection power well, can realize the automatic mensuration of wire harness, can effectively ensure the quality of tiny harness lead, be particularly suitable for the detection of the vehicle-mounted control circuit higher to reliability requirement.
Brief description of the drawings
Fig. 1 is structural representation of the present invention.
Fig. 2 is the schematic diagram of transmission and dynamic structure.
Fig. 3 is that connection terminal is fixed and conductor clamping schematic diagram.
Embodiment
Known by Fig. 1, the pulling force of horizontal fine rule bundle detects a machine, is rotarilyd actuate servo motor 13 and is formed by control panel 1, connection terminal clamping mould 2, wire lock-screw 3, wire compact heap 4, wire pressed seat 5, wire harness 6, fuselage guide chute 7, ball axle sleeve 8, ball-screw 9, shaft coupling 10, traversing driving servo motor 11, fuselage 12, connection terminal.1 control panel is fixed on 12 fuselages, and connection terminal clamping mould 2 and connection terminal rotarily actuate servo motor 13 and be connected to form connection terminal fixing device by belt, are fixed on 12 fuselages.
Being known by Fig. 2, is the schematic diagram of transmission and dynamic structure.Wire lock-screw 3 is arranged on wire pressed seat 5 by wire compact heap 4 and is fixed in the guide chute 7 of fuselage 12.Ball axle sleeve 8, ball-screw 9, shaft coupling 10, traversing driving servo motor 11 are connected as one.Operative employee is according to beam diameter, the connection terminal end of wire harness 6 is fixed in the corresponding draw-in groove of connection terminal clamping mould 2, is arranged between wire pressed seat 5 after the conductor part of wire harness 7 is fixed on wire compact heap 4, and locked by wire lock-screw 3.Operative employee arranges the power that needs detection on control panel 1, drives servo motor 11 to drive ball axle sleeve 8, ball-screw 9, shaft coupling 10 and wire compact heap 4, wire pressed seat 5 to move, thereby pulls wire harness.It is out of service in the time that traversing driving servo motor 11 detects that outputting power reaches the value of control panel 1 interior setting.If now the rectilinear direction of the intact proof wire harness 6 of wire harness is stressed is qualified.
As Fig. 3 knows, be that connection terminal is fixed and conductor clamping schematic diagram.After the power of carrying out rectilinear direction at wire harness 6 detects, connection terminal clamping mould 2 rotarilys actuate servo motor 13 at connection terminal and is rotated action under driving, and detects wire harness and be subject to force intensity in the time that distortion is stressed.
Claims (3)
1. the pulling force of a horizontal fine rule bundle detects machine, by control panel (1), connection terminal clamping mould (2), wire compact heap (4), wire pressed seat (5), wire harness (6), guide chute (7), traversing driving servo motor (11), fuselage (12) and connection terminal rotarily actuate servo motor (13) composition, connection terminal clamping mould (2) and connection terminal rotarily actuate servo motor (13) and are fixed on fuselage (12), wire compact heap (4) and wire pressed seat (5) can slide in the guide chute of fuselage (12) (7), it is characterized in that: the connection terminal end of described wire harness (6) is fixed in the draw-in groove of connection terminal clamping mould (2), the conductor part of wire harness (6) is compressed by wire compact heap (4) and wire pressed seat (5), drive servo motor (11) by ball-screw (9) will drive wire compact heap (4) and wire pressed seat (5) traversing, pull wire harness (7) to reach the required detection power value of control panel (1).
2. the pulling force of a kind of horizontal fine rule bundle according to claim 1 detects machine, it is characterized in that: the conductor clamping device motion that described driving servo motor (11) drives the traversing drive wire of the gearing compact heap (4), wire pressed seat (5), the wire lock-screw (3) that are made up of ball axle sleeve (8), ball-screw (9), shaft coupling (10) to form, thereby pull wire harness (6), out of service in the time detecting that outputting power reaches the value of setting in control panel (1).
3. the pulling force of a kind of sleeping examination fine rule bundle according to claim 1 detects machine, it is characterized in that: described connection terminal clamping mould (2) can be rotated under connection terminal rotarilys actuate the driving of servo motor (13), can detect wire harness (6) and be subject to force intensity in the time that distortion is stressed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410147290.2A CN103884594A (en) | 2014-04-14 | 2014-04-14 | Horizontal thin wire harness tension detector |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410147290.2A CN103884594A (en) | 2014-04-14 | 2014-04-14 | Horizontal thin wire harness tension detector |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103884594A true CN103884594A (en) | 2014-06-25 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410147290.2A Pending CN103884594A (en) | 2014-04-14 | 2014-04-14 | Horizontal thin wire harness tension detector |
Country Status (1)
| Country | Link |
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| CN (1) | CN103884594A (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105067441A (en) * | 2015-05-11 | 2015-11-18 | 奥可利电子(昆山)有限公司 | Thermocouple pulling force test apparatus |
| CN105352689A (en) * | 2015-11-10 | 2016-02-24 | 广州广电计量检测无锡有限公司 | Engine wiring harness fatigue testing device for vehicle |
| CN105445089A (en) * | 2015-12-31 | 2016-03-30 | 苏州卓德电子有限公司 | Strength detection device for automobile wire harness |
| CN105680277A (en) * | 2016-04-11 | 2016-06-15 | 安庆市凌康机电产品设计有限公司 | Drawing device, capable of detection, of riveting machine |
| CN110057677A (en) * | 2019-03-12 | 2019-07-26 | 中国人民解放军陆军军事交通学院镇江校区 | Completely new pull force calculation machine |
| CN111896862A (en) * | 2020-08-04 | 2020-11-06 | 广东金田半导体科技有限公司 | Device for improving reliability of semiconductor package |
| CN113358476A (en) * | 2021-08-11 | 2021-09-07 | 江苏柏盛家纺有限公司 | Tensile property testing system and method for cotton textile yarns |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2101749A (en) * | 1981-05-18 | 1983-01-19 | Fira Furniture Industry Resear | An apparatus and a method for applying and measuring tensile force |
| CN201285394Y (en) * | 2008-11-04 | 2009-08-05 | 上海瑞纺仪器有限公司 | Stretching-strength tester for knitted fabric |
| CN101504348A (en) * | 2008-02-04 | 2009-08-12 | 西北工业大学 | Hyper-elastic material high-speed stretching tester and experiment method |
| CN201421420Y (en) * | 2009-06-15 | 2010-03-10 | 鹤壁海昌专用设备有限公司 | Tension plate used in tension tester |
| CN103134730A (en) * | 2011-12-05 | 2013-06-05 | 万向钱潮（上海）汽车系统有限公司 | Wiring harness stretch performance detection device |
-
2014
- 2014-04-14 CN CN201410147290.2A patent/CN103884594A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2101749A (en) * | 1981-05-18 | 1983-01-19 | Fira Furniture Industry Resear | An apparatus and a method for applying and measuring tensile force |
| CN101504348A (en) * | 2008-02-04 | 2009-08-12 | 西北工业大学 | Hyper-elastic material high-speed stretching tester and experiment method |
| CN201285394Y (en) * | 2008-11-04 | 2009-08-05 | 上海瑞纺仪器有限公司 | Stretching-strength tester for knitted fabric |
| CN201421420Y (en) * | 2009-06-15 | 2010-03-10 | 鹤壁海昌专用设备有限公司 | Tension plate used in tension tester |
| CN103134730A (en) * | 2011-12-05 | 2013-06-05 | 万向钱潮（上海）汽车系统有限公司 | Wiring harness stretch performance detection device |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105067441A (en) * | 2015-05-11 | 2015-11-18 | 奥可利电子(昆山)有限公司 | Thermocouple pulling force test apparatus |
| CN105067441B (en) * | 2015-05-11 | 2018-05-25 | 奥可利电子(昆山)有限公司 | A kind of thermocouple device for testing tensile force |
| CN105352689A (en) * | 2015-11-10 | 2016-02-24 | 广州广电计量检测无锡有限公司 | Engine wiring harness fatigue testing device for vehicle |
| CN105445089A (en) * | 2015-12-31 | 2016-03-30 | 苏州卓德电子有限公司 | Strength detection device for automobile wire harness |
| CN105680277A (en) * | 2016-04-11 | 2016-06-15 | 安庆市凌康机电产品设计有限公司 | Drawing device, capable of detection, of riveting machine |
| CN110057677A (en) * | 2019-03-12 | 2019-07-26 | 中国人民解放军陆军军事交通学院镇江校区 | Completely new pull force calculation machine |
| CN110057677B (en) * | 2019-03-12 | 2024-03-26 | 中国人民解放军陆军军事交通学院镇江校区 | Tension detector |
| CN111896862A (en) * | 2020-08-04 | 2020-11-06 | 广东金田半导体科技有限公司 | Device for improving reliability of semiconductor package |
| CN113358476A (en) * | 2021-08-11 | 2021-09-07 | 江苏柏盛家纺有限公司 | Tensile property testing system and method for cotton textile yarns |
| CN113358476B (en) * | 2021-08-11 | 2021-10-01 | 江苏柏盛家纺有限公司 | Tensile property testing system and method for cotton textile yarns |
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Application publication date: 20140625 |