CN105470761A - Machine body wiring harness - Google Patents
Machine body wiring harness Download PDFInfo
- Publication number
- CN105470761A CN105470761A CN201511017798.1A CN201511017798A CN105470761A CN 105470761 A CN105470761 A CN 105470761A CN 201511017798 A CN201511017798 A CN 201511017798A CN 105470761 A CN105470761 A CN 105470761A
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- Prior art keywords
- connector
- wire harness
- wire
- wiring harness
- group
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Classifications
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R31/00—Coupling parts supported only by co-operation with counterpart
- H01R31/06—Intermediate parts for linking two coupling parts, e.g. adapter
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R27/00—Coupling parts adapted for co-operation with two or more dissimilar counterparts
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R2201/00—Connectors or connections adapted for particular applications
- H01R2201/26—Connectors or connections adapted for particular applications for vehicles
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- Insulated Conductors (AREA)
- Installation Of Indoor Wiring (AREA)
Abstract
The invention discloses a machine body wiring harness. The machine body wiring harness comprises a first wiring harness, a second wiring harness, a third wiring harness, a fourth wiring harness, a fifth wiring harness, a sixth wiring harness, a seventh wiring harness, an eighth wiring harness, a ninth wiring harness, a tenth wiring harness, an eleventh wiring harness and a twelfth wiring harness; and the junctions of wire groups of each wiring harness are fixed through cable ties. Multiple cable ties are arranged on the wire groups connected with each connector, so that the wire groups can be arranged and fixed in an ordered manner; the overall wiring harness strength and the concentration ratio of the wires are high, and the phenomenon of loosening and separating of the wires caused by external force does not occur easily; the machine body wiring harness is reasonable in wiring manner, and high in wiring harness transmission stability; and in addition, the machine body wiring harness is simple in structure, high in transmission quality, low in processing cost and long in service life.
Description
Technical field:
The invention belongs to wire harness technical field, specifically relate to a kind of fuselage wire harness.
Background technology:
Wire harness (wireharness) provides the overall of service equipment, as trunk, switch, control system etc. for certain load source group.Wire harness is generally made up of wire, insulating sleeve, binding post and wrapper material.After wire harness refers to and crimped with electric wire by the contact terminal (connector) of copper product punching, outside is plastic compression insulator or added metal housing etc. again, ties up the assembly forming connecting circuit with wire harness.Automotive wire bundle mainly comprises engine wiring harness and overall wire sheaves, and wherein, engine wiring harness, except transducer wire harness and ECU wire harness, connects the wire harness of other circuit in addition, and such as charge heating wire harness, cranking-motor relay control wire harness, generator excitation wire harness etc.Wire harness is of a great variety, and without good fixed form, and easy in transport and assembling process because protecting not in place, to cause wire harness to be stepped on disconnected.
But existing harness wiring mode is unreasonable, coated effect is also not satisfactory, the concentration degree of wire harness is not high, and depend merely on the bulk strength that adhesive tape also cannot guarantee wire harness, especially near binding post place, easily be subject to external force to occur loosening and obscission, and existing wire harness normally adopts a cable, if when wire harness is made up of multi-cable, the two ends of cable connect one or more connector respectively, when a connector connects multi-cable, the cable of link easily causes confusion, thus affects the transmission stability of whole wire harness.Particularly for the device that multiple wire harness connects, wire laying mode is unreasonable, and easily cause winding displacement chaotic, transmission stability is poor.
Summary of the invention:
For this reason, technical problem to be solved by this invention is that the concentration degree between the overall bunch intensity of wire harness in prior art and wire is lower, and easily occur loosening and break-off by external force, the wire laying mode of multiple wire harness is unreasonable, affect the transmission stability of wire harness, thus propose a kind of fuselage wire harness.
For achieving the above object, technical scheme of the present invention is as follows:
A kind of fuselage wire harness, comprising:
First wire harness, the first wire group that described first wire harness comprises the first connector and is connected with described first connector.
Second wire harness, the second wire group that described second wire harness comprises the second connector and is connected with described second connector.
3rd wire harness, the privates group that described 3rd wire harness comprises the 3rd connector and is connected with described 3rd connector.
Quad bundle, described quad bundle comprises the 4th connector, the privates group be connected with described 4th connector, the 5th connector, the 5th wire group that is connected with described 5th connector.
5th wire harness and the 6th wire harness, described 5th wire harness and described 6th wire harness are symmetrical arranged, the 6th wire group that described 5th wire harness comprises the 6th connector and is connected with described 6th connector, described 6th wire harness comprises the 7th connector, the 7th wire group be connected with described 7th connector, the 8th connector, the 8th wire group that is connected with described 8th connector.
7th wire harness and the 8th wire harness, described 7th wire harness is identical with described 8th wiring harness structure and be symmetrical arranged, the 9th wire group that described 7th wire harness comprises the 9th connector and is connected with described 9th connector.
9th wire harness and the tenth wire harness, described 9th wire harness is identical with described tenth wiring harness structure and be symmetrical arranged, the tenth wire group that described 9th wire harness comprises the tenth connector and is connected with described tenth connector.
11 wire harness, the 11 wire group that described 11 wire harness comprises the tenth a connector and is connected with described tenth a connector.
12 wire harness, the 12 wire group that described 12 wire harness comprises the 12 connector and is connected with described 12 connector.
The junction of described first wire group, described second wire group, described second wire group, described privates group, described 5th wire group, described 6th wire group, described 7th wire group, described 8th wire group, described 9th wire group, described tenth wire group, described 11 wire group, described 12 wire group is all fixed by cable tie.
Preferred as technique scheme, described first connector is identical with described 4th connector construction, and described first connector and described 4th connector are D-SUB Combination connector.
Preferred as technique scheme, described 3rd connector is D-SUB connector, and described 3rd connector is the D-SUB connector of two row's pins.
Preferred as technique scheme, described 5th connector is D-SUB connector, and described 5th connector is the D-SUB connector of two row's pins.
Preferred as technique scheme, described 6th connector, described 7th connector, described tenth a connector structure are identical, and described 6th connector, described 7th connector, described tenth a connector are the FCT connector of two row's pins.
Preferred as technique scheme, described cable tie adopts white Nylon band.
Beneficial effect of the present invention is: it arranges multiple cable tie by the wire group that connects at each connector, can orderly arrangement be carried out to wire group and fix, concentration degree between the overall bunch intensity of wire harness and wire is high, be not easy to be subject to external force to occur loosening and break-off, wire laying mode is reasonable, and wire harness transmission stability is high.Structure of the present invention is simple, and transmission quality is high, and processing cost is low, long service life.
Accompanying drawing illustrates:
The following drawings is only intended to schematically illustrate the present invention and explain, not delimit the scope of the invention.Wherein:
Fig. 1 is the fuselage wiring harness structure schematic diagram of one embodiment of the invention;
Fig. 2 is the first connector construction end view of one embodiment of the invention;
Fig. 3 is the 3rd connector construction end view of one embodiment of the invention;
Fig. 4 is the 5th connector construction end view of one embodiment of the invention;
Fig. 5 is the 6th connector construction end view of one embodiment of the invention.
Symbol description in figure
1-first wire harness, 2-second wire harness, 3-the 3rd wire harness, 4-quad bundle, 5-the 5th wire harness, 6-the 6th wire harness, 7-the 7th wire harness, 8-the 8th wire harness, 9-the 9th wire harness, 10-the tenth speed limit, 11-the 11 wire harness, 12-the 12 wire harness, 13-cable tie, 101-first connector, 102-first wire group, 201-second connector, 202-second wire group, 301-the 3rd connector, 302-privates group, 401-the 4th connector, 402-privates group, 403-the 5th connector, 404-the 5th wire group, 501-the 6th connector, 502-the 6th wire group, 601-the 7th connector, 602-the 7th wire group, 603-the 8th connector, 604-the 8th wire group, 7801-the 9th connector, 7802-the 9th wire group, 9101-the tenth connector, 9102-the tenth wire group, 1101-the tenth a connector, 1102-the 11 wire group, 1201-the 12 connector, 1202-the 12 wire group, 1011-first bolt hole, position, 1012-first hole, 3011-second bolt hole, position, 3012-second hole, 4031-the 3rd bolt hole, 4032-the 3rd position, hole, 5011-the 4th bolt hole, 5012-the 4th position, hole.
Embodiment:
As shown in Figure 1, fuselage wire harness of the present invention, comprising:
First wire harness 1, the first wire group 102 that described first wire harness 1 comprises the first connector 101 and is connected with described first connector 101.As shown in Figure 2, described first connector 101 is D-SUB Combination connector, is provided with symmetrically arranged two the first bolts hole 1011 and three the first positions, hole 1012.
Second wire harness 2, the second wire group 202 that described second wire harness 2 comprises the second connector 201 and is connected with described second connector 201.
3rd wire harness 3, the privates group 302 that described 3rd wire harness 3 comprises the 3rd connector 301 and is connected with described 3rd connector 301.Described 3rd connector 301 is D-SUB connector, and as shown in Figure 3, described 3rd connector 301 is the D-SUB connector of two row 37 pins, comprises symmetrically arranged two the second bolts hole 3011 and 37 the second positions, hole 3012.
Quad bundle 4, described quad bundle 4 comprises the 4th connector 401, the privates group 402 be connected with described 4th connector 401, the 5th connector 403, the 5th wire group 404 that is connected with described 5th connector 403.Described 4th connector 401 is D-SUB Combination connector, and described first connector 101 is identical with described 4th connector 401 structure.Described 5th connector 403 is D-SUB connector, and as shown in Figure 4, described 5th connector 403 is the D-SUB connector of two row 22 pins, comprises symmetrically arranged two the 3rd bolts hole 4031 and 22 the 3rd positions, hole 4032.
5th wire harness 5 and the 6th wire harness 6, described 5th wire harness 5 and described 6th wire harness 6 are symmetrical arranged, the 6th wire group 502 that described 5th wire harness 5 comprises the 6th connector 501 and is connected with described 6th connector 501, described 6th wire harness 6 comprises the 7th connector 601, the 7th wire group 602 be connected with described 7th connector 601, the 8th connector 603, the 8th wire group 604 that is connected with described 8th connector 603.As shown in Figure 5, described 6th connector 501 is the FCT connector of two row 9 pins, and described 6th connector 501 comprises symmetrically arranged two the 4th bolts hole 5011 and 9 the 4th positions, hole 5012.Described 7th connector 601 is the FCT connector of two row 9 pins, and described 7th connector 601 is identical with described 6th connector 501 structure.
7th wire harness 7 and the 8th wire harness 8, described 7th wire harness 7 is identical with described 8th wire harness 8 structure and be symmetrical arranged, the 9th wire group 7802 that described 7th wire harness 7 comprises the 9th connector 7801 and is connected with described 9th connector 7801.
9th wire harness 9 and the tenth wire harness 10, described 9th wire harness 9 is identical with described tenth wire harness 10 structure and be symmetrical arranged, the tenth wire group 9102 that described 9th wire harness 9 comprises the tenth connector 9101 and is connected with described tenth connector 9101.
11 wire harness 11, the 11 wire group 1102 that described 11 wire harness 11 comprises the tenth a connector 1101 and is connected with described tenth a connector 1101.Described tenth a connector 1101 is the FCT connector of two row 9 pins, and described tenth a connector 1101 is identical with described 6th connector 501 structure.
12 wire harness 12, the 12 wire group 1202 that described 12 wire harness 12 comprises the 12 connector 1201 and is connected with described 12 connector 1201.
Described first wire group 102, described second wire group 202, described second wire group 302, described privates group 402, described 5th wire group 404, described 6th wire group 502, described 7th wire group 602, described 8th wire group 604, described 9th wire group 7802, described tenth wire group 9102, described 11 wire group 1102, multiple conducting wires first end in described 12 wire group 1202 is connected with connector own, the second end section of multiple conducting wires or be all connected with other each connectors, wherein connector own is connector corresponding to guide line group, and be connected according to actual needs with other each connector connected modes.
Described first wire group 102, described second wire group 202, described second wire group 302, described privates group 402, described 5th wire group 404, described 6th wire group 502, described 7th wire group 602, described 8th wire group 604, described 9th wire group 7802, described tenth wire group 9102, described 11 wire group 1102, the junction of described 12 wire group 1202 is all fixed by cable tie 13, described junction refers in two line conductor groups the intersection needing to carry out with other connectors each wire be connected, or in multichannel wire group, need the intersection carrying out each wire be connected with other connectors.And each wire group is also provided with cable tie 13, the binding being beneficial to single wire group is fixed, and in the present embodiment, described cable tie 13 adopts white Nylon band.
A kind of fuselage wire harness described in the present embodiment, comprise: the first wire harness, the second wire harness, the 3rd wire harness, quad bundle, the 5th wire harness, the 6th wire harness, the 7th wire harness, the 8th wire harness, the 9th wire harness, the tenth wire harness, the 11 wire harness, the 12 wire harness, the junction of the wire group of each wire harness is all fixed by cable tie.It arranges multiple cable tie by the wire group that connects at each connector, can orderly arrangement be carried out to wire group and fix, concentration degree between the overall bunch intensity of wire harness and wire is high, be not easy to be subject to external force to occur loosening and break-off, wire laying mode is reasonable, and wire harness transmission stability is high.This apparatus structure is simple, and transmission quality is high, and processing cost is low, long service life.
Obviously, above-described embodiment is only for clearly example being described, and the restriction not to execution mode.For those of ordinary skill in the field, can also make other changes in different forms on the basis of the above description.Here exhaustive without the need to also giving all execution modes.And thus the apparent change of extending out or variation be still among the protection range of the invention.
Claims (6)
1. a fuselage wire harness, is characterized in that, comprising:
First wire harness (1), the first wire group (102) that described first wire harness (1) comprises the first connector (101) and is connected with described first connector (101);
Second wire harness (2), the second wire group (202) that described second wire harness (2) comprises the second connector (201) and is connected with described second connector (201);
3rd wire harness (3), the privates group (302) that described 3rd wire harness (3) comprises the 3rd connector (301) and is connected with described 3rd connector (301);
Quad bundle (4), described quad bundle (4) comprises the 4th connector (401), the privates group (402) be connected with described 4th connector (401), the 5th connector (403), the 5th wire group (404) that is connected with described 5th connector (403);
5th wire harness (5) and the 6th wire harness (6), described 5th wire harness (5) and described 6th wire harness (6) are symmetrical arranged, the 6th wire group (502) that described 5th wire harness (5) comprises the 6th connector (501) and is connected with described 6th connector (501), described 6th wire harness (6) comprises the 7th connector (601), the 7th wire group (602) be connected with described 7th connector (601), the 8th connector (603), the 8th wire group (604) that is connected with described 8th connector (603);
7th wire harness (7) and the 8th wire harness (8), described 7th wire harness (7) is identical with described 8th wire harness (8) structure and be symmetrical arranged, the 9th wire group (7802) that described 7th wire harness (7) comprises the 9th connector (7801) and is connected with described 9th connector (7801);
9th wire harness (9) and the tenth wire harness (10), described 9th wire harness (9) is identical with described tenth wire harness (10) structure and be symmetrical arranged, the tenth wire group (9102) that described 9th wire harness (9) comprises the tenth connector (9101) and is connected with described tenth connector (9101);
11 wire harness (11), the 11 wire group (1102) that described 11 wire harness (11) comprises the tenth a connector (1101) and is connected with described tenth a connector (1101);
12 wire harness (12), the 12 wire group (1202) that described 12 wire harness (12) comprises the 12 connector (1201) and is connected with described 12 connector (1201);
Described first wire group (102), described second wire group (202), described second wire group (302), described privates group (402), described 5th wire group (404), described 6th wire group (502), described 7th wire group (602), described 8th wire group (604), described 9th wire group (7802), described tenth wire group (9102), described 11 wire group (1102), the junction of described 12 wire group (1202) is all fixed by cable tie (13).
2. fuselage wire harness according to claim 1, it is characterized in that: described first connector (101) is identical with described 4th connector (401) structure, described first connector (101) and described 4th connector (401) are D-SUB Combination connector.
3. fuselage wire harness according to claim 1, is characterized in that: described 3rd connector (301) is D-SUB connector, and described 3rd connector (301) is the D-SUB connector of two row 37 pins.
4. fuselage wire harness according to claim 1, is characterized in that: described 5th connector (403) is D-SUB connector, and described 5th connector (403) is the D-SUB connector of two row 22 pins.
5. fuselage wire harness according to claim 1, it is characterized in that: described 6th connector (501), described 7th connector (601), described tenth a connector (1101) structure are identical, described 6th connector (501), described 7th connector (601), described tenth a connector (1101) are the FCT connector of two row 9 pins.
6. fuselage wire harness according to claim 1, is characterized in that: described cable tie (13) adopts white Nylon band.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201511017798.1A CN105470761B (en) | 2015-12-31 | 2015-12-31 | A kind of fuselage harness |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201511017798.1A CN105470761B (en) | 2015-12-31 | 2015-12-31 | A kind of fuselage harness |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105470761A true CN105470761A (en) | 2016-04-06 |
| CN105470761B CN105470761B (en) | 2019-01-11 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201511017798.1A Active CN105470761B (en) | 2015-12-31 | 2015-12-31 | A kind of fuselage harness |
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| Country | Link |
|---|---|
| CN (1) | CN105470761B (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN203103668U (en) * | 2012-12-31 | 2013-07-31 | 上海万卡信实业有限公司 | A gold-plated high-sensitive anti-interference automobile air bag wire harness |
| CN203553573U (en) * | 2013-11-22 | 2014-04-16 | 天津市宇龙昊天汽车滤清器有限公司 | Automobile body main wire harness |
| CN203543854U (en) * | 2013-11-22 | 2014-04-16 | 天津市宇龙昊天汽车滤清器有限公司 | Automobile body main wire harness |
| CN204088824U (en) * | 2014-07-28 | 2015-01-07 | 科络普线束技术(太仓)有限公司 | A kind of new work engine wire harness |
| CN205231429U (en) * | 2015-12-31 | 2016-05-11 | 苏州卓德电子有限公司 | Fuselage pencil |
-
2015
- 2015-12-31 CN CN201511017798.1A patent/CN105470761B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN203103668U (en) * | 2012-12-31 | 2013-07-31 | 上海万卡信实业有限公司 | A gold-plated high-sensitive anti-interference automobile air bag wire harness |
| CN203553573U (en) * | 2013-11-22 | 2014-04-16 | 天津市宇龙昊天汽车滤清器有限公司 | Automobile body main wire harness |
| CN203543854U (en) * | 2013-11-22 | 2014-04-16 | 天津市宇龙昊天汽车滤清器有限公司 | Automobile body main wire harness |
| CN204088824U (en) * | 2014-07-28 | 2015-01-07 | 科络普线束技术(太仓)有限公司 | A kind of new work engine wire harness |
| CN205231429U (en) * | 2015-12-31 | 2016-05-11 | 苏州卓德电子有限公司 | Fuselage pencil |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105470761B (en) | 2019-01-11 |
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