CN110233404A - A kind of method and Aircraft Cable Shield receipts head for making Aircraft Cable Shield and receiving head - Google Patents
A kind of method and Aircraft Cable Shield receipts head for making Aircraft Cable Shield and receiving head Download PDFInfo
- Publication number
- CN110233404A CN110233404A CN201910516531.9A CN201910516531A CN110233404A CN 110233404 A CN110233404 A CN 110233404A CN 201910516531 A CN201910516531 A CN 201910516531A CN 110233404 A CN110233404 A CN 110233404A
- Authority
- CN
- China
- Prior art keywords
- lead
- housing
- cable shield
- head
- aircraft cable
- 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.)
- Pending
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Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R13/00—Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
- H01R13/648—Protective earth or shield arrangements on coupling devices, e.g. anti-static shielding
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R13/00—Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
- H01R13/648—Protective earth or shield arrangements on coupling devices, e.g. anti-static shielding
- H01R13/658—High frequency shielding arrangements, e.g. against EMI [Electro-Magnetic Interference] or EMP [Electro-Magnetic Pulse]
- H01R13/6591—Specific features or arrangements of connection of shield to conductive members
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R13/00—Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
- H01R13/648—Protective earth or shield arrangements on coupling devices, e.g. anti-static shielding
- H01R13/658—High frequency shielding arrangements, e.g. against EMI [Electro-Magnetic Interference] or EMP [Electro-Magnetic Pulse]
- H01R13/6591—Specific features or arrangements of connection of shield to conductive members
- H01R13/6597—Specific features or arrangements of connection of shield to conductive members the conductive member being a contact of the connector
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R43/00—Apparatus or processes specially adapted for manufacturing, assembling, maintaining, or repairing of line connectors or current collectors or for joining electric conductors
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R43/00—Apparatus or processes specially adapted for manufacturing, assembling, maintaining, or repairing of line connectors or current collectors or for joining electric conductors
- H01R43/02—Apparatus or processes specially adapted for manufacturing, assembling, maintaining, or repairing of line connectors or current collectors or for joining electric conductors for soldered or welded connections
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Shielding Devices Or Components To Electric Or Magnetic Fields (AREA)
Abstract
This application discloses a kind of methods and Aircraft Cable Shield receipts head for making Aircraft Cable Shield and receiving head.The method that the production Aircraft Cable Shield receives head includes: step 1: stripping to the outer protective sleeve of the end of one end of cable, exposes housing；Step 2: the housing of exposing being pushed and pulled to another extreme direction, exposes cable insulation length；Step 3: the housing of exposing is trimmed；Step 4: cutting off electric wire as lead；Step 5: peelling off the insulated hull of lead ends, the core of lead is dispersed as sector；Step 6: the core of lead being put on the housing of cable, and flushes insulating layer end, and core is flattened；Step 7: choosing welded pipe, the tin ring in welded pipe is made to be in the middle position at housing and gage lap；Step 8: melting tin ring sufficiently with heat gun heating, cover included glue heat-shrinkable tube, sealing ring fusing is shunk.The application can be improved the safety and reliability of Aircraft Cables institute control system.
Description
Technical field
This application involves aircraft strand design technical fields, more particularly to a kind of side for making Aircraft Cable Shield and receiving head
Method and Aircraft Cable Shield receive head.
Background technique
The purpose of cable shield ground connection is mainly the electromagnetic interference prevented in cable signal transmittance process.Because in powerful arteries and veins
It rushes around electrical current carriers and will form powerful electromagnetic field, electric energy can be coupled in neighbouring cable, the coupling of this energy
Aircraft system where will lead to cable generates failure.When being affected such as the cable of some transmission electric impulse signals, pulse
Signal will be distorted, and working characteristics changes, and indicated failure, caused system function abnormal.And shielded cable only exists
Just effective when shielded layer is grounded, therefore, cable shield should shield continuous and reliable ground aboard, let out to prevent electromagnetic field
Leakage.Housing when single shielded cable or more similar cables are connected at harness with EWIS components such as plugs, between cable
Terminal processes should all be carried out, while also needing bonding.
Thus, it is desirable to have a kind of technical solution overcomes or at least mitigates at least one drawbacks described above of the prior art.
Apply for content
The application be designed to provide it is a kind of make Aircraft Cable Shield receive the method for head overcome or at least mitigate it is existing
There is at least one drawbacks described above in technology.
To achieve the above object, the application provides a kind of method for making Aircraft Cable Shield and receiving head, the production aircraft
The method that cable shield receives head includes the following steps:
Step 1: the outer protective sleeve of the end of one end of cable being stripped, housing is exposed；
Step 2: the housing of exposing being pushed and pulled to another extreme direction, exposes cable insulation length；
Step 3: the housing of exposing is trimmed；
Step 4: cutting off electric wire as lead；
Step 5: peelling off the insulated hull of lead ends, the core of lead is dispersed as sector；
Step 6: the core of lead being put on the housing of cable, and flushes insulating layer end, and core is flattened；
Step 7: choosing welded pipe, the tin ring in welded pipe is made to be in the middle position at housing and gage lap；
Step 8: melting tin ring sufficiently with heat gun heating, cover included glue heat-shrinkable tube, sealing ring fusing is shunk.
Optionally, lead 22# lead.
Optionally, lead 20# lead.
Present invention also provides a kind of Aircraft Cable Shields to receive head, and the Aircraft Cable Shield receives head using as described above
The method that production Aircraft Cable Shield receives head is made.
The method that the production Aircraft Cable Shield of the application receives head can be improved the safety of Aircraft Cables institute control system
And reliability, while significantly improving the length of service of aircraft, mitigate very big burden to the work of engineering cable maintenance and reducing maintenance
Expense.The shielding receives head method and is able to satisfy various complex electromagnetic environments and badly natural environment and mechanical environment.Of the invention
A kind of design method that head is received in shielding is to extract the shielded layer of shielded cable out, then by installing shielding scolding tin pipe additional and installing additional mutual
Housing between similar cable is interconnected, finally carries out mode single-end earthed with connecting terminal, reach and shield well by even lead
Effect is covered, realizes that cable electromagnetic protection requires and resistance to badly natural environment and the requirement of the sealing protection of mechanical environment.The shielding
It is safe and reliable, stable to receive head design method.
Detailed description of the invention
Fig. 1 is the flow diagram that the method for head is received according to the production Aircraft Cable Shield of the application first embodiment.
Specific embodiment
To keep the purposes, technical schemes and advantages of the application implementation clearer, below in conjunction in the embodiment of the present application
Attached drawing, technical solutions in the embodiments of the present application is further described in more detail.In the accompanying drawings, identical from beginning to end or class
As label indicate same or similar element or element with the same or similar functions.Described embodiment is the application
A part of the embodiment, instead of all the embodiments.The embodiments described below with reference to the accompanying drawings are exemplary, it is intended to use
In explanation the application, and it should not be understood as the limitation to the application.Based on the embodiment in the application, ordinary skill people
Member's every other embodiment obtained without creative efforts, shall fall in the protection scope of this application.Under
Face is described in detail embodiments herein in conjunction with attached drawing.
In the description of the present application, it is to be understood that term " center ", " longitudinal direction ", " transverse direction ", "front", "rear",
The orientation or positional relationship of the instructions such as "left", "right", "vertical", "horizontal", "top", "bottom" "inner", "outside" is based on attached drawing institute
The orientation or positional relationship shown is merely for convenience of description the application and simplifies description, rather than the dress of indication or suggestion meaning
It sets or element must have a particular orientation, be constructed and operated in a specific orientation, therefore should not be understood as protecting the application
The limitation of range.
Fig. 1 is the flow diagram that the method for head is received according to the production Aircraft Cable Shield of the application first embodiment.
The method that production Aircraft Cable Shield as shown in Figure 1 receives head includes the following steps:
Step 1: the outer protective sleeve of the end of one end of cable being stripped, housing is exposed；
Step 2: the housing of exposing being pushed and pulled to another extreme direction, exposes cable insulation length；
Step 3: the housing of exposing is trimmed；
Step 4: cutting off electric wire as lead；
Step 5: peelling off the insulated hull of lead ends, the core of lead is dispersed as sector；
Step 6: the core of lead being put on the housing of cable, and flushes insulating layer end, and core is flattened；
Step 7: choosing welded pipe, the tin ring in welded pipe is made to be in the middle position at housing and gage lap；
Step 8: melting tin ring sufficiently with heat gun heating, cover included glue heat-shrinkable tube, sealing ring fusing is shunk.
The lead of the application can use 22# lead or lead 20# lead.
Present invention also provides a kind of Aircraft Cable Shields to receive head, and the Aircraft Cable Shield receives head using as described above
The method that production Aircraft Cable Shield receives head is made.
The method that the production Aircraft Cable Shield of the application receives head can be improved the safety of Aircraft Cables institute control system
And reliability, while significantly improving the length of service of aircraft, mitigate very big burden to the work of engineering cable maintenance and reducing maintenance
Expense.The shielding receives head method and is able to satisfy various complex electromagnetic environments and badly natural environment and mechanical environment.Of the invention
A kind of design method that head is received in shielding is to extract the shielded layer of shielded cable out, then by installing shielding scolding tin pipe additional and installing additional mutual
Housing between similar cable is interconnected, finally carries out mode single-end earthed with connecting terminal, reach and shield well by even lead
Effect is covered, realizes that cable electromagnetic protection requires and resistance to badly natural environment and the requirement of the sealing protection of mechanical environment.The shielding
It is safe and reliable, stable to receive head design method.
Finally it is noted that above embodiments are only to illustrate the technical solution of the application, rather than its limitations.To the greatest extent
Pipe is with reference to the foregoing embodiments described in detail the application, those skilled in the art should understand that: it is still
It is possible to modify the technical solutions described in the foregoing embodiments, or part of technical characteristic is equally replaced
It changes；And these are modified or replaceed, the essence of each embodiment technical solution of the application that it does not separate the essence of the corresponding technical solution
Mind and range.
Claims (4)
1. a kind of method for making Aircraft Cable Shield and receiving head, which is characterized in that the production Aircraft Cable Shield receives the side of head
Method includes the following steps:
Step 1: the outer protective sleeve of the end of one end of cable being stripped, housing is exposed；
Step 2: the housing of exposing being pushed and pulled to another extreme direction, exposes cable insulation length；
Step 3: the housing of exposing is trimmed；
Step 4: cutting off electric wire as lead；
Step 5: peelling off the insulated hull of lead ends, the core of lead is dispersed as sector；
Step 6: the core of lead being put on the housing of cable, and flushes insulating layer end, and core is flattened；
Step 7: choosing welded pipe, the tin ring in welded pipe is made to be in the middle position at housing and gage lap；
Step 8: melting tin ring sufficiently with heat gun heating, cover included glue heat-shrinkable tube, sealing ring fusing is shunk.
2. the method that production Aircraft Cable Shield receives head as described in claim 1, which is characterized in that the lead is drawn with 22#
Line.
3. the method that production Aircraft Cable Shield receives head as described in claim 1, which is characterized in that the lead is drawn with 20#
Line.
4. a kind of Aircraft Cable Shield receives head, which is characterized in that the Aircraft Cable Shield receives head and uses such as claims 1 to 3
Any one of described in production Aircraft Cable Shield receive head method be made.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910516531.9A CN110233404A (en) | 2019-06-14 | 2019-06-14 | A kind of method and Aircraft Cable Shield receipts head for making Aircraft Cable Shield and receiving head |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910516531.9A CN110233404A (en) | 2019-06-14 | 2019-06-14 | A kind of method and Aircraft Cable Shield receipts head for making Aircraft Cable Shield and receiving head |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110233404A true CN110233404A (en) | 2019-09-13 |
Family
ID=67859950
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910516531.9A Pending CN110233404A (en) | 2019-06-14 | 2019-06-14 | A kind of method and Aircraft Cable Shield receipts head for making Aircraft Cable Shield and receiving head |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110233404A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111969384A (en) * | 2020-07-08 | 2020-11-20 | 上海皆泰新能源科技有限公司 | New energy automobile battery wire harness production process |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107275913A (en) * | 2017-05-26 | 2017-10-20 | 北京航天新风机械设备有限责任公司 | A kind of wrapped shielding wire cable socket processing method of Kapton |
| CN107634440A (en) * | 2017-08-30 | 2018-01-26 | 陕西千山航空电子有限责任公司 | A kind of processing method of the screen layer of shielding line |
| CN107993776A (en) * | 2017-11-28 | 2018-05-04 | 上海航天精密机械研究所 | Bunch of cables shielding layer grounding processing method on a kind of bullet |
| CN109638729A (en) * | 2018-12-10 | 2019-04-16 | 中国电建集团河南工程有限公司 | Secondary cable wiring layered peeling ranking method |
-
2019
- 2019-06-14 CN CN201910516531.9A patent/CN110233404A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107275913A (en) * | 2017-05-26 | 2017-10-20 | 北京航天新风机械设备有限责任公司 | A kind of wrapped shielding wire cable socket processing method of Kapton |
| CN107634440A (en) * | 2017-08-30 | 2018-01-26 | 陕西千山航空电子有限责任公司 | A kind of processing method of the screen layer of shielding line |
| CN107993776A (en) * | 2017-11-28 | 2018-05-04 | 上海航天精密机械研究所 | Bunch of cables shielding layer grounding processing method on a kind of bullet |
| CN109638729A (en) * | 2018-12-10 | 2019-04-16 | 中国电建集团河南工程有限公司 | Secondary cable wiring layered peeling ranking method |
Non-Patent Citations (1)
| Title |
|---|
| 马蓉，龙贵林著: "《装备用低频电缆组件组装工艺》", 31 January 2017 * |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111969384A (en) * | 2020-07-08 | 2020-11-20 | 上海皆泰新能源科技有限公司 | New energy automobile battery wire harness production process |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20190913 |