CN202694904U - Heat-resisting and insulated high-voltage ignition cable used for airplane - Google Patents
Heat-resisting and insulated high-voltage ignition cable used for airplane Download PDFInfo
- Publication number
- CN202694904U CN202694904U CN 201220229286 CN201220229286U CN202694904U CN 202694904 U CN202694904 U CN 202694904U CN 201220229286 CN201220229286 CN 201220229286 CN 201220229286 U CN201220229286 U CN 201220229286U CN 202694904 U CN202694904 U CN 202694904U
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- heat
- conductor
- resisting
- layer
- insulation layer
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- Expired - Fee Related
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Abstract
The utility model discloses a heat-resisting and insulated high-voltage ignition cable used for an airplane. The heat-resisting and insulated high-voltage ignition cable comprises a conductor, wherein an insulation layer is wrapped at the outside of the conductor; a weaving layer is wrapped at the outside of the insulation layer; and an organic silicon paint layer is packed at the outside of the weaving layer. The conductor is a stainless steel stranded conductor. The insulation layer is a teflon insulation layer. The weaving layer is a double-layered glass fiber weaving layer. As the insulation layer adopts the teflon insulation layer, the heat-resisting and insulated high-voltage ignition cable is good in heat resistance and corrosive resistance. The weaving layer of the heat-resisting and insulated high-voltage ignition cable is a glass fibre weaving layer, and the cable is good in bending performance and heat resistance.
Description
Technical field
The utility model relates to the resistant to elevated temperatures insulation high-voltage ignition cable of aircraft technical field, and is specifically a kind of for insulation, resistant to elevated temperatures cable on the aircraft.
Background technology
Aircraft high-pressure ignition wire core body is more, and the less then ignition intensity of resistance is higher, and electric current is excessively strong, if do not adopt special packing and shielding material, then can produce electromagnetic interference, and firepower is crossed strong the inadaptable of automobile engine that also cause easily.
High temperature resistant and the insulation property of known normal cable then can't be when aircraft igniter high temperature and the heavy current situation under use, this has just proposed very high requirement to resistance to elevated temperatures and the insulation property of cable.So existing normal cable can't satisfy aircraft and use in the high temperature in when igniting and heavy current situation.
In a word, a kind ofly there is not yet report for resistant to elevated temperatures insulation high-pressure ignition wire cable on the aircraft.
Summary of the invention
It is a kind of for resistant to elevated temperatures insulation high-pressure ignition wire cable on the aircraft that the shortcoming that does not possess resistance to elevated temperatures in order to overcome existing cable, the utility model provide.
The technical scheme that its technical problem that solves the utility model adopts is:
A kind ofly comprise conductor for resistant to elevated temperatures insulation high-pressure ignition wire cable on the aircraft, be surrounded with insulating barrier in the described conductor outside; The described insulating barrier outside is coated with braid; The described braid outside is enclosed with the organosilicon enamelled coating.
Described conductor is the stainless steel wire stranded conductor.
Described insulating barrier is the teflon insulation layer.
Described braid is the braiding of double glazing silk.
The beneficial effects of the utility model are:
1, insulating barrier of the present utility model adopts the teflon insulation layer, has better high temperature resistant and decay resistance.
2, braid of the present utility model is double glazing silk braid, has good bending property and resistance to elevated temperatures.
Description of drawings
Fig. 1 is the utility model cross-sectional view.
The name that symbol is corresponding among the figure is called: 1. conductor, 2. insulating barrier, 3. braid, 4. organosilicon enamelled coating.
Embodiment
Fig. 1 further specifies the utility model below in conjunction with accompanying drawing.
A kind ofly comprise conductor 1 for resistant to elevated temperatures insulation high-pressure ignition wire cable on the aircraft, be surrounded with insulating barrier 2 in described conductor 1 outside; Described insulating barrier 2 outsides are coated with braid 3; Described braid 3 outsides are enclosed with organosilicon enamelled coating 4.
Described conductor 1 is stainless steel wire stranded conductor 1.Described insulating barrier 2 is teflon insulation layer 2.Described braid 3 is the braiding of double glazing silk.
Claims (4)
1. one kind is used for resistant to elevated temperatures insulation high-pressure ignition wire cable on the aircraft, it is characterized in that: comprise conductor, be surrounded with insulating barrier in the described conductor outside;
The described insulating barrier outside is coated with braid;
The described braid outside is enclosed with the organosilicon enamelled coating.
2. by claimed in claim 1 for resistant to elevated temperatures insulation high-pressure ignition wire cable on the aircraft, it is characterized in that: described conductor is the stainless steel wire stranded conductor.
3. by claimed in claim 1 for resistant to elevated temperatures insulation high-pressure ignition wire cable on the aircraft, it is characterized in that: described insulating barrier is the teflon insulation layer.
4. by claimed in claim 1 for resistant to elevated temperatures insulation high-pressure ignition wire cable on the aircraft, it is characterized in that: described braid is the braiding of double glazing silk.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220229286 CN202694904U (en) | 2012-05-21 | 2012-05-21 | Heat-resisting and insulated high-voltage ignition cable used for airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220229286 CN202694904U (en) | 2012-05-21 | 2012-05-21 | Heat-resisting and insulated high-voltage ignition cable used for airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202694904U true CN202694904U (en) | 2013-01-23 |
Family
ID=47550486
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220229286 Expired - Fee Related CN202694904U (en) | 2012-05-21 | 2012-05-21 | Heat-resisting and insulated high-voltage ignition cable used for airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202694904U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105513667A (en) * | 2016-01-12 | 2016-04-20 | 郑飞 | Electrical cable |
| CN107887066A (en) * | 2017-11-03 | 2018-04-06 | 芜湖航天特种电缆厂股份有限公司 | Magnaflux, high temperature resistant harness |
| CN108598733A (en) * | 2018-04-12 | 2018-09-28 | 袁明磊 | A kind of conducting wire and igniter burner |
| CN113096894A (en) * | 2021-04-01 | 2021-07-09 | 昊科微波科技(上海)有限公司 | Manufacturing method of flexible wire resistant to high temperature of 1200 DEG C |
-
2012
- 2012-05-21 CN CN 201220229286 patent/CN202694904U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105513667A (en) * | 2016-01-12 | 2016-04-20 | 郑飞 | Electrical cable |
| CN107887066A (en) * | 2017-11-03 | 2018-04-06 | 芜湖航天特种电缆厂股份有限公司 | Magnaflux, high temperature resistant harness |
| CN108598733A (en) * | 2018-04-12 | 2018-09-28 | 袁明磊 | A kind of conducting wire and igniter burner |
| CN113096894A (en) * | 2021-04-01 | 2021-07-09 | 昊科微波科技(上海)有限公司 | Manufacturing method of flexible wire resistant to high temperature of 1200 DEG C |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130123 Termination date: 20160521 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |