CN206477181U - A kind of high temperature resistant high tenacity aviation rope - Google Patents
A kind of high temperature resistant high tenacity aviation rope Download PDFInfo
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- CN206477181U CN206477181U CN201621471606.4U CN201621471606U CN206477181U CN 206477181 U CN206477181 U CN 206477181U CN 201621471606 U CN201621471606 U CN 201621471606U CN 206477181 U CN206477181 U CN 206477181U
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- insulation layer
- periphery
- central strand
- thermal insulation
- stock
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Abstract
The utility model discloses a kind of high temperature resistant high tenacity aviation rope, including heat insulation layer, thermal insulation layer, adhesive layer, auxiliary stock, central strand and steel wire, the central strand periphery is coated with multiple auxiliary stocks, the central strand is formed by 68 steel wire twistings, the auxiliary stock is formed by 57 steel wire twistings, the auxiliary stock periphery is coated with adhesive layer, and the adhesive layer periphery is provided with thermal insulation layer, and the thermal insulation layer periphery is coated with heat insulation layer.The utility model is formed by 68 steel wire twistings by the auxiliary stock and central strand of central strand periphery cladding and aids in stock to be formed by 57 steel wire twistings, the toughness of aviation rope can be greatly improved, bearing capacity is greatly improved, improve fatigue resistance and service life simultaneously, and pass through adhesive layer, its central strand can be preferably fixed together with auxiliary stock, and by thermal insulation layer and heat insulation layer, the heat-resisting quantity of aviation rope can be greatly improved.
Description
【Technical field】
The utility model is related to a kind of aviation rope, more particularly to a kind of high temperature resistant high tenacity aviation rope.
【Background technology】
Aviation, be it is a kind of be mankind's activity that is complicated and having strategic importance.Referring to aircraft, (air is empty in earth atmosphere
Between) in flying activity, and scientific research and education related to this, industrial manufacture, public transportation, air transport, national defense and military, political affairs
The various fields such as mansion management.By the utilization for air space and aircraft (airborne vehicle), aerospace activity can be subdivided into crowd
More independent industry and field, typically such as aviation, Civil Aviation Industry etc., in aviation field, aviation rope is
A kind of very common equipment, but traditional aviation rope heat-resisting quantity is not fine, and also toughness is nor very strong, in aviation
In field, it is often necessary in face of the challenge of high temperature, if being unable to high temperature resistant, it is likely that serious consequence can be brought.Therefore, we
Propose a kind of high temperature resistant high tenacity aviation rope.
【Utility model content】
Main purpose of the present utility model is to provide a kind of high temperature resistant high tenacity aviation rope, can effectively solve background skill
The problem of in art.
To achieve the above object, the technical scheme that the utility model is taken is：
A kind of high temperature resistant high tenacity aviation rope, including heat insulation layer, thermal insulation layer, adhesive layer, auxiliary stock, central strand and steel wire,
The central strand periphery is coated with multiple auxiliary stocks, and the central strand is formed by 6-8 root steel wire twistings, and the auxiliary stock is by 5-7
Root steel wire twisting is formed, and the auxiliary stock periphery is coated with adhesive layer, and the adhesive layer periphery is provided with thermal insulation layer, the thermal insulation layer
Periphery is coated with heat insulation layer.
Further, the auxiliary stock number of central strand periphery cladding is 5-7.
Further, the heat insulation layer is the high silica wool layer that surface scribbles foamed coating.
Further, the thermal insulation layer is aeroge carpet veneer.
Compared with prior art, the utility model has the advantages that：This kind of high temperature resistant high tenacity aviation rope, passes through
The auxiliary stock and central strand of central strand periphery cladding formed by 6-8 root steel wire twistings and aid in stock by 5-7 root steel wire twistings and
Into, the toughness of aviation rope can be greatly improved, bearing capacity is greatly improved, while fatigue resistance and service life are improved,
And by adhesive layer, its central strand can be preferably fixed together with auxiliary stock, and by thermal insulation layer and heat insulation layer,
The heat-resisting quantity of aviation rope can be greatly improved.
【Brief description of the drawings】
Fig. 1 is the overall cross-sectional view of the utility model high temperature resistant high tenacity aviation rope.
In figure：1st, heat insulation layer；2nd, thermal insulation layer；3rd, adhesive layer；4th, stock is aided in；5th, central strand；6th, steel wire.
【Embodiment】
To be easy to understand technological means, creation characteristic, reached purpose and effect of the utility model realization, below
With reference to embodiment, the utility model is expanded on further.
As shown in figure 1, a kind of high temperature resistant high tenacity aviation rope, including heat insulation layer 1, thermal insulation layer 2, adhesive layer 3, auxiliary stock 4,
Central strand 5 and steel wire 6, the periphery of central strand 5 are coated with multiple auxiliary stocks 4, and the central strand 5 is by the twisting of 6-8 roots steel wire 6
Into the auxiliary stock 4 is formed by the twisting of 5-7 roots steel wire 6, and auxiliary stock 4 periphery is coated with outside adhesive layer 3, the adhesive layer 3
Enclose provided with thermal insulation layer 2, the periphery of thermal insulation layer 2 is coated with heat insulation layer 1.
The utility model high temperature resistant high tenacity aviation rope, by the auxiliary stock 4 and central strand of the periphery of central strand 5 cladding by
The twisting of 6-8 roots steel wire 6 forms and aids in stock 4 to be formed by the twisting of 5-7 roots steel wire 6, can greatly improve the toughness of aviation rope, hold
Gravity is greatly improved, while improve fatigue resistance and service life, and by adhesive layer 3, can by its central strand 5 with
Auxiliary stock 4 is preferably fixed together, and by thermal insulation layer 2 and heat insulation layer 1, can greatly improve the high temperature resistant of aviation rope
Property.
Wherein, the auxiliary stock 4 of the periphery of central strand 5 cladding is 5-7, passes through the auxiliary stock 4 of the periphery of central strand 5 cladding
Number is 5-7, can greatly improve the toughness of aviation rope.
Wherein, the heat insulation layer 1 is the high silica wool layer that surface scribbles foamed coating, is scribbled by heat insulation layer 1 for surface
The high silica wool layer of foamed coating, can play good insulation effect.
Wherein, the thermal insulation layer 2 is aeroge carpet veneer, is aeroge carpet veneer by thermal insulation layer 2, can more preferably play heat-insulated
Effect.
General principle of the present utility model and principal character and advantage of the present utility model has been shown and described above.One's own profession
The technical staff of industry is it should be appreciated that the utility model is not restricted to the described embodiments, described in above-described embodiment and specification
Simply illustrate principle of the present utility model, on the premise of the utility model spirit and scope are not departed from, the utility model is also
Various changes and modifications are had, these changes and improvements are both fallen within the range of claimed the utility model.The utility model
Claimed scope is by appended claims and its equivalent thereof.
Claims (4)
1. a kind of high temperature resistant high tenacity aviation rope, including heat insulation layer（1）, thermal insulation layer（2）, adhesive layer（3）, auxiliary stock（4）, center
Stock（5）And steel wire（6）, it is characterised in that：The central strand（5）Periphery is coated with multiple auxiliary stocks（4）, the central strand（5）
By 6-8 root steel wires（6）Twisting is formed, the auxiliary stock（4）By 5-7 root steel wires（6）Twisting is formed, the auxiliary stock（4）Periphery
It is coated with adhesive layer（3）, the adhesive layer（3）Periphery is provided with thermal insulation layer（2）, the thermal insulation layer（2）Periphery is coated with heat insulation layer
（1）.
2. high temperature resistant high tenacity aviation rope according to claim 1, it is characterised in that：The central strand（5）Periphery cladding
Auxiliary stock（4）Number is 5-7.
3. high temperature resistant high tenacity aviation rope according to claim 1, it is characterised in that：The heat insulation layer（1）Applied for surface
There is the high silica wool layer of foamed coating.
4. high temperature resistant high tenacity aviation rope according to claim 1, it is characterised in that：The thermal insulation layer（2）For aeroge
Carpet veneer.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621471606.4U CN206477181U (en) | 2016-12-30 | 2016-12-30 | A kind of high temperature resistant high tenacity aviation rope |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621471606.4U CN206477181U (en) | 2016-12-30 | 2016-12-30 | A kind of high temperature resistant high tenacity aviation rope |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206477181U true CN206477181U (en) | 2017-09-08 |
Family
ID=59749659
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621471606.4U Expired - Fee Related CN206477181U (en) | 2016-12-30 | 2016-12-30 | A kind of high temperature resistant high tenacity aviation rope |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206477181U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110538945A (en) * | 2019-09-19 | 2019-12-06 | 中国人民解放军陆军装甲兵学院 | Refractory high-entropy alloy stranded wire material, application and preparation method thereof |
| WO2020192111A1 (en) * | 2019-03-28 | 2020-10-01 | 南通神马线业有限公司 | Nylon thread with super-high tension for parachute |
-
2016
- 2016-12-30 CN CN201621471606.4U patent/CN206477181U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020192111A1 (en) * | 2019-03-28 | 2020-10-01 | 南通神马线业有限公司 | Nylon thread with super-high tension for parachute |
| CN110538945A (en) * | 2019-09-19 | 2019-12-06 | 中国人民解放军陆军装甲兵学院 | Refractory high-entropy alloy stranded wire material, application and preparation method thereof |
| CN110538945B (en) * | 2019-09-19 | 2021-04-13 | 中国人民解放军陆军装甲兵学院 | Refractory high-entropy alloy stranded wire material, application and preparation method thereof |
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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: 20170908 Termination date: 20191230 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |