SU433038A1 - S SECURITY OF CONTINUOUS MINING'S HIGHER RUBBER SLEEVES AT THE MELTED DOM - Google Patents
S SECURITY OF CONTINUOUS MINING'S HIGHER RUBBER SLEEVES AT THE MELTED DOMInfo
- Publication number
- SU433038A1 SU433038A1 SU1618768A SU1618768A SU433038A1 SU 433038 A1 SU433038 A1 SU 433038A1 SU 1618768 A SU1618768 A SU 1618768A SU 1618768 A SU1618768 A SU 1618768A SU 433038 A1 SU433038 A1 SU 433038A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- mandrel
- melted
- dom
- security
- rubber sleeves
- Prior art date
Links
Landscapes
- Heating, Cooling, Or Curing Plastics Or The Like In General (AREA)
- Shaping Of Tube Ends By Bending Or Straightening (AREA)
Description
Изобретение относитс к технологии непрерЫЕНОКз изготоЕлени резиноЕЫХ рукавов на выплавл емом полимерном дорне,в частности на трубчатом дорне изполиэтилена.This invention relates to the technology of the continuous manufacture of rubber hoses on a melted polymer mandrel, in particular on a tubular mandrel of polyethylene.
Известные способы непрерывно го изготовлени резиновых рукавов на выплавл емом дорне,например рукавов с металлическими и хлопчатобумажными оплетками,заключаютс в том,что на эластичном полимерном дорне производ т сборку и вул1сани зацию рукава с оплавлением дорна, с последующим удалением материала дорна из рукава.Known methods for the continuous manufacture of rubber hoses on a molded mandrel, such as metal and cotton braided hoses, consist in assembling and vulcanizing the elastic mandrel on an elastic polymer mandrel, followed by removal of the mandrel material from the sleeve.
Известные способы рассчитаны на применение сплошного шнурового дорна из полимерного материала,например из капрона,что приводит к увеличеншо расхода этото сравнительно дорогого по стоимости материале .The known methods are designed for the use of a continuous cord mandrel made of polymeric material, for example, caprone, which leads to an increase in the consumption of this material, which is relatively expensive in cost.
По придлагаемому способу примен ют дорн трубчатый из полиэтилена .According to the attached method, a tubular polyethylene is used.
Этот способ обеспечит уменьшекие расхода материала на.изготовление дорна при непрерывном производстве рукавовThis method will provide reduced material consumption for the manufacture of the mandrel with the continuous production of hoses
Сущность изобретени заключаетс в томучто на трубчатом полимерном дорне с помощью известных машин и устройств производ т сборку и вулканизацию рукава,например рукава с металлическими и хлопчатобумажными оплетками,с .оплавлением дорна в процессе вулканизации и последующим удалением материала дорна из рукава.The invention consists in tomofto on a tubular polymer mandrel using known machines and devices, assembling and curing the sleeve, for example, sleeves with metal and cotton braids, melting the mandrel during the vulcanization process and then removing the material of the mandrel from the sleeve.
Благодар трубчатому дорну из полиэтилена при непрерывной сборке и вулканизации рукавов получаютDue to the tubular mandrel made of polyethylene with continuous assembly and vulcanization of the sleeves receive
0 рукава любой необходимой длины и конструкции при одновременном изготовлении дорна и рукава,уменьшаютс потери сырь и материалов путем исключени операции подрезки0 sleeves of any necessary length and design, while making the mandrel and sleeve, reduce the loss of raw materials and materials by eliminating the trimming operation
5 и обрезки рукавов,так как при вул3 ,4330385 and trim the sleeves, as in Vol3, 433038
канизацйи рЗгкаЕов трубчатый гГоли-ПРЕДМЕТ ИЗОБРЕТЕНЖkazizatsy rzgkaeov tubular gGoli SUBJECT OF THE INVENTION
этиленоБЫй дррн оплаЕл етс щед :СпособнепрерывногоизготОЕле оэ ом ,& тадлическ ми и хлопчатобумажшмиEthylated drrn is generous: Continuous manufacturing, & cotton and cotton
pCS SeTp Sf1l& sS дн-. |лРП | ° АП|:гГри аpCS SeTp Sf1l & sS days-. | LRP | ° AP |: gGry a
. prs;§ s Hfssr. prs; § s Hfssr
S/l g HLSViB f Sr S / l g HLSViB f Sr
оплетками заключаю1щшс Е том,чтоbraids conclude with the fact that
- SSSa- SSSa
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU1618768A SU433038A1 (en) | 1971-02-10 | 1971-02-10 | S SECURITY OF CONTINUOUS MINING'S HIGHER RUBBER SLEEVES AT THE MELTED DOM |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU1618768A SU433038A1 (en) | 1971-02-10 | 1971-02-10 | S SECURITY OF CONTINUOUS MINING'S HIGHER RUBBER SLEEVES AT THE MELTED DOM |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| SU433038A1 true SU433038A1 (en) | 1974-06-25 |
Family
ID=20465224
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SU1618768A SU433038A1 (en) | 1971-02-10 | 1971-02-10 | S SECURITY OF CONTINUOUS MINING'S HIGHER RUBBER SLEEVES AT THE MELTED DOM |
Country Status (1)
| Country | Link |
|---|---|
| SU (1) | SU433038A1 (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2445206C2 (en) * | 2006-07-06 | 2012-03-20 | Эйрбас Оперейшинз Гмбх | Method of producing structural component from composite material reinforced by fibers using formed core, and formed core |
| US8500085B2 (en) | 2006-07-06 | 2013-08-06 | Airbus Operations Gmbh | Method for manufacturing a composite fiber component for aerospace |
| US8906489B2 (en) | 2006-07-06 | 2014-12-09 | Airbus Operations Gmbh | Method for producing a fibre composite component for aviation and spaceflight |
| US9492974B2 (en) | 2006-07-06 | 2016-11-15 | Airbus Operations Gmbh | Method for producing a fiber composite component for aviation and spaceflight |
| US10207463B2 (en) | 2006-07-06 | 2019-02-19 | Airbus Operations Gmbh | Method for producing a fiber composite component for aerospace |
-
1971
- 1971-02-10 SU SU1618768A patent/SU433038A1/en active
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2445206C2 (en) * | 2006-07-06 | 2012-03-20 | Эйрбас Оперейшинз Гмбх | Method of producing structural component from composite material reinforced by fibers using formed core, and formed core |
| US8500085B2 (en) | 2006-07-06 | 2013-08-06 | Airbus Operations Gmbh | Method for manufacturing a composite fiber component for aerospace |
| US8906489B2 (en) | 2006-07-06 | 2014-12-09 | Airbus Operations Gmbh | Method for producing a fibre composite component for aviation and spaceflight |
| US9492974B2 (en) | 2006-07-06 | 2016-11-15 | Airbus Operations Gmbh | Method for producing a fiber composite component for aviation and spaceflight |
| US10207463B2 (en) | 2006-07-06 | 2019-02-19 | Airbus Operations Gmbh | Method for producing a fiber composite component for aerospace |
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