CN2458481Y - Ring-shaped pressure container with fibre coiled composite material rubber liner - Google Patents
Ring-shaped pressure container with fibre coiled composite material rubber liner Download PDFInfo
- Publication number
- CN2458481Y CN2458481Y CN 00267360 CN00267360U CN2458481Y CN 2458481 Y CN2458481 Y CN 2458481Y CN 00267360 CN00267360 CN 00267360 CN 00267360 U CN00267360 U CN 00267360U CN 2458481 Y CN2458481 Y CN 2458481Y
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- China
- Prior art keywords
- pressure container
- rubber liner
- composite material
- pressure vessel
- utility
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- 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.)
- Expired - Lifetime
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Abstract
The utility model relates to an annular pressure container with a fibre coiled composite material rubber liner. The inner surface of the annular pressure container 1 is provided with a rubber liner 2, a coiled structure layer 4 made from the fiber 3 coiled composite material is arranged outside the rubber liner, the annular pressure container 1 is provided with one joint 5 for media in and out at least, and the section of the annular pressure container is round or elliptic. The utility model has the advantages of light weight, low manufacturing cost, short production cycle, stable quality, good fatigue resistance, etc. The utility model solves the problem that a metallic vessel is easily destroyed in low pressure by the existing tiny defects and does not generate large quantity of antipersonnel fragments even the pressure container is ruined.
Description
The utility model belongs to a kind of toroidal pressure vessel.
Aeronautics and Astronautics and military field widespread demand toroidal pressure vessel, but because its structural feature is more special, traditional construction of pressure vessel material mainly is a metallic material.In manufacturing process, exist shortcomings such as quality of product is big, manufacture cost is high, the manufacture cycle is long, poor stability.And in a single day metal pressure container exists tiny flaw that the low pressure breakoff phenomenon can take place, and easily generation can lethal fragment, causes casualty accident.And can not reach Aeronautics and Astronautics and military field to its performance demands with the toroidal pressure vessel that other any single nonmetallic material are made.
The purpose of this utility model is a kind of pressure container with wound composite fiber material and rubber liner of design.This toroidal pressure vessel is organically combined by two kinds of nonmetallic material and makes.It should have product structure rationally, characteristics such as lighter weight, low cost of manufacture, with short production cycle, constant product quality.It also should solve canister and has tiny flaw and the low pressure breakoff phenomenon takes place, and produces the problem of a large amount of lethal fragments.
The purpose of this utility model realizes in the following manner: the internal surface of toroidal pressure vessel 1 is a rubber material inside liner 2, the construction layer 4 that intrinsic fiber 3 wound composites are made on the outside of rubber material inside liner 2, on toroidal pressure vessel 1, be provided with at least one medium turnover joint 5, be connected inside and outside joint 5 and the toroidal pressure vessel 1.
The rubber material inside liner 2 of the utility model toroidal pressure vessel 1 internal surface seals; The construction layer 4 that outer fiber 3 wound composites are made works to bear pressure.So it has product structure structure, light weight, low cost of manufacture, with short production cycle, advantage such as mass stability is high, fatigue performance is good.It has also solved canister and has had tiny flaw and the problem that low pressure is destroyed takes place.Even damaging, this container can not produce a large amount of lethal fragments yet.
Fig. 1 is a plan view of the present utility model, and Fig. 2 is the plan view of Fig. 1, and Fig. 3 is embodiment two a plan view.
Embodiment one: the cross section of the toroidal pressure vessel 1 of present embodiment is circular.The internal surface of toroidal pressure vessel 1 is a rubber material inside liner 2, the outside of rubber material inside liner 2 is winding structure layers 4 that intrinsic fiber 3 wound composites are made, on toroidal pressure vessel 1, be provided with two media turnover joints 5, be connected inside and outside joint 5 and the toroidal pressure vessel 1.
Embodiment two: present embodiment and embodiment one are different is that the cross section of toroidal pressure vessel 1 is for oval.Other composition is identical with embodiment one with annexation.
Claims (3)
1, pressure container with wound composite fiber material and rubber liner, the internal surface that it is characterized in that toroidal pressure vessel (1) is rubber material inside liner (2), the construction layer (4) that intrinsic fiber (3) wound composite is made on the outside of rubber material inside liner (2), on toroidal pressure vessel (1), be set with at least one medium turnover joint (5), be connected inside and outside joint (5) and the toroidal pressure vessel (1).
2, pressure container with wound composite fiber material and rubber liner according to claim 1, the cross section that it is characterized in that toroidal pressure vessel (1) is for circular.
3, pressure container with wound composite fiber material and rubber liner according to claim 1, the cross section that it is characterized in that toroidal pressure vessel (1) is for oval.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 00267360 CN2458481Y (en) | 2000-12-29 | 2000-12-29 | Ring-shaped pressure container with fibre coiled composite material rubber liner |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 00267360 CN2458481Y (en) | 2000-12-29 | 2000-12-29 | Ring-shaped pressure container with fibre coiled composite material rubber liner |
Publications (1)
Publication Number | Publication Date |
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CN2458481Y true CN2458481Y (en) | 2001-11-07 |
Family
ID=33621205
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN 00267360 Expired - Lifetime CN2458481Y (en) | 2000-12-29 | 2000-12-29 | Ring-shaped pressure container with fibre coiled composite material rubber liner |
Country Status (1)
Country | Link |
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CN (1) | CN2458481Y (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN100427822C (en) * | 2003-02-03 | 2008-10-22 | 国立大学法人九州大学 | Pressure shell, high-pressure tank with the pressure shell, and method and apparatus for manufacturing the high-pressure tank |
CN100430640C (en) * | 2006-11-06 | 2008-11-05 | 哈尔滨工业大学 | High pressure nitrogen storage bottle made of PBO fiber and carbon fiber composite material and its preparation method |
CN110869662A (en) * | 2017-07-06 | 2020-03-06 | 全耐塑料高级创新研究公司 | Improved pressure vessel |
CN114777008A (en) * | 2022-05-09 | 2022-07-22 | 光年探索(江苏)空间技术有限公司 | Ring pipe gas cylinder structure and manufacturing method thereof |
-
2000
- 2000-12-29 CN CN 00267360 patent/CN2458481Y/en not_active Expired - Lifetime
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN100427822C (en) * | 2003-02-03 | 2008-10-22 | 国立大学法人九州大学 | Pressure shell, high-pressure tank with the pressure shell, and method and apparatus for manufacturing the high-pressure tank |
CN100430640C (en) * | 2006-11-06 | 2008-11-05 | 哈尔滨工业大学 | High pressure nitrogen storage bottle made of PBO fiber and carbon fiber composite material and its preparation method |
CN110869662A (en) * | 2017-07-06 | 2020-03-06 | 全耐塑料高级创新研究公司 | Improved pressure vessel |
US11421825B2 (en) | 2017-07-06 | 2022-08-23 | Plastic Omnium New Energies France | Pressure vessel |
CN114777008A (en) * | 2022-05-09 | 2022-07-22 | 光年探索(江苏)空间技术有限公司 | Ring pipe gas cylinder structure and manufacturing method thereof |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C17 | Cessation of patent right | ||
CX01 | Expiry of patent term |
Expiration termination date: 20101229 Granted publication date: 20011107 |