EP0344025B1 - Speicherungsbehälter für eine Flüssigkeit unter Druck - Google Patents
Speicherungsbehälter für eine Flüssigkeit unter Druck Download PDFInfo
- Publication number
- EP0344025B1 EP0344025B1 EP89401095A EP89401095A EP0344025B1 EP 0344025 B1 EP0344025 B1 EP 0344025B1 EP 89401095 A EP89401095 A EP 89401095A EP 89401095 A EP89401095 A EP 89401095A EP 0344025 B1 EP0344025 B1 EP 0344025B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- envelope
- container according
- end part
- thickness
- bulged
- 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.)
- Expired - Lifetime
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C1/00—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge
- F17C1/14—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge constructed of aluminium; constructed of non-magnetic steel
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C1/00—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge
- F17C1/02—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge involving reinforcing arrangements
- F17C1/04—Protecting sheathings
- F17C1/06—Protecting sheathings built-up from wound-on bands or filamentary material, e.g. wires
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/01—Shape
- F17C2201/0104—Shape cylindrical
- F17C2201/0109—Shape cylindrical with exteriorly curved end-piece
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/05—Size
- F17C2201/056—Small (<1 m3)
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/05—Size
- F17C2201/058—Size portable (<30 l)
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0602—Wall structures; Special features thereof
- F17C2203/0607—Coatings
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0602—Wall structures; Special features thereof
- F17C2203/0612—Wall structures
- F17C2203/0614—Single wall
- F17C2203/0619—Single wall with two layers
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0602—Wall structures; Special features thereof
- F17C2203/0612—Wall structures
- F17C2203/0614—Single wall
- F17C2203/0621—Single wall with three layers
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0634—Materials for walls or layers thereof
- F17C2203/0636—Metals
- F17C2203/0646—Aluminium
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0634—Materials for walls or layers thereof
- F17C2203/0658—Synthetics
- F17C2203/0663—Synthetics in form of fibers or filaments
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
- F17C2205/03—Fluid connections, filters, valves, closure means or other attachments
- F17C2205/0302—Fittings, valves, filters, or components in connection with the gas storage device
- F17C2205/0305—Bosses, e.g. boss collars
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2209/00—Vessel construction, in particular methods of manufacturing
- F17C2209/21—Shaping processes
- F17C2209/2154—Winding
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2221/00—Handled fluid, in particular type of fluid
- F17C2221/01—Pure fluids
- F17C2221/011—Oxygen
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2221/00—Handled fluid, in particular type of fluid
- F17C2221/01—Pure fluids
- F17C2221/013—Carbone dioxide
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2221/00—Handled fluid, in particular type of fluid
- F17C2221/01—Pure fluids
- F17C2221/014—Nitrogen
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2221/00—Handled fluid, in particular type of fluid
- F17C2221/03—Mixtures
- F17C2221/031—Air
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/01—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
- F17C2223/0107—Single phase
- F17C2223/0123—Single phase gaseous, e.g. CNG, GNC
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2260/00—Purposes of gas storage and gas handling
- F17C2260/01—Improving mechanical properties or manufacturing
- F17C2260/011—Improving strength
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2260/00—Purposes of gas storage and gas handling
- F17C2260/01—Improving mechanical properties or manufacturing
- F17C2260/012—Reducing weight
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2260/00—Purposes of gas storage and gas handling
- F17C2260/01—Improving mechanical properties or manufacturing
- F17C2260/017—Improving mechanical properties or manufacturing by calculation
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2270/00—Applications
- F17C2270/01—Applications for fluid transport or storage
- F17C2270/0102—Applications for fluid transport or storage on or in the water
- F17C2270/0131—Submarines
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2270/00—Applications
- F17C2270/01—Applications for fluid transport or storage
- F17C2270/0186—Applications for fluid transport or storage in the air or in space
- F17C2270/0194—Applications for fluid transport or storage in the air or in space for use under microgravity conditions, e.g. space
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2270/00—Applications
- F17C2270/05—Applications for industrial use
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2270/00—Applications
- F17C2270/07—Applications for household use
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2270/00—Applications
- F17C2270/07—Applications for household use
- F17C2270/0781—Diving equipments
Definitions
- the present invention relates to a container for the storage of pressurized fluid.
- the invention relates to so-called “bottle” containers for storing gases, such as air, oxygen, nitrogen, carbon dioxide, used in different industrial sectors .
- such a container for the storage of gas under pressure generally comprising an inner casing having a central cylindrical part and two curved end parts. , and a hooping of resistant fibers coated with a curable binder, surrounding said envelope.
- the envelope is of constant thickness, both in the cylindrical central part and in the two curved end parts.
- document GB-A-1 072 420 describes a container, in particular intended to form the envelope of a rocket engine, comprising an inner envelope of revolution form around a longitudinal axis XX ′, having a cylindrical central part and two end parts, at least one of said end parts being curved outwards and having an external contour which has, in longitudinal section, an at least approximately elliptical shape, a hoop of resistant fibers coated with 'a curable binder surrounding said envelope and having at least one planetary winding leaving free, at said curved end portion, a cap centered on said axis X, X ′.
- the present invention relates to a container for the storage of pressurized fluid, of the type described for another use by document GB-A-1 072 420 and making it possible to avoid the drawback mentioned above with regard to the container of the document US-A-3 508 677. It relates to a pressurized fluid storage container adapted to present the best possible weight / resistance ratio.
- the container according to the invention has the best possible weight / resistance ratio, since it does not include any additional thickness in the central cylindrical part of the envelope.
- the elliptical shape of the curved end portions makes it possible to obtain a greater volume, for example compared to a hemispherical shape, for the same length, that is to say the same size, of the container.
- this elliptical shape provides better seating for the planetary winding.
- said ratio G is such that: 0.34 ⁇ G ⁇ 0.35.
- the inner contour of said curved end portion of the envelope has, in longitudinal section, an at least approximately elliptical shape.
- the two end parts of the envelope are curved outwards, at least one of said parts being provided with a filling orifice.
- an end portion of the envelope has a neck, and, at least at the periphery of said end portion, the outer contour of the latter has, in longitudinal section, a at least approximately elliptical shape according to formula (I) and, at least at said periphery, the thickness of said end portion varies according to formula (II).
- the internal contour of the latter has, in longitudinal section, an at least approximately elliptical shape.
- said hooping rests on said neck.
- said hooping comprises at least one circumferential winding on said planetary winding, in correspondence with at least the cylindrical central part of the envelope.
- said hooping consists of an alternation of planetary windings and circumferential windings.
- said envelope can be made of metal, for example aluminum.
- Figure 1 is a longitudinal sectional view of a container according to the invention.
- FIG. 2 shows, on an enlarged scale, a curved end portion of the container of FIG. 1.
- Figure 3 is a view similar to Figure 2 showing an alternation of planetary windings and circumferential windings.
- Figure 4 is a view similar to Figure 1 of a container, according to the invention, having a neck.
- the container 1 for the storage of pressurized fluid comprises an inner casing 2, for example made of aluminum, of shape of revolution around a longitudinal axis X, X ′, having a central part cylindrical 2a and two end portions 2b curved outwards.
- One of the end parts 2b, on the right in FIG. 1 has an orifice 3 for filling the container with a fluid.
- the container 1 has a hooping 4 of resistant fibers (for example glass, Kevlar (registered trademark), carbon, boron) coated with a curable binder, surrounding the envelope 2.
- the hooping 4 shown in Figures 1 and 2 comprises a single planetary winding 5, leaving open, at the end portions 2b, a cap 6 centered on the axis X, X ′.
- the hooping 4 generally consists of an alternation of planetary windings 5 and circumferential windings 7. Each of the latter applies to the planetary winding 5 immediately below , in correspondence with the cylindrical central part 2a of the envelope 2.
- said ratio G can be such that: 0.34 ⁇ G ⁇ 0.35
- each curved end portion 2b of the envelope 2 has, in longitudinal section, an at least approximately elliptical shape.
- FIG. 4 illustrates another example of embodiment of a container 1 according to the invention, in which an end portion 2b curved towards the outside has a neck 10, the planetary winding 5 of the hoop 4 resting on the neck 10.
- the outer contour 12 of the latter has, in longitudinal section, an at least approximately elliptical shape according to formula (I) and, at least at said periphery 11, the thickness of said end portion 2b varies according to formula (II).
- the inner contour 13 of the latter has, in longitudinal section, an at least approximately elliptical shape.
Claims (10)
- Behälter zur Lagerung von mit Druck beaufschlagten flüssigen oder gasförmigen Medien, der mit einer Innenverkleidung in Umlaufsform um die Längsachse X, X′ ausgebildet ist, der einen mittleren Zylinderteil sowie zwei Endteile aufweist, von denen zumindest einer nach außen gewölbt ist, und einen äußeren Umriß aufweist, der im Längsschnitt eine zumindest annähernd elliptische Form hat und der eine Bandagierung aus widerstandsfähigen, mit einem härtbaren Bindemittel umhüllten Fasern aufweist, die die Verkleidung umgibt und zumindest eine planetare oder umlaufende Wicklung besitzt, die am gewölbten Endteil ein auf die Achse X, X′ zentrierte Kappe freiläßt, dadurch gekennzeichnet,
daß der zumindest annähernd elliptische äußere Umriß (8) des gewölblen Endteils (2b) der Verkleidung (2) so ist, daß die Beziehung G der halben kleinen Achse zur großen AchseRi = dem Abstand zur Axhse X, X′ von der Stelle des äußeren Umrisses (8) des gewölbten Endteils (2b), an dem die Dicke ei gemessen wird,e = der Dicke der Verkleidung (2) in deren Mittelzylinderteil,R = dem Aussenradius des Mittelzylinderteils (2a) der Verkleidung (2),R₁ = dem Grundflächenradius der Kappe (6) unde₁ = der Dicke der Verkleidung (2) für Ri = R₁,wobei die Dicke der Kappe (6) zumindest gleich e₁ ist. - Behälter nach einem der vorhergehenden Ansprüche 1 oder 2, dadurch gekennzeichnet, daß der innere Umriß (9) des gewölbten Endteils (2b) der Verkleidung (2) im Längsschnitt eine zumindest annähernde elliptische Form aufweist.
- Behälter nach einem der vorhergehenden Ansprüche 1 bis 3, dadurch gekennzeichnet, daß die beiden Endteile (2b) der Verkleidung (2) nach außen gewölbt sind, wobei zumindest einer dieser Teile mit einer Einfüllöffnung (3, 10) versehen ist.
- Behälter nach Anspruch 4, dadurch gekennzeichnet, daß einer der Endteile (2b) der Verkleidung (2) einen engen Hals (10) aufweist und daß zumindest am Umfang (11) des Endteils dessen äußerer Umriß im Längsschnitt eine zumindest annähernde Ellipsenform nach der Formel (I) hat und die Dicke des Endteils (2b) zumindest am Umfang nach der Formel (II) variiert.
- Behälter nach Anspruch 5, dadurch gekennzeichnet, daß zumindest auf seinem Umfang (11) des den engen Hals (10) aufweisende Endteils (2b) dessen innerer Umriß (13) im Längsschnitt eine zumindest annähernd elliptische Form hat.
- Behälter nach einem der vorhergehenden Ansprüche 5 oder 6, dadurch gekennzeichnet, daß die Bandagierung (4) sich an den engen Hals (10) anlehnt.
- Behälter nach einem der vorhergehenden Ansprüche 1 bis 7, dadurch gekennzeichnet, daß die Bandagierung (4) zumindest eine Umfangswicklung (7) auf der planetaren oder umlaufenden Wicklung (5) in Entsprechung mit zumindest dem Mittelzylinderteil (2a) der Verkleidung (2) aufweist.
- Behälter nach Anspruch 8, dadurch gekennzeichnet, daß die Bandagierung (4) aus abwechselnden planetaren oder umlaufenden Wicklungen (5) und Umfangswicklungen (7) gebildet ist.
- Behälter nach einem der vorhergehenden Ansprüche 1 bis 9, dadurch gekennzeichnet, daß die Verkleidung (2) aus Metall, beispielshalber aus Aluminium hergestellt wird.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AT89401095T ATE84606T1 (de) | 1988-04-27 | 1989-04-19 | Speicherungsbehaelter fuer eine fluessigkeit unter druck. |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8805618A FR2630810B1 (fr) | 1988-04-27 | 1988-04-27 | Recipient pour le stockage de fluide sous pression |
FR8805618 | 1988-04-27 |
Publications (2)
Publication Number | Publication Date |
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EP0344025A1 EP0344025A1 (de) | 1989-11-29 |
EP0344025B1 true EP0344025B1 (de) | 1993-01-13 |
Family
ID=9365747
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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EP89401095A Expired - Lifetime EP0344025B1 (de) | 1988-04-27 | 1989-04-19 | Speicherungsbehälter für eine Flüssigkeit unter Druck |
Country Status (11)
Country | Link |
---|---|
US (1) | US5018638A (de) |
EP (1) | EP0344025B1 (de) |
JP (1) | JP2714434B2 (de) |
AT (1) | ATE84606T1 (de) |
CA (1) | CA1312295C (de) |
DE (2) | DE68904354T2 (de) |
DK (1) | DK167506B1 (de) |
ES (1) | ES2020903T3 (de) |
FR (1) | FR2630810B1 (de) |
GR (2) | GR910300090T1 (de) |
NO (1) | NO170171C (de) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10940341B2 (en) | 2013-03-06 | 2021-03-09 | Airbus Canada Limited Partnership | Interface between fire suppressant conduit and cargo compartment of an aircraft |
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FR2668098A1 (fr) * | 1990-10-17 | 1992-04-24 | Aerospatiale | Procede pour fretter et maintenir sous pression un noyau par une enveloppe en materiau composite et appareillage pour la mise en óoeuvre d'un tel procede. |
WO1994012396A1 (en) * | 1992-11-20 | 1994-06-09 | Ngv Systems, Inc. | Compressed gas container and method of manufacture |
EP0842696B1 (de) * | 1996-11-14 | 2004-11-10 | Instituut Voor Agrotechnologisch Onderzoek (Ato-Dlo) | Hochdruckreaktor |
DE19711844B4 (de) * | 1997-03-21 | 2005-06-02 | Metall-Spezialrohr Gmbh | Verfahren zum Herstellen eines Druckgasbehälters |
NO315248B1 (no) * | 2000-12-15 | 2003-08-04 | Knutsen Oas Shipping As | Anordning ved gassflaske |
DE102006006902B4 (de) * | 2006-02-09 | 2008-02-21 | Gräfenthaler Kunststofftechnik GmbH | Druckbehälter aus Kunststoff und Verfahren zu seiner Herstellung |
DE102006038713A1 (de) * | 2006-05-10 | 2007-11-29 | Schunk Kohlenstofftechnik Gmbh | Druckfester fluidbeaufschlagter Körper |
PL206178B1 (pl) * | 2007-01-25 | 2010-07-30 | Stako Irena Staniuk Jacek Staniuk Marek Staniuk Spółka Jawnastako Irena Staniuk Jacek Staniuk Marek Staniuk Spółka Jawna | Zbiornik kompozytowy |
US8474647B2 (en) * | 2008-02-08 | 2013-07-02 | Vinjamuri Innovations, Llc | Metallic liner with metal end caps for a fiber wrapped gas tank |
DE102010017413B4 (de) * | 2010-06-17 | 2012-08-30 | Xperion Gmbh | Druckbehälter zum Speichern eines Fluides |
WO2013026140A1 (en) * | 2011-08-22 | 2013-02-28 | Tranzgaz Inc. | Method of fabricating type 4 cylinders and arranging in transportation housings for transport of gaseous fluids |
CN106662290B (zh) * | 2014-08-04 | 2019-01-22 | 日产自动车株式会社 | 高压罐和高压罐制造方法 |
JP6381563B2 (ja) * | 2016-03-01 | 2018-08-29 | 株式会社日本製鋼所 | 圧力容器およびフープラップ複合圧力容器 |
KR20180017377A (ko) * | 2016-08-09 | 2018-02-21 | 현대자동차주식회사 | 고압 용기 |
JP7066995B2 (ja) * | 2017-08-10 | 2022-05-16 | トヨタ自動車株式会社 | 高圧容器 |
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US2744043A (en) * | 1950-01-23 | 1956-05-01 | Fels & Company | Method of producing pressure containers for fluids |
US2848133A (en) * | 1954-10-28 | 1958-08-19 | Einar M Ramberg | Pressure vessels and methods of making such vessels |
US3047191A (en) * | 1957-11-26 | 1962-07-31 | Hercules Powder Co Ltd | Filament wound vessels and methods for forming same |
NL269849A (de) * | 1960-10-05 | |||
US3137405A (en) * | 1961-12-18 | 1964-06-16 | North American Aviation Inc | Pressure vessel |
US3303079A (en) * | 1963-08-23 | 1967-02-07 | Richard P Carter | Method of manufacture of rocket chambers having an integral insulator or liner |
US3321101A (en) * | 1964-08-13 | 1967-05-23 | James R Griffith | Filament-wound hollow cylindrical articles |
GB1072420A (en) * | 1964-12-21 | 1967-06-14 | Aerojet General Co | Fibre pressure vessel |
US3358867A (en) * | 1965-04-07 | 1967-12-19 | Union Carbide Corp | Double-walled thermally insulated container |
US3508677A (en) * | 1968-08-20 | 1970-04-28 | Whittaker Corp | Vessel for storing high-pressure gases |
US3815773A (en) * | 1971-05-17 | 1974-06-11 | Brunswick Corp | Cyclic pressure vessel |
US3843010A (en) * | 1971-10-13 | 1974-10-22 | Brunswick Corp | Metal lined pressure vessel |
US3907149A (en) * | 1971-10-26 | 1975-09-23 | Amalga Corp | Pressure vessel having a sealed port |
US4391301A (en) * | 1981-08-27 | 1983-07-05 | A. O. Smith Corporation | Hole reinforcement |
US4438858A (en) * | 1982-02-03 | 1984-03-27 | Brunswick Corporation | Filament wound vessel with improved polar fitting |
US4785956A (en) * | 1982-08-23 | 1988-11-22 | Essef Industries, Inc. | Tank fitting for a filament-wound vessel |
US4619374A (en) * | 1984-05-21 | 1986-10-28 | Ecodyne Corporation | Pressure vessel with an improved sidewall structure |
FR2575966B1 (fr) * | 1985-01-15 | 1987-12-18 | Commissariat Energie Atomique | Procede de bobinage d'un recipient |
SE452284B (sv) * | 1986-03-10 | 1987-11-23 | Saab Composite Ab | Tryckkerl av kompositmaterial med i lindningen infogade gavelstycken |
DE3631975A1 (de) * | 1986-09-19 | 1988-04-07 | Eugen Ehs | Trocknerbehaelter fuer eine klimaanlage |
-
1988
- 1988-04-27 FR FR8805618A patent/FR2630810B1/fr not_active Expired - Fee Related
-
1989
- 1989-04-11 US US07/336,129 patent/US5018638A/en not_active Expired - Lifetime
- 1989-04-12 DK DK174089A patent/DK167506B1/da not_active IP Right Cessation
- 1989-04-19 EP EP89401095A patent/EP0344025B1/de not_active Expired - Lifetime
- 1989-04-19 DE DE8989401095T patent/DE68904354T2/de not_active Expired - Fee Related
- 1989-04-19 DE DE198989401095T patent/DE344025T1/de active Pending
- 1989-04-19 AT AT89401095T patent/ATE84606T1/de not_active IP Right Cessation
- 1989-04-19 ES ES198989401095T patent/ES2020903T3/es not_active Expired - Lifetime
- 1989-04-26 JP JP1104810A patent/JP2714434B2/ja not_active Expired - Fee Related
- 1989-04-26 NO NO891736A patent/NO170171C/no not_active IP Right Cessation
- 1989-04-27 CA CA000598114A patent/CA1312295C/fr not_active Expired - Fee Related
-
1991
- 1991-12-10 GR GR91300090T patent/GR910300090T1/el unknown
-
1993
- 1993-01-28 GR GR930400182T patent/GR3006935T3/el unknown
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10940341B2 (en) | 2013-03-06 | 2021-03-09 | Airbus Canada Limited Partnership | Interface between fire suppressant conduit and cargo compartment of an aircraft |
Also Published As
Publication number | Publication date |
---|---|
NO170171B (no) | 1992-06-09 |
DE68904354D1 (de) | 1993-02-25 |
FR2630810B1 (fr) | 1990-08-10 |
NO170171C (no) | 1992-09-16 |
ES2020903A4 (es) | 1991-10-16 |
DE68904354T2 (de) | 1993-05-13 |
US5018638A (en) | 1991-05-28 |
NO891736D0 (no) | 1989-04-26 |
DK174089A (da) | 1989-10-28 |
NO891736L (no) | 1989-10-30 |
ES2020903T3 (es) | 1993-07-16 |
DK174089D0 (da) | 1989-04-12 |
JP2714434B2 (ja) | 1998-02-16 |
ATE84606T1 (de) | 1993-01-15 |
DE344025T1 (de) | 1992-01-16 |
GR910300090T1 (en) | 1991-12-10 |
FR2630810A1 (fr) | 1989-11-03 |
JPH01316598A (ja) | 1989-12-21 |
EP0344025A1 (de) | 1989-11-29 |
CA1312295C (fr) | 1993-01-05 |
GR3006935T3 (de) | 1993-06-30 |
DK167506B1 (da) | 1993-11-08 |
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