EP0707697A1 - Reservoir de carburant sous pression - Google Patents

Reservoir de carburant sous pression

Info

Publication number
EP0707697A1
EP0707697A1 EP94920333A EP94920333A EP0707697A1 EP 0707697 A1 EP0707697 A1 EP 0707697A1 EP 94920333 A EP94920333 A EP 94920333A EP 94920333 A EP94920333 A EP 94920333A EP 0707697 A1 EP0707697 A1 EP 0707697A1
Authority
EP
European Patent Office
Prior art keywords
vessel
pressurized fuel
enclosure
vessel according
annular portion
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.)
Withdrawn
Application number
EP94920333A
Other languages
German (de)
English (en)
Other versions
EP0707697A4 (fr
Inventor
Donald Scott Robinson
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of EP0707697A1 publication Critical patent/EP0707697A1/fr
Publication of EP0707697A4 publication Critical patent/EP0707697A4/en
Withdrawn legal-status Critical Current

Links

Classifications

    • 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
    • F17C1/08—Integral reinforcements, e.g. ribs
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
    • B60K15/00—Arrangement in connection with fuel supply of combustion engines or other fuel consuming energy converters, e.g. fuel cells; Mounting or construction of fuel tanks
    • B60K15/03—Fuel tanks
    • 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
    • F17C2201/0133—Shape toroidal
    • 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
    • F17C2201/0147—Shape complex
    • F17C2201/0152—Lobes
    • 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
    • F17C2201/0147—Shape complex
    • F17C2201/0166—Shape complex divided in several chambers
    • 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
    • F17C2201/0147—Shape complex
    • F17C2201/0171—Shape complex comprising a communication hole between chambers
    • 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
    • F17C2201/03—Orientation
    • F17C2201/032—Orientation with substantially vertical main axis
    • 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)
    • 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
    • F17C2203/0639—Steels
    • F17C2203/0643—Stainless steels
    • 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
    • F17C2209/22—Assembling processes
    • F17C2209/221—Welding
    • 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
    • F17C2260/018—Adapting dimensions
    • 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
    • F17C2270/0165—Applications for fluid transport or storage on the road
    • F17C2270/0168—Applications for fluid transport or storage on the road by vehicles

Definitions

  • the present invention relates to a pressurized fuel vessel which, while it is adapte for automotive use, may be used in other areas.
  • GB 2095808 discloses a toroidal vessel and NL 7703630 discloses a somewhat squashed substantially toroidal vessel in -which the axis of the vessel is sealed off by a sleeve to define a toroidal chamber for the fuel.
  • a pressurized fuel vessel for automotive or other use having opposed axial end walls connected at or adjacent an outer periphery to define an enclosed chamber, said vessel being of greater diametrical dimension than axial dimension, with internal reinforcing means extending between the opposed axial end walls, the internal reinforcing means comprising at least one reinforcing wall means which extends within the chamber at least substantially about an axis of the vessel intermediate the axis and the outer periphery, and the at least one reinforcing wall means being adapted to permit pressurized fuel to flow between portions of the chamber respectively disposed radially inwardly and radially outwardly thereof.
  • the present invention is directed to an improvement of the embodiments of pressurized fuel vessel described in my aforementioned earlier patent applications although many of the optional features described therein may be adopted with the present invention and my earlier patent applications are therefore incorporated herein by reference.
  • a pressurized fuel vessel for automotive or other use having opposed axial end walls connected at or adjacent an outer periphery to define an enclosed chamber, said vessel being of greater diametrical dimension (as herein defined) than axial dimension, and wherein internal reinforcing means extends between the opposed axial end walls, said internal reinforcing means comprising a reinforcing wall which extends within the chamber about an axis of the vessel intermediate the axis and the outer periphery, said reinforcing wall being adapted to permit pressurized fuel to flow between portions of the chamber respectively disposed radially inwardly and radially outwardly thereof, wherein said vessel comprises a preformed enclosure having opposed ends and a peripheral wall defining, respectively, radially inner portions of the opposed axial end walls of the vessel and the reinforcing wall whereby the enclosure forms the radially inwardly disposed portion of the chamber, and said vessel further comprises an annular portion secured to the enclosure to form the radially outwardly disposed portion
  • preformed enclosure as used in "preformed enclosure” herein should be constru merely to mean the enclosure is formed at some stage before the annular portion secured to the enclosure.
  • the pressurized fuel vessel in accordance with the invention may advantageously be sized to fit into a spare wheel well in the bo of the automobile.
  • the well may be provided in the floor of t boot or, for example, in a wing of the automobile in which case the vessel woul likely only be partially received in the well in an upright manner.
  • th fuel vessel may be supported externally, as for example in a truck.
  • the vessel preferably has a substantially circular cross-section (optionally with segmental portion removed therefrom to allow the vessel to fit better in a well in wing of an automobile) and the term "diametrical dimension" should be construe in relation to the smallest circle within which the vessel can be located.
  • th cross-section may be rectangular or any other non-circular cross-section, such ellipsoidal, if desired.
  • the axis about which the reinforcing wall extends will usual be the central axis of such smallest circle, but not necessarily, depending upon th shape of the annular portion.
  • the term “annular portion” should be construe merely as meaning that said portion extends about the preformed enclosure.
  • Th preformed enclosure may itself have any suitable cross-section, but preferabl circular.
  • the diametrical dimension of the fu vessel is preferably at least twice the axial dimension, and, for example, th respective dimensions may be 600 mm and 240 mm, but where the vessel is intende to fit in the spare wheel well the dimensions may be determined by the size of th well.
  • the internal reinforcing means is provided to reduce the minimum permissible thickness of the opposed axial end walls of the vessel.
  • the internal reinforcing means may include additional reinforcing means to the reinforcing wall, for example another reinforcing wall and/or one or more columns which extend parallel to the axis of the vessel and which are welded or otherwise secured to the opposed axial end walls.
  • One column may be on the axis of the vessel and/or plural columns may be equally angularly spaced about the axis.
  • the fuel vessel may be secured in position in the automobile or other support by, for example external strapping, but in one embodiment the or at least one of the columnar reinforcing means projects through at least one of the opposed axial end walls and may be threaded exteriorly of the chamber to facilitate securement of the vessel either directly to the support or through appropriate strapping.
  • the or at least one of the columnar reinforcing means may be hollow and open at each end to the exterior of the vessel to receive a locating bolt or stud therethrough.
  • the outer periphery of the vessel is most preferably defined by a substantially axially extending outer wall which may be strengthened if necessary by, for example, giving it a rippled configuration or by making it externally convex.
  • the preformed enclosure is conveniently formed in steel and may have convex opposed ends to increase their strength. Since the pressure on both sides of the peripheral wall of the preformed enclosure will be the same in use of the vessel, no special reinforcing of the peripheral wall of the preformed enclosure is required.
  • the peripheral wall of the -preformed enclosure is substantially cylindrical.
  • the preformed enclosure may be formed in a variety of ways -which will be well understood by those skilled in the art, but in a preferred embodiment it is formed as two shells which are welded together aroimd the peripheral wall, most preferably as two substantially identical shells which are welded together along a diametrical plane which intersects the centre of the preformed enclosure.
  • the two shells need not be substantially identical, and one of the. shells may comprise a greater part of the peripheral wall than the other, or all of the peripheral wall, but preferably the two shells are welded together along a diametrical plane.
  • the annular portion of the vessel may also conveniently be formed in steel and is most advantageously welded to the preformed enclosure.
  • the annular portion radially inwardly overlaps the peripheral wall of the preformed enclosure and is secured at each end to the respective opposed end of the preformed enclosure.
  • the radially outer portions of the opposed axial end walls of the vessel defined by the annular portion are conve
  • annular portion With the annular portion overlapping the preformed enclosure, it is necessary to form the annular portion in at least two parts which are secured together, preferably by welding, around the preformed enclosure.
  • two parts are formed as substantially identical shells which are welded together on the outer periphery of the vessel along a diametrical plane which intersects the centre of the vessel.
  • the two shells need not be substantially identical, and one of the shells may comprise a greater part of the peripheral wall than the other, or all of the peripheral wall, but preferably the two shells are welded together along a diametrical plane.
  • Figure 1 is a sectional view of the vessel taken along the axial plane I-I in
  • Figure 2 is a plan view of the vessel.
  • the vessel 10 is formed of mild steel and comprises a preformed inner enclosure 12 and an annular outer enclosure 14.
  • the preformed enclosure has a cylindrical peripheral wall 16 and opposed convex end walls 18 and 20.
  • the inner enclosure is formed in two substantially identical halves which are secured together along a diametrical plane which intersects the centre of the vessel by a joggle-butt weld 22.
  • the peripheral wall 16 has a variety of openings therethrough, 24, 26, 28 and 30, to allow fluid flow therethrough between the inner enclosure 12 and outer enclosure 14.
  • the outer enclosure 14 is formed from two substantially identical annular shells 32 and 34 which are welded together at a joggle-butt joint 36 in the axially extending peripheral wall 38 of the vessel 10.
  • the axial opening 40 (see Figure 2) defined by the shells 32 and 34 has a smaller diameter than the diameter of the inner enclosure 12 so that shells 32 and 34 are welded together after they have been disposed over the respective end walls 18 and 20 of the inner enclosure.
  • the axial end portions 42 and 44 of the annular outer enclosure 14 are also convex when viewed on respective sides of the axis of the vessel, and the radially inner edges thereof defining the opening 40 abut the end walls 18 and 20 of the inner enclosure at approximately right angles, for example between 80 and 100 ⁇ , adjacent where those end walls 18 and 20 merge with the peripheral wall 16.
  • the annular joins are then welded exteriorly at 46 and 48.
  • the axial lengths of the inner and outer enclosures 12 and 14 are substantially the same so that the opposed end walls of the vessel defined by the wall portions 18 and 42 and 20 and 44, respectively, extend substantially in respective planes.
  • a valve 50 is shown generally in the peripheral wall 38 of the vessel and may be in the form of a known multi-valve assembly. Alternatively, plural valve openings may be provided.
  • An advantage of providing the convex formations 18 and 42 in the bottom axial end wall of the vessel (when the vessel is used in the orientation shown in Figure 1) is that the internal concavity of the inner enclosure 12 defined by the end wall 18 beneath the openings 24 and 26 may act as a reserve of fuel which is tapped only after the fuel in the remainder of the vessel has been used.
  • Both the inner and outer enclosures may conveniently be formed in, for example, mild steel or stainless steel and the inner enclosure can advantageously be formed on a production line for small pressurized gas vessels such as are used for barbeques.
  • a major advantage of the vessel 10 is the simplicity of manufacture since the shells 32 and 34 of the outer enclosure can be automatically centralised on the inner enclosure prior to welding. Since the internal reinforcing wall is integrally formed with the inner enclosure, it may give improved strength and fatigue or pulsation resistance to the vessel as a whole while allowing substantially greater internal volume for fuel storage than the known toroidal vessels. Furthermore, it will be noted that the weld lines all extend perpendicularly to the longitudinal axis of the vessel -which gives considerably greater strength than longitudinal welds.
  • joggle-butt welds may be replaced by, for example, butt welds using a backing plate.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Transportation (AREA)
  • General Engineering & Computer Science (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)

Abstract

Un réservoir de carburant sous pression (10) à usage automobile possède une dimension diamétrale supérieure à la dimension axiale et est défini par une enceinte préconstituée (12), dont la paroi périphérique (16) est composée d'une paroi de renforcement du réservoir traversée par des ouvertures (24, 26, 28, 30) et d'une partie annulaire (14) soudée à l'enceinte, afin de définir avec cette dernière la chambre du réservoir. Les extrémités opposées (42, 44) de la partie annulaire chevauchent radialement et vers l'intérieur la paroi périphérique de l'enceinte et sont soudées aux extrémités opposées (18, 20) de ladite enceinte.
EP94920333A 1993-07-06 1994-07-06 Reservoir de carburant sous pression Withdrawn EP0707697A1 (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
AUPL980993 1993-07-06
AUPL9809/93 1993-07-06
PCT/AU1994/000375 WO1995002152A1 (fr) 1993-07-06 1994-07-06 Reservoir de carburant sous pression

Publications (2)

Publication Number Publication Date
EP0707697A1 true EP0707697A1 (fr) 1996-04-24
EP0707697A4 EP0707697A4 (fr) 1996-06-05

Family

ID=3777037

Family Applications (1)

Application Number Title Priority Date Filing Date
EP94920333A Withdrawn EP0707697A1 (fr) 1993-07-06 1994-07-06 Reservoir de carburant sous pression

Country Status (3)

Country Link
EP (1) EP0707697A1 (fr)
JP (1) JPH08512384A (fr)
WO (1) WO1995002152A1 (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR19990044504A (ko) * 1995-09-05 1999-06-25 스캇 로빈슨 도널드 이중 챔버를 구비한 유체 저장 용기
JP2002321535A (ja) * 2001-04-27 2002-11-05 Chuo Motor Wheel Co Ltd 自動車用高圧容器
EP1431096A3 (fr) 2002-12-18 2006-04-26 Conception et Développement Michelin S.A. Réservoir pour le stockage à haute pression d'un carburant sur un véhicule
DE202004015329U1 (de) * 2004-09-30 2005-02-17 Barthel, Christoph Dieter Kraftstoffreservoir
WO2014204414A2 (fr) * 2013-06-17 2014-12-24 Nilvichean Neil Réservoir de gaz naturel d'automobile toroïdal rempli par le centre

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2585446A1 (fr) * 1985-07-25 1987-01-30 Picard Jean Reservoir de fluide sous pression, notamment reservoir de gaz de petrole liquefie pour vehicule automobile

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB371327A (en) * 1929-10-12 1932-05-19 Hermann Debor Improvements in and relating to pressure fluid containers
DE705439C (de) * 1939-01-19 1941-04-28 Paolo Ribi Dr Ing Kugelzonenbehaelter
GB595135A (en) * 1943-10-07 1947-11-27 Chicago Bridge & Iron Co Improvements in or relating to pressure vessels or containers
US2920784A (en) * 1955-12-01 1960-01-12 Chicago Bridge & Iron Co Liquid storage vessel
DE1944315A1 (de) * 1969-09-01 1971-03-04 Erhard Frese Kugelzonenbehaelter
WO1992006324A1 (fr) * 1990-10-09 1992-04-16 Donald Scott Robinson Reservoir de carburant sous pression

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2585446A1 (fr) * 1985-07-25 1987-01-30 Picard Jean Reservoir de fluide sous pression, notamment reservoir de gaz de petrole liquefie pour vehicule automobile

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of WO9502152A1 *

Also Published As

Publication number Publication date
WO1995002152A1 (fr) 1995-01-19
JPH08512384A (ja) 1996-12-24
EP0707697A4 (fr) 1996-06-05

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