US1668179A - Container - Google Patents

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US1668179A
US1668179A US122580A US12258026A US1668179A US 1668179 A US1668179 A US 1668179A US 122580 A US122580 A US 122580A US 12258026 A US12258026 A US 12258026A US 1668179 A US1668179 A US 1668179A
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United States
Prior art keywords
plates
lobes
shell
members
radial
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Expired - Lifetime
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US122580A
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Arthur H T Williams
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C1/00Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge
    • F17C1/02Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge involving reinforcing arrangements
    • F17C1/08Integral reinforcements, e.g. ribs
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2201/00Vessel construction, in particular geometry, arrangement or size
    • F17C2201/01Shape
    • F17C2201/0147Shape complex
    • F17C2201/0152Lobes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2201/00Vessel construction, in particular geometry, arrangement or size
    • F17C2201/05Size
    • F17C2201/056Small (<1 m3)
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/01Reinforcing or suspension means
    • F17C2203/011Reinforcing means
    • F17C2203/012Reinforcing means on or in the wall, e.g. ribs
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0602Wall structures; Special features thereof
    • F17C2203/0612Wall structures
    • F17C2203/0614Single wall
    • F17C2203/0617Single wall with one layer
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634Materials for walls or layers thereof
    • F17C2203/0636Metals
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2205/00Vessel construction, in particular mounting arrangements, attachments or identifications means
    • F17C2205/01Mounting arrangements
    • F17C2205/0123Mounting arrangements characterised by number of vessels
    • F17C2205/013Two or more vessels
    • F17C2205/0149Vessel mounted inside another one
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2209/00Vessel construction, in particular methods of manufacturing
    • F17C2209/22Assembling processes
    • F17C2209/221Welding
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2209/00Vessel construction, in particular methods of manufacturing
    • F17C2209/22Assembling processes
    • F17C2209/228Assembling processes by screws, bolts or rivets
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2209/00Vessel construction, in particular methods of manufacturing
    • F17C2209/23Manufacturing of particular parts or at special locations
    • F17C2209/232Manufacturing of particular parts or at special locations of walls
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2223/00Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/01Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
    • F17C2223/0107Single phase
    • F17C2223/0123Single phase gaseous, e.g. CNG, GNC
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2223/00Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/03Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
    • F17C2223/036Very high pressure (>80 bar)
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2260/00Purposes of gas storage and gas handling
    • F17C2260/01Improving mechanical properties or manufacturing
    • F17C2260/018Adapting dimensions
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2270/00Applications
    • F17C2270/07Applications for household use

Definitions

  • This invention relates enerally to the art of Constructing meta shells with or withoutv closed ends for the pur ose of using same for containers or con nits.
  • he main object of this invention is to construct a metal shell in such a manner that a relatively thin wall can be employed, considering the cross sectional area of the shell and the pressure to which it maybe sub'ected.
  • he second object is to construct a shell capable of resisting large internal pressures and having a shape whlch will permit same of buildings.
  • the fifth object is ,to construct a shell especially adapted for the fabrication of high pressure containers for gas to be used within ordinary low pressure containers,
  • the sixth object is to construct the shelll so that the rivets in its joints willbe in shear instead of in tension.
  • Figure 1 is a cross section of a form of the shell employing riveted joints.
  • Figure 2 is a fragmentary side elevation showing a tank having a shell as shown in Figure 1 and having bulging ends.
  • Figure 3 is a cross section similar to Figure 1 but showing welded joints instead of riveted.
  • Figure 4 :
  • Figure 5 is a section taken along the line 5-5 in Figure 4.
  • Figure 6 is a section taken along the line 6 6 in Figure 4.
  • t e entire shell consists of three units or lobes 10* which are parts of true cylinders having their over-lapped portions cut away and substituted by straight walls or webs 11 i'oined at the center 12 and connected to the obes 10 by the sides 13.
  • Curved plates 14 which conform with the shape of the lobes 1O connect the lobrs l0 and the plates 11. The stresses in the material of the lobes 10 are carried by the members 13, the plate 11 being required only to sustain the resultant force between its pair of members 13.
  • the function of the curved plates 14 is merely to maintain the cylindrical shape of the lobes 10 at all points, except those in which the sides can be subjected to counter-acting pressures.
  • members 13 are not subjected to lateral pressures from within the tank at any time, it being necessary to provide openings 15 in the members 13 to prevent any possible accumulation of pressure between the memhere 1]., 13 and 14. v
  • heads 16 or bottoms can be in any convenient form ranging from a fiat bottom for an open tank to the inwardly or outwardly bulging heads 16 or even. emispherical ends without departing from the spirit of the invention.
  • the radial plates also serve to stay these heads at their intersections.
  • Suitable brace members can be provided for members normally in tension to enable same to withstand compression if desired. 7
  • a shell having three segmental lobes whose centers are disposed around the center of said shell and having plates radiating from said center passing through the points of'intersection of said lobes and projecting beyond such points of intersection, said projecting portions having longitudinal structural members attached thereto parallel with 5 the center lines of said lobes, and tension means between the adjacent lateral edges of said lobes bearing against said structural members.

Description

May 1, 1928. v 1,668,179 I A. H. T, WILLIAMS CONTAINER Filed July 15. 1926 INVENTOR A.H.T. WILLIA Ms ATTORNEY.
Patented May 1, 1928. v I
UNITED STATES PATENT OFFICE.
ARTHUR H. 'I'. WILLIAMS, OI PORTLAND, OBEGON.
CONTAINER.
Application filed July 15, 1928. Serial Io. 188,580.
This invention relates enerally to the art of Constructing meta shells with or withoutv closed ends for the pur ose of using same for containers or con nits.
he main object of this invention is to construct a metal shell in such a manner that a relatively thin wall can be employed, considering the cross sectional area of the shell and the pressure to which it maybe sub'ected.
he second object is to construct a shell capable of resisting large internal pressures and having a shape whlch will permit same of buildings.
The fifth object is ,to construct a shell especially adapted for the fabrication of high pressure containers for gas to be used within ordinary low pressure containers,
specici reference bein made to my co-pend ing application, Seria Number 121,801..
The sixth object is to construct the shelll so that the rivets in its joints willbe in shear instead of in tension. K
These, and other objects, will become more apparent from the specification following as illustrated in the accompanying drawing, in which 2.
Figure 1 is a cross section of a form of the shell employing riveted joints. Figure 2 is a fragmentary side elevation showing a tank having a shell as shown in Figure 1 and having bulging ends. Figure 3 is a cross section similar to Figure 1 but showing welded joints instead of riveted. Figure 4:
is an enlarged cross section through a riveted joint. Figure 5 is a section taken along the line 5-5 in Figure 4. Figure 6 is a section taken along the line 6 6 in Figure 4.
Similar numbers of reference refer to the similar parts throughout the several views.
Referring in detail to the drawing in the simpler form of shell employing welded joints, as illustrated in Figure 3, t e entire shell consists of three units or lobes 10* which are parts of true cylinders having their over-lapped portions cut away and substituted by straight walls or webs 11 i'oined at the center 12 and connected to the obes 10 by the sides 13. Curved plates 14 which conform with the shape of the lobes 1O connect the lobrs l0 and the plates 11. The stresses in the material of the lobes 10 are carried by the members 13, the plate 11 being required only to sustain the resultant force between its pair of members 13.
The function of the curved plates 14 is merely to maintain the cylindrical shape of the lobes 10 at all points, except those in which the sides can be subjected to counter-acting pressures. members 13 are not subjected to lateral pressures from within the tank at any time, it being necessary to provide openings 15 in the members 13 to prevent any possible accumulation of pressure between the memhere 1]., 13 and 14. v
If heads 16 or bottoms are required these can be in any convenient form ranging from a fiat bottom for an open tank to the inwardly or outwardly bulging heads 16 or even. emispherical ends without departing from the spirit of the invention.
Figures 1, 2, 4, 5 and .6 the construction is similar to that shown in Figure 3,
' except that the material in the lobes 10"- is Alternating with the straps 17 are-the straps 19 which join the'plates 11 to the plates In other wordsthe 11 on the opposite sides of which are secured the channel irons 20. The curved lates M- connect the lobes 10 to the mom ers 11 It can be seen that in this form of the device, or that described in Figure 3," that the straight central plates 11 or 11 will handle only up roximately the resultant of the forces to w ich the plates 13 or 13* are subjected Althou h I have so arranged the an ular relation tween the members 13 an the plate .11 and the members 13- and the plate 11*- in a manner to ually divide the forces, it is obvious that,.ow1ng to the lateral thrust against the plates 14 and 14 that the tension on these members will be somewhat greater than on the material in the outer shell, although by this construction it is possible tomake the members 11 or 11* much lighter than would otherwise be practical.
If heads are employed the radial plates also serve to stay these heads at their intersections.
The construction shown for the longitudinal joints'also applies tothe intersections of the various end plates (if used) with the radial stays.
Suitable brace members (not shown) can be provided for members normally in tension to enable same to withstand compression if desired. 7
- It must be understood that the same construction would apply where three or more vertical shells are overlapped and joined together as when cylindrical shells are so lobe consisting of a straight portion tangent to its curved portion, the tangent portions of adjacent sides having spaced joining strap means, an I-beam outside of said strap means, a radial web between each pair of lobes, strap means between said first mentioned strap means for joining said radial member to its I-beam, each ,radial plate forming an angle with each of said tangent plates approximately equal to the smaller angle between the radial plates themselves, means for joining said radial lates at their lines of intersection curved filer plates between said lobes and radial plates adapted to prevent said tangent plates from being subjected to lateral pressure and end means for said shell.
3. A shell having three segmental lobes whose centers are disposed around the center of said shell and having plates radiating from said center passing through the points of'intersection of said lobes and projecting beyond such points of intersection, said projecting portions having longitudinal structural members attached thereto parallel with 5 the center lines of said lobes, and tension means between the adjacent lateral edges of said lobes bearing against said structural members.
ARTHUR H. T, WILLIAMS.
US122580A 1926-07-15 1926-07-15 Container Expired - Lifetime US1668179A (en)

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Cited By (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2431693A (en) * 1944-02-09 1947-12-02 Chicago Bridge & Iron Co Storage tank
US2433335A (en) * 1943-10-06 1947-12-30 Chicago Bridge & Iron Co Storage vessel
US2457118A (en) * 1943-10-07 1948-12-28 Chicago Bridge & Iron Co Spheroidal pressure vessel
US2462064A (en) * 1944-10-09 1949-02-15 Chicago Bridge & Iron Co Pressure vessel for storage of liquids at abnormally high or low temperatures
US2503792A (en) * 1944-11-28 1950-04-11 George M Brandon Truck body
US2514364A (en) * 1945-12-18 1950-07-11 Robert M Bates Ammunition container
US2860806A (en) * 1956-05-31 1958-11-18 Exxon Research Engineering Co Circular bay tank structure
US3070131A (en) * 1957-12-06 1962-12-25 Gen Motors Corp By-pass duct for gas turbine engine
US3315278A (en) * 1965-08-18 1967-04-25 Bilnor Corp Swimming pool structure
US3522614A (en) * 1968-10-14 1970-08-04 Doughboy Ind Inc Swimming pool structure
US3625258A (en) * 1970-03-16 1971-12-07 Warren Petroleum Corp Multipassage pipe
US3645415A (en) * 1970-04-23 1972-02-29 Warren Petroleum Corp Multicylinder tanks
DE3417461A1 (en) * 1984-05-11 1985-11-14 Bissinger GmbH Behälter- und Stahlbau, 7129 Zaberfeld Multi-chamber silo
US4602465A (en) * 1983-07-19 1986-07-29 Jansens & Dieperink B.V. Supporting structure for large volume containers
US5236016A (en) * 1990-09-24 1993-08-17 Dipl.-Ing. Dr. Ernst Vogelsang Gmbh & Co. Kg Cable-guide assembly of plastic tubes joined by webs
US5388719A (en) * 1993-09-29 1995-02-14 Yamashou Sangyo Kabushiki Kaisha Fitting structure of partition plates to structure
WO1996023721A1 (en) * 1995-02-02 1996-08-08 Thiokol Corporation Composite conformable pressure vessel
US20040074547A1 (en) * 2002-09-07 2004-04-22 Safa Kirma Arrangement for storing and conveying liquid, especially in an aircraft
US20090050635A1 (en) * 2007-08-20 2009-02-26 Alliant Techsystems Inc. Seamless multi-section pressure vessel
US20110031257A1 (en) * 2008-12-22 2011-02-10 Wew Westerwalder Eisenwerk Gmbh Pressure Container for a Transport Container Arrangement
US20160290564A1 (en) * 2013-11-08 2016-10-06 United Technologies Corporation High conformal pressure vessel
US20170299122A1 (en) * 2014-10-07 2017-10-19 United Technologies Research Center Pressure vessel fluid manifold assembly
US20170343160A1 (en) * 2014-10-07 2017-11-30 United Technologies Research Center Pressure vessel assembly and method of forming
US20210301978A1 (en) * 2018-07-26 2021-09-30 Gaztransport Et Technigaz Self-bracing watertight tank wall
US11427399B2 (en) * 2017-11-07 2022-08-30 The Yokohama Rubber Co., Ltd. Aircraft water tank
US11525545B2 (en) 2014-10-07 2022-12-13 Raytheon Technologies Corporation Composite pressure vessel assembly and method of manufacturing

Cited By (40)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2433335A (en) * 1943-10-06 1947-12-30 Chicago Bridge & Iron Co Storage vessel
US2457118A (en) * 1943-10-07 1948-12-28 Chicago Bridge & Iron Co Spheroidal pressure vessel
US2431693A (en) * 1944-02-09 1947-12-02 Chicago Bridge & Iron Co Storage tank
US2462064A (en) * 1944-10-09 1949-02-15 Chicago Bridge & Iron Co Pressure vessel for storage of liquids at abnormally high or low temperatures
US2503792A (en) * 1944-11-28 1950-04-11 George M Brandon Truck body
US2514364A (en) * 1945-12-18 1950-07-11 Robert M Bates Ammunition container
US2860806A (en) * 1956-05-31 1958-11-18 Exxon Research Engineering Co Circular bay tank structure
US3070131A (en) * 1957-12-06 1962-12-25 Gen Motors Corp By-pass duct for gas turbine engine
US3315278A (en) * 1965-08-18 1967-04-25 Bilnor Corp Swimming pool structure
US3522614A (en) * 1968-10-14 1970-08-04 Doughboy Ind Inc Swimming pool structure
US3625258A (en) * 1970-03-16 1971-12-07 Warren Petroleum Corp Multipassage pipe
US3645415A (en) * 1970-04-23 1972-02-29 Warren Petroleum Corp Multicylinder tanks
US4602465A (en) * 1983-07-19 1986-07-29 Jansens & Dieperink B.V. Supporting structure for large volume containers
DE3417461A1 (en) * 1984-05-11 1985-11-14 Bissinger GmbH Behälter- und Stahlbau, 7129 Zaberfeld Multi-chamber silo
US5236016A (en) * 1990-09-24 1993-08-17 Dipl.-Ing. Dr. Ernst Vogelsang Gmbh & Co. Kg Cable-guide assembly of plastic tubes joined by webs
US5388719A (en) * 1993-09-29 1995-02-14 Yamashou Sangyo Kabushiki Kaisha Fitting structure of partition plates to structure
KR100499230B1 (en) * 1995-02-02 2006-01-27 앨리언트 테크시스템즈 인코포레이티드 Compound Pressure Vessel
USRE41142E1 (en) * 1995-02-02 2010-02-23 Alliant Techsystems Inc. Composite conformable pressure vessel
US6095367A (en) * 1995-02-02 2000-08-01 Cordant Technologies Inc. Composite conformable pressure vessel
US5577630A (en) * 1995-02-02 1996-11-26 Thiokol Corporation Composite conformable pressure vessel
WO1996023721A1 (en) * 1995-02-02 1996-08-08 Thiokol Corporation Composite conformable pressure vessel
US7681585B2 (en) 2002-09-07 2010-03-23 Airbus Deutschland Gmbh Arrangement for storing and conveying liquid, especially in an aircraft
US20060254658A1 (en) * 2002-09-07 2006-11-16 Airbus Deutschland Gmbh Arrangement for storing and conveying liquid especially in an aircraft
US7537021B2 (en) 2002-09-07 2009-05-26 Airbus Deutschland Gmbh Arrangement for storing and conveying liquid especially in an aircraft
US20090199920A1 (en) * 2002-09-07 2009-08-13 Airbus Deutschland Gmbh Arrangement for storing and conveying liquid, especially in an aircraft
US7100640B2 (en) * 2002-09-07 2006-09-05 Airbus Deutschland Gmbh Arrangement for storing and conveying liquid, especially in an aircraft
US20040074547A1 (en) * 2002-09-07 2004-04-22 Safa Kirma Arrangement for storing and conveying liquid, especially in an aircraft
US20090050635A1 (en) * 2007-08-20 2009-02-26 Alliant Techsystems Inc. Seamless multi-section pressure vessel
US8020722B2 (en) 2007-08-20 2011-09-20 Richards Kevin W Seamless multi-section pressure vessel
US20110031257A1 (en) * 2008-12-22 2011-02-10 Wew Westerwalder Eisenwerk Gmbh Pressure Container for a Transport Container Arrangement
US20160290564A1 (en) * 2013-11-08 2016-10-06 United Technologies Corporation High conformal pressure vessel
US10222001B2 (en) * 2013-11-08 2019-03-05 United Technologies Corporation High conformal pressure vessel
US20170299122A1 (en) * 2014-10-07 2017-10-19 United Technologies Research Center Pressure vessel fluid manifold assembly
US20170343160A1 (en) * 2014-10-07 2017-11-30 United Technologies Research Center Pressure vessel assembly and method of forming
US10221999B2 (en) * 2014-10-07 2019-03-05 United Technologies Corporation Pressure vessel fluid manifold assembly
US10648616B2 (en) * 2014-10-07 2020-05-12 United Technologies Corporation Pressure vessel assembly and method of forming
US11525545B2 (en) 2014-10-07 2022-12-13 Raytheon Technologies Corporation Composite pressure vessel assembly and method of manufacturing
US11898701B2 (en) 2014-10-07 2024-02-13 Rtx Corporation Composite pressure vessel assembly and method of manufacturing
US11427399B2 (en) * 2017-11-07 2022-08-30 The Yokohama Rubber Co., Ltd. Aircraft water tank
US20210301978A1 (en) * 2018-07-26 2021-09-30 Gaztransport Et Technigaz Self-bracing watertight tank wall

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