US3603096A - Apparatus for installing a reinforced vessel in an underground cavity - Google Patents

Apparatus for installing a reinforced vessel in an underground cavity Download PDF

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US3603096A
US3603096A US883703A US3603096DA US3603096A US 3603096 A US3603096 A US 3603096A US 883703 A US883703 A US 883703A US 3603096D A US3603096D A US 3603096DA US 3603096 A US3603096 A US 3603096A
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vessel
bore
cavity
column
spray head
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US883703A
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William M Wells
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US Atomic Energy Commission (AEC)
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65GTRANSPORT OR STORAGE DEVICES, e.g. CONVEYORS FOR LOADING OR TIPPING, SHOP CONVEYOR SYSTEMS OR PNEUMATIC TUBE CONVEYORS
    • B65G5/00Storing fluids in natural or artificial cavities or chambers in the earth

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  • This invention relates to subterranean cavities or galleries. More particularly, it relates to the emplacement of fluid pressuretight vessels or liners within subterranean cavities formed in a bore, well, shaft or tunnel. In particular, it relates to a method and apparatus for the emplacement of a reinforced, pressuretight vessel or liner within such a cavity.
  • the present invention provides a method and apparatus whereby an expandable subterranean vessel may be placed in a cavity, and after expansion may be lined completely with a high strength material such as steel, sprayed on in an electric arc molten spray process to any desired thickness, i.e., to a thickness of several inches if necessary, by remote control without the necessity of personnel being present.
  • a high strength material such as steel
  • FIG. 1 is a cross section of a subterranean bore having a cavity underreamed in it, and showing an emplaced vessel in the process of being reinforced according to the invention
  • FIG. 2 is an elevational view, partly in cross section, of a collapsed vessel ready for insertion through the bore and into the cavity, before distension and reinforcement.
  • FIG. 1 there is shown a bore 10 drilled from the surface of the earth 12 and extending downwardly, in the example shown, to a cavity 14, formed at the end of the bore by underreaming with an expansible bit, or in any other suitable manner.
  • the bore 10 is lined with a casing 16 which terminates, in the exemplification shown, at the neck 18 of the cavity 14.
  • a vessel 20 of steel plate or other suitable material is shown lining the cavity 14.
  • the vessel 20, of a length appropriate to the length of the cavity 14, is formed with its sidewall in one or more pleats or folds 22, so that the cross-sectional shape as shown in figure, is petalous or stellate.
  • the vessel 20 has' its sidewall pleated about its entire circumference; however, any appropriate number of pleats may be used, as indicated for the material and stresses involved.
  • the vessel 20 is welded at 24 to the end of the casing 10 and in its collapsed or pleated form as seen in FIG. 2, is of a diameter that can be passed through the bore 10 into the cavity 14.
  • the vessel. 20 in the cavity 14 it is first welded at 24 to the adjoining section of casing 16, which in turn is joined to the next section of casing, and so on.
  • the casing, with the vessel welded to it, is lowered into the bore, subsequent sections of casing being added to the string until the vessel has passed into the cavity 14 and is in proper position for expansion.
  • Internal pressure is then applied to the vessel hydraulically, explosively, or in any other well-known manner until it is distended or inflated to its desired size.
  • a spraying apparatus 26 is lowered into the vessel until its end rests on a seat 30 disposed at the bottom of the vessel.
  • a spray head generally indicated at 32 is disposed on a supporting column 28, the column 28 and the spray head 32 being arranged so that the spray head is controllable and manipulatable remotely from the surface 12 and can be made to transverse back and forth along the axis of the vessel and can be rotated as desired, about the interior of the vessel.
  • the details of the spray head and the traversing and rotating mechanism form no part of this invention, but spraying, traversing and rotating can be readily accomplished by means well known and available commercially.
  • the spray head 32 is provided with one or more radially disposed arms 34, having spray nozzles 36 located at their outboard ends so that the nozzles are positioned at the proper working distance from the wall of the vessel 20. Pivotal mounting 38 of the arms 34 enables them to be retracted so that the spraying apparatus 26 and the supporting column 38 can be passed through the casing 16.
  • the particular type of metal spraying apparatus to be employed forms no part of this invention.
  • One particular type that has been used and is suitable is known as an arc spray, in which two wires, made of the material to be sprayed, are fed continuously to the nozzle and an electric are maintained between them.
  • a gas jet usually air, blows the molten metal onto the surface to be coated.
  • the melting rate for commercial arc-spraying equipment is comparatively great and thick coatings can be readily built up with additional thicknesses for reinforcing ribs or hoops, if desired.
  • the spraying apparatus 26 is withdrawn from the vessel through the casing 16.
  • a spray head disposed within said vessel for depositing a reinforcing coating upon the interior thereof, said spray head being supported by said column and being movable rotationally and translationally about and along the interior of said vessel;
  • pivot means mounting said arm means to permit retraction thereof so that said spray head and column can be inserted into and withdrawn from said vessel through said opening and said bore.

Abstract

A distensible vessel, reduced in diameter by means of folds in its sidewall, is passed through a bore into a cavity and is expanded to size by internal pressure. The interior of the vessel is then reinforced by building up a suitably thick deposit of material applied to the walls in an adherent spray by means of an arc-spray gun arranged to traverse the interior of the vessel.

Description

United States Patent William M. Wells Livermore, Calif.
Dec. 10, 1969 Sept. 7, 1971 The United States of America as represented by the United States Atomic Energy Commission Inventor Appl. No. Filed Patented Assignee APPARATUS FOR INSTALLING A REINFORCED VESSEL IN AN UNDERGROUND CAVITY 1 Claim, 2 Drawing Figs.
1111.01 B65g 5/00, B05b 13/06 Field of Search 61 /.5,46,
[56] References Cited UNITED STATES PATENTS 2,868,163 1/1959 Boyd 118/317 3,013,528 12/1961 Bland 118/317 X 3,330,122 7/1967 .lanner.... 61/46 3,351,289 11/1967 Demaison 118/317 X Primary Examiner-Jacob Shapiro Attorney-Roland A. Anderson ABSTRACT: A distensible vessel, reduced in diameter by means of folds in its sidewall, is passed through a bore into a cavity and is expanded to size by internal pressure. The interior of the vessel is then reinforced by building up a suitably thick deposit of material applied to the walls in an adherent spray by means of an arc-spray gun arranged to traverse the interior of the vessel.
PATENTEU SEP 7 m INVENTOR. WILLIAM M. WELLS //r.w( a W APPARATUS FOR INSTALLING A REINFORCED VESSEL IN AN UNDERGROUND CAVITY BACKGROUND OF THE INVENTION This invention relates to subterranean cavities or galleries. More particularly, it relates to the emplacement of fluid pressuretight vessels or liners within subterranean cavities formed in a bore, well, shaft or tunnel. In particular, it relates to a method and apparatus for the emplacement of a reinforced, pressuretight vessel or liner within such a cavity.
For a variety of reasons in conjunction with underground operations such as mining, geophysical exploration, earth works, and for other purposes, it is often necessary to enlarge a portion of a subterranean bore to form a cavity or chamber within which can be placed geophysical instruments or other equipment. Frequently, the earth formation within which the cavity must be located is instable or is in a region of subsurface water so that it is difficult to maintain a dry, fiuidtight cavity or chamber, impenetrable to ground water and capable of withstanding crushing pressure from the surrounding rock walls. It has been customary in the prior art to support the walls of the chamber and to seal them against the intrusion of ground water by means of struts, concreting and steel linings. Whatever the means employed, it has usually been necessary to make the bore sufficiently large to permit the installation of to skip or cage and to lower men into the cavity, to line or reinforce it or to assemble a vessel or liner. Where the earth formation is instable or wet, the hazards to personnel are at once apparent.
Various methods have been proposed for lining such a cavi ty without the presence of personnel, one method being shown in U.S. Pat. No. 3,330,122 granted July 11, 1967 to Karl .lanner for a Method of forming Underground Nuclear Reactor Installation, whereby a collapsed metallic reactor vessel is lowered into a cavity at the bottom of a bore and expanded to the desired size, in situ. Where there is great likelihood of shifting of the surrounding rock formation, or if the cavity is located at great depth so that the hydrostatic pressure of ground water is very great, a distensible vessel of the type shown in the aforesaid patent to Janner, in order to withstand these conditions, would have to be made with its walls impractically thick and incapable of proper expansion.
SUMMARY OF THE INVENTION The present invention provides a method and apparatus whereby an expandable subterranean vessel may be placed in a cavity, and after expansion may be lined completely with a high strength material such as steel, sprayed on in an electric arc molten spray process to any desired thickness, i.e., to a thickness of several inches if necessary, by remote control without the necessity of personnel being present.
This is accomplished by lowering into the expanded vessel an arc-spray gun, positioned within the vessel so that its spray or sprays are proximate the wall of the vessel, and causing the spray head to sweep about and along the wall until the desired thickness of coating is built up. In a practical application of the present technique it has been found that very high strength coatings can be readily built up, from an suitable material, the steels being particularly usable in the process.
Accordingly, it is an object of the invention to provide a novel technique for remotely forming a pressure vessel or liner in an underground cavity.
It is a further object of the invention to provide a novel method of reinforcing a pressure vessel emplaced in an underground cavity.
It is still another object of the invention to provide a novel method and apparatus enabling emplacement of a reinforced pressure vessel within an underground cavity, without the necessity of personnel being present within the cavity.
It is still further object of the invention to provide a novel method and apparatus for reinforcing the wall of an underground vessel emplaced within a cavity, by coating the interior wall of the vessel with an adherent lining of any desired thickness, sprayed in place.
These and other objects of the invention will be apparent as the ensuing description proceeds, and from the appended drawing.
BRIEF DESCRIPTION OF THE DRAWING FIG. 1 is a cross section of a subterranean bore having a cavity underreamed in it, and showing an emplaced vessel in the process of being reinforced according to the invention; and
FIG. 2 is an elevational view, partly in cross section, of a collapsed vessel ready for insertion through the bore and into the cavity, before distension and reinforcement.
DESCRIPTION OF A PREFERRED EMBODIMENT Referring to FIG. 1, there is shown a bore 10 drilled from the surface of the earth 12 and extending downwardly, in the example shown, to a cavity 14, formed at the end of the bore by underreaming with an expansible bit, or in any other suitable manner. The bore 10 is lined with a casing 16 which terminates, in the exemplification shown, at the neck 18 of the cavity 14.
In FIG. 1, a vessel 20 of steel plate or other suitable material is shown lining the cavity 14. Referring to FIG. 2, the vessel 20, of a length appropriate to the length of the cavity 14, is formed with its sidewall in one or more pleats or folds 22, so that the cross-sectional shape as shown in figure, is petalous or stellate. In the example shown in FIG. 2, the vessel 20 has' its sidewall pleated about its entire circumference; however, any appropriate number of pleats may be used, as indicated for the material and stresses involved. The vessel 20 is welded at 24 to the end of the casing 10 and in its collapsed or pleated form as seen in FIG. 2, is of a diameter that can be passed through the bore 10 into the cavity 14.
To emplace the vessel. 20 in the cavity 14, it is first welded at 24 to the adjoining section of casing 16, which in turn is joined to the next section of casing, and so on. The casing, with the vessel welded to it, is lowered into the bore, subsequent sections of casing being added to the string until the vessel has passed into the cavity 14 and is in proper position for expansion. Internal pressure is then applied to the vessel hydraulically, explosively, or in any other well-known manner until it is distended or inflated to its desired size.
After the vessel 20 is expanded to its desired size within the cavity 14, it is ready to be reinforced. A spraying apparatus 26, is lowered into the vessel until its end rests on a seat 30 disposed at the bottom of the vessel. A spray head generally indicated at 32 is disposed on a supporting column 28, the column 28 and the spray head 32 being arranged so that the spray head is controllable and manipulatable remotely from the surface 12 and can be made to transverse back and forth along the axis of the vessel and can be rotated as desired, about the interior of the vessel. The details of the spray head and the traversing and rotating mechanism form no part of this invention, but spraying, traversing and rotating can be readily accomplished by means well known and available commercially.
The spray head 32 is provided with one or more radially disposed arms 34, having spray nozzles 36 located at their outboard ends so that the nozzles are positioned at the proper working distance from the wall of the vessel 20. Pivotal mounting 38 of the arms 34 enables them to be retracted so that the spraying apparatus 26 and the supporting column 38 can be passed through the casing 16.
As previously indicated, the particular type of metal spraying apparatus to be employed forms no part of this invention. One particular type that has been used and is suitable is known as an arc spray, in which two wires, made of the material to be sprayed, are fed continuously to the nozzle and an electric are maintained between them. A gas jet, usually air, blows the molten metal onto the surface to be coated. The melting rate for commercial arc-spraying equipment is comparatively great and thick coatings can be readily built up with additional thicknesses for reinforcing ribs or hoops, if desired. After the coating 40 is deposited, by repeated traverses of the interior surface of the vessel as may be necessary, the spraying apparatus 26 is withdrawn from the vessel through the casing 16. In the preceding discussion, a preferred embodiment of the invention has been described and illustrated. It will be apparent, however, to those skilled in the art, that modifications locating means affixed to the interior of said vessel at a location opposite said opening;
a supporting column extending into said vessel from said bore through said opening, one end of said column being positioned by said locating means;
a spray head disposed within said vessel for depositing a reinforcing coating upon the interior thereof, said spray head being supported by said column and being movable rotationally and translationally about and along the interior of said vessel;
arm means mounted upon said spray head and disposed generally radially of said column;
spray nozzle means carried by said arm means and directed toward the wall of said vessel, and
pivot means mounting said arm means to permit retraction thereof so that said spray head and column can be inserted into and withdrawn from said vessel through said opening and said bore.

Claims (1)

1. In means for lining an underground chamber, said chamber constituting an enlargement in a bore, the combination of: a vessel emplaced within said underground chamber, the walls of said vessel being disposed in proximity to the walls of said chamber and having an opening therethrough directed toward said bore; locating means affixed to the interior of said vessel at a location opposite said opening; a supporting column extending into said vessel from said bore through said opening, one end of said column being positioned by said locating means; a spray head disposed within said vessel for depositing a reinforcing coating upon the interior thereof, said spray head being supported by said column and being movable rotationally and translationally about and along the interior of said vessel; arm means mounted upon said spray head and disposed generally radially of said column; spray nozzle means carried by said arm means and directed toward the wall of said vessel, and pivot means mounting said arm means to permit retraction thereof so that said spray head and column can be inserted into and withdrawn from said vessel through said opening and said bore.
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Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4068535A (en) * 1975-11-10 1978-01-17 David L. Ray Method and apparatus for controlling the tension of drive belts
US4504525A (en) * 1982-08-05 1985-03-12 Chicago Bridge & Iron Company Method of coating the walls of narrow vertical elongated spaces
US4786525A (en) * 1982-05-14 1988-11-22 Humes Limited Pipe linings
US5653555A (en) * 1995-05-19 1997-08-05 Inliner, U.S.A. Multiple resin system for rehabilitating pipe
US5699838A (en) * 1995-05-22 1997-12-23 Inliner, U.S.A. Apparatus for vacuum impregnation of a flexible, hollow tube
US20060108058A1 (en) * 2004-11-24 2006-05-25 Chapman Michael R Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections
US7096890B2 (en) 2002-06-19 2006-08-29 Saint-Gobain Technical Fabrics Canada, Ltd. Inversion liner and liner components for conduits
US20080230652A1 (en) * 2004-04-06 2008-09-25 Biornstad Robert D Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
US7478650B2 (en) 2002-06-19 2009-01-20 Saint-Gobain Technical Fabrics Canada, Ltd. Inversion liner and liner components for conduits
US20100083504A1 (en) * 2004-04-06 2010-04-08 The Boeing Company Methods of manufacturing structural panels
US8042767B2 (en) 2007-09-04 2011-10-25 The Boeing Company Composite fabric with rigid member structure
US8061035B2 (en) 2004-09-23 2011-11-22 The Boeing Company Splice joints for composite aircraft fuselages and other structures
US8388795B2 (en) 2007-05-17 2013-03-05 The Boeing Company Nanotube-enhanced interlayers for composite structures
US20150354903A1 (en) * 2012-11-01 2015-12-10 Skanska Sverige Ab Thermal energy storage comprising an expansion space
WO2019244148A1 (en) * 2018-06-20 2019-12-26 Augwind Ltd. System for storing compressed fluid

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2868163A (en) * 1954-05-06 1959-01-13 Gen Electric Apparatus for coating cavities
US3013528A (en) * 1957-09-30 1961-12-19 Standard Oil Co Metallizing gun for internal surfaces
US3330122A (en) * 1962-06-09 1967-07-11 Siemens Ag Method of forming underground nuclear reactor installation
US3351289A (en) * 1965-05-06 1967-11-07 Quigley Co Apparatus for applying a protective refractory coating to the refractory linings of basic oxygen furnaces

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2868163A (en) * 1954-05-06 1959-01-13 Gen Electric Apparatus for coating cavities
US3013528A (en) * 1957-09-30 1961-12-19 Standard Oil Co Metallizing gun for internal surfaces
US3330122A (en) * 1962-06-09 1967-07-11 Siemens Ag Method of forming underground nuclear reactor installation
US3351289A (en) * 1965-05-06 1967-11-07 Quigley Co Apparatus for applying a protective refractory coating to the refractory linings of basic oxygen furnaces

Cited By (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4068535A (en) * 1975-11-10 1978-01-17 David L. Ray Method and apparatus for controlling the tension of drive belts
US4786525A (en) * 1982-05-14 1988-11-22 Humes Limited Pipe linings
US4504525A (en) * 1982-08-05 1985-03-12 Chicago Bridge & Iron Company Method of coating the walls of narrow vertical elongated spaces
US5653555A (en) * 1995-05-19 1997-08-05 Inliner, U.S.A. Multiple resin system for rehabilitating pipe
US5699838A (en) * 1995-05-22 1997-12-23 Inliner, U.S.A. Apparatus for vacuum impregnation of a flexible, hollow tube
US7478650B2 (en) 2002-06-19 2009-01-20 Saint-Gobain Technical Fabrics Canada, Ltd. Inversion liner and liner components for conduits
US7096890B2 (en) 2002-06-19 2006-08-29 Saint-Gobain Technical Fabrics Canada, Ltd. Inversion liner and liner components for conduits
US8496206B2 (en) 2004-04-06 2013-07-30 The Boeing Company Structural panels for use in aircraft fuselages and other structures
US20110073708A1 (en) * 2004-04-06 2011-03-31 The Boeing Company Composite Barrel Sections for Aircraft Fuselages and Other Structures, and Methods and Systems for Manufacturing Such Barrel Sections
US8382037B2 (en) 2004-04-06 2013-02-26 The Boeing Company Composite barrel sections for aircraft fuselages and other structures
US7527222B2 (en) 2004-04-06 2009-05-05 The Boeing Company Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
US20100083504A1 (en) * 2004-04-06 2010-04-08 The Boeing Company Methods of manufacturing structural panels
US7716835B2 (en) 2004-04-06 2010-05-18 The Boeing Company Methods of manufacturing structural panels
US20100223772A1 (en) * 2004-04-06 2010-09-09 The Boeing Company Structural Panels for Use in Aircraft Fuselages and Other Structures
US20080230652A1 (en) * 2004-04-06 2008-09-25 Biornstad Robert D Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
US8182628B2 (en) 2004-04-06 2012-05-22 The Boeing Company Composite barrel sections for aircraft fuselages and other structures, and methods for systems for manufacturing such barrel sections
US8157212B2 (en) 2004-04-06 2012-04-17 The Boeing Company Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
US8061035B2 (en) 2004-09-23 2011-11-22 The Boeing Company Splice joints for composite aircraft fuselages and other structures
US8882040B2 (en) 2004-09-23 2014-11-11 The Boeing Company Splice joints for composite aircraft fuselages and other structures
US9738371B2 (en) 2004-09-23 2017-08-22 The Boeing Company Splice joints for composite aircraft fuselages and other structures
US8869403B2 (en) 2004-09-23 2014-10-28 The Boeing Company Splice joints for composite aircraft fuselages and other structures
US10689086B2 (en) 2004-09-23 2020-06-23 The Boeing Company Splice joints for composite aircraft fuselages and other structures
US8303758B2 (en) 2004-11-24 2012-11-06 The Boeing Company Methods for manufacturing composite sections for aircraft fuselages and other structures
US8418740B2 (en) 2004-11-24 2013-04-16 The Boeing Company Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections
US20060108058A1 (en) * 2004-11-24 2006-05-25 Chapman Michael R Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections
US8168023B2 (en) 2004-11-24 2012-05-01 The Boeing Company Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections
US7503368B2 (en) * 2004-11-24 2009-03-17 The Boeing Company Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections
US8657990B2 (en) 2007-05-17 2014-02-25 The Boeing Company Nanotube-enhanced interlayers for composite structures
US8388795B2 (en) 2007-05-17 2013-03-05 The Boeing Company Nanotube-enhanced interlayers for composite structures
US8728263B2 (en) 2007-09-04 2014-05-20 The Boeing Company Composite fabric with rigid member structure
US8042767B2 (en) 2007-09-04 2011-10-25 The Boeing Company Composite fabric with rigid member structure
US20150354903A1 (en) * 2012-11-01 2015-12-10 Skanska Sverige Ab Thermal energy storage comprising an expansion space
US9823026B2 (en) * 2012-11-01 2017-11-21 Skanska Sverige Ab Thermal energy storage with an expansion space
WO2019244148A1 (en) * 2018-06-20 2019-12-26 Augwind Ltd. System for storing compressed fluid
US11827463B2 (en) 2018-06-20 2023-11-28 Augwind Ltd. System for storing compressed fluid

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