US2824364A - Method of assembling and evacuating an insulated vacuum panel - Google Patents

Method of assembling and evacuating an insulated vacuum panel Download PDF

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US2824364A
US2824364A US452661A US45266154A US2824364A US 2824364 A US2824364 A US 2824364A US 452661 A US452661 A US 452661A US 45266154 A US45266154 A US 45266154A US 2824364 A US2824364 A US 2824364A
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panel
evacuating
assembling
evacuation
bat
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US452661A
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Harold P Bovenkerk
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General Electric Co
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General Electric Co
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    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04BGENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B1/00Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
    • E04B1/62Insulation or other protection; Elements or use of specified material therefor
    • E04B1/74Heat, sound or noise insulation, absorption, or reflection; Other building methods affording favourable thermal or acoustical conditions, e.g. accumulating of heat within walls
    • E04B1/76Heat, sound or noise insulation, absorption, or reflection; Other building methods affording favourable thermal or acoustical conditions, e.g. accumulating of heat within walls specifically with respect to heat only
    • E04B1/78Heat insulating elements
    • E04B1/80Heat insulating elements slab-shaped
    • E04B1/803Heat insulating elements slab-shaped with vacuum spaces included in the slab
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B30/00Compositions for artificial stone, not containing binders
    • C04B30/02Compositions for artificial stone, not containing binders containing fibrous materials
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C2/00Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
    • E04C2/02Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials
    • E04C2/26Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials composed of materials covered by two or more of groups E04C2/04, E04C2/08, E04C2/10 or of materials covered by one of these groups with a material not specified in one of the groups
    • E04C2/284Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials composed of materials covered by two or more of groups E04C2/04, E04C2/08, E04C2/10 or of materials covered by one of these groups with a material not specified in one of the groups at least one of the materials being insulating
    • E04C2/292Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials composed of materials covered by two or more of groups E04C2/04, E04C2/08, E04C2/10 or of materials covered by one of these groups with a material not specified in one of the groups at least one of the materials being insulating composed of insulating material and sheet metal
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16LPIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L59/00Thermal insulation in general
    • F16L59/04Arrangements using dry fillers, e.g. using slag wool which is added to the object to be insulated by pouring, spreading, spraying or the like
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25DREFRIGERATORS; COLD ROOMS; ICE-BOXES; COOLING OR FREEZING APPARATUS NOT OTHERWISE PROVIDED FOR
    • F25D23/00General constructional features
    • F25D23/06Walls
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25DREFRIGERATORS; COLD ROOMS; ICE-BOXES; COOLING OR FREEZING APPARATUS NOT OTHERWISE PROVIDED FOR
    • F25D23/00General constructional features
    • F25D23/06Walls
    • F25D23/065Details
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25DREFRIGERATORS; COLD ROOMS; ICE-BOXES; COOLING OR FREEZING APPARATUS NOT OTHERWISE PROVIDED FOR
    • F25D2201/00Insulation
    • F25D2201/10Insulation with respect to heat
    • F25D2201/12Insulation with respect to heat using an insulating packing material
    • F25D2201/124Insulation with respect to heat using an insulating packing material of fibrous type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25DREFRIGERATORS; COLD ROOMS; ICE-BOXES; COOLING OR FREEZING APPARATUS NOT OTHERWISE PROVIDED FOR
    • F25D2201/00Insulation
    • F25D2201/10Insulation with respect to heat
    • F25D2201/14Insulation with respect to heat using subatmospheric pressure
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02ATECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
    • Y02A30/00Adapting or protecting infrastructure or their operation
    • Y02A30/24Structural elements or technologies for improving thermal insulation
    • Y02A30/242Slab shaped vacuum insulation
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02BCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
    • Y02B80/00Architectural or constructional elements improving the thermal performance of buildings
    • Y02B80/10Insulation, e.g. vacuum or aerogel insulation

Definitions

  • Vacuum insulating structures may be made to include a sealed envelope with a suitable filler material, such as glass fiber insulation, within the envelope to support the Walls against external atmospheric pressure.
  • suitable filler material such as glass fiber insulation
  • Such structures may be made in accordance with the invention of Herbert M. Strong and Francis P. Bundy, Serial No. 236,788, filed July 14, 1951, now abandoned, and assigned to the General Electric Company, the assignee of the present invention.
  • Absorbed panel gases must be baked off and evacuated from such panels prior to sealing off thereof to prolong the thermal insulating properties.
  • the close packed fibers oiier high impedance to the diffusion of evolved gases when low pressures are reached. It is desirable to reduce the time which is required to evacuate such panels because the evacuation period is almost directly proportional to the quantity of adsorbed gases to be removed to insure low pressure for prolonged periods.
  • panel filler material is preheated before its insertion into the panel to reduce gas evolution during evacuation.
  • Fig. 1 is a sectional view of a bat of ller material within an oven
  • Fig. 2 is a sectional View of a partially assembled thermal insulating panel
  • Fig. 3 is a sectional view of a thermal insulating panel under compression
  • Fig, 4 is a sectional view of an assembled thermal insulating panel
  • Fig. 5 is a sectional view of a thermal insulating panel within a bakeout oven which is equipped for panel evacuation.
  • a conventional type of heating oven which is shown generally at 10, comprises a casing 11 to define a chamber 12 therein.
  • a pair of upstanding members 13 with a support member 14 in the form of a perforated metal plate are positioned within chamber 12 to support a bat or layer of filler material 15 thereon.
  • a pair of opposed heating elements 16 of any suitable construction are mounted on the inner walls of casing 11 to provide a heat source.
  • A11 inert gas or air is preferably -.,:reduce ⁇ ;the.tirne pericd of subsequent b akeout.
  • a glass fiber bat may be heated up to approximately 600 C. which is the softening point of the glass therein. Treatment of a layer of glass fiber filler material at 450 C. for one hour reduces the gas evolution from this bat in an evacuation cycle of 350 C. bakeout by a factor of about seven.
  • a partially assembled thermal insulating panel 17 which comprises a wall 18 of a thin, ilexible sheet of a material of relatively high thermal conductivity, such as low carbon steel, and a second wall 19 of a thin, flexible sheet of a material of relatively low thermal conductivity, such as stainless steel.
  • a port 20 is provided adjacent one end of wall 18 to evacuate panel 17. After bat 1S is preheated in oven 10, it is inserted hot between walls 18 and 19 of panel 17.
  • panel 17 is compressed by any suitable means, such as, for example, by opposed compression blocks 21 and 22 to close the panel edges which are then seam welded.
  • Hot bat 15 is enclosed between opposed panel walls 18 and 19 to provide a panel structure which is then baked out and evacuated.
  • a vacuum system (not shown) is connected to port 20 to evacuate panel 17 or if it is desired, panel 17 may be evacuated without the bakeout.
  • Port 20 is then permanently sealed oif by any suitable means, such as, for example, a weld to provide a vacuum type panel.
  • FIG. 4 an assembled thermal insulating panel is shown which comprises opposed, spaced walls 18 and 19 with a seal at their edges to define an evacuated chamber in which a bat of filler material 15 is positioned.
  • Evacuation port 20 is provided with a permanent seal 23 to maintain the panel vacuum.
  • a second method is shown to manufacture a vacuum type panel which comprises assembling opposed walls 18 and 19 together with a bat of filler material 15 therebetween to form panel 17. The panel edges are then sealed together by a weld.
  • Wall 18 is provided with evacuation port 20 and an inert gas inlet 24.
  • Panel 17 is positioned on a pair of supports 25 within oven 10 which is provided with heating elements 16 and a pair of apertures 26 and 27.
  • a tube 28 connects port 20 through aperture 26 with a vacuum system (not shown).
  • Gas inlet 24 is connected by a tube 29 through aperture 27 with an inert gas source (not shown).
  • Panel 17 is heated in oven 10 at a high temperature to preheat bat 15 therein.
  • preheat treatment reduces the time period of subsequent bakeout.
  • an inert gas is forced through tube 29 and from panel 17 through tube 28.
  • Such gas ushes evolved gases from the interior of the panel.
  • an inert gas may be flushed through panel 17 after the preheat treatment While the panel is hot.
  • Port 24 is then sealed oil to allow panel 17 to be baked cut and evacuated during a shortened time period.
  • Preheat treatment with an inert gas reduces the evolution of panel gases during the bakeout and evacuation cycle to provide a shortened cycle.
  • port 20 may be temporarily capped and panel 17 removed from oven 10. Such a panel does not readsorb gases from the atmosphere. Thus, panel 17 may be stored prior to evacuation without adverse effects.
  • the method of shortening the evacuation cycle of an insulated vacuum panel containing a liber glass material therein which comprises the steps of, placing the filler Y i 4 material in a panel, heating said panel and glass filler to substantially 450 C., maintaining said temperature for approximately one hour, simultaneously ushing said filler with an inert gas to aid in the removal of adsorbed gases, reducing the said temperature to approximately 350 C., and evacuating and sealing said panel.

Description

4 6 4 `nl 2 G N I M wm AN mmm N C7 EGA2 mv.. WLDM. BMWA .mwa HFmF O wm m m Feb. 25, 1958 In Vnor Harold o Ven/(er fills Attorney.
United States Pata-1ro" METHOD-OF ASSEMBLING EVACUATING AN INSULATED VACUUM PANEL Y assignr to Harold l. vBo .v. e,1,1l eris, .lal.ltstn11` .InkaY vGeneral ,Electric Company, a corporation of New )Cork Application August27, 1954,-Serial No. 452,661 1 Claim. (Cl. 29-455) My invention relates to thermal insulating structures of the vacuum type and more particularly to methods of manufacturing such structures.
Vacuum insulating structures may be made to include a sealed envelope with a suitable filler material, such as glass fiber insulation, within the envelope to support the Walls against external atmospheric pressure. Such structures may be made in accordance with the invention of Herbert M. Strong and Francis P. Bundy, Serial No. 236,788, filed July 14, 1951, now abandoned, and assigned to the General Electric Company, the assignee of the present invention.
Absorbed panel gases must be baked off and evacuated from such panels prior to sealing off thereof to prolong the thermal insulating properties. In conventional evacuation of such glass liber insulating panels, the close packed fibers oiier high impedance to the diffusion of evolved gases when low pressures are reached. It is desirable to reduce the time which is required to evacuate such panels because the evacuation period is almost directly proportional to the quantity of adsorbed gases to be removed to insure low pressure for prolonged periods.
Accordingly, it is an object of my invention to provide an improved method to manufacture a thermal insulating panel.
It is another object of the invention to provide an improved method to evacuate a thermal insulating structure.
It is a further object of the invention to provide an improved method to reduce the time period of gas evolution during panel bakeout and evacuation.
In carrying out my invention in one form, panel filler material is preheated before its insertion into the panel to reduce gas evolution during evacuation.
These and various other objects, features and advantages will be better understood from the following description taken in connection with the accompanyingy drawing in which:
Fig. 1 is a sectional view of a bat of ller material within an oven;
Fig. 2 is a sectional View of a partially assembled thermal insulating panel;
Fig. 3 is a sectional view of a thermal insulating panel under compression;
Fig, 4 is a sectional view of an assembled thermal insulating panel; and
Fig. 5 is a sectional view of a thermal insulating panel within a bakeout oven which is equipped for panel evacuation.
In Fig. 1 of the drawing, a conventional type of heating oven, which is shown generally at 10, comprises a casing 11 to define a chamber 12 therein. A pair of upstanding members 13 with a support member 14 in the form of a perforated metal plate are positioned within chamber 12 to support a bat or layer of filler material 15 thereon. A pair of opposed heating elements 16 of any suitable construction are mounted on the inner walls of casing 11 to provide a heat source. A11 inert gas or air is preferably -.,:reduce`;the.tirne pericd of subsequent b akeout.
Patented Fel'n25, 1958 10 by a circulating fan (not shown) l=.to
supplied to oven a reduction in reduce the vapor-,pressure therein. Such vvapor pressure provides greater evolution of gas frornbat 21,15.
lathe manufactureioffathermal insulating panel in aean insulating panel. Thelarge V,surface area of finely di- ,"videdsbat.15..;contributesa maior share of evolved gas which isnemoverliby preheatirlg at; a high temperature :t0 A glass fiber bat may be heated up to approximately 600 C. which is the softening point of the glass therein. Treatment of a layer of glass fiber filler material at 450 C. for one hour reduces the gas evolution from this bat in an evacuation cycle of 350 C. bakeout by a factor of about seven.
In Fig. 2 of the drawing, a partially assembled thermal insulating panel 17 is shown which comprises a wall 18 of a thin, ilexible sheet of a material of relatively high thermal conductivity, such as low carbon steel, and a second wall 19 of a thin, flexible sheet of a material of relatively low thermal conductivity, such as stainless steel. A port 20 is provided adjacent one end of wall 18 to evacuate panel 17. After bat 1S is preheated in oven 10, it is inserted hot between walls 18 and 19 of panel 17.
In Fig. 3, panel 17 is compressed by any suitable means, such as, for example, by opposed compression blocks 21 and 22 to close the panel edges which are then seam welded. Hot bat 15 is enclosed between opposed panel walls 18 and 19 to provide a panel structure which is then baked out and evacuated. A vacuum system (not shown) is connected to port 20 to evacuate panel 17 or if it is desired, panel 17 may be evacuated without the bakeout. Port 20 is then permanently sealed oif by any suitable means, such as, for example, a weld to provide a vacuum type panel.
In Fig. 4, an assembled thermal insulating panel is shown which comprises opposed, spaced walls 18 and 19 with a seal at their edges to define an evacuated chamber in which a bat of filler material 15 is positioned. Evacuation port 20 is provided with a permanent seal 23 to maintain the panel vacuum.
In Fig. 5, a second method is shown to manufacture a vacuum type panel which comprises assembling opposed walls 18 and 19 together with a bat of filler material 15 therebetween to form panel 17. The panel edges are then sealed together by a weld. Wall 18 is provided with evacuation port 20 and an inert gas inlet 24. Panel 17 is positioned on a pair of supports 25 within oven 10 which is provided with heating elements 16 and a pair of apertures 26 and 27. A tube 28 connects port 20 through aperture 26 with a vacuum system (not shown). Gas inlet 24 is connected by a tube 29 through aperture 27 with an inert gas source (not shown).
Panel 17 is heated in oven 10 at a high temperature to preheat bat 15 therein. Such preheat treatment reduces the time period of subsequent bakeout. During this heating, an inert gas is forced through tube 29 and from panel 17 through tube 28. Such gas ushes evolved gases from the interior of the panel. If it is desired, an inert gas may be flushed through panel 17 after the preheat treatment While the panel is hot. Port 24 is then sealed oil to allow panel 17 to be baked cut and evacuated during a shortened time period. Preheat treatment with an inert gas reduces the evolution of panel gases during the bakeout and evacuation cycle to provide a shortened cycle.
After preheat treatment, port 20 may be temporarily capped and panel 17 removed from oven 10. Such a panel does not readsorb gases from the atmosphere. Thus, panel 17 may be stored prior to evacuation without adverse effects.
As will be apparent to those skilled in the art,A the' objects of my invention are attained by preheating filler material to reduce the bakeout and evacuation period of a vacuum insulating structure in which such filler material is used.
While other modifications of this invention and variations of apparatus which may be employed within the scope of the invention have not been described,l the'nvention is intended to include al1 such as may be embraced within the following claim.
What I claim as new and desire to secure by Letters Patent of the United States is:
The method of shortening the evacuation cycle of an insulated vacuum panel containing a liber glass material therein which comprises the steps of, placing the filler Y i 4 material in a panel, heating said panel and glass filler to substantially 450 C., maintaining said temperature for approximately one hour, simultaneously ushing said filler with an inert gas to aid in the removal of adsorbed gases, reducing the said temperature to approximately 350 C., and evacuating and sealing said panel.
References Cited in the'le of this patent UNITED STATES PATENTS 1,780,739 Berg Nov. 4, 193,0 1,942,162 Campbell Jan. 2, 1934 2,700,633 Bovenkerk Jan. 25, 1955 2,747,269 Atchison May 29, 1956
US452661A 1952-10-23 1954-08-27 Method of assembling and evacuating an insulated vacuum panel Expired - Lifetime US2824364A (en)

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Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2939811A (en) * 1957-03-25 1960-06-07 Gen Electric Heat-insulating units for refrigerator cabinets
US2961116A (en) * 1956-01-03 1960-11-22 Applied Radiation Corp Thermally insulated wall structure
US2987813A (en) * 1957-05-01 1961-06-13 American Resistor Corp Hermetically sealing a tubular element or container
US3073268A (en) * 1957-04-04 1963-01-15 Gen Dynamics Corp Apparatus for braze-bonding metallic parts
US3110961A (en) * 1959-04-06 1963-11-19 North American Aviation Inc Honeycomb sandwich panel brazing
US3123900A (en) * 1964-03-10 Method of manufacture of a flow element or pulsation dampener
US3156975A (en) * 1959-02-16 1964-11-17 Evacuated Insulation Res Ltd Method of making heat insulating panels
US3167159A (en) * 1959-07-30 1965-01-26 Gen Electric Insulating structures with variable thermal conductivity and method of evacuation
US4325183A (en) * 1976-09-07 1982-04-20 Welwyn Electric Limited Process for producing an electrical resistor having a metal foil bonded to a ceramic or glass-ceramic substrate
US4979919A (en) * 1987-05-15 1990-12-25 Hitachi, Ltd. Method and apparatus for manufacturing cathode-ray tubes
US5098498A (en) * 1989-10-10 1992-03-24 Manville Corporation Apparatus and method for encapsulating contoured articles
WO1996001346A1 (en) * 1994-07-06 1996-01-18 Owens Corning Vacuum insulation panel and method for manufacturing
US5795639A (en) * 1995-03-16 1998-08-18 Owens Fiberglas Technology, Inc. Vacuum insulation panel having blended wool filler and method for manufacturing
WO2008071637A2 (en) * 2006-12-11 2008-06-19 Single Buoy Moorings Inc. Cryogenic transfer hose having a fibrous insulating layer and method of constructing such a transfer hose
WO2008071373A2 (en) * 2006-12-13 2008-06-19 Woschko Winlite Gmbh Method of producing a vacuum panel, one such vacuum panel, and a masonry block using said panel
EP3590672A1 (en) * 2010-11-05 2020-01-08 Lightweight Labs, LLC Thermal processing and consolidation system and method
US11435132B2 (en) 2020-05-15 2022-09-06 Whirlpool Corporation Method for manufacturing a vacuum insulated structure

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1780739A (en) * 1930-04-12 1930-11-04 Berg Joseph Insulating block
US1942162A (en) * 1933-02-24 1934-01-02 Charles H Campbell Heat insulation
US2700633A (en) * 1952-05-02 1955-01-25 Gen Electric Insulating structure and method of forming same
US2747269A (en) * 1952-09-27 1956-05-29 Gen Electric Insulating structures

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1780739A (en) * 1930-04-12 1930-11-04 Berg Joseph Insulating block
US1942162A (en) * 1933-02-24 1934-01-02 Charles H Campbell Heat insulation
US2700633A (en) * 1952-05-02 1955-01-25 Gen Electric Insulating structure and method of forming same
US2747269A (en) * 1952-09-27 1956-05-29 Gen Electric Insulating structures

Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3123900A (en) * 1964-03-10 Method of manufacture of a flow element or pulsation dampener
US2961116A (en) * 1956-01-03 1960-11-22 Applied Radiation Corp Thermally insulated wall structure
US2939811A (en) * 1957-03-25 1960-06-07 Gen Electric Heat-insulating units for refrigerator cabinets
US3073268A (en) * 1957-04-04 1963-01-15 Gen Dynamics Corp Apparatus for braze-bonding metallic parts
US2987813A (en) * 1957-05-01 1961-06-13 American Resistor Corp Hermetically sealing a tubular element or container
US3156975A (en) * 1959-02-16 1964-11-17 Evacuated Insulation Res Ltd Method of making heat insulating panels
US3110961A (en) * 1959-04-06 1963-11-19 North American Aviation Inc Honeycomb sandwich panel brazing
US3167159A (en) * 1959-07-30 1965-01-26 Gen Electric Insulating structures with variable thermal conductivity and method of evacuation
US4325183A (en) * 1976-09-07 1982-04-20 Welwyn Electric Limited Process for producing an electrical resistor having a metal foil bonded to a ceramic or glass-ceramic substrate
US4979919A (en) * 1987-05-15 1990-12-25 Hitachi, Ltd. Method and apparatus for manufacturing cathode-ray tubes
US5098498A (en) * 1989-10-10 1992-03-24 Manville Corporation Apparatus and method for encapsulating contoured articles
WO1996001346A1 (en) * 1994-07-06 1996-01-18 Owens Corning Vacuum insulation panel and method for manufacturing
US5795639A (en) * 1995-03-16 1998-08-18 Owens Fiberglas Technology, Inc. Vacuum insulation panel having blended wool filler and method for manufacturing
WO2008071637A2 (en) * 2006-12-11 2008-06-19 Single Buoy Moorings Inc. Cryogenic transfer hose having a fibrous insulating layer and method of constructing such a transfer hose
WO2008071637A3 (en) * 2006-12-11 2008-09-04 Single Buoy Moorings Cryogenic transfer hose having a fibrous insulating layer and method of constructing such a transfer hose
US20100024911A1 (en) * 2006-12-11 2010-02-04 Single Buoy Moorings Inc. Cryogenic transfer hose having a fibrous insulating layer and method of constructing such a transfer hose
CN101589262B (en) * 2006-12-11 2011-10-26 单点系泊公司 Cryogenic transfer hose having a fibrous insulating layer and method of constructing such a transfer hose
US8122914B2 (en) 2006-12-11 2012-02-28 Single Buoy Moorings Inc. Cryogenic transfer hose having a fibrous insulating layer and method of constructing such a transfer hose
AU2007332612B2 (en) * 2006-12-11 2012-03-22 Trelleborg Industrie Sas Cryogenic transfer hose having a fibrous insulating layer and method of constructing such a transfer hose
RU2571696C2 (en) * 2006-12-11 2015-12-20 Треллеборг Индустри Сас Cryogenic transfer hose with fibrous insulating ply
WO2008071373A2 (en) * 2006-12-13 2008-06-19 Woschko Winlite Gmbh Method of producing a vacuum panel, one such vacuum panel, and a masonry block using said panel
WO2008071373A3 (en) * 2006-12-13 2008-09-18 Woschko Winlite Gmbh Method of producing a vacuum panel, one such vacuum panel, and a masonry block using said panel
EP3590672A1 (en) * 2010-11-05 2020-01-08 Lightweight Labs, LLC Thermal processing and consolidation system and method
US11435132B2 (en) 2020-05-15 2022-09-06 Whirlpool Corporation Method for manufacturing a vacuum insulated structure

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