US2824364A - Method of assembling and evacuating an insulated vacuum panel - Google Patents
Method of assembling and evacuating an insulated vacuum panel Download PDFInfo
- Publication number
- 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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- Expired - Lifetime
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- 238000000034 method Methods 0.000 title description 7
- 239000007789 gas Substances 0.000 description 14
- 239000000463 material Substances 0.000 description 13
- 239000000945 filler Substances 0.000 description 11
- 239000011261 inert gas Substances 0.000 description 7
- 238000010438 heat treatment Methods 0.000 description 5
- 239000011521 glass Substances 0.000 description 4
- 239000003365 glass fiber Substances 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- 241001658031 Eris Species 0.000 description 1
- 229910001209 Low-carbon steel Inorganic materials 0.000 description 1
- 208000014769 Usher Syndromes Diseases 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 239000007799 cork Substances 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000004904 shortening Methods 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
Images
Classifications
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
- E04B1/00—Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
- E04B1/62—Insulation or other protection; Elements or use of specified material therefor
- E04B1/74—Heat, sound or noise insulation, absorption, or reflection; Other building methods affording favourable thermal or acoustical conditions, e.g. accumulating of heat within walls
- E04B1/76—Heat, 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
- E04B1/78—Heat insulating elements
- E04B1/80—Heat insulating elements slab-shaped
- E04B1/803—Heat insulating elements slab-shaped with vacuum spaces included in the slab
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B30/00—Compositions for artificial stone, not containing binders
- C04B30/02—Compositions for artificial stone, not containing binders containing fibrous materials
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
- E04C2/02—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials
- E04C2/26—Building 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
- E04C2/284—Building 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
- E04C2/292—Building 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L59/00—Thermal insulation in general
- F16L59/04—Arrangements using dry fillers, e.g. using slag wool which is added to the object to be insulated by pouring, spreading, spraying or the like
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25D—REFRIGERATORS; COLD ROOMS; ICE-BOXES; COOLING OR FREEZING APPARATUS NOT OTHERWISE PROVIDED FOR
- F25D23/00—General constructional features
- F25D23/06—Walls
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25D—REFRIGERATORS; COLD ROOMS; ICE-BOXES; COOLING OR FREEZING APPARATUS NOT OTHERWISE PROVIDED FOR
- F25D23/00—General constructional features
- F25D23/06—Walls
- F25D23/065—Details
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25D—REFRIGERATORS; COLD ROOMS; ICE-BOXES; COOLING OR FREEZING APPARATUS NOT OTHERWISE PROVIDED FOR
- F25D2201/00—Insulation
- F25D2201/10—Insulation with respect to heat
- F25D2201/12—Insulation with respect to heat using an insulating packing material
- F25D2201/124—Insulation with respect to heat using an insulating packing material of fibrous type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25D—REFRIGERATORS; COLD ROOMS; ICE-BOXES; COOLING OR FREEZING APPARATUS NOT OTHERWISE PROVIDED FOR
- F25D2201/00—Insulation
- F25D2201/10—Insulation with respect to heat
- F25D2201/14—Insulation with respect to heat using subatmospheric pressure
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
- Y02A30/00—Adapting or protecting infrastructure or their operation
- Y02A30/24—Structural elements or technologies for improving thermal insulation
- Y02A30/242—Slab shaped vacuum insulation
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
- Y02B80/00—Architectural or constructional elements improving the thermal performance of buildings
- Y02B80/10—Insulation, 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
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US452661A US2824364A (en) | 1952-10-23 | 1954-08-27 | Method of assembling and evacuating an insulated vacuum panel |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US760942XA | 1952-10-23 | 1952-10-23 | |
US452661A US2824364A (en) | 1952-10-23 | 1954-08-27 | Method of assembling and evacuating an insulated vacuum panel |
Publications (1)
Publication Number | Publication Date |
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US2824364A true US2824364A (en) | 1958-02-25 |
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Application Number | Title | Priority Date | Filing Date |
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US452661A Expired - Lifetime US2824364A (en) | 1952-10-23 | 1954-08-27 | Method of assembling and evacuating an insulated vacuum panel |
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Cited By (17)
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)
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 |
-
1954
- 1954-08-27 US US452661A patent/US2824364A/en not_active Expired - Lifetime
Patent Citations (4)
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)
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 |
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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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