WO2006083314A2 - Insulation process - Google Patents
Insulation process Download PDFInfo
- Publication number
- WO2006083314A2 WO2006083314A2 PCT/US2005/023257 US2005023257W WO2006083314A2 WO 2006083314 A2 WO2006083314 A2 WO 2006083314A2 US 2005023257 W US2005023257 W US 2005023257W WO 2006083314 A2 WO2006083314 A2 WO 2006083314A2
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- insulation
- aircraft
- vacuum
- vacuum elements
- article
- Prior art date
Links
- 238000009413 insulation Methods 0.000 title claims abstract description 93
- 238000000034 method Methods 0.000 title claims abstract description 43
- 230000008569 process Effects 0.000 title claims abstract description 40
- 239000003981 vehicle Substances 0.000 claims description 35
- 239000011521 glass Substances 0.000 claims description 17
- 239000010410 layer Substances 0.000 claims description 15
- 239000000463 material Substances 0.000 claims description 15
- 229920006254 polymer film Polymers 0.000 claims description 8
- 239000011241 protective layer Substances 0.000 claims description 8
- 239000011159 matrix material Substances 0.000 claims description 6
- 239000004005 microsphere Substances 0.000 claims description 6
- 230000001681 protective effect Effects 0.000 claims description 6
- 239000002184 metal Substances 0.000 claims description 2
- 229910052751 metal Inorganic materials 0.000 claims description 2
- 229920000642 polymer Polymers 0.000 claims description 2
- 150000002739 metals Chemical class 0.000 claims 1
- 239000010408 film Substances 0.000 description 29
- 239000000853 adhesive Substances 0.000 description 18
- 230000001070 adhesive effect Effects 0.000 description 18
- 239000004834 spray adhesive Substances 0.000 description 11
- 230000004888 barrier function Effects 0.000 description 9
- 229920000728 polyester Polymers 0.000 description 7
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 7
- 238000000576 coating method Methods 0.000 description 6
- 239000011152 fibreglass Substances 0.000 description 6
- NIXOWILDQLNWCW-UHFFFAOYSA-N acrylic acid group Chemical group C(C=C)(=O)O NIXOWILDQLNWCW-UHFFFAOYSA-N 0.000 description 5
- 238000009833 condensation Methods 0.000 description 5
- 230000005494 condensation Effects 0.000 description 5
- 238000010276 construction Methods 0.000 description 5
- 238000012546 transfer Methods 0.000 description 5
- 239000000443 aerosol Substances 0.000 description 4
- 239000011248 coating agent Substances 0.000 description 4
- 239000006260 foam Substances 0.000 description 4
- 230000014759 maintenance of location Effects 0.000 description 4
- 239000012298 atmosphere Substances 0.000 description 3
- 239000013039 cover film Substances 0.000 description 3
- 239000012528 membrane Substances 0.000 description 3
- 230000008439 repair process Effects 0.000 description 3
- 238000007789 sealing Methods 0.000 description 3
- 239000002023 wood Substances 0.000 description 3
- 230000007423 decrease Effects 0.000 description 2
- 239000002274 desiccant Substances 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000007689 inspection Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 230000035515 penetration Effects 0.000 description 2
- 229920002620 polyvinyl fluoride Polymers 0.000 description 2
- 125000006850 spacer group Chemical group 0.000 description 2
- KXGFMDJXCMQABM-UHFFFAOYSA-N 2-methoxy-6-methylphenol Chemical compound [CH]OC1=CC=CC([CH])=C1O KXGFMDJXCMQABM-UHFFFAOYSA-N 0.000 description 1
- KHOITXIGCFIULA-UHFFFAOYSA-N Alophen Chemical compound C1=CC(OC(=O)C)=CC=C1C(C=1N=CC=CC=1)C1=CC=C(OC(C)=O)C=C1 KHOITXIGCFIULA-UHFFFAOYSA-N 0.000 description 1
- 241000288673 Chiroptera Species 0.000 description 1
- 239000004820 Pressure-sensitive adhesive Substances 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 239000002216 antistatic agent Substances 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 229920006231 aramid fiber Polymers 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 239000011230 binding agent Substances 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 239000000356 contaminant Substances 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 239000003063 flame retardant Substances 0.000 description 1
- -1 for example Substances 0.000 description 1
- 230000008014 freezing Effects 0.000 description 1
- 238000007710 freezing Methods 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 239000012774 insulation material Substances 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 230000000737 periodic effect Effects 0.000 description 1
- 230000035699 permeability Effects 0.000 description 1
- 239000005011 phenolic resin Substances 0.000 description 1
- 229920001568 phenolic resin Polymers 0.000 description 1
- 229920006327 polystyrene foam Polymers 0.000 description 1
- 230000002940 repellent Effects 0.000 description 1
- 239000005871 repellent Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60R—VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
- B60R13/00—Elements for body-finishing, identifying, or decorating; Arrangements or adaptations for advertising purposes
- B60R13/08—Insulating elements, e.g. for sound insulation
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/12—Construction or attachment of skin panels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60R—VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
- B60R13/00—Elements for body-finishing, identifying, or decorating; Arrangements or adaptations for advertising purposes
- B60R13/08—Insulating elements, e.g. for sound insulation
- B60R13/0815—Acoustic or thermal insulation of passenger compartments
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/066—Interior liners
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/40—Sound or heat insulation, e.g. using insulation blankets
-
- 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
-
- 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
- F16L59/06—Arrangements using an air layer or vacuum
- F16L59/065—Arrangements using an air layer or vacuum using vacuum
-
- 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
- This invention relates to processes for providing thermal and/or acoustic shielding to, for example, transportation vehicles such as aircraft.
- Blankets providing thermal and/or acoustic insulation are used in aircraft and other vehicles to shield passengers from engine and aerodynamic noise and from temperature extremes.
- One problem with such blankets is moisture uptake. This problem is particularly significant in aircraft, where weight increases due to water entrapment in the blankets can be dramatic.
- a commercial airliner at cruising altitude experiences exterior temperatures significantly below freezing, often temperatures as low as -4O 0 C.
- the passengers and crew of the aircraft produce significant amounts of water vapor within the fuselage, and this water vapor tends to condense on cold surfaces presented either on the interior cabin wall, within the insulation in the space between the interior cabin wall and the exterior skin of the aircraft, or on the inside of the exterior skin.
- Condensation on the interior cabin wall is undesirable from a passenger comfort aspect. Condensation within the insulation is undesirable because it decreases the efficiency of the insulation and because the added weight from the condensed water increases the cost of operation of the aircraft and decreases its payload capacity.
- the fiberglass blankets work well when initially installed. However, the necessary holes in the exterior membrane allow water to enter into the blankets. It is estimated that this water can increase the weight of the thermal blanket three fold within a three-year period of typical airline service. Another shortcoming of the fiberglass blankets is that they generally do not effectively address low frequency sounds (for example, frequencies below about 500 Hertz).
- this invention provides such a process, which comprises providing a vehicle with an insulation system comprising at least one insulation article comprising a plurality of discrete, vacuum-containing cells.
- the vehicle can be, for example, an automobile, truck, train, boat, ship, or aircraft (preferably, an aircraft; more preferably, a commercial aircraft; most preferably, a commercial jet that has a passenger capacity of at least about 100).
- the article comprises a matrix material (more preferably, a flexible or semi- rigid matrix material; most preferably, a polymeric film).
- the cells of the article can be integral to the article (that is, formed by the matrix material), but, preferably, a second material is used to form vacuum elements that can be, for example, enclosed by the matrix material or attached thereto.
- vacuum-based insulation Not only is a vacuum the ultimate insulation material from an acoustic and thermal standpoint (as sound, including low frequency sound, cannot travel through a vacuum, and thermal energy is not transferred through a vacuum by conduction or convection), but vacuum-based insulation also does not require perforations or vents to avoid the ballooning problems associated with pressure/altitude changes.
- the insulation articles used in the process of the invention provide effective thermal and acoustic insulation with little or no moisture uptake and/or retention. Since the articles rely upon multiple independent vacuums for their effectiveness, a loss of vacuum in one part of the article (due, for example, to a puncture or tear) does not necessarily destroy the insulation characteristics of the entire article. Thus, the articles are more durable (and more robust during installation and removal) than articles that comprise a single vacuum. At least some embodiments of the process of the invention therefore meet the need for processes that provide effective thermal and/or acoustic shielding without significant moisture uptake and/or retention problems.
- Insulation articles useful in carrying out the process of the invention include those that comprise a plurality of discrete, vacuum-containing cells.
- the articles comprise at least one material that is capable of holding (preferably, for at least about one year) a vacuum (for example, of about 0.5 atmosphere (380 torr) or less) and that does not collapse under the vacuum due to its own inherent rigidity, or due to the assistance of a support structure (or spacer), which can be either separate or integral (for example, a microstructure generated in or on the material itself).
- the articles comprise materials that are relatively light in weight; more preferably, at least some of the materials are flexible, so as to provide articles that are at least somewhat flexible in nature. Numerous useful configurations can be envisioned.
- insulation articles comprising vacuum-containing spheres ("spherical vacuum elements") made of a rigid material (for example, glass microspheres) can be utilized.
- Such articles can be in the form of a panel (for example, a foam panel) comprising the spheres, or, alternatively, the articles can optionally further comprise one or more protective layers or even a protective casing or bag (for example, comprising polymer film) that substantially or even fully encloses the spheres.
- the layers and/or bag can be either flexible, semi-rigid, or rigid.
- microspheres can be preferred because of their greater durability and resistance to damage from impact and vibration, larger spheres can also be utilized.
- the spheres can be attached to the protective layer(s) or bag, and/or a binder can be added to the spheres to increase the rigidity of the article and to prevent or reduce sphere movement.
- a rigid material for example, glass, metal, or a rigid polymer
- multiple vacuum elements each comprising a vacuum- containing cell
- These vacuum elements can be placed into (and/or attached to) a protective bag (for example, comprising polymer film) or can be supported on, attached to, and/or encased in, for example, one or more protective layers of polymer film to form a vacuum-containing sheet that is somewhat analogous to bubble wrap.
- the resulting insulation article can be flexible (for example, due to the flexibility of the film extending between vacuum elements) yet still hold a vacuum.
- insulation articles comprising multiple flexible vacuum elements can be utilized.
- a flexible film for example, a polymeric film having low gas permeability, a metallized polymer film, a multi-layer film, or a combination thereof
- the elements can be in the form of sheets that can be stacked or layered to produce an insulation article.
- Spacers for example, gas-containing or vacuum-containing microspheres; a stiff, light-weight, nonwoven skeletal structure; or a film microstructure such as a plurality of micro-pins
- film supports for example, gas-containing or vacuum-containing microspheres; a stiff, light-weight, nonwoven skeletal structure; or a film microstructure such as a plurality of micro-pins
- the articles can further comprise one or more protective layers or even a protective casing or bag (for example, comprising polymer film) that substantially or even fully encloses the flexible vacuum elements.
- the protective layers and/or bag can be either flexible, semi-rigid, or rigid, and the flexible vacuum elements can optionally be attached thereto.
- the article can further comprise one or more high-temperature resistant materials (including, for example, materials that are resistant to flame propagation and/or flame penetration), one or more adhesive compositions or films, one or more scrims (for example, woven polymeric fabric), one or more water repellent coatings, one or more intumescent additives or coatings, one or more reflective films (for example, for controlling radiant energy), and one or more polymer films (which can optionally be metallized), as well as flame retardants, antistatic agents, anti-mildew agents, and the like.
- high-temperature resistant materials including, for example, materials that are resistant to flame propagation and/or flame penetration
- one or more adhesive compositions or films including, for example, materials that are resistant to flame propagation and/or flame penetration
- scrims for example, woven polymeric fabric
- water repellent coatings for example, woven polymeric fabric
- intumescent additives or coatings for example, for controlling radiant energy
- reflective films for example, for controlling radiant energy
- polymer films which can optional
- the above-described insulation articles can be manufactured by known methods and can further comprise one or more attachment devices for use in attaching the articles to each other and/or to the vehicle.
- Useful attachment devices include adhesives (for example, pressure-sensitive adhesives or non-tacky adhesives), re-closable fasteners (for example, hook and loop fasteners or dual lock fasteners), mechanical interlocks (for example, tongue and groove, buttons and button holes, snaps, and shaped "puzzle-like" edges or structures), clips, pins, and the like, and combinations thereof.
- the attachment devices are preferably an integral part of the article, but separate attachment devices can be utilized, if desired.
- the articles can be of any shape and size that facilitates coverage of a vehicle surface.
- the shapes can be designed to match the shapes of vehicle surfaces (for example, to form custom-shaped articles) and can be provided with one or more cuts or holes to accommodate surface protrusions, etc.
- usefully shaped articles include spherical articles and "two-dimensional" panels or sheets or thicker versions thereof (three-dimensional "solids") that are, for example, square (six faces), rectangular (six faces), triangular (five faces), hexagonal (eight faces), octagonal (ten faces), doughnut-shaped, and the like.
- the particular shape and size of the articles that is chosen for carrying out the process of the invention will vary, depending, for example, upon the size of the vehicle and its surface configurations.
- the vehicle can be provided with the insulation articles in any desired manner (for example, by bringing the articles in or on the vehicle or one or more of its components, for example, by placement, application, or attachment).
- the insulation articles can, for example, be attached to the vehicle and/or to each other to form the insulation system. This can be accomplished using any attachment device that is capable of use with the materials comprising the insulation articles and with the vehicle surface.
- the insulation articles can be coated with a first adhesive that will adhere only to itself and will release when pulled upon. Such an adhesive generally cannot aggressively bind dirt or other contaminants.
- a second adhesive can be used to attach the insulation articles to the vehicle surface.
- mechanical fastening systems can be used to attach the articles to each other, and an adhesive can be used to attach the articles to the vehicle surface.
- the insulation articles When the insulation articles are in the form of panels or sheets, they can be laid down in an overlapping manner similar to the manner in which roofing shingles are laid down. Such overlap can reduce thermal and acoustic leakage at the joints between the insulation articles and increase the insulating properties of the system. This approach can facilitate installation in confined spaces and enable desirable thermal and acoustic properties to be achieved in such spaces.
- adhesive can be used on one side of the panels or sheets for attachment both to the vehicle surface and to other panels or sheets. Mechanical fasteners can also be used to hold each sheet to the one below.
- the insulation process of the invention is particularly useful in insulating aircraft by providing (for example, applying or attaching) the insulation system to an area anywhere between and including (i) the interior surface of the exterior skin of the aircraft and (ii) the exterior surface of the interior compartments of the aircraft (including the underside of the floor of the passenger compartment).
- at least one interior panel of the vehicle can comprise the insulation article (which can be, for example, attached to the panel or an integral part of the panel).
- the insulation articles can be designed to be flexible enough to push around irregular shapes on the aircraft surface or can simply be positioned to allow wire penetrations, etc.
- the insulation articles can be designed to be sufficiently stiff yet elastic to enable them to be snapped into place over the frame. Such insulation articles can insulate the frame and also provide attachment sites for the remainder of the insulation system.
- An insulation article is constructed by first cutting OrcofilmTM AN-54W cover film (a heat-sealable, metallized polyvinyl fluoride film available from Orcon Corporation, Union City, California) into two 1 m 2 pieces. Four one meter lengths of wood, 5 mm by 25 mm, are then cut and joined together with wood glue to produce a i m 2 wood frame, 25 mm thick. One piece of the cover film is then placed on the wooden frame and taped to it using OrcotapeTM OT-54W tape (a reinforced, metallized, pressure sensitive polyvinyl fluoride tape available from Orcon Corporation, Union City, California) to seal off one of the two open faces of the frame.
- OrcofilmTM AN-54W cover film a heat-sealable, metallized polyvinyl fluoride film available from Orcon Corporation, Union City, California
- the frame is then filled with 3MTM ScotchliteTM Kl Glass Bubbles (hollow glass microspheres having an internal pressure in the range of 1/3 of an atmosphere, available from 3M Company, St Paul, Minnesota) to a depth of slightly more than 25 mm.
- the frame with the glass bubbles is vibrated by hand to consolidate their packing volume.
- a straight edge in the form of a one-meter rule is then run over the exposed surface of the glass bubbles to level them to a depth of 25 mm.
- the second piece of cover film is then placed over the exposed glass bubbles and the remaining open face of the frame and taped in place as previously described to provide an insulation article.
- the insulation article is attached to a vehicle by using 3MTM Adhesive Transfer Tape 468MP (comprising an acrylic type of adhesive, available from 3M Company, St. Paul, Minnesota).
- Example 2 Vehicle Insulation Process Using Insulation Article Comprising Glass Bubbles
- 3MTM ScotchliteTM Kl Glass Bubbles are heat treated under vacuum to further reduce their internal pressure. This is done by placing the glass bubbles in an ultra high vacuum chamber Model LVC1220-HU (available from LACO Technology Incorporated, Salt Lake City, Utah), reducing the chamber pressure to at least Ix 10 "9 Torr, and increasing the temperature to 900°C. After one week under these conditions, to facilitate pressure equalization, the glass bubbles are slowly cooled to room temperature and then returned to atmospheric pressure. The resulting reduced pressure glass bubbles are used to construct an insulation article and to attach it to a vehicle as described in Example 1.
- Model LVC1220-HU available from LACO Technology Incorporated, Salt Lake City, Utah
- Non-spherical Glass Vacuum Elements Individual non-spherical, glass vacuum elements measuring approximately 50 mm long by 30 mm wide by 10 mm thick and having an internal reduced pressure of IxIO "7 Torr are made by means of conventional glass technology. A wall thickness of 0.2 to 2.0 mm is selected to provide durability without excessive weight.
- An insulation article is constructed by adhering the vacuum elements in place on a sheet of MylarTM SBL heat sealable film (a multilayer, polyester-based film having a metallized coating and heat sealable layers, available from Dupont Teijin FilmsTM, Hopewell, Virginia) using 3MTM Super 77TM Spray Adhesive (an aerosol spray adhesive available from 3M Company, St
- the heat sealable film has a thickness in the range of 25.4 micrometers to 127 micrometers.
- the spacing between each of the elements is on the order of 2 to 10 mm, which is sufficient to allow a resulting insulation article comprising 10 mm thick elements to be conformable.
- a second sheet of MylarTM SBL heat sealable film is then adhered over the vacuum elements and to the first sheet of film, again using 3MTM Super 77TM Spray Adhesive.
- the resulting construction is then heat sealed around its edges and between the rows and columns of vacuum elements using a standard heat sealer available from Packco Incorporated, Rocky Mount, Missouri, to provide an insulation article.
- the insulation article is attached to a vehicle by using 3MTM Adhesive Transfer Tape 468MP (comprising an acrylic type of adhesive, available from 3M Company, St. Paul, Minnesota).
- Individual vacuum elements are made by vacuum sealing a core of INSTILL foam (a micro-cellular, open-cell polystyrene foam available from Dow Chemical Company, Midland, Michigan) measuring 50 mm long by 20 mm wide by 10 mm thick within MylarTM SBL barrier film (a multilayer, polyester-based film having a metallized coating and heat sealable layers, available from Dupont Teijin FilmsTM, Hopewell, Virginia).
- INSTILL foam a micro-cellular, open-cell polystyrene foam available from Dow Chemical Company, Midland, Michigan
- MylarTM SBL barrier film a multilayer, polyester-based film having a metallized coating and heat sealable layers, available from Dupont Teijin FilmsTM, Hopewell, Virginia.
- a vacuum chamber equipped with a thermal sealing means is employed to achieve a vacuum of approximately 0.05 Torr.
- a desiccant is incorporated into each individual vacuum element.
- a plurality of the elements is placed on a sheet of MylarTM SBL barrier film using 3MTM Super 77TM Spray Adhesive (an aerosol spray adhesive available from 3M Company, St Paul, Minnesota) to hold the elements in position.
- the spacing between each of the elements is on the order of 2 to 10 mm, which is sufficient to allow a resulting insulation article comprising 10 mm thick elements to be conformable.
- a second sheet of MylarTM SBL barrier film is then positioned over the plurality of elements and held in position by using 3MTM Super 77TM Spray Adhesive.
- the resulting construction is then heat sealed around its edges and between the rows and columns of vacuum elements to provide an insulation article.
- the insulation article is attached to a vehicle by using 3MTM Adhesive Transfer Tape 468MP (comprising an acrylic type of adhesive, available from 3M Company, St. Paul, Minnesota).
- a flexible, multilayer insulation article is constructed by laying two of the flexible insulation articles described in Example 4 on top of each other. In order to improve insulation performance, the articles are offset by 10 mm in the width direction and 25 mm in the length direction, so as to be overlapping. The two layers are held together with 3MTM Super 77TM Spray Adhesive (an aerosol spray adhesive available from 3M Company, St Paul, Minnesota).
- the resulting two-layer construction is placed on a comparably sized piece of MylarTM SBL barrier film (a multilayer, polyester-based film having a metallized coating and heat sealable layers, available from Dupont Teijin FilmsTM, Hopewell, Virginia) and held in position on the barrier film using 3MTM Super 77TM Spray Adhesive.
- a second, similarly sized piece of barrier film is then adhered to the top layer of the two-layer construction in a similar manner.
- the edges of the two pieces of barrier film are then heat-sealed together to provide a multilayer, flexible insulation article.
- the insulation article is attached to a vehicle by using 3MTM Adhesive Transfer Tape 468MP (comprising an acrylic type of adhesive, available from 3M Company, St. Paul, Minnesota).
- An insulation article is constructed by cutting a 25 mm thick PlascoreTM PN2 NomexTM honeycomb core (an aramid fiber honeycomb made from DuPont NomexTM paper and coated or impregnated with a heat resistant phenolic resin, available from Plascore, Zeeland, Michigan) into a i m 2 section.
- a 0.5 mm thick sheet of MylarTM PET (a polyester-based film, available from Dupont Teijin FilmsTM, Hopewell, Virginia) measuring approximately 1 m 2 is adhered to each major surface of the core using 3MTM Super 77TM Spray Adhesive (an aerosol spray adhesive available from 3M Company, St Paul, Minnesota).
- a small amount of desiccant is added to the cells of the core.
- the resulting construction is a one-meter square panel with a plurality of individually sealed cells.
- Openings or apertures measuring approximately 0.5 mm in diameter are made into each of the cells through one of the polyester sheets. (Alternatively, one of the polyester sheets is provided with perforations prior to adhering it to the core.)
- the resulting film- covered core is then vacuum sealed within MylarTM SBL barrier film (a multilayer, polyester-based film having a metallized coating and heat sealable layers, available from Dupont Teijin FilmsTM, Hopewell, Virginia) using a vacuum chamber equipped with a thermal sealing means to achieve a vacuum of approximately 0.05 Torr.
- the barrier film seals each cell to provide an insulation article comprising a plurality of discrete, vacuum- containing cells.
- the insulation article is attached to a vehicle by using 3MTM Adhesive Transfer Tape 468MP (comprising an acrylic type of adhesive, available from 3M Company, St. Paul, Minnesota).
Abstract
Description
Claims
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BRPI0512884-6A BRPI0512884A (en) | 2004-07-01 | 2005-06-29 | insulation process |
CA002572587A CA2572587A1 (en) | 2004-07-01 | 2005-06-29 | Insulation process |
EP05856864A EP1768896A2 (en) | 2004-07-01 | 2005-06-29 | Insulation process |
JP2007519425A JP2008505008A (en) | 2004-07-01 | 2005-06-29 | Isolation method |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US58458804P | 2004-07-01 | 2004-07-01 | |
US60/584,588 | 2004-07-01 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2006083314A2 true WO2006083314A2 (en) | 2006-08-10 |
WO2006083314A3 WO2006083314A3 (en) | 2006-10-05 |
Family
ID=36616828
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2005/023257 WO2006083314A2 (en) | 2004-07-01 | 2005-06-29 | Insulation process |
Country Status (7)
Country | Link |
---|---|
EP (1) | EP1768896A2 (en) |
JP (1) | JP2008505008A (en) |
KR (1) | KR20070027763A (en) |
CN (1) | CN1980831A (en) |
BR (1) | BRPI0512884A (en) |
CA (1) | CA2572587A1 (en) |
WO (1) | WO2006083314A2 (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2007147885A1 (en) * | 2006-06-23 | 2007-12-27 | Airbus Deutschland Gmbh | Vacuum insulation panels for aircraft interiors |
DE102006039291A1 (en) * | 2006-08-22 | 2008-03-13 | Airbus Deutschland Gmbh | Frame element for use in installation of storage bin in aircraft, has longitudinal parallel struts that extend parallel to ribs of aircraft structure, when frame element is mounted to aircraft structure |
WO2019158246A1 (en) * | 2018-02-16 | 2019-08-22 | Va-Q-Tec Ag | Method for the thermal insulation of vehicles or of vehicle parts |
EP3632787A1 (en) * | 2018-10-05 | 2020-04-08 | Intumescent Systems Limited | Fire proof panel for boats and the like |
EP3725672A1 (en) | 2019-04-17 | 2020-10-21 | Airbus Operations GmbH | Interior cladding section for covering a fuselage structure of an aircraft |
FR3138651A1 (en) * | 2022-12-06 | 2024-02-09 | Airbus Operations (S.A.S.) | Method for thermal insulation of an aerostructure and aircraft comprising at least one cryogenic tank as well as an aerostructure insulated according to said method |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
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GB108035A (en) * | 1900-01-01 | |||
JPS6253221B2 (en) * | 1978-08-28 | 1987-11-09 | Torobin Leonard B | |
CH640039A5 (en) * | 1979-03-27 | 1983-12-15 | Emil Baechli | Thermal insulation |
US4513041A (en) * | 1983-08-12 | 1985-04-23 | Delluc Rene | Tubular vacuum-tight enclosures for thermal and acoustical insulating panels |
DE10025321A1 (en) * | 2000-05-22 | 2002-01-10 | Wolff Walsrode Ag | Foil laminates as high barrier foils and their use in vacuum insulation panels |
JP2002340280A (en) * | 2001-05-18 | 2002-11-27 | Jamco Corp | Vacuum insulating block |
WO2003072684A1 (en) * | 2002-02-26 | 2003-09-04 | Technology Applications, Inc. | Microsphere insulation systems |
-
2005
- 2005-06-29 EP EP05856864A patent/EP1768896A2/en not_active Withdrawn
- 2005-06-29 CA CA002572587A patent/CA2572587A1/en not_active Abandoned
- 2005-06-29 CN CNA2005800225748A patent/CN1980831A/en active Pending
- 2005-06-29 BR BRPI0512884-6A patent/BRPI0512884A/en not_active Application Discontinuation
- 2005-06-29 KR KR1020077002465A patent/KR20070027763A/en not_active Application Discontinuation
- 2005-06-29 WO PCT/US2005/023257 patent/WO2006083314A2/en active Application Filing
- 2005-06-29 JP JP2007519425A patent/JP2008505008A/en active Pending
Non-Patent Citations (1)
Title |
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None |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2007147885A1 (en) * | 2006-06-23 | 2007-12-27 | Airbus Deutschland Gmbh | Vacuum insulation panels for aircraft interiors |
US8490365B2 (en) | 2006-06-23 | 2013-07-23 | Airbus Deutschland Gmbh | Aircraft side fairing |
DE102006039291A1 (en) * | 2006-08-22 | 2008-03-13 | Airbus Deutschland Gmbh | Frame element for use in installation of storage bin in aircraft, has longitudinal parallel struts that extend parallel to ribs of aircraft structure, when frame element is mounted to aircraft structure |
US8226033B2 (en) | 2006-08-22 | 2012-07-24 | Airbus Deutchland Gmbh | Frame element, storage bin and method for installing a storage bin in an aircraft |
WO2019158246A1 (en) * | 2018-02-16 | 2019-08-22 | Va-Q-Tec Ag | Method for the thermal insulation of vehicles or of vehicle parts |
EP3632787A1 (en) * | 2018-10-05 | 2020-04-08 | Intumescent Systems Limited | Fire proof panel for boats and the like |
EP3725672A1 (en) | 2019-04-17 | 2020-10-21 | Airbus Operations GmbH | Interior cladding section for covering a fuselage structure of an aircraft |
DE102019205578A1 (en) * | 2019-04-17 | 2020-10-22 | Airbus Operations Gmbh | INTERIOR PANELING PART FOR CLADDING A HULL STRUCTURE OF AN AIRCRAFT |
US11420721B2 (en) | 2019-04-17 | 2022-08-23 | Airbus Operations Gmbh | Internal cladding part for cladding a fuselage structure of an aircraft |
US11661171B2 (en) | 2019-04-17 | 2023-05-30 | Airbus Operations Gmbh | Internal cladding part for cladding a fuselage structure of an aircraft |
FR3138651A1 (en) * | 2022-12-06 | 2024-02-09 | Airbus Operations (S.A.S.) | Method for thermal insulation of an aerostructure and aircraft comprising at least one cryogenic tank as well as an aerostructure insulated according to said method |
Also Published As
Publication number | Publication date |
---|---|
CA2572587A1 (en) | 2006-08-10 |
BRPI0512884A (en) | 2008-04-15 |
CN1980831A (en) | 2007-06-13 |
JP2008505008A (en) | 2008-02-21 |
KR20070027763A (en) | 2007-03-09 |
WO2006083314A3 (en) | 2006-10-05 |
EP1768896A2 (en) | 2007-04-04 |
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