WO2002002986A1 - Evacuated panel for thermal insulation of cylindrical bodies - Google Patents
Evacuated panel for thermal insulation of cylindrical bodies Download PDFInfo
- Publication number
- WO2002002986A1 WO2002002986A1 PCT/IT2001/000338 IT0100338W WO0202986A1 WO 2002002986 A1 WO2002002986 A1 WO 2002002986A1 IT 0100338 W IT0100338 W IT 0100338W WO 0202986 A1 WO0202986 A1 WO 0202986A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- panel
- panel according
- thickness
- curve
- filling material
- Prior art date
Links
Classifications
-
- 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
-
- 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
Definitions
- the present invention relates to an evacuated panel which enables the thermal insulation of a substantially cylindrical body to be obtained.
- Evacuated panels, and particularly those made with plastic materials, are being increasingly used in all the fields wherein thermal insulation at temperatures lower than about 100 °C is required.
- an evacuated panel is formed of an envelope, having generally a thickness of some tens or hundreds of micrometers, wherein a filling material having a thickness between some millimeters and some centimeters is provided.
- the heat transport between the two faces of the panel is due to the sum of four main phenomena, namely conduction in the filling material; convection due to the presence of gas traces in the panel; radiative transport inside the panel; and finally conduction in the sheet or sheets which form the envelope, known in the field as "skin effect", possibly through the thermal bridge which is formed at the edge of the panel at the welding zones of said sheets.
- the envelope has the function of preventing (or reducing as much as possible) the entrance of atmospheric gases inside the panel, so as to reduce the contribution of convection to the total heat transport.
- the envelope is made with so-called "barrier" sheets, characterized by having gas permeability being as low'as possible, which can be formed of a single component but more frequently are multi-layers of different components.
- the barrier effect is conferred by one of the component layers, whereas the other layers generally have functions of mechanical support and protection of the barrier layer.
- the most potent barrier effect is obtained by inserting a metal sheet (generally aluminum having a thickness of about 4-10 ⁇ m) between two or more sheets of plastic material; since the metals are good heat conductors, the tlnckness of the aluminum layer is determined by the compromise between the need of maximizing the barrier to the gas entrance and that of minimizing the skin effect.
- the filling material has the function of spacing apart the two opposite faces of the envelope when vacuum is created in the panel.
- This material can be inorganic, such as silica powder, glass fibers, aerogels, diatomaceous earth, etc., or organic, such as rigid foams of polyurethane or polystyrene, both in the fonn of boards and of powders.
- the filling material must be anyway porous or discontinuous, so that the porosities or the interstices can be evacuated.
- the thickness of the filling material (and therefore of the panel) is determined by the required features of insulation: a better insulation is obviously obtained with higher thickness values of the filling material.
- these panels contain in most cases also one or more materials (generally referred to as getter materials) capable of sorbing these gases so as to maintain the pressure inside the panel at the desired values.
- the known evacuated panels are rigid, and generally have a planar conformation.
- the surfaces which have to be insulated are curved, and mainly cylindrical.
- the insulating material can be applied externally and in sight, like in the case of the piping for transportation of a fluid having a temperature different from the room temperature, for example pipings for air-conditioning or heating, or for the fluid transport in industrial plants.
- the insulant can be placed inside an interspace, like in the case of the bath-heaters, of the containers such as Dewar or thermal bottles, or of the pipings used for oil transportation in the arctic regions.
- One of the methods used up to now for carrying out the thermal insulation of bodies having non-planar surfaces consists in connecting several plane panels to each other, for example by sticking together the edges thereof by means of a glue, so as to obtain a composite structure which can be bent along the junction lines so as to adapt it to the shape of the body which has to be insulated.
- This solution is however not very satisfying, because the assembly of the panels does not contact closely (with the exception of a few points) the surfaces which have to be insulated and, in addition to this, heat transfers take place at the junctions, with the result of a scarce efficiency of thermal insulation.
- Patent application WO 96/32605 in the name of the British company ICI describes a method for manufacturing rigid evacuated panels having a non-planar shape.
- the method consists in making in the filling material (a board of a polymeric foam having a thickness equal to that of the desired panel), prior to the evacuating step, grooves ananged in the desired direction and having suitable width and depth. Subsequently, the filling material is inserted into an envelope and the assembly is subjected to the evacuating step. Finally, the evacuated panel is sealed.
- the envelope is forced by the atmospheric pressure to adhere to the surface of the grooves; due to the tensile forces which are exerted on the envelope, the panels bend along the grooves and take on the final non-planar shape.
- the resulting shape of the panel is nearly cylindrical.
- the thickness of the panel is not regular in all the parts thereof, being lower at the bending lines, with the result of reduced thermal insulation properties along these bending lines.
- breakings also microscopic, can be created in the envelope and become preferential channels for the permeation of gases towards the inside of the panel, thus permanently compromising the properties of thermal insulation of the panel itself.
- the shape, size, distances and reciprocal positioning of the grooves fixedly determine the final shape of the non-planar panel, so that these panels have to be specially produced for every single application.
- the curving of these panels takes place at the first exposure to air, and therefore during the manufacturing process or immediately after that: consequently these panels have, as soon as they are manufactured, a notable overall size which makes unprofitable their storage and transport.
- object of the present invention is providing an evacuated panel for the thermal insulation of bodies having a cylindrical curved lateral surface, which is free from said drawbacks. Said object is obtained by an evacuated panel whose main features are specified in the first claim and other features are specified in the following claims.
- FIG. 1 shows an example of cylinder according to the broad geometrical definition thereof
- - Figure 2 shows a right cylindrical body obtained from Figure 1, which can be thermally insulated by means of a panel according to the invention
- FIG. 3 shows a cutaway view of an evacuated panel according to the present invention in its planar form
- - Figure 4 schematically shows a geometrical requirement which has to be met by the panels according to the invention
- the panels according to the invention differ from those according to the prior art because they make up the required total insulating thickness rolling a panel having a low thickness at least twice around the body which is to be insulated.
- Tins new configuration brings about a number of advantages.
- the portion in contact with the environment transmits heat through the envelope to a subsequent layer of the rolled panel. Therefore, the heat must cover a spiral path along the lower face of the panel in before reaching said body which is to be insulated. In this way, the skin effect is largely reduced to negligible values as a contribute of heat conduction between the two faces of the panel.
- the insulation thickness is obtained as a multiple of the constant thickness of the panel, thus avoiding the grooves of patent application WO 96/32605 which represent zones having a reduced thickness and therefore of higher thermal conductivity between the two faces of the panel.
- the several small creases formed on the internal side of the envelope during the curving cannot, because of their small entity, cause a breaking of the envelope itself and therefore a permeation of atmospheric gases towards the inside of the panel.
- the evacuated panels of the present invention are manufactured, stored and transported to the place of final application in the plane fonn, with notable gain of space and costs; each panel is then rolled and fastened around the body to be insulated at the time and place of the effective use.
- the tenn "cylinder” (and the tenns therefrom derived) will be used in the present invention in the broadest meaning thereof, shown in figure 1, that is the surface S determined by a straight line R intersecting a plane P with an angle ⁇ and moving parallely to itself along a close curved line C laying on said plane P.
- Figure 2 shows a generic solid body 1 which can be thermally insulated by means of a panel according to the present invention: this solid body has a lateral wall S' which is fonned of a portion of the cylindrical surface S of figure 1 having length L, and two bases which have the curve C as their perimeter; said two bases are ⁇ defined by the intersection of surface S with two parallel planes, shown in this case perpendicular to straight line R, so that curves C and C are equal in the case that angle ⁇ is 90°.
- Body 1 can be solid, but in the common applications of the evacuated panels can be internally empty, for example in the case of a container or a piping for fluids.
- the most important practical application of the panels according to the invention is for thennally insulating bodies whose lateral wall S' is a portion of surface S obtained when angle ⁇ is equal to 90° and curve C is a circumference (the common said cylinders).
- evacuated panel 2 is shown to be formed in a known way of a filling material 3 closed inside an envelope 4, for example multi-layer.
- Panel 2 has the shape of a parallelepiped having a very reduced thickness, h, and lateral dimensions l ⁇ and 1 .
- the shape can be conferred to the panel by the filling material when it is a board, for example of a polymeric foam.
- the panel is shaped during the manufacture, by introducing the powder in an envelope, evacuating the envelope while it is kept in a suitable die, and by finally sealing the open edge of the envelope so as to form the final envelope; the shape conferred by means of the die is then maintained because of the external pressure exerted through the envelope on the powders, thus keeping them compact.
- Preferred for the purposes of the invention is the use as filling material of boards of polymeric foams, particularly the open cell rigid polyurethane, well known in the field of evacuated panels.
- the multi-layer sheets which generally comprise at least one layer, having a relatively high thickness, of a polymeric material provided with good mechanical features, particularly plasticity, which fonns the mechanical support of the multi-layer; at least one layer of a material having barrier properties towards atmospheric gases, which can be polymeric or inorganic, preferably a metal and even more preferably aluminum; and at least another polymeric layer, as a covering and mechanical protection for the barrier layer.
- Multi-layers formed of five, six or even more layers laid one over the other are also common. The manufacture of the envelope starting from these is generally made by heat-sealing, by techniques known in the field.
- the panels according to the invention preferably contain one or more getter materials, that is materials capable of chemically sorbing moisture and other atmospheric gases.
- getter materials that is materials capable of chemically sorbing moisture and other atmospheric gases.
- getter systems with two or three getter materials, containing at least one moisture chemical sorber and at. least one component selected among a transition metal oxide (having mainly the function of sorbing hydrogen, CO and hydrocarbons) and an alloy based on barium and lithium (having mainly the function of nitrogen sorption).
- a transition metal oxide having mainly the function of sorbing hydrogen, CO and hydrocarbons
- an alloy based on barium and lithium having mainly the function of nitrogen sorption
- the thickness of the panel, h must be such that the panel can be bent without damaging the integrity thereof. This feature depends both on the filling material of the panel, and on the foreseen application. It is generally known that it is possible to elastically defonn a planar flexible body so as to curve it, by applying a force in different points thereof; said force is directly proportional to the cube of the thickness thereof and inversely proportional to the bending radius which is desired, with a proportionality constant different for each material which depends on the mechanical properties thereof. According to this relation, an increase of the curvature is obtained by applying increasing forces to an initially plane panel having a certain thickness. However, if the panel is subjected to an excessive force, it breaks.
- h/r ratio wherein h is the panel thickness and r is the bending radius of the curve C (which fo ⁇ ns the cross-section of body 1): with reference to the drawing of figure 4, the panel according to the invention must be such that, in every point of the curve C, the ratio h/r is not higher than a given value for each filling material. It has been found that this maximum value of the ratio h/r is about 0.20 for polyurethane rigid foams, about 0.18 for boards in polystyrene foams and about 0.10 for powder filling materials.
- a panel having a filling in polyurethane foam to be rolled around a body having a minimum bending radius of about 50 mm can have a maximum thickness of about 10 mm.
- a board of polyurethane foam having this thickness can be obtained by cutting horizontally, that is parallely to the main faces thereof, the thicker boards which are usually employed for the production of plane panels of the known kind.
- the panel shown in figure 4 is suitable for being rolled at least twice around the curved lateral wall S' of a cylindrical body; therefore the two main opposite sides of said panel have the shape of a long rectangle, having sides l ⁇ and 1 .
- One of the dimensions (1 in the example of the drawing) is about double with respect to the length of curve C, so that it is possible to make at least two rollings around the body to be insulated.
- the side ⁇ ⁇ is equal to the length L of the body that has to be insulated, or to a submultiple thereof; as a matter of fact, as shown in figure 5, .
- body 1 unless body 1 has an excessive size the thennal insulation thereof can be made with only one panel 2; alternatively, as shown in figure 6, if the size L is large (for example, if body 1 is a tube), it is preferable to make the body insulation with more panels 2', 2", 2'", ... placed side by side.
- the panels according to the invention can be placed in sight, for instance in order to insulate pipings for civil applications.
- these panels can be placed inside interspaces, particularly when the difference of temperature to be kept between the surface S' and the environment is high; these conditions occurr for example in the applications of the Dewars, in thermal bottles, or in cryogenic pipings or placed in particularly cold regions, such as the arctic regions.
- the thickness h of the panel in addition to meeting the above mentioned requirements, will have to be not higher than half the thickness of the interspace.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Thermal Insulation (AREA)
- Laminated Bodies (AREA)
- Building Environments (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
Description
Claims
Priority Applications (8)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BR0112022-0A BR0112022A (en) | 2000-06-30 | 2001-06-27 | Evacuated panel for thermal insulation of cylindrical bodies |
PL01358804A PL358804A1 (en) | 2000-06-30 | 2001-06-27 | Evacuated panel for thermal insulation of cylindrical bodies |
MXPA02012690A MXPA02012690A (en) | 2000-06-30 | 2001-06-27 | Evacuated panel for thermal insulation of cylindrical bodies. |
AU2001271003A AU2001271003A1 (en) | 2000-06-30 | 2001-06-27 | Evacuated panel for thermal insulation of cylindrical bodies |
EP01949893A EP1297278A1 (en) | 2000-06-30 | 2001-06-27 | Evacuated panel for thermal insulation of cylindrical bodies |
JP2002507214A JP2004502117A (en) | 2000-06-30 | 2001-06-27 | Vacuum panel for thermal insulation of cylindrical objects |
CA002411940A CA2411940A1 (en) | 2000-06-30 | 2001-06-27 | Evacuated panel for thermal insulation of cylindrical bodies |
US10/331,887 US20030101683A1 (en) | 2000-06-30 | 2002-12-30 | Evacuated panel for thermal insulation of cylindrical bodies |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT2000MI001488A IT1318099B1 (en) | 2000-06-30 | 2000-06-30 | EVACUATED PANEL FOR THERMAL INSULATION OF CYLINDRICAL BODIES |
ITMI2000A001488 | 2000-06-30 |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US10/331,887 Continuation US20030101683A1 (en) | 2000-06-30 | 2002-12-30 | Evacuated panel for thermal insulation of cylindrical bodies |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2002002986A1 true WO2002002986A1 (en) | 2002-01-10 |
Family
ID=11445390
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/IT2001/000338 WO2002002986A1 (en) | 2000-06-30 | 2001-06-27 | Evacuated panel for thermal insulation of cylindrical bodies |
Country Status (12)
Country | Link |
---|---|
US (1) | US20030101683A1 (en) |
EP (1) | EP1297278A1 (en) |
JP (1) | JP2004502117A (en) |
KR (1) | KR20030011934A (en) |
AU (1) | AU2001271003A1 (en) |
BR (1) | BR0112022A (en) |
CA (1) | CA2411940A1 (en) |
IT (1) | IT1318099B1 (en) |
MX (1) | MXPA02012690A (en) |
PL (1) | PL358804A1 (en) |
TW (1) | TW494207B (en) |
WO (1) | WO2002002986A1 (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2003059600A1 (en) * | 2001-12-27 | 2003-07-24 | Saes Getters S.P.A. | Method for producing thermo-insulating cylindrical vacuum panels and panels thereby obtained |
WO2003098094A1 (en) * | 2002-05-21 | 2003-11-27 | Saes Getters S.P.A. | Thermoinsulating system |
US7334375B2 (en) | 2000-06-30 | 2008-02-26 | Saes Getters S.P.A. | Evacuated panel for thermal insulation of a body having non-planar surfaces |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ITMI20011458A1 (en) * | 2001-07-09 | 2003-01-09 | Getters Spa | SYSTEM FOR THE THERMAL INSULATION OF TUBULAR BODIES |
US20060272727A1 (en) * | 2005-06-06 | 2006-12-07 | Dinon John L | Insulated pipe and method for preparing same |
US7523532B2 (en) * | 2006-04-10 | 2009-04-28 | Federal Mogul World Wide, Inc. | Non-woven self-wrapping acoustic sleeve and method of construction thereof |
EP2123426A1 (en) * | 2008-05-23 | 2009-11-25 | Rockwool International A/S | Pipe section and methods for its production |
US20090311456A1 (en) * | 2008-06-12 | 2009-12-17 | Harris David A | Non-woven, self-wrapping thermal sleeve |
US20100282356A1 (en) * | 2009-05-07 | 2010-11-11 | Scott Sawyer | Low emissive radiant barrier flex (LOW-E FLEX) |
DE102016103446A1 (en) | 2016-02-26 | 2017-09-14 | Uponor Innovation Ab | Isolated pipe |
EP3354959B1 (en) | 2017-01-31 | 2019-11-06 | Powerpipe Systems AB | Improved pipe insulation |
CN113325535B (en) * | 2021-06-15 | 2023-01-13 | 长飞光纤光缆股份有限公司 | Optical fiber airtight interface device and manufacturing method thereof |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1297839A (en) * | 1970-10-27 | 1972-11-29 | ||
WO1996032605A1 (en) | 1995-04-13 | 1996-10-17 | Imperial Chemical Industries Plc | Non-planar evacuated insulation panels and a method for making same |
EP0757920A2 (en) | 1995-08-07 | 1997-02-12 | SAES GETTERS S.p.A. | Combination of getter materials and device for containing the same |
EP0769117B1 (en) | 1994-07-07 | 1998-09-23 | SAES GETTERS S.p.A. | Device for maintaining vacuum in thermally insulating jackets and process for manufacturing such a device |
EP0937939A1 (en) * | 1998-02-19 | 1999-08-25 | Wacker-Chemie GmbH | Plate like evacuated element and method of thermal insulation |
-
2000
- 2000-06-30 IT IT2000MI001488A patent/IT1318099B1/en active
-
2001
- 2001-06-22 TW TW090115320A patent/TW494207B/en not_active IP Right Cessation
- 2001-06-27 AU AU2001271003A patent/AU2001271003A1/en not_active Abandoned
- 2001-06-27 KR KR1020027017930A patent/KR20030011934A/en not_active Application Discontinuation
- 2001-06-27 MX MXPA02012690A patent/MXPA02012690A/en unknown
- 2001-06-27 CA CA002411940A patent/CA2411940A1/en not_active Abandoned
- 2001-06-27 JP JP2002507214A patent/JP2004502117A/en active Pending
- 2001-06-27 WO PCT/IT2001/000338 patent/WO2002002986A1/en not_active Application Discontinuation
- 2001-06-27 PL PL01358804A patent/PL358804A1/en unknown
- 2001-06-27 EP EP01949893A patent/EP1297278A1/en not_active Withdrawn
- 2001-06-27 BR BR0112022-0A patent/BR0112022A/en not_active Application Discontinuation
-
2002
- 2002-12-30 US US10/331,887 patent/US20030101683A1/en not_active Abandoned
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1297839A (en) * | 1970-10-27 | 1972-11-29 | ||
EP0769117B1 (en) | 1994-07-07 | 1998-09-23 | SAES GETTERS S.p.A. | Device for maintaining vacuum in thermally insulating jackets and process for manufacturing such a device |
WO1996032605A1 (en) | 1995-04-13 | 1996-10-17 | Imperial Chemical Industries Plc | Non-planar evacuated insulation panels and a method for making same |
US5843353A (en) * | 1995-04-13 | 1998-12-01 | Imperial Chemical Industries Plc | Non-planar evacuated insulation panels and a method for making same |
EP0757920A2 (en) | 1995-08-07 | 1997-02-12 | SAES GETTERS S.p.A. | Combination of getter materials and device for containing the same |
EP0937939A1 (en) * | 1998-02-19 | 1999-08-25 | Wacker-Chemie GmbH | Plate like evacuated element and method of thermal insulation |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7334375B2 (en) | 2000-06-30 | 2008-02-26 | Saes Getters S.P.A. | Evacuated panel for thermal insulation of a body having non-planar surfaces |
WO2003059600A1 (en) * | 2001-12-27 | 2003-07-24 | Saes Getters S.P.A. | Method for producing thermo-insulating cylindrical vacuum panels and panels thereby obtained |
WO2003098094A1 (en) * | 2002-05-21 | 2003-11-27 | Saes Getters S.P.A. | Thermoinsulating system |
Also Published As
Publication number | Publication date |
---|---|
JP2004502117A (en) | 2004-01-22 |
CA2411940A1 (en) | 2002-01-10 |
PL358804A1 (en) | 2004-08-23 |
US20030101683A1 (en) | 2003-06-05 |
TW494207B (en) | 2002-07-11 |
KR20030011934A (en) | 2003-02-11 |
AU2001271003A1 (en) | 2002-01-14 |
EP1297278A1 (en) | 2003-04-02 |
MXPA02012690A (en) | 2003-04-25 |
ITMI20001488A0 (en) | 2000-06-30 |
IT1318099B1 (en) | 2003-07-23 |
BR0112022A (en) | 2003-05-13 |
ITMI20001488A1 (en) | 2001-12-30 |
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