FR2594747A1 - Method for assembling a superinsulating material in the form of plies - Google Patents
Method for assembling a superinsulating material in the form of plies Download PDFInfo
- Publication number
- FR2594747A1 FR2594747A1 FR8602385A FR8602385A FR2594747A1 FR 2594747 A1 FR2594747 A1 FR 2594747A1 FR 8602385 A FR8602385 A FR 8602385A FR 8602385 A FR8602385 A FR 8602385A FR 2594747 A1 FR2594747 A1 FR 2594747A1
- Authority
- FR
- France
- Prior art keywords
- screen
- perforations
- separator
- assembling
- constitutes
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/12—Layered products comprising a layer of synthetic resin next to a fibrous or filamentary layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/74—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by welding and severing, or by joining and severing, the severing being performed in the area to be joined, next to the area to be joined, in the joint area or next to the joint area
- B29C65/743—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by welding and severing, or by joining and severing, the severing being performed in the area to be joined, next to the area to be joined, in the joint area or next to the joint area using the same tool for both joining and severing, said tool being monobloc or formed by several parts mounted together and forming a monobloc
- B29C65/7437—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by welding and severing, or by joining and severing, the severing being performed in the area to be joined, next to the area to be joined, in the joint area or next to the joint area using the same tool for both joining and severing, said tool being monobloc or formed by several parts mounted together and forming a monobloc the tool being a perforating tool
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/112—Single lapped joints
- B29C66/1122—Single lap to lap joints, i.e. overlap joints
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/20—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines
- B29C66/21—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being formed by a single dot or dash or by several dots or dashes, i.e. spot joining or spot welding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
- B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles
- B29C66/45—Joining of substantially the whole surface of the articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/71—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/36—Layered products comprising a layer of synthetic resin comprising polyesters
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form
- B32B3/26—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
- B32B3/266—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by an apertured layer, the apertures going through the whole thickness of the layer, e.g. expanded metal, perforated layer, slit layer regular cells B32B3/12
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/04—Interconnection of layers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C13/00—Details of vessels or of the filling or discharging of vessels
- F17C13/001—Thermal insulation specially adapted for cryogenic vessels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2255/00—Coating on the layer surface
- B32B2255/10—Coating on the layer surface on synthetic resin layer or on natural or synthetic rubber layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2255/00—Coating on the layer surface
- B32B2255/20—Inorganic coating
- B32B2255/205—Metallic coating
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/38—Meshes, lattices or nets
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/03—Thermal insulations
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0634—Materials for walls or layers thereof
- F17C2203/0636—Metals
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0634—Materials for walls or layers thereof
- F17C2203/0658—Synthetics
- F17C2203/066—Plastics
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2209/00—Vessel construction, in particular methods of manufacturing
- F17C2209/22—Assembling processes
- F17C2209/221—Welding
Abstract
Description
L'invention vise des matériaux de super isolation qui sont notamment utilisés dans des réservoirs cryogéniques. The invention relates to super-insulation materials which are used in particular in cryogenic tanks.
De tels matériaux comprennent une feuille très mince métallisée et perforée de polyester qui constitue un écran réfléchissant et un séparateur constitué d'un tulle mince de polyester. Généralement la feuille et le tulle sont rendus solidaires par l'un de leur bord. Une telle disposition est peu pratique, car le matériau tend à plisser, surtout s'il s'agit de nappes ayant des dimensions importantes.Such materials include a very thin metallized and perforated polyester sheet which constitutes a reflecting screen and a separator made of a thin polyester tulle. Generally the sheet and the tulle are made integral by one of their edge. Such an arrangement is impractical, because the material tends to wrinkle, especially if it is plies having large dimensions.
L'un des buts de la présente invention est de remédier à cet inconvénient. One of the aims of the present invention is to remedy this drawback.
Le procédé, selon l'invention vise l'assemblage d'un matériau super isolant se présentant en nappes et formé d'au moins une feuille perforée très mince métallisée de ployester qui constitue un écran et d'au moins un tulle mince de polyester qui constitue un séparateur et est caractérisé en ce qu'il consiste à pratiquer au travers de l'écran et du séparateur des perforations à l'aide d'un outil chauffant de manière à réaliser entre l'écran et le séparateur le long du bord des perforations, une soudure. The method according to the invention relates to the assembly of a super-insulating material in layers and formed of at least one very thin perforated sheet of metallized ployester which constitutes a screen and of at least one thin polyester tulle which constitutes a separator and is characterized in that it consists in practicing through the screen and the separator perforations using a heating tool so as to produce between the screen and the separator along the edge of the perforations, a weld.
Ainsi on obtient un matériau qui ne plisse pas et qui est plus facile à utiliser. This produces a material that does not wrinkle and is easier to use.
Lorsqu'on utilise le matériau formé d'un empilage d'écrans et de séparateurs correspondants, afin d'éviter les ponts thermiques on réalise les perforations à l'aide de l'outil chauffant, décalées dans l'épaisseur du matériau. When using the material formed by a stack of screens and corresponding separators, in order to avoid thermal bridges, the perforations are made using the heating tool, offset in the thickness of the material.
L'invention va maintenant être décrite avec plus de détails en se référant à des modes de réalisation particuliers donnés à titre d'exemple seulement et représentés au dessins annexés, dans lesquels
Figure 1 est une vue en perspective montrant un matériau isolant en nappe.The invention will now be described in more detail with reference to particular embodiments given by way of example only and shown in the accompanying drawings, in which
Figure 1 is a perspective view showing an insulating sheet material.
Figure 2 est une vue en coupe. Figure 2 is a sectional view.
Le matériau isolant représenté à la figure 1 comprend une feuille très mince 1 de polyester métallisée pourvue de perforations 2 et constituant un écran et un tulle mince de polyester 3 constituant un séparateur. The insulating material shown in FIG. 1 comprises a very thin sheet 1 of metallized polyester provided with perforations 2 and constituting a screen and a thin polyester tulle 3 constituting a separator.
Pour réaliser l'assemblage entre l'écran et le tulle, on perfore de place en place ces deux éléments avec un outil chauffant pour réaliser ainsi une soudure le long du bord des perforations 5. To make the assembly between the screen and the tulle, these two elements are punctured from place to place with a heating tool to thus achieve a weld along the edge of the perforations 5.
On peut également réaliser comme cela est représenté à la figure 2 l'assemblage de tout une série de nappes formées de plusieurs écrans 1 entre lesquels sont insérés les séparateurs 3, ces ensembles étant perforés avec un outil chauffant de manière qu'ils soient solidarisés le long des bords des perforations 5. It is also possible, as shown in FIG. 2, to assemble a whole series of plies formed of several screens 1 between which the separators 3 are inserted, these assemblies being perforated with a heating tool so that they are secured together. along the edges of the perforations 5.
On peut aussi prévoir lorsqu'on utilise un grand nombre de nappes d'écrans 1 et de séparateurs 3 que les perforations soients décalées dans l'épaisseur de l'ensemble des nappes pour éviter la formation de ponts thermiques trop importants. Ainsi, si on suppose que le matériau comprend dix écrans superposés l avec des séparateurs correspondants 3, on pourrait réaliser une première série de perforations pour solidariser les quatre écrans supérieurs et les séparateurs correspondants, une seconde série de perforations 5 pour solidariser les second, troisième, quatrième, cinquième et sixième écrans et les séparateurs correspondants, une troisième série de perforations pour solidariser les quatrième, cinquième, sixième, septième et huitienne écrans et séparateurs et ainsi de suite. It can also be provided when a large number of screen plies 1 and separators 3 are used that the perforations are offset in the thickness of all of the plies to avoid the formation of excessive thermal bridges. Thus, if it is assumed that the material comprises ten superimposed screens l with corresponding separators 3, one could make a first series of perforations to secure the four upper screens and the corresponding separators, a second series of perforations 5 to secure the second, third , fourth, fifth and sixth screens and the corresponding separators, a third series of perforations for securing the fourth, fifth, sixth, seventh and eighth screens and separators and so on.
Bien entendu, l'invention n'est pas limitée aux modes de réalisation qui viennent d'être décrits et représentés. On pourra y apporter de nombreuses modifications de détail sans sortir pour cela du cadre de l'invention. Of course, the invention is not limited to the embodiments which have just been described and shown. Many modifications of detail can be made without departing from the scope of the invention.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8602385A FR2594747A1 (en) | 1986-02-21 | 1986-02-21 | Method for assembling a superinsulating material in the form of plies |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8602385A FR2594747A1 (en) | 1986-02-21 | 1986-02-21 | Method for assembling a superinsulating material in the form of plies |
Publications (1)
Publication Number | Publication Date |
---|---|
FR2594747A1 true FR2594747A1 (en) | 1987-08-28 |
Family
ID=9332376
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8602385A Withdrawn FR2594747A1 (en) | 1986-02-21 | 1986-02-21 | Method for assembling a superinsulating material in the form of plies |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2594747A1 (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0361652A2 (en) * | 1988-07-29 | 1990-04-04 | Southwall Technologies, Inc. | Perforated through-coated plastic sheets |
WO2009140692A1 (en) * | 2008-05-16 | 2009-11-19 | Lawrence Livermore National Security, Llc | Cryogenic capable high pressure containers for compact storage of hydrogen onboard vehicles |
EP2458256A1 (en) * | 2010-11-30 | 2012-05-30 | Converteam Technology Ltd | Insulation for a cryogenic component |
RU2666884C1 (en) * | 2017-04-21 | 2018-09-12 | Общество с ограниченной ответственностью НПП "ПОЛИПЛЕН" | Material for screen vacuum thermal insulation and method of its manufacture |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR895069A (en) * | 1943-05-28 | 1945-01-15 | Celluloid Fabrik A G Deutsche | Method and device for interconnecting objects made of thermoplastic materials |
FR1025343A (en) * | 1950-09-30 | 1953-04-14 | Further development in the manufacture of cushions, mattresses and other pneumatic bags | |
US3012918A (en) * | 1956-01-03 | 1961-12-12 | Kendall & Co | Differential heat-sealability in differentially crystalline sheet materials, products made therefrom and process and apparatus for making |
FR1370339A (en) * | 1963-09-27 | 1964-08-21 | Process for perforating and fusing flat textile products made of synthetic fibers and sheets | |
FR1500049A (en) * | 1965-06-17 | 1967-11-03 | Union Carbide Corp | Plastic book with heat-welded binding |
US3379590A (en) * | 1965-04-07 | 1968-04-23 | Dorr Oliver Inc | Method of making a wrinkle-free endless fabric filter belt |
US3817802A (en) * | 1971-06-21 | 1974-06-18 | Ultrasonic Systems | Ultrasonic sewing |
JPS54113685A (en) * | 1978-02-27 | 1979-09-05 | Masami Kogata | Production of air entrapped multilayer synthetic resin film |
-
1986
- 1986-02-21 FR FR8602385A patent/FR2594747A1/en not_active Withdrawn
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR895069A (en) * | 1943-05-28 | 1945-01-15 | Celluloid Fabrik A G Deutsche | Method and device for interconnecting objects made of thermoplastic materials |
FR1025343A (en) * | 1950-09-30 | 1953-04-14 | Further development in the manufacture of cushions, mattresses and other pneumatic bags | |
US3012918A (en) * | 1956-01-03 | 1961-12-12 | Kendall & Co | Differential heat-sealability in differentially crystalline sheet materials, products made therefrom and process and apparatus for making |
FR1370339A (en) * | 1963-09-27 | 1964-08-21 | Process for perforating and fusing flat textile products made of synthetic fibers and sheets | |
US3379590A (en) * | 1965-04-07 | 1968-04-23 | Dorr Oliver Inc | Method of making a wrinkle-free endless fabric filter belt |
FR1500049A (en) * | 1965-06-17 | 1967-11-03 | Union Carbide Corp | Plastic book with heat-welded binding |
US3817802A (en) * | 1971-06-21 | 1974-06-18 | Ultrasonic Systems | Ultrasonic sewing |
JPS54113685A (en) * | 1978-02-27 | 1979-09-05 | Masami Kogata | Production of air entrapped multilayer synthetic resin film |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0361652A2 (en) * | 1988-07-29 | 1990-04-04 | Southwall Technologies, Inc. | Perforated through-coated plastic sheets |
EP0361652A3 (en) * | 1988-07-29 | 1991-03-20 | Southwall Technologies, Inc. | Perforated through-coated plastic sheets |
WO2009140692A1 (en) * | 2008-05-16 | 2009-11-19 | Lawrence Livermore National Security, Llc | Cryogenic capable high pressure containers for compact storage of hydrogen onboard vehicles |
EP2458256A1 (en) * | 2010-11-30 | 2012-05-30 | Converteam Technology Ltd | Insulation for a cryogenic component |
WO2012072481A1 (en) * | 2010-11-30 | 2012-06-07 | Converteam Technology Ltd | Insulation for a cryogenic component |
CN103415734A (en) * | 2010-11-30 | 2013-11-27 | Ge能源能量变换技术有限公司 | Insulation for cryogenic component |
US9163773B2 (en) | 2010-11-30 | 2015-10-20 | Ge Energy Power Conversion Technology, Ltd. | Insulation for a cryogenic component |
CN103415734B (en) * | 2010-11-30 | 2016-06-15 | Ge能源能量变换技术有限公司 | For spacer and the partition method thereof of superconduction electricmachine cryogenic element |
RU2666884C1 (en) * | 2017-04-21 | 2018-09-12 | Общество с ограниченной ответственностью НПП "ПОЛИПЛЕН" | Material for screen vacuum thermal insulation and method of its manufacture |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP2393652B1 (en) | Honeycomb core structure for use in a structural panel for a jet engine nacelle | |
EP0457676B1 (en) | Process for the manufacture of a separator plate for a stack in an exchange device | |
EP1201420B1 (en) | Sound absorbing panel particularly for aircraft engine | |
CA2279094C (en) | Honeycomb structure, especially for sound absorption, and its manufacturing process | |
EP2393651B1 (en) | Method for manufacturing a structure with cellular cores for a turbojet nacelle | |
WO2003107325A1 (en) | Method for making a soundproofing panel with at least one double resonator | |
WO2011061430A1 (en) | Acoustic skin for an aircraft nacelle acoustic panel | |
EP2140445A2 (en) | Method for making an acoustic absorption panel in particular for the nacelle of an aircraft engine | |
WO2006030076A1 (en) | Draining geocomposite and a method for the production thereof | |
EP0117770B1 (en) | Impact- and bullet-resistant glass, and method of manufacturing the same | |
FR2594747A1 (en) | Method for assembling a superinsulating material in the form of plies | |
EP3823831A1 (en) | Method for manufacturing an acoustic panel | |
FR3036061B1 (en) | COMPOSITE PANEL AND AIRCRAFT TURBOBOREACTEUR NACELLE COMPRISING SUCH A PANEL | |
FR2745295A1 (en) | PROCESS FOR THE PRODUCTION OF A GLUE ASSEMBLY BETWEEN PLANAR OR FLAT PARTS | |
FR2718670A1 (en) | Part has core and composite material coating covering faces | |
WO2015036716A1 (en) | Method for repairing a skin of a composite panel | |
FR2659122A1 (en) | Flat gasket | |
EP4169706A1 (en) | Resistive skin element for acoustic panel for aircraft | |
EP0521793A1 (en) | Method for connecting composite superstructures to a metal ship hull | |
CA2801130C (en) | Fibrous structure forming a flange and a counter-flange | |
EP0215717B1 (en) | Method of producing a flame holder of composite material and flame holder produced according to this method | |
FR2773645A1 (en) | Aircraft radome repair technique | |
FR2635349A1 (en) | Panel provided with reinforcement stiffeners | |
EP3908468B1 (en) | Method for producing a hinge of an information sheet of an identity document, information sheet of an identity document comprising a hinge obtained according to said method and identity document comprising said information sheet | |
EP2419269A1 (en) | Cellular panel |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |