FR2177640B1 - - Google Patents

Info

Publication number
FR2177640B1
FR2177640B1 FR7211660A FR7211660A FR2177640B1 FR 2177640 B1 FR2177640 B1 FR 2177640B1 FR 7211660 A FR7211660 A FR 7211660A FR 7211660 A FR7211660 A FR 7211660A FR 2177640 B1 FR2177640 B1 FR 2177640B1
Authority
FR
France
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.)
Expired
Application number
FR7211660A
Other languages
French (fr)
Other versions
FR2177640A1 (it
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Dassault Aviation SA
Original Assignee
Dassault Aviation SA
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Dassault Aviation SA filed Critical Dassault Aviation SA
Priority to FR7211660A priority Critical patent/FR2177640B1/fr
Priority to GB1516273A priority patent/GB1420009A/en
Priority to US346285A priority patent/US3886023A/en
Priority to DE2316061A priority patent/DE2316061A1/de
Publication of FR2177640A1 publication Critical patent/FR2177640A1/fr
Application granted granted Critical
Publication of FR2177640B1 publication Critical patent/FR2177640B1/fr
Expired legal-status Critical Current

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
    • 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
    • B32B3/10—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 discontinuous layer, i.e. formed of separate pieces of material
    • B32B3/12—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 discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D24/00—Producing articles with hollow walls
    • B29D24/002—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled
    • B29D24/005—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled the structure having joined ribs, e.g. honeycomb
    • 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
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/20—Layered products comprising a layer of metal comprising aluminium or copper
    • 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
    • E04C2/30—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
    • E04C2/34—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts
    • E04C2/36—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by transversely-placed strip material, e.g. honeycomb panels
    • E04C2/365—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by transversely-placed strip material, e.g. honeycomb panels by honeycomb structures
    • 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
    • F16L59/02—Shape or form of insulating materials, with or without coverings integral with the insulating materials
    • F16L59/029—Shape or form of insulating materials, with or without coverings integral with the insulating materials layered
    • 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
    • B32B2305/02—Cellular or porous
    • B32B2305/024—Honeycomb
    • 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
    • B32B2607/00—Walls, panels
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor
    • Y10T156/1002—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
    • Y10T156/1003—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina by separating laminae between spaced secured areas [e.g., honeycomb expanding]
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor
    • Y10T156/1052—Methods of surface bonding and/or assembly therefor with cutting, punching, tearing or severing
    • Y10T156/1056—Perforating lamina
    • Y10T156/1057—Subsequent to assembly of laminae
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24149—Honeycomb-like
    • Y10T428/24157—Filled honeycomb cells [e.g., solid substance in cavities, etc.]

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Architecture (AREA)
  • General Engineering & Computer Science (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Panels For Use In Building Construction (AREA)
  • Laminated Bodies (AREA)
  • Joining Of Building Structures In Genera (AREA)
FR7211660A 1972-03-31 1972-03-31 Expired FR2177640B1 (it)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR7211660A FR2177640B1 (it) 1972-03-31 1972-03-31
GB1516273A GB1420009A (en) 1972-03-31 1973-03-29 Structural panels of the sandwich type
US346285A US3886023A (en) 1972-03-31 1973-03-30 Structural panels of the sandwich type
DE2316061A DE2316061A1 (de) 1972-03-31 1973-03-30 Sandwichplatte und verfahren zu deren herstellung

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7211660A FR2177640B1 (it) 1972-03-31 1972-03-31

Publications (2)

Publication Number Publication Date
FR2177640A1 FR2177640A1 (it) 1973-11-09
FR2177640B1 true FR2177640B1 (it) 1975-03-21

Family

ID=9096249

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7211660A Expired FR2177640B1 (it) 1972-03-31 1972-03-31

Country Status (4)

Country Link
US (1) US3886023A (it)
DE (1) DE2316061A1 (it)
FR (1) FR2177640B1 (it)
GB (1) GB1420009A (it)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2425014B2 (de) * 1974-05-24 1976-08-26 Vereinigte Flugtechnische Werke-Fokker GmbH, 2800 Bremen Verfahren zum herstellen von leichtbauplatten
DE2736132C2 (de) * 1977-08-11 1981-12-17 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Verfahren zum Herstellen von Sandwichbauteilen
US4416715A (en) * 1978-08-31 1983-11-22 Doralyn Ann Hardy Method and apparatus for fabricating insulative panel
US4510010A (en) * 1980-05-27 1985-04-09 Schramm Arthur G Method and apparatus for fabricating insulative panel
US4715801A (en) * 1981-07-15 1987-12-29 Corning Glass Works Apparatus for high speed manifolding of honeycomb structures
SE466299B (sv) * 1983-08-04 1992-01-27 Micropore International Ltd Vaermeisolerande kropp och saett att framstaella den, innefattande en armerande bikakestruktur och ett vaermeisolationsmaterial
FR2591257A1 (fr) * 1985-12-06 1987-06-12 Borie Panneaux de revetement de facade en fibre de verre et polyester
US4964936A (en) * 1988-10-11 1990-10-23 Imi-Tech Corporation Method of making foam-filled cellular structures
NL8900398A (nl) * 1989-02-17 1990-09-17 Schreiner Luchtvaart Werkwijze voor het aanbrengen van een plaatselijke versterking in een sandwichconstructie.
ATE173195T1 (de) * 1991-07-12 1998-11-15 Hexcel Corp Verfahren und vorrichtung zur herstellung von verschweissten thermoplastischen wabenstrukturen
FI982743A (fi) * 1998-12-18 2000-06-19 System 300 Group Oy Keilaradan rakennuselementti ja keilarata
US20040115414A1 (en) * 2002-03-15 2004-06-17 Joseph Wycech Method for stiffening or reinforcing a member in a cost effective manner and a member which is made in accordance with the method
US6884055B2 (en) * 2002-05-29 2005-04-26 The Boeing Company Potting compound injection apparatus and method of injecting potting compound into panel cells
DE102004013146B4 (de) * 2004-03-17 2008-01-24 Airbus Deutschland Gmbh Verfahren zur Verstärkung von Kernstrukturen zur Bildung von beidseitig mit Deckschichten versehenen Kernverbunden
US8506743B2 (en) 2004-03-17 2013-08-13 Airbus Deutschland Gmbh Composite sandwich structure with integrated reinforcement area and method of producing the same
DE102004013145B4 (de) * 2004-03-17 2010-04-01 Airbus Deutschland Gmbh Verfahren zur Randabdichtung eines Kernverbundes
US7749420B2 (en) * 2004-03-17 2010-07-06 Airbus Deutschland Gmbh Method and apparatus for processing open three-dimensional core structures such as folded honeycomb structures
US7666493B2 (en) * 2004-03-17 2010-02-23 Airbus Deutschland Gmbh Locally reinforced core structure for composite sandwich structure and method of producing the same
DE102014118514B4 (de) * 2014-12-12 2016-10-06 Ross Design Gmbh Verfahren zur Herstellung von Leichtbauelementen und Leichtbauelemente
DE102017108627B4 (de) * 2017-04-24 2023-09-07 Ross Design Gmbh Verfahren zur Herstellung eines Leichtbauelements

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US829267A (en) * 1905-09-19 1906-08-21 John K Graham Templet.
FR1237054A (fr) * 1958-10-06 1960-07-22 Bristol Aircraft Ltd Revêtement armé, en particulier pour l'aviation
GB885395A (en) * 1958-10-06 1961-12-28 Bristol Aerojet Ltd Reinforced skin structures
GB994952A (en) * 1963-07-25 1965-06-10 Riegel Textile Corp Laminated textile product and method of manufacture same
US3578526A (en) * 1968-01-22 1971-05-11 United Aircraft Corp Method of making reinforced honeycomb sandwich
US3485282A (en) * 1968-01-26 1969-12-23 Hughes Aircraft Co Expandable insert for solid and cellular structures
US3481427A (en) * 1968-11-29 1969-12-02 Mc Donnell Douglas Corp Acoustical panel structure
US3742673A (en) * 1971-03-22 1973-07-03 Rex Chainbelt Inc Panel edge fastening means

Also Published As

Publication number Publication date
GB1420009A (en) 1976-01-07
FR2177640A1 (it) 1973-11-09
DE2316061A1 (de) 1973-10-11
US3886023A (en) 1975-05-27

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Legal Events

Date Code Title Description
ST Notification of lapse