DE2316061A1 - Sandwichplatte und verfahren zu deren herstellung - Google Patents
Sandwichplatte und verfahren zu deren herstellungInfo
- Publication number
- DE2316061A1 DE2316061A1 DE2316061A DE2316061A DE2316061A1 DE 2316061 A1 DE2316061 A1 DE 2316061A1 DE 2316061 A DE2316061 A DE 2316061A DE 2316061 A DE2316061 A DE 2316061A DE 2316061 A1 DE2316061 A1 DE 2316061A1
- Authority
- DE
- Germany
- Prior art keywords
- plate
- composition
- cells
- ing
- holes
- 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.)
- Pending
Links
- 238000004519 manufacturing process Methods 0.000 title description 7
- 239000000203 mixture Substances 0.000 claims description 22
- 210000004027 cell Anatomy 0.000 claims description 18
- 238000000034 method Methods 0.000 claims description 13
- 210000003850 cellular structure Anatomy 0.000 claims description 11
- 239000004033 plastic Substances 0.000 claims description 9
- 239000000463 material Substances 0.000 claims description 8
- 229920003002 synthetic resin Polymers 0.000 claims description 6
- 239000000057 synthetic resin Substances 0.000 claims description 6
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 5
- 229910052814 silicon oxide Inorganic materials 0.000 claims description 5
- 239000007788 liquid Substances 0.000 claims description 3
- 240000005702 Galium aparine Species 0.000 claims description 2
- 230000001413 cellular effect Effects 0.000 claims 1
- 238000003754 machining Methods 0.000 claims 1
- 230000009974 thixotropic effect Effects 0.000 description 4
- 238000005266 casting Methods 0.000 description 3
- 238000005253 cladding Methods 0.000 description 3
- 238000005192 partition Methods 0.000 description 3
- 229910045601 alloy Inorganic materials 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 210000002421 cell wall Anatomy 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 238000005553 drilling Methods 0.000 description 2
- 238000002347 injection Methods 0.000 description 2
- 239000007924 injection Substances 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 238000004026 adhesive bonding Methods 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000003054 catalyst Substances 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 229910003460 diamond Inorganic materials 0.000 description 1
- 239000010432 diamond Substances 0.000 description 1
- 239000003822 epoxy resin Substances 0.000 description 1
- 239000011796 hollow space material Substances 0.000 description 1
- 238000007731 hot pressing Methods 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 229920000647 polyepoxide Polymers 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
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 shape; Layered products comprising a layer 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 shape; Layered products comprising a layer 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 shape; Layered products comprising a layer 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)
- Joining Of Building Structures In Genera (AREA)
- Laminated Bodies (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7211660A FR2177640B1 (it) | 1972-03-31 | 1972-03-31 |
Publications (1)
Publication Number | Publication Date |
---|---|
DE2316061A1 true DE2316061A1 (de) | 1973-10-11 |
Family
ID=9096249
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE2316061A Pending DE2316061A1 (de) | 1972-03-31 | 1973-03-30 | Sandwichplatte und verfahren zu deren herstellung |
Country Status (4)
Country | Link |
---|---|
US (1) | US3886023A (it) |
DE (1) | DE2316061A1 (it) |
FR (1) | FR2177640B1 (it) |
GB (1) | GB1420009A (it) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102004013146A1 (de) * | 2004-03-17 | 2005-10-13 | Airbus Deutschland Gmbh | Verfahren zur Verstärkung von Kernstrukturen zur Bildung von beidseitig mit Deckschichten versehenen Kernverbunden sowie lokal verstärkter Kernverbund |
US7658810B2 (en) | 2004-03-17 | 2010-02-09 | Airbus Deutschland Gmbh | Method for sealing edges of a core of a composite sandwich structure |
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 |
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 |
US8506743B2 (en) | 2004-03-17 | 2013-08-13 | Airbus Deutschland Gmbh | Composite sandwich structure with integrated reinforcement area and method of producing the same |
Families Citing this family (16)
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. |
ES2126596T3 (es) * | 1991-07-12 | 1999-04-01 | Hexcel Corp | Procedimiento y dispositivo de fabricacion de estructuras en forma de panal de abejas termoplasticas fundidas termicamente. |
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 |
EP2422756A1 (en) * | 2010-08-26 | 2012-02-29 | Restored Hearing Ltd. | A container comprising a thixotropic material |
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)
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 |
-
1972
- 1972-03-31 FR FR7211660A patent/FR2177640B1/fr not_active Expired
-
1973
- 1973-03-29 GB GB1516273A patent/GB1420009A/en not_active Expired
- 1973-03-30 DE DE2316061A patent/DE2316061A1/de active Pending
- 1973-03-30 US US346285A patent/US3886023A/en not_active Expired - Lifetime
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102004013146A1 (de) * | 2004-03-17 | 2005-10-13 | Airbus Deutschland Gmbh | Verfahren zur Verstärkung von Kernstrukturen zur Bildung von beidseitig mit Deckschichten versehenen Kernverbunden sowie lokal verstärkter Kernverbund |
DE102004013146B4 (de) * | 2004-03-17 | 2008-01-24 | Airbus Deutschland Gmbh | Verfahren zur Verstärkung von Kernstrukturen zur Bildung von beidseitig mit Deckschichten versehenen Kernverbunden |
US7658810B2 (en) | 2004-03-17 | 2010-02-09 | Airbus Deutschland Gmbh | Method for sealing edges of a core of a composite sandwich structure |
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 |
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 |
US8506743B2 (en) | 2004-03-17 | 2013-08-13 | Airbus Deutschland Gmbh | Composite sandwich structure with integrated reinforcement area and method of producing the same |
Also Published As
Publication number | Publication date |
---|---|
GB1420009A (en) | 1976-01-07 |
FR2177640A1 (it) | 1973-11-09 |
FR2177640B1 (it) | 1975-03-21 |
US3886023A (en) | 1975-05-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
OHW | Rejection |