GB845003A - Method and apparatus for producing a composite metal honeycomb structure - Google Patents
Method and apparatus for producing a composite metal honeycomb structureInfo
- Publication number
- GB845003A GB845003A GB31442/56A GB3144256A GB845003A GB 845003 A GB845003 A GB 845003A GB 31442/56 A GB31442/56 A GB 31442/56A GB 3144256 A GB3144256 A GB 3144256A GB 845003 A GB845003 A GB 845003A
- Authority
- GB
- United Kingdom
- Prior art keywords
- core
- sandwich
- skin
- skins
- dies
- 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.)
- Expired
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B31—MAKING ARTICLES OF PAPER, CARDBOARD OR MATERIAL WORKED IN A MANNER ANALOGOUS TO PAPER; WORKING PAPER, CARDBOARD OR MATERIAL WORKED IN A MANNER ANALOGOUS TO PAPER
- B31D—MAKING ARTICLES OF PAPER, CARDBOARD OR MATERIAL WORKED IN A MANNER ANALOGOUS TO PAPER, NOT PROVIDED FOR IN SUBCLASSES B31B OR B31C
- B31D3/00—Making articles of cellular structure, e.g. insulating board
- B31D3/02—Making articles of cellular structure, e.g. insulating board honeycombed structures, i.e. the cells having an essentially hexagonal section
- B31D3/0207—Making articles of cellular structure, e.g. insulating board honeycombed structures, i.e. the cells having an essentially hexagonal section of particular shape or construction
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C37/00—Manufacture of metal sheets, bars, wire, tubes or like semi-manufactured products, not otherwise provided for; Manufacture of tubes of special shape
- B21C37/06—Manufacture of metal sheets, bars, wire, tubes or like semi-manufactured products, not otherwise provided for; Manufacture of tubes of special shape of tubes or metal hoses; Combined procedures for making tubes, e.g. for making multi-wall tubes
- B21C37/15—Making tubes of special shape; Making tube fittings
- B21C37/154—Making multi-wall tubes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D47/00—Making rigid structural elements or units, e.g. honeycomb structures
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K1/00—Soldering, e.g. brazing, or unsoldering
- B23K1/0008—Soldering, e.g. brazing, or unsoldering specially adapted for particular articles or work
- B23K1/0014—Brazing of honeycomb sandwich structures
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Laminated Bodies (AREA)
Abstract
845,003. Making sheet material; brazing. SOLAR, AIRCRAFT CO. Oct. 16, 1956 [Oct. 17, 1955], No. 31442/56. Classes 83 (2) and 83 (4). In producing a composite metal honeycomb structure comprising a honeycomb core bonded to at least one skin or sheet, the skin &c. is placed on the core with cohesive bonding material applied at one or both sides of the core at the core edges or at accessible points adjacent the cell wall joints, a substantially complete contact is made between the core edges and the skin &c., the temperature of the assembly is raised by creating relative movement between the assembly and a localized heat source to melt the bonding material which flows and cohesively diffuses into the core cell edges and contacting portions of the skin &c. and the temperature is allowed to decrease while maintaining the substantially complete contact. The core and skins may be cleaned by acid dip and brazing material, e.g. silver solder powder may be held in place in the open cells by sprayed acrylic resin or dilute polystyrene-methylchloride solution or a paste of acrylic resin and the powder may be used. A flux may be applied to the core and skin if a reducing atmospheric furnace is not used and the skin may be spot welded to the core edges before brazing. The assembly may be pressed between stainless steel, high alloy metal or ceramic dies. In an embodiment a core 33, Fig. 2, and a pair of skins 31 forming a sandwich are assembled between dies 35, which may be preheated to a temperature 50‹ F. above brazing temperature, with a resilient metallic or non- metallic sheet 36 or layer of asbestos or powdered ceramic between each skin and die to provide uniform pressure. Reinforcing channels 24, Fig. 7, may be provided at the ends of the core and brazing material held in perforations 26 melts during heating by a localized source of heat moved relatively to the sandwich to braze the channels to the skins. In a modification perforated plates provided with brazing material may be arranged between the skins and an unperforated channel. Alternatively the sandwich and die assembly is sealed in a stainless steel envelope 37, Fig. 3, which is partially evacuated before brazing and in a modification the dies may be omitted. In making a curved sandwich, the sandwich with core edge stiffeners spot welded to the core or skins is arranged between dies as shown in Fig. 10. Curved uniform thickness dies may be used. For use with a vacuum or pressure envelope a rigid die 35, Fig. 12, and a relatively flexible die 104 having metal squares 106 spot welded to a sheet 108 is employed. In order to attach fittings to the sandwich the core may be locally strengthened by using heavier core material or more closely spaced cells. In making a long narrow sandwich an electric tunnel furnace 150, Fig. 17, is moved along a track 152 by a motor 153 and the sandwich is enclosed in a metal bag 156 partially evacuated and held under tension. Asbestos sheets may be provided between the sandwich and bag and curved rollers may be provided on the furnace to shape the sandwich. The sandwich assemblies in dies (Fig. 10) or in vacuum bags (Fig. 3) may be held between tensioned sheets or positioned on a sheet with an upper tension sheet and moved relatively to a tunnel furnace. In a modification the sandwich may be arranged vertically when the furnace travels vertically up and down. In the continuous production of flat or curved sandwiches the skins 31, Fig. 25, are fed from rolls to engage a continuously fed core 33 which is supplied with brazing material and flux by rolls, brushes or by dipping. The assembly passes between positioning rolls 142, radiant gas heater heated rolls 144 and water-cooled rolls 146, 148. The rolls 142, 144 and 146 may alternatively be located inside a furnace. Specification 838,516 is referred to.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US345802XA | 1955-10-17 | 1955-10-17 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB845003A true GB845003A (en) | 1960-08-17 |
Family
ID=21877307
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB31442/56A Expired GB845003A (en) | 1955-10-17 | 1956-10-16 | Method and apparatus for producing a composite metal honeycomb structure |
Country Status (4)
Country | Link |
---|---|
BE (1) | BE551841A (en) |
CH (1) | CH345802A (en) |
FR (1) | FR1162692A (en) |
GB (1) | GB845003A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2502519A1 (en) * | 1981-03-30 | 1982-10-01 | Lerolland Marcel | Method of fabricating large half round shell - entails fixing thin plate to mandrel to receive carcass to which it is fixed and then released from mandrel |
WO2008064257A2 (en) * | 2006-11-22 | 2008-05-29 | Johnson Controls Technology Company | Method for brazing and hot forming a multichannel heat exchanger, the hot forming using the heating energy of the brazing step |
CN103028853A (en) * | 2012-12-28 | 2013-04-10 | 江阴东大新材料研究院 | Method for manufacturing honeycomb ceramic sandwich plate on surface of steel plate in self-propagating manner with assistance of resistance spot welding |
CN111069598A (en) * | 2018-10-16 | 2020-04-28 | 戴弗根特技术有限公司 | Method and apparatus for manufacturing optimized panels and other composite structures |
CN112453760A (en) * | 2020-10-30 | 2021-03-09 | 中国航发北京航空材料研究院 | Titanium-based brazing filler metal and method for preparing pure titanium multilayer structure by using same |
CN113145962A (en) * | 2021-03-09 | 2021-07-23 | 哈尔滨工业大学(威海) | Heterogeneous metal material honeycomb sandwich structure and preparation method thereof |
EP4241898A1 (en) * | 2022-03-07 | 2023-09-13 | The Boeing Company | Metallic structures with additively manufactured metallic articles and methods for fabrication |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3093104A (en) * | 1958-06-27 | 1963-06-11 | Bukata Stephen | Furnace |
US3068565A (en) * | 1958-10-16 | 1962-12-18 | Nat Distillers Chem Corp | Method of making honeycomb laminate |
LU37841A1 (en) * | 1958-10-28 | |||
US3094775A (en) * | 1958-10-28 | 1963-06-25 | Northrop Corp | Method of brazing honeycomb sandwich with edge members and inserts |
US3110961A (en) * | 1959-04-06 | 1963-11-19 | North American Aviation Inc | Honeycomb sandwich panel brazing |
US3011254A (en) * | 1959-04-06 | 1961-12-05 | North American Aviation Inc | Double differential pressure honeycomb sandwich panel brazing |
US3087046A (en) * | 1959-11-16 | 1963-04-23 | Ryan Aeronautical Co | Brazing and heat treating apparatus for honeycomb core panels |
US3151591A (en) * | 1960-10-07 | 1964-10-06 | Bell Aerospace Corp | Heat bonding apparatus |
US3091684A (en) * | 1961-07-13 | 1963-05-28 | Gen Dynamics Corp | Brazing apparatus |
GB2061791B (en) * | 1979-10-29 | 1983-05-11 | Rohr Industries Inc | Making a noise attenuation panel |
FR2526694A1 (en) * | 1982-05-13 | 1983-11-18 | Alloy Spot Welders Inc | Method of brazing honeycomb and panel assemblies - has individual braze ribbons between honeycomb cell vertices to flow into cell nodes when heated |
NO833435L (en) * | 1982-10-06 | 1984-04-09 | Hercules Inc | SHIRT-ANGLED PUT BODY WITH LIGHT CORE |
FR2542668B1 (en) * | 1983-03-15 | 1986-06-20 | Claude Morin | PROCESS FOR PRODUCING A CURVED SURFACE ELEMENT FROM A RIGID BOARD OF A MATERIAL OF THE "HONEYCOMB" TYPE AND PRODUCT OBTAINED |
-
0
- BE BE551841D patent/BE551841A/xx unknown
-
1956
- 1956-10-16 GB GB31442/56A patent/GB845003A/en not_active Expired
- 1956-10-17 FR FR1162692D patent/FR1162692A/en not_active Expired
- 1956-10-17 CH CH345802D patent/CH345802A/en unknown
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2502519A1 (en) * | 1981-03-30 | 1982-10-01 | Lerolland Marcel | Method of fabricating large half round shell - entails fixing thin plate to mandrel to receive carcass to which it is fixed and then released from mandrel |
WO2008064257A2 (en) * | 2006-11-22 | 2008-05-29 | Johnson Controls Technology Company | Method for brazing and hot forming a multichannel heat exchanger, the hot forming using the heating energy of the brazing step |
WO2008064257A3 (en) * | 2006-11-22 | 2008-11-20 | Johnson Controls Tech Co | Method for brazing and hot forming a multichannel heat exchanger, the hot forming using the heating energy of the brazing step |
CN103028853A (en) * | 2012-12-28 | 2013-04-10 | 江阴东大新材料研究院 | Method for manufacturing honeycomb ceramic sandwich plate on surface of steel plate in self-propagating manner with assistance of resistance spot welding |
CN103028853B (en) * | 2012-12-28 | 2015-04-29 | 江阴东大新材料研究院 | Method for manufacturing honeycomb ceramic sandwich plate on surface of steel plate in self-propagating manner with assistance of resistance spot welding |
CN111069598A (en) * | 2018-10-16 | 2020-04-28 | 戴弗根特技术有限公司 | Method and apparatus for manufacturing optimized panels and other composite structures |
CN112453760A (en) * | 2020-10-30 | 2021-03-09 | 中国航发北京航空材料研究院 | Titanium-based brazing filler metal and method for preparing pure titanium multilayer structure by using same |
CN113145962A (en) * | 2021-03-09 | 2021-07-23 | 哈尔滨工业大学(威海) | Heterogeneous metal material honeycomb sandwich structure and preparation method thereof |
CN113145962B (en) * | 2021-03-09 | 2022-12-06 | 哈尔滨工业大学(威海) | Heterogeneous metal material honeycomb sandwich structure and preparation method thereof |
EP4241898A1 (en) * | 2022-03-07 | 2023-09-13 | The Boeing Company | Metallic structures with additively manufactured metallic articles and methods for fabrication |
Also Published As
Publication number | Publication date |
---|---|
FR1162692A (en) | 1958-09-16 |
BE551841A (en) | |
CH345802A (en) | 1960-04-15 |
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