GB750610A - Improvements in metal cores for use in the production of rigid panels - Google Patents

Improvements in metal cores for use in the production of rigid panels

Info

Publication number
GB750610A
GB750610A GB31504/52A GB3150452A GB750610A GB 750610 A GB750610 A GB 750610A GB 31504/52 A GB31504/52 A GB 31504/52A GB 3150452 A GB3150452 A GB 3150452A GB 750610 A GB750610 A GB 750610A
Authority
GB
United Kingdom
Prior art keywords
production
metal cores
rigid panels
aircraft
strips
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
Application number
GB31504/52A
Inventor
Alfred Holt
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.)
AV Roe and Co Ltd
Original Assignee
AV Roe and Co Ltd
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 AV Roe and Co Ltd filed Critical AV Roe and Co Ltd
Priority to GB31504/52A priority Critical patent/GB750610A/en
Publication of GB750610A publication Critical patent/GB750610A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings

Abstract

750,610. Aircraft framework. ROE & CO., Ltd., A. V. Aug. 28, 1953 [Dec. 12, 1952], No. 31504/52. Class 4. [Also in Groups I and X] A panel for the wings and fuselage of aircraft comprises two parallel sheets a between which is a core, which is easily bent, comprising corrugated strips a, the corrugations of adjacent strips being offset and having straight parts cemented together.
GB31504/52A 1952-12-12 1952-12-12 Improvements in metal cores for use in the production of rigid panels Expired GB750610A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB31504/52A GB750610A (en) 1952-12-12 1952-12-12 Improvements in metal cores for use in the production of rigid panels

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB31504/52A GB750610A (en) 1952-12-12 1952-12-12 Improvements in metal cores for use in the production of rigid panels

Publications (1)

Publication Number Publication Date
GB750610A true GB750610A (en) 1956-06-20

Family

ID=10324082

Family Applications (1)

Application Number Title Priority Date Filing Date
GB31504/52A Expired GB750610A (en) 1952-12-12 1952-12-12 Improvements in metal cores for use in the production of rigid panels

Country Status (1)

Country Link
GB (1) GB750610A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3057057A (en) * 1958-10-01 1962-10-09 Engelhard Ind Inc Method of making a honeycomb sandwich structure
US3067507A (en) * 1958-02-07 1962-12-11 Goodyear Aircraft Corp Method of making sandwich structures
US3432379A (en) * 1965-10-22 1969-03-11 Atomic Energy Commission Three dimensional flexible dovetail honeycomb
LU92548B1 (en) * 2014-09-17 2016-03-18 Euro Composites HONEYCOMB, ESPECIALLY DEFORMABLE HONEYCOMB, FOR LIGHTWEIGHT COMPONENTS, CORRESPONDING PRODUCTION PROCESS AND SANDWICH COMPONENT
WO2022028649A1 (en) 2020-08-04 2022-02-10 Technische Universität Dresden Method for producing a wave-walled honeycomb core, wave-walled honeycomb core and use

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3067507A (en) * 1958-02-07 1962-12-11 Goodyear Aircraft Corp Method of making sandwich structures
US3057057A (en) * 1958-10-01 1962-10-09 Engelhard Ind Inc Method of making a honeycomb sandwich structure
US3432379A (en) * 1965-10-22 1969-03-11 Atomic Energy Commission Three dimensional flexible dovetail honeycomb
LU92548B1 (en) * 2014-09-17 2016-03-18 Euro Composites HONEYCOMB, ESPECIALLY DEFORMABLE HONEYCOMB, FOR LIGHTWEIGHT COMPONENTS, CORRESPONDING PRODUCTION PROCESS AND SANDWICH COMPONENT
WO2016042107A1 (en) * 2014-09-17 2016-03-24 Euro-Composites S.A. Honeycomb, in particular deformable honeycomb, for lightweight components, corresponding production method, and sandwich component
JP2017529471A (en) * 2014-09-17 2017-10-05 ユーロ‐コンポジテス エス．ア． Honeycomb for lightweight components, in particular deformable honeycomb, corresponding production method, and sandwich component
EP3194681B1 (en) 2014-09-17 2018-07-18 Euro-Composites S.A. Honeycomb, in particular deformable honeycomb, for lightweight component and a block for production of the honeycomb and corresponding production method.
RU2684796C2 (en) * 2014-09-17 2019-04-15 Евро-Композитс С.А. Honeycomb, in particular deformable honeycomb, for lightweight components, corresponding production method and sandwich component
US11001029B2 (en) 2014-09-17 2021-05-11 Euro-Composites S.A. Honeycomb, in particular deformable honeycomb, for lightweight components, corresponding production method, and sandwich component
WO2022028649A1 (en) 2020-08-04 2022-02-10 Technische Universität Dresden Method for producing a wave-walled honeycomb core, wave-walled honeycomb core and use
DE102020120558A1 (en) 2020-08-04 2022-02-10 Technische Universität Dresden Process for the production of a corrugated web honeycomb core, corrugated web honeycomb core, use and component

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