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 GB3150452A GB3150452A GB750610A GB 750610 A GB750610 A GB 750610A GB 3150452 A GB3150452 A GB 3150452A GB 3150452 A GB3150452 A GB 3150452A GB 750610 A GB750610 A GB 750610A
Authority
GB
Grant status
Application
Patent type
Prior art keywords
aircraft
strips
dec
together
use
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
GB3150452A
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.)
A V ROE AND CO Ltd
Original Assignee
A V 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

Links

Classifications

    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C2/00Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
    • E04C2/30Building 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
    • E04C2/34Building 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
    • E04C2/36Building 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings

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.
GB3150452A 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
GB3150452A 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
GB3150452A 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 true GB750610A (en) 1956-06-20

Family

ID=10324082

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3150452A 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 (4)

* 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
LU92548A1 (en) * 2014-09-17 2016-03-18 Euro Composites Wabe particular deformable wabe, for light parts, corresponding method and sandwich component

Cited By (5)

* 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
LU92548A1 (en) * 2014-09-17 2016-03-18 Euro Composites Wabe particular deformable wabe, for light parts, corresponding method 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

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