GB555496A - Improvements in or relating to structures built up of plywood or other light-weight laminated material - Google Patents

Improvements in or relating to structures built up of plywood or other light-weight laminated material

Info

Publication number
GB555496A
GB555496A GB229542A GB229542A GB555496A GB 555496 A GB555496 A GB 555496A GB 229542 A GB229542 A GB 229542A GB 229542 A GB229542 A GB 229542A GB 555496 A GB555496 A GB 555496A
Authority
GB
United Kingdom
Prior art keywords
plywood
sheet
light
synthetic resin
resin adhesive
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
GB229542A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB229542A priority Critical patent/GB555496A/en
Publication of GB555496A publication Critical patent/GB555496A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/08—Geodetic or other open-frame structures

Abstract

555,496. Aircraft framework: ships' hulls. KREMER, H. Feb. 20, 1942, No. 2295. [Classes 4 and 113 (ii)] [Also in Group XXIII] A light-weight structural unit of substantial strength and rigidity adapted for aeroplane fuselages or wings or for the bodies of small boats comprises a reticulated sheet formed by a relatively thick sheet of plywood 10 or similar multi-ply material from which holes 11, e.g., of triangular, diamond or square shape are cut through the thickness at regular intervals throughout the area to leave only comparatively narrow stringers 12, 13 integrally connected at their crossing points and a relatively thin solid sheet 19, e.g., of plywood or similar multi-ply material, or of fabric secured over one or each side of the reticulated sheet. When used for aeroplane parts of geodetic construction the stringers extend along geodetic lines. Synthetic resin adhesive may be used. According to the Provisional Specification, the parts may be impregnated prior to assembly with synthetic resin adhesive.
GB229542A 1942-02-20 1942-02-20 Improvements in or relating to structures built up of plywood or other light-weight laminated material Expired GB555496A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB229542A GB555496A (en) 1942-02-20 1942-02-20 Improvements in or relating to structures built up of plywood or other light-weight laminated material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB229542A GB555496A (en) 1942-02-20 1942-02-20 Improvements in or relating to structures built up of plywood or other light-weight laminated material

Publications (1)

Publication Number Publication Date
GB555496A true GB555496A (en) 1943-08-25

Family

ID=9737053

Family Applications (1)

Application Number Title Priority Date Filing Date
GB229542A Expired GB555496A (en) 1942-02-20 1942-02-20 Improvements in or relating to structures built up of plywood or other light-weight laminated material

Country Status (1)

Country Link
GB (1) GB555496A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2224000A (en) * 1988-11-10 1990-04-25 Genrikh Vasilievich Novozhilov Fuselage or pressure vessel structure
CN102602528A (en) * 2012-03-06 2012-07-25 大连理工大学 Orthogonal grating cylindrical shell provided with reinforcement ribs and circular opening and made of composite materials
EP2481667A1 (en) * 2011-01-31 2012-08-01 Airbus Opérations SAS Stiffened structure including an opening
EP2719618A1 (en) * 2012-10-10 2014-04-16 Deutsches Zentrum für Luft- und Raumfahrt e.V. Hull structure component for vehicles, particularly for aircraft and/or spacecraft
EP3018051A1 (en) * 2014-11-06 2016-05-11 Airbus Operations GmbH Structural component and method for producing a structural component

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2638708A1 (en) * 1988-11-10 1990-05-11 Novozhilov Genrikh IMPROVEMENT TO A FUSELAGE
GB2224000B (en) * 1988-11-10 1992-05-27 Genrikh Vasilievich Novozhilov Aircraft fuselage or other pressure vessel.
GB2224000A (en) * 1988-11-10 1990-04-25 Genrikh Vasilievich Novozhilov Fuselage or pressure vessel structure
US8840980B2 (en) 2011-01-31 2014-09-23 Airbus Operations Sas Stiffened structure integrating an opening
EP2481667A1 (en) * 2011-01-31 2012-08-01 Airbus Opérations SAS Stiffened structure including an opening
CN102616365A (en) * 2011-01-31 2012-08-01 空中客车运营简化股份公司 Stiffened structure integrating an opening
FR2970941A1 (en) * 2011-01-31 2012-08-03 Airbus Operations Sas RAIDIE STRUCTURE INTEGRATING AN ORIFICE
CN102616365B (en) * 2011-01-31 2016-08-03 空中客车运营简化股份公司 The enhancing structure of integral finish
CN102602528A (en) * 2012-03-06 2012-07-25 大连理工大学 Orthogonal grating cylindrical shell provided with reinforcement ribs and circular opening and made of composite materials
CN102602528B (en) * 2012-03-06 2014-11-12 大连理工大学 Orthogonal grating cylindrical shell provided with reinforcement ribs and circular opening and made of composite materials
EP2719618A1 (en) * 2012-10-10 2014-04-16 Deutsches Zentrum für Luft- und Raumfahrt e.V. Hull structure component for vehicles, particularly for aircraft and/or spacecraft
EP3018051A1 (en) * 2014-11-06 2016-05-11 Airbus Operations GmbH Structural component and method for producing a structural component
US9988136B2 (en) 2014-11-06 2018-06-05 Airbus Operations Gmbh Structural component and method for producing a structural component

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