FR1513521A - Structured panel, especially for aircraft construction - Google Patents

Structured panel, especially for aircraft construction

Info

Publication number
FR1513521A
FR1513521A FR89936A FR89936A FR1513521A FR 1513521 A FR1513521 A FR 1513521A FR 89936 A FR89936 A FR 89936A FR 89936 A FR89936 A FR 89936A FR 1513521 A FR1513521 A FR 1513521A
Authority
FR
France
Prior art keywords
protrusions
elements
rows
face
row
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
FR89936A
Other languages
French (fr)
Inventor
Jeremie Malczewski
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.)
Bronzavia SA
Original Assignee
Bronzavia SA
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 Bronzavia SA filed Critical Bronzavia SA
Priority to FR89936A priority Critical patent/FR1513521A/en
Priority to GB58659/67A priority patent/GB1216990A/en
Application granted granted Critical
Publication of FR1513521A publication Critical patent/FR1513521A/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
    • B64C1/12—Construction or attachment of skin panels
    • 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
    • E04C2/32—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 formed of corrugated or otherwise indented sheet-like material; composed of such layers with or without layers of flat sheet-like material
    • E04C2/326—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 formed of corrugated or otherwise indented sheet-like material; composed of such layers with or without layers of flat sheet-like material with corrugations, incisions or reliefs in more than one direction of the element
    • 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
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Abstract

1,216,990. Metal laminate. SOC. ANON. BRONZAVIA. 27 Dec., 1967 [4 Jan., 1967], No. 58659/67. Heading B5N. [Also in Divisions E1-E2] A composite structure comprises sheet-like metal elements and one element 1 has a plurality of substantially identical spaced elongated, hollow protrusions 2 formed on one face thereof, the protrusions being disposed to lie in two sets of parallel regularly spaced rows, with the protrusions of one set of rows extending transversely of the protrusions of the other set of rows, the protrusions in each row being offset, along said row, with respect to the protrusions in each immediately adjacent row of the same set, and each protrusion of said one set of rows being disposed between two successive protrusions of a respective row of said other set, the other face of the element 1 being applied against one face of a second element, the two elements being rigidly secured together over at least part of their area of contact. The second element may be flat or have protrusions or longitudinal ribs on its outer face. The elements may be glued, brazed, spot-welded or riveted together. When both elements have protrusions these may be aligned with each other, or placed in parallel, or oriented slantwise with respect to each other. The protrusions of different elements may be of different sizes and project by different amounts. The protrusions may be formed by pressing. The structure may be flat, or follow the surface of a cylinder or cone, or may be curved in two directions by forming the elements on a press before assembly.
FR89936A 1967-01-04 1967-01-04 Structured panel, especially for aircraft construction Expired FR1513521A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR89936A FR1513521A (en) 1967-01-04 1967-01-04 Structured panel, especially for aircraft construction
GB58659/67A GB1216990A (en) 1967-01-04 1967-12-27 Improvements in or relating to composite structures

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR89936A FR1513521A (en) 1967-01-04 1967-01-04 Structured panel, especially for aircraft construction

Publications (1)

Publication Number Publication Date
FR1513521A true FR1513521A (en) 1968-02-16

Family

ID=8623375

Family Applications (1)

Application Number Title Priority Date Filing Date
FR89936A Expired FR1513521A (en) 1967-01-04 1967-01-04 Structured panel, especially for aircraft construction

Country Status (2)

Country Link
FR (1) FR1513521A (en)
GB (1) GB1216990A (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3803062A1 (en) * 1988-01-29 1989-08-10 Herbst Donald BENDABLE SHUTTERING FILM
GB2231597A (en) * 1989-02-04 1990-11-21 Steelpress Metal cladding panel
US5271986A (en) * 1991-04-19 1993-12-21 United Technologies Corporation Structural member having a stiffener bead therein and comprising plies of composite material extending for the full length and width of the structural member and continuously through the stiffener bead, and the article so made
DE102009018825A1 (en) * 2009-04-24 2010-10-28 Emitec Gesellschaft Für Emissionstechnologie Mbh Sheet metal layer with anti-diffusion structures and metallic honeycomb body with at least one such sheet metal layer
US10611118B2 (en) * 2015-01-09 2020-04-07 President And Fellows Of Harvard College Negative poisson's ratio waffle structures

Also Published As

Publication number Publication date
GB1216990A (en) 1970-12-23

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