IL101542A0 - Structural component and a method of manufacturing same - Google Patents

Structural component and a method of manufacturing same

Info

Publication number
IL101542A0
IL101542A0 IL101542A IL10154292A IL101542A0 IL 101542 A0 IL101542 A0 IL 101542A0 IL 101542 A IL101542 A IL 101542A IL 10154292 A IL10154292 A IL 10154292A IL 101542 A0 IL101542 A0 IL 101542A0
Authority
IL
Israel
Prior art keywords
sheet
component part
pct
front face
date oct
Prior art date
Application number
IL101542A
Other languages
English (en)
Original Assignee
Short Brothers Plc
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 Short Brothers Plc filed Critical Short Brothers Plc
Publication of IL101542A0 publication Critical patent/IL101542A0/xx

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form
    • B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
    • B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/14—Layered products comprising a layer of metal next to a fibrous or filamentary layer
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/20—Layered products comprising a layer of metal comprising aluminium or copper
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • B32B5/024—Woven fabric
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • B32B5/12—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer characterised by the relative arrangement of fibres or filaments of different layers, e.g. the fibres or filaments being parallel or perpendicular to each other
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04—Interconnection of layers
    • B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
    • 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
    • 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
    • B64C1/068—Fuselage sections
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/02—Synthetic macromolecular fibres
    • B32B2262/0261—Polyamide fibres
    • B32B2262/0269—Aromatic polyamide fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10—Inorganic fibres
    • B32B2262/101—Glass fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10—Inorganic fibres
    • B32B2262/106—Carbon fibres, e.g. graphite fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2305/00—Condition, form or state of the layers or laminate
    • B32B2305/08—Reinforcements
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/20—Properties of the layers or laminate having particular electrical or magnetic properties, e.g. piezoelectric
    • B32B2307/202—Conductive
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/20—Properties of the layers or laminate having particular electrical or magnetic properties, e.g. piezoelectric
    • B32B2307/206—Insulating
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2311/00—Metals, their alloys or their compounds
    • B32B2311/12—Copper
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2311/00—Metals, their alloys or their compounds
    • B32B2311/24—Aluminium
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2605/00—Vehicles
    • B32B2605/18—Aircraft
    • 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
    • B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials
IL101542A 1991-04-12 1992-04-09 Structural component and a method of manufacturing same IL101542A0 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB919107766A GB9107766D0 (en) 1991-04-12 1991-04-12 A structural component

Publications (1)

Publication Number Publication Date
IL101542A0 true IL101542A0 (en) 1992-12-30

Family

ID=10693125

Family Applications (1)

Application Number Title Priority Date Filing Date
IL101542A IL101542A0 (en) 1991-04-12 1992-04-09 Structural component and a method of manufacturing same

Country Status (11)

Country Link
US (1) US5417385A (pt)
EP (1) EP0579675B1 (pt)
JP (1) JPH06508801A (pt)
AT (1) ATE160533T1 (pt)
AU (1) AU655463B2 (pt)
BR (1) BR9205701A (pt)
CA (1) CA2100241A1 (pt)
DE (1) DE69223316D1 (pt)
GB (2) GB9107766D0 (pt)
IL (1) IL101542A0 (pt)
WO (1) WO1992018329A1 (pt)

Families Citing this family (44)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10160315A1 (de) * 2001-12-07 2003-11-13 Airbus Gmbh Einrichtung zur Landeanflug-Steuerung eines Flugszeuges
NL1019957C2 (nl) * 2002-02-13 2003-10-03 Stork Fokker Aesp Bv Gelamineerd paneel met discontinue inwendige laag.
US7014143B2 (en) 2002-10-11 2006-03-21 The Boeing Company Aircraft lightning strike protection and grounding technique
WO2005032812A2 (en) * 2003-09-30 2005-04-14 The Boeing Company Applique
DE05819580T1 (de) * 2004-09-01 2008-04-24 Bell Helicopter Textron, Inc., Fort Worth Pressgeformte teile mit einer eingebetteten leiterschicht und herstellungsverfahren dafür
US20070141927A1 (en) * 2005-12-21 2007-06-21 Brown Arlene M Method and system for exterior protection of an aircraft
US8709584B2 (en) * 2006-01-31 2014-04-29 Sikorsky Aircraft Corporation Composite aircraft floor system
EP2363429A1 (en) 2006-03-10 2011-09-07 Goodrich Corporation Low density lightining strike protection for use in airplanes
US7277266B1 (en) 2006-03-29 2007-10-02 The Boeing Company Lightning protection system for composite structure
WO2007130979A2 (en) † 2006-05-02 2007-11-15 Rohr, Inc. Modification of reinforcing fiber tows used in composite materials by using nanoreinforcements
GB0613386D0 (en) * 2006-07-05 2006-08-16 Flight Refueling Ltd A drogue assembly for in-flight refuelling
DE102006031436B4 (de) * 2006-07-07 2012-12-06 Airbus Operations Gmbh Strukturelement, Verfahren zur Herstellung eines derartigen Strukturelements und Flugzeug mit einem derartigen Strukturelement
US7628879B2 (en) * 2007-08-23 2009-12-08 The Boeing Company Conductive scrim embedded structural adhesive films
DE102007062082A1 (de) * 2007-12-21 2009-07-23 Airbus Deutschland Gmbh Kernverbundstruktur
US8163379B2 (en) 2007-12-21 2012-04-24 Airbus Deutschland Gmbh Sandwich structure
DE102008010228A1 (de) * 2008-02-21 2009-09-03 Airbus Deutschland Gmbh Verfahren und Vorrichtung zur Herstellung faserverstärkter Kunststoffprofilteile
GB0805640D0 (en) * 2008-03-28 2008-04-30 Hexcel Composites Ltd Improved composite materials
US8206823B2 (en) * 2008-04-14 2012-06-26 The Boeing Company System and method for fabrication of integrated lightning strike protection material
GB0817591D0 (en) * 2008-09-26 2008-11-05 Hexcel Composites Ltd Improvements in composite materials
CA2771377C (en) * 2009-08-21 2018-05-22 Scott Duquette Energy dissipative tubes, sealing devices, and methods of fabricating and installing the same
US8561934B2 (en) 2009-08-28 2013-10-22 Teresa M. Kruckenberg Lightning strike protection
ES2402466B1 (es) * 2010-12-14 2014-03-13 Airbus Operations, S.L. Disposicion de proteccion de rayos y corrosion en un componente estructural de una aeronave.
US8882023B2 (en) 2011-04-11 2014-11-11 The Boeing Company Aircraft structural assembly with electromagnetic protection
US9567104B2 (en) 2011-04-12 2017-02-14 The Boeing Company Utilization of aircraft bondline embedded current sensors in the determination of a lightning damage index
WO2013028830A2 (en) 2011-08-25 2013-02-28 Lord Corporation Lightning strike protection system
WO2014004704A1 (en) 2012-06-26 2014-01-03 California Institute Of Technology Systems and methods for implementing bulk metallic glass-based macroscale gears
EP2716436B1 (de) 2012-10-04 2020-03-18 Magna Steyr Fahrzeugtechnik AG & Co KG Kohlenstoffverbundbauteil
EP2730508B1 (en) * 2012-11-12 2016-09-14 Airbus Operations GmbH Lining/fairing panel and method for measuring the electrical bonding resistance of a lining/fairing panel
DK2987212T3 (da) * 2013-02-20 2023-01-09 Techhold Llc Overspændingsbeskyttelse for strømsystemer
US9681527B2 (en) 2013-03-29 2017-06-13 The Boeing Company Method and apparatus for providing a current return network in an aircraft structure
US20140342179A1 (en) 2013-04-12 2014-11-20 California Institute Of Technology Systems and methods for shaping sheet materials that include metallic glass-based materials
US9541225B2 (en) 2013-05-09 2017-01-10 Titeflex Corporation Bushings, sealing devices, tubing, and methods of installing tubing
FR3023210B1 (fr) * 2014-07-07 2017-02-24 Safran Procede de fabrication de piece en materiau composite comportant au moins une portion formant portion d'introduction d'effort ou surepaisseur locale
US10151377B2 (en) 2015-03-05 2018-12-11 California Institute Of Technology Systems and methods for implementing tailored metallic glass-based strain wave gears and strain wave gear components
US10968527B2 (en) 2015-11-12 2021-04-06 California Institute Of Technology Method for embedding inserts, fasteners and features into metal core truss panels
WO2018063970A1 (en) * 2016-09-27 2018-04-05 3M Innovative Properties Company Protection film
US11273622B2 (en) * 2016-12-14 2022-03-15 The Boeing Company Stiffening elements that comprise integral current flowpaths
US11198181B2 (en) 2017-03-10 2021-12-14 California Institute Of Technology Methods for fabricating strain wave gear flexsplines using metal additive manufacturing
EP3630395A4 (en) 2017-05-24 2020-11-25 California Institute of Technology HYPOEUTECTIC AMORPHIC METAL BASED MATERIALS FOR ADDITIVE MANUFACTURING
WO2018223117A2 (en) 2017-06-02 2018-12-06 California Institute Of Technology High toughness metallic glass-based composites for additive manufacturing
JP7034849B2 (ja) * 2018-06-28 2022-03-14 三菱重工業株式会社 複合材、複合材の製造方法、及び複合材の硬化方法
JP7039401B2 (ja) * 2018-06-28 2022-03-22 三菱重工業株式会社 複合材及び複合材の硬化方法
US11680629B2 (en) 2019-02-28 2023-06-20 California Institute Of Technology Low cost wave generators for metal strain wave gears and methods of manufacture thereof
IL298453A (en) 2020-05-22 2023-01-01 Techhold Llc Overvoltage protection assembly

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1342898A (en) * 1970-10-24 1974-01-03 British Aircraft Corporaton Lt Composite panels
US4198454A (en) * 1978-10-27 1980-04-15 American Air Filter Company, Inc. Lightweight composite panel
FR2486875A1 (fr) * 1980-07-17 1982-01-22 Dassault Avions Procede pour metalliser au moins partiellement la surface d'une piece stratifiee
US4349859A (en) * 1980-09-24 1982-09-14 Mcdonnell Douglas Corporation Shielded structural or containment member
US4599255A (en) * 1981-12-28 1986-07-08 The Boeing Company Composite structures having conductive surfaces
US4542056A (en) * 1983-08-26 1985-09-17 The Boeing Company Composite structure having conductive surfaces
AT384189B (de) * 1983-10-10 1987-10-12 Fischer Gmbh Bauplatte
DE3481290D1 (de) * 1984-01-09 1990-03-15 Boeing Co Kompositmaterialstruktur mit vollem feuerschutz.
DE3419192A1 (de) * 1984-05-23 1985-11-28 Gebr. Happich Gmbh, 5600 Wuppertal Ascher oder dergleichen einbauteil fuer fahrzeuge
DE3419292C2 (de) * 1984-05-24 1986-07-17 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Sandwich-Bauteil
US4888451A (en) * 1988-11-29 1989-12-19 United Technologies Corporation Electrical continuity means for composite joints
US5127601A (en) * 1989-01-23 1992-07-07 Lightning Diversion Systems Conformal lightning shield and method of making

Also Published As

Publication number Publication date
EP0579675A1 (en) 1994-01-26
CA2100241A1 (en) 1992-10-13
GB2255314B (en) 1995-05-24
DE69223316D1 (de) 1998-01-08
AU655463B2 (en) 1994-12-22
BR9205701A (pt) 1994-05-24
JPH06508801A (ja) 1994-10-06
GB9207842D0 (en) 1992-05-27
GB2255314A (en) 1992-11-04
EP0579675B1 (en) 1997-11-26
WO1992018329A1 (en) 1992-10-29
US5417385A (en) 1995-05-23
GB9107766D0 (en) 1991-06-05
ATE160533T1 (de) 1997-12-15
AU1539292A (en) 1992-11-17

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