BR9205701A - Componente estrutural, aeronave, processo de fabricaçao de um componente e porta de capota de ventilador para um motor de aviaçao - Google Patents

Componente estrutural, aeronave, processo de fabricaçao de um componente e porta de capota de ventilador para um motor de aviaçao

Info

Publication number
BR9205701A
BR9205701A BR9205701A BR9205701A BR9205701A BR 9205701 A BR9205701 A BR 9205701A BR 9205701 A BR9205701 A BR 9205701A BR 9205701 A BR9205701 A BR 9205701A BR 9205701 A BR9205701 A BR 9205701A
Authority
BR
Brazil
Prior art keywords
sheet
component part
pct
aircraft
front face
Prior art date
Application number
BR9205701A
Other languages
English (en)
Inventor
Michael John Arnold
Charles Euan Douglas
Arthur Brian Hamill
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 BR9205701A publication Critical patent/BR9205701A/pt

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
BR9205701A 1991-04-12 1992-04-09 Componente estrutural, aeronave, processo de fabricaçao de um componente e porta de capota de ventilador para um motor de aviaçao BR9205701A (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB919107766A GB9107766D0 (en) 1991-04-12 1991-04-12 A structural component
PCT/GB1992/000636 WO1992018329A1 (en) 1991-04-12 1992-04-09 A structural component

Publications (1)

Publication Number Publication Date
BR9205701A true BR9205701A (pt) 1994-05-24

Family

ID=10693125

Family Applications (1)

Application Number Title Priority Date Filing Date
BR9205701A BR9205701A (pt) 1991-04-12 1992-04-09 Componente estrutural, aeronave, processo de fabricaçao de um componente e porta de capota de ventilador para um motor de aviaçao

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)

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US7014143B2 (en) * 2002-10-11 2006-03-21 The Boeing Company Aircraft lightning strike protection and grounding technique
US8715824B2 (en) * 2003-09-30 2014-05-06 The Boeing Company Applique
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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
WO2008048705A2 (en) 2006-03-10 2008-04-24 Goodrich Corporation Low density lightning strike protection for use in airplanes
US7277266B1 (en) 2006-03-29 2007-10-02 The Boeing Company Lightning protection system for composite structure
EP2013408B2 (en) † 2006-05-02 2016-09-28 Rohr, Inc. Nacelles and components thereof 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
CA3060376C (en) 2009-08-21 2021-11-16 Titeflex Corporation 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
US9007739B2 (en) 2011-08-25 2015-04-14 Lord Corporation Lightning strike protection system
US20150047463A1 (en) 2012-06-26 2015-02-19 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
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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
EP3519176A1 (en) * 2016-09-27 2019-08-07 3M Innovative Properties Company Protection film
US11273622B2 (en) * 2016-12-14 2022-03-15 The Boeing Company Stiffening elements that comprise integral current flowpaths
JP2020512482A (ja) 2017-03-10 2020-04-23 カリフォルニア インスティチュート オブ テクノロジー 金属積層造形を用いた波動歯車フレクスプラインの製造方法
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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
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Also Published As

Publication number Publication date
GB2255314A (en) 1992-11-04
GB9107766D0 (en) 1991-06-05
CA2100241A1 (en) 1992-10-13
EP0579675A1 (en) 1994-01-26
ATE160533T1 (de) 1997-12-15
AU655463B2 (en) 1994-12-22
JPH06508801A (ja) 1994-10-06
EP0579675B1 (en) 1997-11-26
GB9207842D0 (en) 1992-05-27
US5417385A (en) 1995-05-23
IL101542A0 (en) 1992-12-30
WO1992018329A1 (en) 1992-10-29
GB2255314B (en) 1995-05-24
AU1539292A (en) 1992-11-17
DE69223316D1 (de) 1998-01-08

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Legal Events

Date Code Title Description
EE Request for examination
FB36 Technical and formal requirements: requirement - article 36 of industrial property law
FA8 Dismissal: dismissal - article 36, par. 1 of industrial property law