MX337023B - Panel de fibra de carbono de astronave con lamina metalica integral de regreso de energia. - Google Patents

Panel de fibra de carbono de astronave con lamina metalica integral de regreso de energia.

Info

Publication number
MX337023B
MX337023B MX2013012036A MX2013012036A MX337023B MX 337023 B MX337023 B MX 337023B MX 2013012036 A MX2013012036 A MX 2013012036A MX 2013012036 A MX2013012036 A MX 2013012036A MX 337023 B MX337023 B MX 337023B
Authority
MX
Mexico
Prior art keywords
astronave
carbon fiber
fiber panel
energy return
return sheet
Prior art date
Application number
MX2013012036A
Other languages
English (en)
Other versions
MX2013012036A (es
Inventor
Richard W Aston
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Publication of MX2013012036A publication Critical patent/MX2013012036A/es
Publication of MX337023B publication Critical patent/MX337023B/es

Links

Classifications

    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K1/00—Printed circuits
    • H05K1/02—Details
    • H05K1/09—Use of materials for the conductive, e.g. metallic pattern
    • 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
    • B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B15/08—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • 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
    • B32B27/00—Layered products comprising a layer of synthetic resin
    • B32B27/18—Layered products comprising a layer of synthetic resin characterised by the use of special additives
    • B32B27/20—Layered products comprising a layer of synthetic resin characterised by the use of special additives using fillers, pigments, thixotroping agents
    • 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 shape; Layered products comprising a layer 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 shape; Layered products comprising a layer 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 shape; Layered products comprising a layer 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
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/42—Arrangements or adaptations of power supply systems
    • B64G1/428—Power distribution and management
    • 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
    • B32B2605/00—Vehicles
    • B32B2605/18—Aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Laminated Bodies (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)

Abstract

Se provee una estructura aeroespacial que incluye un miembro compuesto y un elemento conductor unido al miembro compuesto caracterizado porque el elemento conductor es configurado para conducir electricidad a través de por lo menos una porción del miembro compuesto. La estructura aeroespacial puede también incluir un sistema de distribución de energía y el elemento conductor es una parte del sistema de distribución de energía para la estructura aeroespacial.
MX2013012036A 2012-10-24 2013-10-15 Panel de fibra de carbono de astronave con lamina metalica integral de regreso de energia. MX337023B (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US13/659,092 US9072184B2 (en) 2012-10-24 2012-10-24 Carbon fiber spacecraft panel with integral metallic foil power return

Publications (2)

Publication Number Publication Date
MX2013012036A MX2013012036A (es) 2014-04-28
MX337023B true MX337023B (es) 2016-02-10

Family

ID=49485503

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2013012036A MX337023B (es) 2012-10-24 2013-10-15 Panel de fibra de carbono de astronave con lamina metalica integral de regreso de energia.

Country Status (3)

Country Link
US (1) US9072184B2 (es)
EP (2) EP3517446A1 (es)
MX (1) MX337023B (es)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10414358B2 (en) 2016-02-03 2019-09-17 The Boeing Company Composite panel power system

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2840807C2 (de) * 1978-09-20 1981-12-17 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Krafteinleitungselement für ein Sandwichbauteil
US5310141A (en) * 1992-09-21 1994-05-10 General Electric Co. Battery thermal control arrangement
US6508910B2 (en) * 2000-05-18 2003-01-21 Hexcel Corporation Self-adhesive prepreg face sheet for sandwich panels
WO2002047899A1 (en) * 2000-12-12 2002-06-20 Shri Diksha Corporation Lightweight circuit board with conductive constraining cores
US7126052B2 (en) * 2002-10-02 2006-10-24 The Boeing Company Isoelectronic surfactant induced sublattice disordering in optoelectronic devices
US20050011551A1 (en) * 2003-07-14 2005-01-20 Simburger Edward J. Thin film solar cell electrical contacts
US7281318B2 (en) * 2004-05-19 2007-10-16 The Boeing Company Method of manufacturing a composite structural member having an integrated electrical circuit
US7474249B1 (en) * 2004-08-12 2009-01-06 Lockheed Martin Corporation Systems and methods for dedicating power to a radar module
US7686905B2 (en) * 2005-09-06 2010-03-30 The Boeing Company Copper grid repair technique for lightning strike protection
US7583506B1 (en) * 2005-10-14 2009-09-01 The Boeing Company Multi operational system apparatus and method
US7277266B1 (en) * 2006-03-29 2007-10-02 The Boeing Company Lightning protection system for composite structure
JP2008201971A (ja) 2007-02-22 2008-09-04 Shin Etsu Chem Co Ltd 繊維強化複合材料用液状付加硬化性シリコーン組成物、繊維強化シリコーン複合材料およびその製造方法
US7644891B2 (en) 2007-05-25 2010-01-12 The Boeing Company Spacecraft low tumble linear release system
US7934676B2 (en) * 2007-06-28 2011-05-03 The Boeing Company Pre-fabricated article for EME protection of an aircraft
DE102008006523A1 (de) 2008-01-29 2009-07-30 Airbus Deutschland Gmbh Faserverbundbauteil für ein Luft- oder Raumfahrzeug
US8206823B2 (en) * 2008-04-14 2012-06-26 The Boeing Company System and method for fabrication of integrated lightning strike protection material
DE102008042452A1 (de) * 2008-09-29 2010-04-08 Airbus Deutschland Gmbh Faserverbundbauteil zur Energieabsorption im Crash-Fall für ein Luft- oder Raumfahrzeug, Rumpfstrukturabschnitt eines Luft- oder Raumfahrzeugs und Luft- oder Raumfahrzeug
US8031458B2 (en) * 2008-11-24 2011-10-04 The Boeing Company Current return network
CA2746455C (en) * 2008-12-15 2017-01-03 3M Innovative Properties Company Surfacing film for composites with barrier layer
US8231080B2 (en) * 2009-02-26 2012-07-31 The Boeing Company Distributing power in systems having a composite structure
FR2963499B1 (fr) * 2010-07-28 2013-07-12 Airbus Operations Sas Systeme d'alimentation electrique d'un aeronef
DE102010041335A1 (de) 2010-09-24 2012-03-29 Airbus Operations Gmbh Rumpfanordnung, Luft- oder Raumfahrzeug sowie Verfahren
ES2386176B1 (es) * 2010-12-27 2013-06-21 Airbus Operations, S.L. Material compuesto multifuncional con intercapa visco-elástica.

Also Published As

Publication number Publication date
EP2724946A3 (en) 2017-11-22
EP2724946B1 (en) 2019-05-08
US20140110158A1 (en) 2014-04-24
US9072184B2 (en) 2015-06-30
MX2013012036A (es) 2014-04-28
EP2724946A2 (en) 2014-04-30
EP3517446A1 (en) 2019-07-31

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