ES2531154T3 - Aeroestructura ventilada, aeronave y métodos asociados - Google Patents

Aeroestructura ventilada, aeronave y métodos asociados Download PDF

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Publication number
ES2531154T3
ES2531154T3 ES13167336T ES13167336T ES2531154T3 ES 2531154 T3 ES2531154 T3 ES 2531154T3 ES 13167336 T ES13167336 T ES 13167336T ES 13167336 T ES13167336 T ES 13167336T ES 2531154 T3 ES2531154 T3 ES 2531154T3
Authority
ES
Spain
Prior art keywords
micro
lattice structure
aerostructure
ventilated
aircraft
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.)
Active
Application number
ES13167336T
Other languages
English (en)
Inventor
Robert E Doty
Richard W Burns
Alan Jon Jacobsen
Sophia Shu Yang
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.)
Boeing Co
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
Application granted granted Critical
Publication of ES2531154T3 publication Critical patent/ES2531154T3/es
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/20Integral or sandwich constructions
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00Layered 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
    • B32B3/26Layered 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 particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
    • B32B3/28Layered 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 particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by a layer comprising a deformed thin sheet, i.e. the layer having its entire thickness deformed out of the plane, e.g. corrugated, crumpled
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00Layered 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
    • B32B3/10Layered 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
    • B32B3/12Layered 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/26Construction, shape, or attachment of separate skins, e.g. panels
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2305/00Condition, form or state of the layers or laminate
    • B32B2305/02Cellular or porous
    • B32B2305/024Honeycomb
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2305/00Condition, form or state of the layers or laminate
    • B32B2305/38Meshes, lattices or nets
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/70Other properties
    • B32B2307/724Permeability to gases, adsorption
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2605/00Vehicles
    • B32B2605/18Aircraft
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10Methods of surface bonding and/or assembly therefor
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10Methods of surface bonding and/or assembly therefor
    • Y10T156/1002Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
  • Motor Or Generator Cooling System (AREA)
  • Linear Motors (AREA)
  • Iron Core Of Rotating Electric Machines (AREA)

Abstract

Una aeroestructura ventilada, que comprende: una estructura de micro-celosía que tiene un primer lado y un segundo lado, donde la estructura de micro-celosía incluye una pluralidad de elementos de armadura, y donde la pluralidad de elementos de armadura define una pluralidad de nodos en intersecciones de dos o más elementos de armadura; y un núcleo alveolar acoplado operativamente al primer lado de la estructura de micro-celosía, donde el núcleo alveolar incluye una pluralidad de paredes que definen una pluralidad de células alargadas; donde una interfaz entre el núcleo alveolar y la estructura de micro-celosía se configura para permitir el flujo de aire hacia y desde el núcleo alveolar a través de la estructura de micro-celosía.
ES13167336T 2012-05-11 2013-05-10 Aeroestructura ventilada, aeronave y métodos asociados Active ES2531154T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US13/469,913 US9321241B2 (en) 2012-05-11 2012-05-11 Ventilated aero-structures, aircraft and associated methods

Publications (1)

Publication Number Publication Date
ES2531154T3 true ES2531154T3 (es) 2015-03-11

Family

ID=48482904

Family Applications (1)

Application Number Title Priority Date Filing Date
ES13167336T Active ES2531154T3 (es) 2012-05-11 2013-05-10 Aeroestructura ventilada, aeronave y métodos asociados

Country Status (3)

Country Link
US (2) US9321241B2 (es)
EP (1) EP2662207B1 (es)
ES (1) ES2531154T3 (es)

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US10556670B2 (en) * 2010-08-15 2020-02-11 The Boeing Company Laminar flow panel
US9771998B1 (en) 2014-02-13 2017-09-26 Hrl Laboratories, Llc Hierarchical branched micro-truss structure and methods of manufacturing the same
CN103887605B (zh) * 2014-04-04 2016-08-24 西安电子科技大学 结构功能一体化机翼天线
US9733429B2 (en) 2014-08-18 2017-08-15 Hrl Laboratories, Llc Stacked microlattice materials and fabrication processes
US9162416B1 (en) * 2014-08-18 2015-10-20 Hrl Laboratories, Llc Basal plane reinforced microlattice
US9783324B2 (en) * 2014-08-26 2017-10-10 The Boeing Company Vessel insulation assembly
US10427336B2 (en) 2014-11-20 2019-10-01 Baker Hughes, A Ge Company, Llc Periodic structured composite and articles therefrom
US10358821B2 (en) * 2015-03-02 2019-07-23 The Boeing Company Thermoplastic truss structure for use in wing and rotor blade structures and methods for manufacture
CA2949257C (en) * 2016-02-12 2020-12-22 The Boeing Company Laminar flow panel
US10179428B2 (en) * 2016-11-17 2019-01-15 The Boeing Company Mechanically reinforced foam insulation panel and methods of making the same
US10479520B2 (en) * 2017-05-25 2019-11-19 The Boeing Company Composite structure assembly having an interconnected layered core
US10203169B2 (en) * 2017-06-12 2019-02-12 Microsoft Technology Licensing, Llc Thermal management devices, systems and methods
DE102017128497A1 (de) * 2017-11-30 2019-06-06 Airbus Operations Gmbh Vorderkantenanordnung für einen Strömungskörper eines Fahrzeugs
US11034460B2 (en) * 2017-12-08 2021-06-15 The Boeing Company Additively manufactured septa for acoustic panels
EP3539865A1 (en) 2018-03-12 2019-09-18 Ge Avio S.r.l. Fan blade support assembly
US11577815B2 (en) * 2020-01-30 2023-02-14 Textron Innovations Inc. Isogrid patterns for structural aircraft panels
US12172415B2 (en) 2023-01-12 2024-12-24 The Boeing Company Sandwich panels and methods of manufacturing sandwich panels
WO2024256037A1 (de) * 2023-06-12 2024-12-19 Enerkite Gmbh Aerodynamische hohlkammer-strukturen

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US3261576A (en) * 1962-06-14 1966-07-19 Olin Mathieson Aircraft structure
US4749150A (en) * 1985-12-24 1988-06-07 Rohr Industries, Inc. Turbofan duct with noise suppression and boundary layer control
US4671841A (en) * 1986-01-06 1987-06-09 Rohr Industries, Inc. Method of making an acoustic panel with a triaxial open-weave face sheet
DE3720371A1 (de) * 1987-06-19 1989-01-05 Messerschmitt Boelkow Blohm Leichtbauverbundplatte und verfahren zu deren herstellung
US4990391A (en) * 1989-02-03 1991-02-05 Rohr Industries, Inc. Reticulated core to perforate sheet bonding and galvanic barrier
US5721402A (en) * 1996-09-09 1998-02-24 Northrop Grumman Corporation Noise suppression system for a jet engine
DE19804718C2 (de) * 1998-02-06 2001-09-13 Eurocopter Deutschland Schall absorbierende Sandwichwand
DE10154063B4 (de) * 2001-11-02 2013-11-28 Airbus Operations Gmbh Doppelwandiger Kernverbund, vorzugsweise Faserverbund
WO2005014216A2 (en) * 2003-02-14 2005-02-17 University Of Virginia Patent Foundation Methods for manufacture of multilayered multifunctional truss structures and related structures there from
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US8191616B2 (en) * 2006-11-02 2012-06-05 The Boeing Company Combined thermal protection and surface temperature control system
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US8079443B2 (en) * 2008-01-07 2011-12-20 Pelzer Acoustic Products Gmbh Aircraft trim panel with integrated adjustable acoustic properties
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Also Published As

Publication number Publication date
US10183736B2 (en) 2019-01-22
US20160194070A1 (en) 2016-07-07
EP2662207A1 (en) 2013-11-13
US20130303067A1 (en) 2013-11-14
US9321241B2 (en) 2016-04-26
EP2662207B1 (en) 2015-01-28

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