ES2107077T3 - Estructura portante para una superficie aerodinamica. - Google Patents

Estructura portante para una superficie aerodinamica.

Info

Publication number
ES2107077T3
ES2107077T3 ES94107015T ES94107015T ES2107077T3 ES 2107077 T3 ES2107077 T3 ES 2107077T3 ES 94107015 T ES94107015 T ES 94107015T ES 94107015 T ES94107015 T ES 94107015T ES 2107077 T3 ES2107077 T3 ES 2107077T3
Authority
ES
Spain
Prior art keywords
elements
nerves
support structure
deck
aerodynamic surface
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 - Lifetime
Application number
ES94107015T
Other languages
English (en)
Inventor
Richard Bauer
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.)
Airbus Operations GmbH
Original Assignee
Airbus Operations GmbH
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 Airbus Operations GmbH filed Critical Airbus Operations GmbH
Application granted granted Critical
Publication of ES2107077T3 publication Critical patent/ES2107077T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
  • Body Structure For Vehicles (AREA)
  • Wind Motors (AREA)
  • Bridges Or Land Bridges (AREA)

Abstract

EN UNA ESTRUCTURA SOPORTE PARA UNA SUPERFICIE AERODINAMICA EN UN AVION, COMPUESTA AL MENOS DE DOS LARGUEROS, MULTIPLES NERVIOS COMPUESTOS DE ELEMENTOS DE NERVIOS Y DOS CUBIERTAS COMPUESTAS DE MULTIPLES ELEMENTOS DE CUBIERTA, DONDE LOS NERVIOS SE EXTIENDEN EN LA DIRECCION DE LA PROFUNDIDAD DE PERFIL DE LA ESTRUCTURA SOPORTE Y LA EXTENSION LONGITUDINAL DEL LARGUERO Y DE LA CUBIERTA CORRESPONDE APROXIMADAMENTE A LA ANCHURA DE LA SUJECION DE LA ESTRUCTURA SOPORTE, LA INVENCION BASA SU OBJETIVO EN QUE, LA CUBIERTA Y LOS NERVIOS EN LA DIRECCION DE LA PROFUNDIDAD PERFILADA ESTEN SUBDIVIDIDOS CON UNA DISTRIBUCION APROXIMADAMENTE IGUAL EN MULTIPLES ELEMENTOS 24,25,34,35 DE CUBIERTA O ELEMENTOS 26A,26B,36A,36B DE NERVIOS Y QUE LA ESTRUCTURA SOPORTE ESTE CONFIGURADA A BASE DE MULTIPLES ELEMENTOS 21,22 DE ESTRUCTURA, QUE SE COMPONEN RESPECTIVAMENTE A PARTIR DE UN LARGUERO 5 HASTA 9 DE DOS ELEMENTOS 24,25,34,35 DE CUBIERTA Y MULTIPLES ELEMENTOS 26A, 26B, 36A, 36B DE NERVIOS Y QUE LOS ELEMENTOS 21,22 DEESTRUCTURA ESTEN CONECTADOS UNO CON OTRO, DE TAL FORMA QUE UN ELEMENTO 21,22 DE ESTRUCTURA QUE SIGUE A CONTINUACION SEA ENCAJABLE EN UN ELEMENTO 21,22 DE ESTRUCTURA QUE LE PRECEDE. DE AQUI ES ESPECIALMENTE VENTAJOSO, QUE LA ESTRUCTURA SOPORTE SEA ELABORABLE SIN PROBLEMAS, SI LA SUPERFICIE DISPONE DE UN ESPESOR DE PERFIL PEQUEÑO Y UNA PROFUNDIDAD DE PERFIL RELATIVAMENTE GRANDE Y QUE SE DISPONGA DE UNA SOLUCION EN FORMA DE NUCLEO DE PANAL.
ES94107015T 1993-05-11 1994-05-05 Estructura portante para una superficie aerodinamica. Expired - Lifetime ES2107077T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE4315600A DE4315600C2 (de) 1993-05-11 1993-05-11 Tragstruktur für eine aerodynamische Fläche

Publications (1)

Publication Number Publication Date
ES2107077T3 true ES2107077T3 (es) 1997-11-16

Family

ID=6487740

Family Applications (1)

Application Number Title Priority Date Filing Date
ES94107015T Expired - Lifetime ES2107077T3 (es) 1993-05-11 1994-05-05 Estructura portante para una superficie aerodinamica.

Country Status (7)

Country Link
US (1) US5501414A (es)
EP (1) EP0624513B1 (es)
JP (1) JPH07125694A (es)
CA (1) CA2123393C (es)
DE (2) DE4315600C2 (es)
ES (1) ES2107077T3 (es)
RU (1) RU2133693C1 (es)

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US6513757B1 (en) * 1999-07-19 2003-02-04 Fuji Jukogyo Kabushiki Kaisha Wing of composite material and method of fabricating the same
ES2197727B1 (es) * 2000-07-27 2005-04-01 Construcciones Aeronauticas, S.A. Borde de ataque de superficies sustentadoras de aeronaves.
US6386481B1 (en) 2001-01-08 2002-05-14 Patria Finavicomp Oy Arrangement for fastening stringers to aircraft wing ribs
US7243879B2 (en) * 2001-12-06 2007-07-17 Kazak Composites, Incorporated Lattice fin for missiles or other fluid-born bodies and method for producing same
DE10301445B4 (de) * 2003-01-16 2005-11-17 Airbus Deutschland Gmbh Leichtbau-Strukturbauteil insbesondere für Flugzeuge und Verfahren zu seiner Herstellung
DE102004018579A1 (de) * 2004-04-16 2005-11-03 Airbus Deutschland Gmbh Verkleidung für eine Struktur eines Flugzeugs
US8276847B2 (en) * 2004-04-16 2012-10-02 Airbus Operations Gmbh Cover for an aircraft structure
US20060060696A1 (en) * 2004-08-26 2006-03-23 Cordy Clifford B Jr Link between the wing and canard for flutter reduction
DE102005038851A1 (de) 2005-08-17 2007-03-01 Airbus Deutschland Gmbh Fachwerk-Mittelkasten für einen Flügel
GB0606079D0 (en) * 2006-03-27 2006-05-03 Airbus Uk Ltd Aircraft component
DE102006027707A1 (de) * 2006-06-14 2007-12-20 Airbus Deutschland Gmbh Heckstruktur für ein Luft- oder Raumfahrzeug
DE102006056568A1 (de) * 2006-11-30 2008-06-05 Airbus Deutschland Gmbh Kernstruktur und Verfahren zur Herstellung einer Kernstruktur
ES2346834B1 (es) * 2007-04-30 2011-08-17 Airbus Operations, S.L. Estructura de costilla para cajones de torsion de un ala o de un estabilizador de una aeronave.
US7829829B2 (en) * 2007-06-27 2010-11-09 Kazak Composites, Incorporated Grid fin control system for a fluid-borne object
ES2372828B1 (es) * 2008-12-17 2012-12-13 Airbus Operations, S.L. Costilla-herraje.
GB0918750D0 (en) * 2009-10-27 2009-12-09 Airbus Uk Ltd Cover trailing edge profile
DE102010010168B4 (de) 2010-03-03 2013-09-19 Airbus Operations Gmbh Verstrebungsanordnung zur Stabilisierung der Außenhaut eines aerodynamischen Flugzeugteils bei einem Verkehrsflugzeug
ES2398287B1 (es) * 2010-03-29 2014-01-29 Airbus Operations S.L. Fuselaje de aeronave resistente al impacto y tolerante al daño.
US9156559B2 (en) * 2011-10-19 2015-10-13 The Boeing Company Segmented aircraft wing having solar arrays
ES2426111B1 (es) * 2012-04-17 2015-03-24 Airbus Operations S.L. Interfaz para superficie de sustentación de aeronave
EP2735502B1 (en) * 2012-11-21 2016-08-24 Airbus Operations S.L. An optimized torsion box for an aircraft
RU2532254C2 (ru) * 2013-02-07 2014-11-10 Общество с ограниченной ответственностью "Научно-технологический испытательный центр АпАТэК-Дубна" Кессон крыла из композиционного материала
US9341207B2 (en) * 2013-07-30 2016-05-17 Gulfstream Aerospace Corporation Web component and method of making a web component
FR3059303B1 (fr) * 2016-11-30 2020-11-06 Airbus Operations Sas Ensemble pour aeronef comprenant un panneau auto-raidi comportant une portion de hauteur croissante par laquelle le panneau est fixe a un element structurel
US10597141B2 (en) * 2018-03-30 2020-03-24 The Boeing Company Wing flap with torque member and method for forming thereof
US10647407B2 (en) * 2018-03-30 2020-05-12 The Boeing Company Wing flap with torque member and method for forming thereof
US11459085B2 (en) * 2019-04-30 2022-10-04 Textron Innovations Inc. Energy attenuation stabilizers and methods
DE102019123012A1 (de) * 2019-08-28 2021-03-04 Airbus Operations Gmbh Verfahren zum Herstellen eines Torsionskasten für eine Struktur eines Flugzeugs sowie ein Torsionskasten für eine Struktur eines Flugzeugs
US11352124B2 (en) * 2019-11-01 2022-06-07 The Boeing Company Continuous skin leading edge slats
US11623734B2 (en) 2020-12-02 2023-04-11 The Boeing Company Apparatus, system and method for supporting a wing flap of an aircraft

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Also Published As

Publication number Publication date
RU2133693C1 (ru) 1999-07-27
EP0624513A1 (de) 1994-11-17
DE59403600D1 (de) 1997-09-11
EP0624513B1 (de) 1997-08-06
JPH07125694A (ja) 1995-05-16
DE4315600A1 (de) 1994-11-17
CA2123393C (en) 2000-12-12
RU94015834A (ru) 1996-08-27
DE4315600C2 (de) 1996-07-25
US5501414A (en) 1996-03-26
CA2123393A1 (en) 1994-11-12

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