ES2197727A1 - Borde de ataque de superficies sustentadoras de aeronaves. - Google Patents

Borde de ataque de superficies sustentadoras de aeronaves.

Info

Publication number
ES2197727A1
ES2197727A1 ES200001888A ES200001888A ES2197727A1 ES 2197727 A1 ES2197727 A1 ES 2197727A1 ES 200001888 A ES200001888 A ES 200001888A ES 200001888 A ES200001888 A ES 200001888A ES 2197727 A1 ES2197727 A1 ES 2197727A1
Authority
ES
Spain
Prior art keywords
leading edge
aircraft
primary structure
frontal
aerodynamic surfaces
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.)
Granted
Application number
ES200001888A
Other languages
English (en)
Other versions
ES2197727B1 (es
Inventor
Castro Nodal Manuel De
Pancorbo Carlos Cerezo
Casado Rafael Dominguez
Diez Casado Grueso
Diez Cesar Grueso
Garcia Manuel Huertas
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 Defence and Space SA
Original Assignee
Construcciones Aeronauticas CASA SA
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 Construcciones Aeronauticas CASA SA filed Critical Construcciones Aeronauticas CASA SA
Priority to ES200001888A priority Critical patent/ES2197727B1/es
Priority to AT01500095T priority patent/ATE434559T1/de
Priority to DE60139052T priority patent/DE60139052D1/de
Priority to EP01500095A priority patent/EP1176089B1/en
Priority to CA002343590A priority patent/CA2343590C/en
Priority to US09/828,292 priority patent/US6616101B2/en
Publication of ES2197727A1 publication Critical patent/ES2197727A1/es
Application granted granted Critical
Publication of ES2197727B1 publication Critical patent/ES2197727B1/es
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/28—Leading or trailing edges attached to primary structures, e.g. forming fixed slots
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/20—Integral or sandwich constructions

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
  • Catching Or Destruction (AREA)
  • Vibration Dampers (AREA)
  • Body Structure For Vehicles (AREA)

Abstract

Borde de ataque de superficies sustentadoras de aeronaves. Una estructura primaria (EP) realizada sin costillas se ensambla con una zona frontal (ZF) especifica contra impactos, comprendiendo la estructura primaria dos paneles de revestimiento superior e interior (1, 2) y dos largueros diagonal y frontal (3, 4), que constituyen el conjunto estructural rígido y resistente del borde de ataque (BA), y estando formada la zona frontal (ZF) por una o dos piezas elementales que determinan una especie de teja que cierra el contorno aerodinámico exterior del perfil del borde de ataque (BA) y proporciona un buen comportamiento frente a erosión, impactos operacionales en tierra e impacto de pájaro en vuelo. La invención es aplicable a alas, estabilizadores y superficies de mando de aviones.
ES200001888A 2000-07-27 2000-07-27 Borde de ataque de superficies sustentadoras de aeronaves. Expired - Fee Related ES2197727B1 (es)

Priority Applications (6)

Application Number Priority Date Filing Date Title
ES200001888A ES2197727B1 (es) 2000-07-27 2000-07-27 Borde de ataque de superficies sustentadoras de aeronaves.
AT01500095T ATE434559T1 (de) 2000-07-27 2001-04-04 Nase einer aerodynamischen fläche eines flugzeuges
DE60139052T DE60139052D1 (de) 2000-07-27 2001-04-04 Nase einer aerodynamischen Fläche eines Flugzeuges
EP01500095A EP1176089B1 (en) 2000-07-27 2001-04-04 Leading edge of aerodynamic surfaces of aircraft
CA002343590A CA2343590C (en) 2000-07-27 2001-04-06 Leading edge of supporting surfaces of aircraft
US09/828,292 US6616101B2 (en) 2000-07-27 2001-04-06 Leading edge of supporting surfaces of aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES200001888A ES2197727B1 (es) 2000-07-27 2000-07-27 Borde de ataque de superficies sustentadoras de aeronaves.

Publications (2)

Publication Number Publication Date
ES2197727A1 true ES2197727A1 (es) 2004-01-01
ES2197727B1 ES2197727B1 (es) 2005-04-01

Family

ID=8494455

Family Applications (1)

Application Number Title Priority Date Filing Date
ES200001888A Expired - Fee Related ES2197727B1 (es) 2000-07-27 2000-07-27 Borde de ataque de superficies sustentadoras de aeronaves.

Country Status (6)

Country Link
US (1) US6616101B2 (es)
EP (1) EP1176089B1 (es)
AT (1) ATE434559T1 (es)
CA (1) CA2343590C (es)
DE (1) DE60139052D1 (es)
ES (1) ES2197727B1 (es)

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BE1015867A3 (fr) 2004-01-22 2005-10-04 Sonaca Sa Ensemble de bord d'attaque d'un element de voilure d'aeronef et element de voilure equipee d'au moins un tel ensemble.
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
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EP1764307A1 (en) * 2005-09-14 2007-03-21 EADS Construcciones Aeronauticas, S.A. Process for manufacturing a monolithic leading edge
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DE102005060958A1 (de) * 2005-12-20 2007-06-21 Airbus Deutschland Gmbh Schutzvorrichtung
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US7721525B2 (en) * 2006-07-19 2010-05-25 Rohr, Inc. Aircraft engine inlet having zone of deformation
FR2918036A1 (fr) * 2007-06-26 2009-01-02 Sogeclair Sa Dispositif formant bord d'attaque pour une voilure d'aeronef et voilure equipee d'un tel dispositif.
FI20080208L (fi) * 2008-03-13 2008-03-27 Patria Aerostructures Oy Ilma-aluksen johtoreunaelementti, menetelmä sen valmistamiseksi sekä siipi ja vakain
GB0906850D0 (en) * 2009-04-22 2009-06-03 Rolls Royce Plc Method of manufacturing an aerofoil
ES2403361B1 (es) * 2010-12-17 2014-04-29 Airbus Operations, S.L. Optimización de estructuras sometidas a corrientes de gases calientes.
CN102390520B (zh) * 2011-09-29 2014-06-18 西北工业大学 一种能够提高飞机抗鸟撞性能的尾翼
ES2426111B1 (es) * 2012-04-17 2015-03-24 Airbus Operations S.L. Interfaz para superficie de sustentación de aeronave
ES2606245T3 (es) * 2012-07-17 2017-03-23 Airbus Operations, S.L. Borde de ataque altamente integrado de una superficie sustentadora de una aeronave
EP2922752A4 (en) * 2012-11-20 2017-01-25 Saab Ab An airframe leading edge
EP2886452B1 (en) * 2013-12-18 2017-09-13 Airbus Operations GmbH Flow body, method for manufacturing a flow body and aircraft having such a flow body
EP2886449A1 (en) 2013-12-23 2015-06-24 Airbus Operations S.L. Leading edge for an aircraft lifting surface
EP2962840A1 (en) * 2014-06-30 2016-01-06 Airbus Operations, S.L. A leading edge for an aircraft lifting surface and manufacturing method thereof
GB2550403A (en) 2016-05-19 2017-11-22 Airbus Operations Ltd Aerofoil body with integral curved spar-cover
EP3330174B1 (en) * 2016-12-02 2019-10-30 Airbus Operations, S.L. Aircraft stabilizer leading edge integration with torsion box and fuselage
EP3335986B1 (en) * 2016-12-19 2019-11-20 Airbus Operations S.L. Impact resistant dorsal fin
CN106986003B (zh) * 2017-03-15 2019-09-24 西北工业大学 一种有单斜板的抗鸟撞飞机尾翼前缘
ES2874336T3 (es) * 2018-04-11 2021-11-04 Airbus Operations Sl Superficie laminar de elevación multilarguero para aeronaves
CN108791814B (zh) * 2018-06-19 2020-02-04 吉林化工学院 一种具有抗冲击性能的飞行器整流罩
CN109625245A (zh) * 2018-11-02 2019-04-16 中国航空工业集团公司西安飞机设计研究所 一种通用飞机复合材料方向舵及制作方法
CN109572996B (zh) * 2018-12-04 2022-04-19 中国航空工业集团公司西安飞机设计研究所 一种考虑温度变化的尾翼抗鸟撞附加蒙皮前缘结构
CN109850123A (zh) * 2019-04-04 2019-06-07 上海助者机电设备有限公司 一种改善飞机操纵品质的主动式飞机侧杆
US11459085B2 (en) * 2019-04-30 2022-10-04 Textron Innovations Inc. Energy attenuation stabilizers and methods
US11518502B2 (en) * 2019-04-30 2022-12-06 Textron Innovations Inc. Energy absorption stabilizers and methods
US11046420B2 (en) * 2019-10-23 2021-06-29 The Boeing Company Trailing edge flap having a waffle grid interior structure
US11453476B2 (en) 2020-05-21 2022-09-27 The Boeing Company Structural composite airfoils with an improved leading edge, and related methods
US11554848B2 (en) 2020-05-21 2023-01-17 The Boeing Company Structural composite airfoils with a single spar, and related methods
US20210362828A1 (en) * 2020-05-21 2021-11-25 The Boeing Company Structural composite airfoils with directly coupled front spars, and related methods
US11401026B2 (en) 2020-05-21 2022-08-02 The Boeing Company Structural composite airfoils with a single spar, and related methods
US11572152B2 (en) 2020-05-21 2023-02-07 The Boeing Company Structural composite airfoils with a single spar, and related methods
CN112407244B (zh) * 2020-11-27 2022-05-24 中国商用飞机有限责任公司 飞机前缘组件
CN114771802A (zh) 2021-01-22 2022-07-22 波音公司 空气动力学结构以及形成空气动力学结构的方法

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US1956823A (en) * 1929-06-13 1934-05-01 Cairns Dev Company Wing structure
DE717431C (de) * 1937-07-22 1942-06-03 Hanns Klemm Dr Ing Verfahren zum Herstellen holmartiger Koerper
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EP0361286A2 (de) * 1988-09-28 1990-04-04 Dornier, Conrado Angeströmtes Bauteil von Flugkörpern

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FR646469A (fr) * 1927-05-18 1928-11-12 Nieuport Astra Procédé d'assemblage des tôles utilisées dans la construction métallique
US1956823A (en) * 1929-06-13 1934-05-01 Cairns Dev Company Wing structure
DE717431C (de) * 1937-07-22 1942-06-03 Hanns Klemm Dr Ing Verfahren zum Herstellen holmartiger Koerper
US4667905A (en) * 1983-09-29 1987-05-26 The Boeing Company High strength to weight horizontal and vertical aircraft stabilizer
GB2189204A (en) * 1986-04-17 1987-10-21 Westland Group Plc Titanium alloy erosion shield for aerofoil
EP0361286A2 (de) * 1988-09-28 1990-04-04 Dornier, Conrado Angeströmtes Bauteil von Flugkörpern

Also Published As

Publication number Publication date
ATE434559T1 (de) 2009-07-15
DE60139052D1 (de) 2009-08-06
ES2197727B1 (es) 2005-04-01
EP1176089A3 (en) 2003-12-03
CA2343590C (en) 2009-10-06
EP1176089B1 (en) 2009-06-24
US20020011540A1 (en) 2002-01-31
EP1176089A2 (en) 2002-01-30
CA2343590A1 (en) 2002-01-27
US6616101B2 (en) 2003-09-09

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