ES2421410A2 - Borde de salida de una superficie aerodinamica de una aeronave - Google Patents

Borde de salida de una superficie aerodinamica de una aeronave

Info

Publication number
ES2421410A2
ES2421410A2 ES201230300A ES201230300A ES2421410A2 ES 2421410 A2 ES2421410 A2 ES 2421410A2 ES 201230300 A ES201230300 A ES 201230300A ES 201230300 A ES201230300 A ES 201230300A ES 2421410 A2 ES2421410 A2 ES 2421410A2
Authority
ES
Spain
Prior art keywords
trailing edge
aerodynamic surface
aircraft aerodynamic
section
peak
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
ES201230300A
Other languages
English (en)
Other versions
ES2421410R1 (es
ES2421410B1 (es
Inventor
Gregorio Hurtado Yolanda De
Gonzalez Alberto Balsa
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 SL
Original Assignee
Airbus Operations SL
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 SL filed Critical Airbus Operations SL
Priority to ES201230300A priority Critical patent/ES2421410B1/es
Priority to US13/775,471 priority patent/US9108721B2/en
Publication of ES2421410A2 publication Critical patent/ES2421410A2/es
Publication of ES2421410R1 publication Critical patent/ES2421410R1/es
Application granted granted Critical
Publication of ES2421410B1 publication Critical patent/ES2421410B1/es
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/02—Tailplanes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/10—Shape of wings
    • B64C3/14—Aerofoil profile
    • B64C2003/147—Aerofoil profile comprising trailing edges of particular shape

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Laminated Bodies (AREA)
  • User Interface Of Digital Computer (AREA)

Abstract

La invención divulga un borde de salida (2) de una superficie aerodinámica de una aeronave, el cual comprende un revestimiento superior (6) y un revestimiento inferior (7), estando los revestimientos superior e inferior (6, 7) realizados en material compuesto. En una parte final (13) de los revestimientos superior e inferior (6, 7) del borde de salida (2), se monta una pieza ligera (1). La pieza ligera (1) está cubierta por una lámina metálica (8), y tiene una sección con forma de "V" con brazos y pico, en la pieza ligera (1) el pico de la sección con forma de "V" es redondeado y está situado opuesto a la parte final (13) de los revestimientos superior e inferior (6, 7).
ES201230300A 2012-02-29 2012-02-29 Borde de salida de una superficie aerodinamica de una aeronave Active ES2421410B1 (es)

Priority Applications (2)

Application Number Priority Date Filing Date Title
ES201230300A ES2421410B1 (es) 2012-02-29 2012-02-29 Borde de salida de una superficie aerodinamica de una aeronave
US13/775,471 US9108721B2 (en) 2012-02-29 2013-02-25 Trailing edge of an aircraft aerodynamic surface

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES201230300A ES2421410B1 (es) 2012-02-29 2012-02-29 Borde de salida de una superficie aerodinamica de una aeronave

Publications (3)

Publication Number Publication Date
ES2421410A2 true ES2421410A2 (es) 2013-09-02
ES2421410R1 ES2421410R1 (es) 2014-02-13
ES2421410B1 ES2421410B1 (es) 2014-10-28

Family

ID=48980557

Family Applications (1)

Application Number Title Priority Date Filing Date
ES201230300A Active ES2421410B1 (es) 2012-02-29 2012-02-29 Borde de salida de una superficie aerodinamica de una aeronave

Country Status (2)

Country Link
US (1) US9108721B2 (es)
ES (1) ES2421410B1 (es)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9452819B2 (en) * 2014-03-24 2016-09-27 The Boeing Company Flight control surface seal
EP3210883B1 (en) 2016-02-29 2020-01-29 Airbus Operations, S.L. Aircraft airfoil having a stitched trailing edge and manufacturing method thereof
CN107434031A (zh) 2016-05-25 2017-12-05 空中客车简化股份公司 飞行器翼体的结构部件和包括该结构部件的飞行器
US10532804B2 (en) * 2017-02-08 2020-01-14 The Boeing Company Aerodynamic control surface and associated trailing edge close-out method
ES2896930T3 (es) * 2019-01-18 2022-02-28 Airbus Operations Slu Superficie de control de vuelo para una aeronave y método para fabricar dicha superficie de control de vuelo
CN112093029A (zh) * 2019-06-18 2020-12-18 成都飞机工业（集团）有限责任公司 一种飞机翼面后缘
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
EP4155192A1 (en) * 2021-09-28 2023-03-29 Airbus Operations, S.L.U. Profile for a trailing edge of an airfoil and method to repair thereof
EP4180323B1 (en) * 2021-11-11 2024-09-11 Aciturri Engineering, S.L. Joining element for trailing edge

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3779487A (en) * 1971-04-19 1973-12-18 L Ashton Light weight contoured load carrying structure
US4667906A (en) * 1985-04-02 1987-05-26 Grumman Aerospace Corporation Replaceable tip for aircraft leading edge
FR2741590B1 (fr) * 1995-11-29 1998-01-30 Eurocopter France Pale a blindage de protection renforcee contre la foudre, pour rotor de giravion
US6779757B2 (en) * 2002-06-28 2004-08-24 Lockheed Martin Corporation Preforms for acute structural edges
DK1603798T3 (da) * 2003-03-03 2011-02-14 Flexsys Inc Tilpasningsdygtigt og fleksibelt vinge- og rotorsystem
US7871041B2 (en) * 2007-10-17 2011-01-18 Lockheed Martin Corporation System, method, and apparatus for leading edge structures and direct manufacturing thereof
JP2009107515A (ja) * 2007-10-31 2009-05-21 Shin Meiwa Ind Co Ltd 航空機の複合材製構造体の製造方法及びその構造体
US8123167B2 (en) * 2008-12-15 2012-02-28 Embraer S.A. Impact resistant aircraft leading edge structures and aircraft including the same
ES2367935B1 (es) * 2008-12-18 2012-09-18 Airbus Operations, S.L. Borde de salida de superficie estabilizadora de aeronave.

Also Published As

Publication number Publication date
ES2421410R1 (es) 2014-02-13
ES2421410B1 (es) 2014-10-28
US20140339370A1 (en) 2014-11-20
US9108721B2 (en) 2015-08-18

Similar Documents

Publication Publication Date Title
ES2421410A2 (es) Borde de salida de una superficie aerodinamica de una aeronave
USD824535S1 (en) Pipette tip sheet
USD743321S1 (en) Aircraft cabin
MX2016009964A (es) Aspa del rotor con repisa interior para una tapa del larguero de placa plana.
MY173550A (en) Curved secondary battery
MX341802B (es) Estructura de asiento con un respaldo flexible contorneado.
MX2014004037A (es) Cuchilla para rasurar, cabeza para rasurar y metodos de manufactura.
EP2679487A3 (en) Propeller blade with carbon foam spar core
EP2592002A3 (en) Nacelle
USD731396S1 (en) Aircraft galley
USD745619S1 (en) Expandable broadhead having a body with an integral cutting tip
WO2010070185A3 (es) Borde de salida de superficie estabilizadora de aeronave
GB2490425B (en) Interlocking blade sheath
GB201313165D0 (en) Composite Turbine Engine Blade with Structural Reinforcement
DK201370046A (en) Wind turbine rotor blade assembly with root extension panel and method of assembly
WO2013130181A3 (en) Low loss airfoil platform trailing edge
EP2612991A3 (en) Gas turbine nozzle with a flow groove
EP3106291A3 (en) Enhancing z-conductivity in carbon fiber reinforced plastic composite layups
WO2015099861A3 (en) Fan blade composite segments
EP2617944A3 (en) Turbomachine blade tip shroud
EP2746152A3 (en) Variable-width aerodynamic device
EP2735503A3 (en) Modular structural assembly
WO2015102715A3 (en) Fan blade composite ribs
EP3034785A3 (en) A gas turbine fan blade with varying fracture resistance
WO2011048064A3 (en) Aircraft horizontal stabiliser fitted with leading-edge strake

Legal Events

Date Code Title Description
FG2A Definitive protection

Ref document number: 2421410

Country of ref document: ES

Kind code of ref document: B1

Effective date: 20141028