WO2010070182A3 - Superficie estabilizadora horizontal de aeronave - Google Patents

Superficie estabilizadora horizontal de aeronave Download PDF

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Publication number
WO2010070182A3
WO2010070182A3 PCT/ES2009/070596 ES2009070596W WO2010070182A3 WO 2010070182 A3 WO2010070182 A3 WO 2010070182A3 ES 2009070596 W ES2009070596 W ES 2009070596W WO 2010070182 A3 WO2010070182 A3 WO 2010070182A3
Authority
WO
WIPO (PCT)
Prior art keywords
aircraft
stabilising surface
horizontal stabilising
horizontal
angle
Prior art date
Application number
PCT/ES2009/070596
Other languages
English (en)
French (fr)
Other versions
WO2010070182A2 (es
Inventor
Raúl Carlos LLAMAS SANDÍN
Miguel Luque Buzo
Original Assignee
Airbus Operations, S.L.
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, S.L. filed Critical Airbus Operations, S.L.
Priority to EP09812436.5A priority Critical patent/EP2371705B1/en
Priority to CA2747689A priority patent/CA2747689C/en
Priority to BRPI0922461A priority patent/BRPI0922461A2/pt
Priority to CN200980154773.2A priority patent/CN102282070B/zh
Priority to RU2011129625/11A priority patent/RU2539308C2/ru
Publication of WO2010070182A2 publication Critical patent/WO2010070182A2/es
Publication of WO2010070182A3 publication Critical patent/WO2010070182A3/es

Links

Classifications

    • 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
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/26—Attaching the wing or tail units or stabilising surfaces

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Tires In General (AREA)
  • Toys (AREA)
  • Mobile Radio Communication Systems (AREA)
  • Paper (AREA)
  • Vehicle Body Suspensions (AREA)

Abstract

Superficie estabilizadora horizontal (8) de una aeronave en la que el ángulo de flecha (40) de dicha superficie (8), siendo este ángulo (40) el que forma la proyección de la línea de referencia de puntos al 25% de la cuerda local (19) de la superficie estabilizadora horizontal (8) sobre un plano perpendicular al plano de simetría (21) de la aeronave, conteniendo además este plano a la dirección de vuelo de la citada aeronave, con respecto al plano de simetría (21) de la aeronave, es menor de 90 grados, estando medido dicho ángulo (40) en la dirección de vuelo de la aeronave. Además, la conexión estructural de la citada superficie estabilizadora horizontal (8) al fuselaje (1 ) de la aeronave se realiza a través de una cuaderna (13) de dicho fuselaje (1).
PCT/ES2009/070596 2008-12-17 2009-12-17 Superficie estabilizadora horizontal de aeronave WO2010070182A2 (es)

Priority Applications (5)

Application Number Priority Date Filing Date Title
EP09812436.5A EP2371705B1 (en) 2008-12-17 2009-12-17 Horizontal stabilising surface of an aircraft
CA2747689A CA2747689C (en) 2008-12-17 2009-12-17 Aircraft horizontal stabilizer surface
BRPI0922461A BRPI0922461A2 (pt) 2008-12-17 2009-12-17 superfície do estabilizador horizontal de aeronave.
CN200980154773.2A CN102282070B (zh) 2008-12-17 2009-12-17 飞机水平稳定器
RU2011129625/11A RU2539308C2 (ru) 2008-12-17 2009-12-17 Поверхность горизонтального стабилизатора летательного аппарата

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ESP200803581 2008-12-17
ES200803581A ES2373812B1 (es) 2008-12-17 2008-12-17 Superficie estabilizadora horizontal de aeronave.

Publications (2)

Publication Number Publication Date
WO2010070182A2 WO2010070182A2 (es) 2010-06-24
WO2010070182A3 true WO2010070182A3 (es) 2010-09-23

Family

ID=42239356

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/ES2009/070596 WO2010070182A2 (es) 2008-12-17 2009-12-17 Superficie estabilizadora horizontal de aeronave

Country Status (8)

Country Link
US (1) US8360359B2 (es)
EP (1) EP2371705B1 (es)
CN (1) CN102282070B (es)
BR (1) BRPI0922461A2 (es)
CA (1) CA2747689C (es)
ES (1) ES2373812B1 (es)
RU (1) RU2539308C2 (es)
WO (1) WO2010070182A2 (es)

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FR2975666B1 (fr) * 2011-05-23 2014-01-17 Airbus Operations Sas Aeronef a partie arriere orientable
WO2013015765A1 (en) * 2011-07-22 2013-01-31 Bell Helicopter Textron Inc. Aft-loading aircraft with-twin t-tail assembly
ES2386217B1 (es) * 2012-03-21 2013-06-24 Ideas Proyectos E Innovaciones S.L. Sistema para despegue y aterrizaje de los aviones de forma rápida y con muy poco recorrido
ES2623000T3 (es) * 2012-07-16 2017-07-10 Airbus Operations, S.L. Superficie sustentadora de aeronave con una distribución de flecha variable a lo largo de la envergadura
WO2014074149A1 (en) * 2012-11-12 2014-05-15 United Technologies Corporation Stabilizer sacrificial surfaces
US9884674B2 (en) * 2012-11-15 2018-02-06 United Technologies Corporation Stabilizer with structural box and sacrificial surfaces
EP2832636A1 (en) 2013-07-30 2015-02-04 Airbus Operations S.L. Rear fuselage section of an aircraft
ES2702873T3 (es) 2013-12-31 2019-03-06 Airbus Operations Sl Aeronave con un estabilizador horizontal trimable que tiene los elementos pivotantes en su lado delantero
US10023294B2 (en) 2014-08-07 2018-07-17 Bell Helicopter Textron Inc. Tail spar spring
CN104443355B (zh) * 2014-11-13 2016-08-24 中航沈飞民用飞机有限责任公司 一种轻型飞机仿生v型尾翼
EP3078586B1 (en) 2015-04-08 2018-02-21 Airbus Operations S.L. Aircraft rear structure
FR3040686B1 (fr) * 2015-09-08 2018-09-07 Airbus Operations Sas Partie arriere d'aeronef comprenant un stabilisateur vertical dont la structure formant caisson comporte une partie inferieure logee dans le fuselage
US10106265B2 (en) 2016-06-24 2018-10-23 General Electric Company Stabilizer assembly for an aircraft AFT engine
ES2841399T3 (es) * 2016-12-16 2021-07-08 Airbus Operations Sl Aeronave con una sección trasera con un revestimiento continuo para el fuselaje y el estabilizador vertical de cola
TWI634457B (zh) * 2017-04-27 2018-09-01 高璁錦 Keyboard with button switch trigger height adjustment function
FR3079207B1 (fr) 2018-03-21 2020-02-28 Airbus Aeronef presentant des empennages horizontaux articules
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
EP3584152B1 (en) * 2018-06-19 2023-06-07 Airbus Operations, S.L.U. Method for manufacturing a multi-spar box with a continuous skin upper shell of a tail cone section for a rear end of an aircraft and a composite assembly
ES2781400A1 (es) * 2019-03-01 2020-09-01 Airbus Operations Slu Aeronave con estabilizador horizontal movil
US11319055B2 (en) 2019-08-31 2022-05-03 Textron Innovations Inc. Compliant tail structure for rotorcraft
US11498674B2 (en) * 2019-12-04 2022-11-15 Textron Aviation Inc. Aircraft floats
CN112699455B (zh) * 2020-10-10 2021-11-16 北京航空航天大学 一种基于t样条的飞机蒙皮无缝成型方法及装置
BR102021017320A2 (pt) * 2020-11-03 2022-07-26 The Boeing Company Sistema e método para prender uma porção de uma fuselagem de uma aeronave a uma porção de uma asa da aeronave
EP4063259A1 (en) * 2021-03-26 2022-09-28 Airbus Operations, S.L.U. Aircraft empennage

Citations (5)

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Publication number Priority date Publication date Assignee Title
FR2519934A1 (fr) * 1982-01-21 1983-07-22 Nguyen Manh Khanh Avion multiplan indeformable
GB2243126A (en) * 1990-04-02 1991-10-23 Jordan Valchev Georgiev Directional stabilisation of aircraft with forward swept wings
WO2003080436A1 (fr) * 2002-03-22 2003-10-02 Sopravia Inc. Avion a trois fuselages et familles d'avions de ce type
EP1550606A2 (de) * 2003-12-29 2005-07-06 Airbus Deutschland GmbH Seitenleitwerksanschluss
WO2007144377A1 (en) * 2006-06-14 2007-12-21 Airbus Deutschland Gmbh Tail structure for an aircraft or spacecraft

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Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2519934A1 (fr) * 1982-01-21 1983-07-22 Nguyen Manh Khanh Avion multiplan indeformable
GB2243126A (en) * 1990-04-02 1991-10-23 Jordan Valchev Georgiev Directional stabilisation of aircraft with forward swept wings
WO2003080436A1 (fr) * 2002-03-22 2003-10-02 Sopravia Inc. Avion a trois fuselages et familles d'avions de ce type
EP1550606A2 (de) * 2003-12-29 2005-07-06 Airbus Deutschland GmbH Seitenleitwerksanschluss
WO2007144377A1 (en) * 2006-06-14 2007-12-21 Airbus Deutschland Gmbh Tail structure for an aircraft or spacecraft

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
JANSSON, FRIDE: "Picture of the Mooney M-20J 201MSE aircraft", 9 September 2006 (2006-09-09), XP002593455, Retrieved from the Internet <URL:http://www.airliners.net/photo/Mooney-M-20J-201MSE/1106706/L/> [retrieved on 20100723] *

Also Published As

Publication number Publication date
CN102282070A (zh) 2011-12-14
ES2373812A1 (es) 2012-02-09
ES2373812B1 (es) 2012-12-18
BRPI0922461A2 (pt) 2015-12-15
RU2539308C2 (ru) 2015-01-20
CA2747689C (en) 2018-01-09
EP2371705B1 (en) 2018-03-07
CA2747689A1 (en) 2010-06-24
RU2011129625A (ru) 2013-01-27
US8360359B2 (en) 2013-01-29
WO2010070182A2 (es) 2010-06-24
CN102282070B (zh) 2014-11-26
US20100148000A1 (en) 2010-06-17
EP2371705A2 (en) 2011-10-05

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