BRPI0922461A2 - superfície do estabilizador horizontal de aeronave. - Google Patents

superfície do estabilizador horizontal de aeronave.

Info

Publication number
BRPI0922461A2
BRPI0922461A2 BRPI0922461A BRPI0922461A BRPI0922461A2 BR PI0922461 A2 BRPI0922461 A2 BR PI0922461A2 BR PI0922461 A BRPI0922461 A BR PI0922461A BR PI0922461 A BRPI0922461 A BR PI0922461A BR PI0922461 A2 BRPI0922461 A2 BR PI0922461A2
Authority
BR
Brazil
Prior art keywords
horizontal stabilizer
aircraft horizontal
aircraft
stabilizer
horizontal
Prior art date
Application number
BRPI0922461A
Other languages
English (en)
Inventor
Miguel Luque Buzo
Raúl Carlos Llamas Sandin
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
Publication of BRPI0922461A2 publication Critical patent/BRPI0922461A2/pt

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)
  • Paper (AREA)
  • Vehicle Body Suspensions (AREA)
  • Mobile Radio Communication Systems (AREA)
BRPI0922461A 2008-12-17 2009-12-17 superfície do estabilizador horizontal de aeronave. BRPI0922461A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ES200803581A ES2373812B1 (es) 2008-12-17 2008-12-17 Superficie estabilizadora horizontal de aeronave.
PCT/ES2009/070596 WO2010070182A2 (es) 2008-12-17 2009-12-17 Superficie estabilizadora horizontal de aeronave

Publications (1)

Publication Number Publication Date
BRPI0922461A2 true BRPI0922461A2 (pt) 2015-12-15

Family

ID=42239356

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0922461A BRPI0922461A2 (pt) 2008-12-17 2009-12-17 superfície do estabilizador horizontal de aeronave.

Country Status (8)

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

Families Citing this family (28)

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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
US10112696B2 (en) * 2012-11-12 2018-10-30 United Technologies Corporation Stabilizer sacrificial surfaces
EP2920068B1 (en) * 2012-11-15 2017-11-29 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
EP2889216B1 (en) * 2013-12-31 2018-09-19 Airbus Operations S.L. Aircraft with a trimmable horizontal stabilizer having the pivot elements in its forward side
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
ES2669493T3 (es) * 2015-04-08 2018-05-28 Airbus Operations S.L. Estructura trasera de aeronave
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
US10647407B2 (en) * 2018-03-30 2020-05-12 The Boeing Company Wing flap with torque member and method for forming thereof
US10597141B2 (en) * 2018-03-30 2020-03-24 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
ES3034191T3 (en) * 2021-03-26 2025-08-13 Airbus Operations Slu Aircraft empennage
CN115795690B (zh) * 2022-12-20 2025-07-25 中国航空工业集团公司西安飞机设计研究所 爆炸冲击波阵风载荷作用下飞机机体载荷及响应计算方法
US12459631B2 (en) * 2024-02-09 2025-11-04 Rtx Corporation Aircraft vertical stabilizer with moveable propulsion system(s)
US12434809B2 (en) 2024-02-29 2025-10-07 Textron Innovations Inc. Dynamically tuned tail assemblies for rotorcraft

Family Cites Families (17)

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Publication number Priority date Publication date Assignee Title
GB1018077A (en) * 1962-07-13 1966-01-26 Messerschmitt Ag Improvements in or relating to aircraft
US3307808A (en) * 1965-12-20 1967-03-07 Helio Aircraft Corp Airplane longitudinal trim control
FR2519934A1 (fr) * 1982-01-21 1983-07-22 Nguyen Manh Khanh Avion multiplan indeformable
GB2243126B (en) * 1990-04-02 1994-12-21 Jordan Valchev Georgiev A method and device for stabilization of a flying apparatus having forward swept wing
RU2055778C1 (ru) * 1994-03-22 1996-03-10 Товарищество с ограниченной ответственностью "Авиатика" Самолет
US6170780B1 (en) * 1997-07-21 2001-01-09 Sam Barlow Williams Twin engine aircraft
FR2837464B1 (fr) * 2002-03-22 2004-12-10 Georges Armand Avion a trois fuselages et familles d'avions de ce type
US7216830B2 (en) * 2003-09-05 2007-05-15 Supersonic Aerospace International, Llc Wing gull integration nacelle clearance, compact landing gear stowage, and sonic boom reduction
US6824092B1 (en) * 2003-10-30 2004-11-30 Supersonic Aerospace International, Llc Aircraft tail configuration for sonic boom reduction
ATE416969T1 (de) * 2003-12-29 2008-12-15 Airbus Gmbh Seitenleitwerksanschluss
US7735744B2 (en) * 2004-03-11 2010-06-15 Nissan Technical Center North America, Inc. Control of coolant flow rate for vehicle heating
WO2006073634A2 (en) * 2004-12-02 2006-07-13 Richard H Lugg Vtol aircraft with forward-swept fixed wing
DE102005038856A1 (de) * 2005-08-17 2007-02-22 Airbus Deutschland Gmbh Kontinuierlicher Rumpfanschluss
ES2291113B1 (es) * 2006-02-28 2008-12-16 Airbus España S.L. Sistema de acoplamiento pivotante de un empenaje con gran diedro al fuselaje de cola de un avion.
DE602006005221D1 (de) * 2006-03-16 2009-04-02 Eads Constr Aeronauticas Sa Elastisch vorgeformte Verkleidung für Flugzeuge und Verfahren zur ihrer Herstellung
FR2898583B1 (fr) * 2006-03-20 2008-04-18 Airbus France Sas Aeronef a impact environnemental reduit
DE102006027707A1 (de) * 2006-06-14 2007-12-20 Airbus Deutschland Gmbh Heckstruktur für ein Luft- oder Raumfahrzeug

Also Published As

Publication number Publication date
WO2010070182A2 (es) 2010-06-24
EP2371705B1 (en) 2018-03-07
US8360359B2 (en) 2013-01-29
ES2373812B1 (es) 2012-12-18
RU2539308C2 (ru) 2015-01-20
CA2747689C (en) 2018-01-09
CA2747689A1 (en) 2010-06-24
EP2371705A2 (en) 2011-10-05
CN102282070A (zh) 2011-12-14
WO2010070182A3 (es) 2010-09-23
CN102282070B (zh) 2014-11-26
ES2373812A1 (es) 2012-02-09
RU2011129625A (ru) 2013-01-27
US20100148000A1 (en) 2010-06-17

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B11D Dismissal acc. art. 38, par 2 of ipl - failure to pay fee after grant in time