WO2012052589A3 - Herraje estanco para la cogida del estabilizador vertical de cola de una aeronave - Google Patents

Herraje estanco para la cogida del estabilizador vertical de cola de una aeronave Download PDF

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Publication number
WO2012052589A3
WO2012052589A3 PCT/ES2011/070719 ES2011070719W WO2012052589A3 WO 2012052589 A3 WO2012052589 A3 WO 2012052589A3 ES 2011070719 W ES2011070719 W ES 2011070719W WO 2012052589 A3 WO2012052589 A3 WO 2012052589A3
Authority
WO
WIPO (PCT)
Prior art keywords
fitting
aircraft
stabiliser
holding
vertical
Prior art date
Application number
PCT/ES2011/070719
Other languages
English (en)
French (fr)
Other versions
WO2012052589A2 (es
Inventor
Diego FOLCH CORTÉS
Elena ARÉVALO RODRÍGUEZ
Enrique Vera Villares
Javier Cabeza Huertas
José María PINA LÓPEZ
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.
Publication of WO2012052589A2 publication Critical patent/WO2012052589A2/es
Publication of WO2012052589A3 publication Critical patent/WO2012052589A3/es

Links

Classifications

    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)

Abstract

Herraje estanco (41) para la cogida del estabilizador vertical de cola de una aeronave en una zona de su fuselaje trasero estructurada en base a un revestimiento (5) fabricado con un material compuesto como una pieza unitaria y unas cuadernas (7) que comprende: una primera pieza (43) que comprende dos cuerpos (45, 45'), que incluyen las orejetas (47, 47') de cogida del estabilizador vertical de cola y unas paredes verticales (49, 49') de unión del herraje (43) a las cuadernas (7) del fuselaje, y un perfil central (51) de estanqueidad; dos parejas de piezas adicionales (55, 55'; 65, 65') con forma de angular, que incluyen unas paredes horizontales (57, 57'; 67, 67') de unión al revestimiento (5) y unas paredes verticales (59, 59'; 69, 69') de unión a dichos cuerpos (45, 45'). Todas las piezas del herraje estanco (41) están fabricadas con un material compuesto.
PCT/ES2011/070719 2010-10-19 2011-10-19 Herraje estanco para la cogida del estabilizador vertical de cola de una aeronave WO2012052589A2 (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ES201031538A ES2400769B1 (es) 2010-10-19 2010-10-19 Herraje estanco para la cogida del estabilizador vertical de cola de una aeronave.
ESP201031538 2010-10-19

Publications (2)

Publication Number Publication Date
WO2012052589A2 WO2012052589A2 (es) 2012-04-26
WO2012052589A3 true WO2012052589A3 (es) 2012-08-09

Family

ID=45463629

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/ES2011/070719 WO2012052589A2 (es) 2010-10-19 2011-10-19 Herraje estanco para la cogida del estabilizador vertical de cola de una aeronave

Country Status (3)

Country Link
US (1) US8783618B2 (es)
ES (1) ES2400769B1 (es)
WO (1) WO2012052589A2 (es)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2990410B1 (fr) * 2012-05-09 2014-06-13 Airbus Operations Sas Poutre en materiau composite integrant une liaison renforcee avec un autre element
IL223443A (en) 2012-12-04 2014-06-30 Elbit Systems Cyclone Ltd Buildings from composite materials with integral composite connectors and manufacturing methods
DE102014106743B4 (de) * 2014-05-13 2023-12-21 Airbus Operations Gmbh Strömungskörper mit einem darin integrierten Lasteinleitungselement, Verfahren zum Herstellen eines Strömungskörpers und Flugzeug mit einem solchen Strömungskörper
DE102017117314A1 (de) 2017-07-31 2019-01-31 Airbus Operations Gmbh Befestigungseinheit zum beweglichen Befestigen einer Luftfahrzeugkomponente an einer Tragstruktur eines Luftfahrzeugs
US20220048610A1 (en) * 2020-08-12 2022-02-17 The Boeing Company Cfrp fuselage frame with securement to vertical tail fin

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102005003296A1 (de) * 2005-01-24 2006-07-27 Eads Deutschland Gmbh Rumpfhecksektion eines Flugzeugs
US20100127127A1 (en) * 2008-11-27 2010-05-27 Manzano Carlos Garcia Assembly between a front fitting and the traction coupling of the two lateral boxes of the horizontal stabilizer of an aircraft
US20100155532A1 (en) * 2008-12-18 2010-06-24 Airbus Espana S.L. Structure of the load introduction zone in the rear end of an aircraft
WO2010122200A2 (es) * 2009-04-21 2010-10-28 Airbus Operations, S.L. Herrajes para la cogida del estabilizador vertical de cola de una aeronave.

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1683269A1 (ru) * 1988-10-30 1995-02-27 Б.А. Волков Устройство для соединения киля с фюзеляжем летательного аппарата

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102005003296A1 (de) * 2005-01-24 2006-07-27 Eads Deutschland Gmbh Rumpfhecksektion eines Flugzeugs
US20100127127A1 (en) * 2008-11-27 2010-05-27 Manzano Carlos Garcia Assembly between a front fitting and the traction coupling of the two lateral boxes of the horizontal stabilizer of an aircraft
US20100155532A1 (en) * 2008-12-18 2010-06-24 Airbus Espana S.L. Structure of the load introduction zone in the rear end of an aircraft
WO2010122200A2 (es) * 2009-04-21 2010-10-28 Airbus Operations, S.L. Herrajes para la cogida del estabilizador vertical de cola de una aeronave.

Also Published As

Publication number Publication date
ES2400769A1 (es) 2013-04-12
US20120091275A1 (en) 2012-04-19
US8783618B2 (en) 2014-07-22
WO2012052589A2 (es) 2012-04-26
ES2400769B1 (es) 2014-02-12

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