ES2585283R1 - Morro de aeronave provisto de una cuaderna de conexión entre el alojamiento del tren de aterrizaje y el revestimiento exterior del fuselaje - Google Patents

Morro de aeronave provisto de una cuaderna de conexión entre el alojamiento del tren de aterrizaje y el revestimiento exterior del fuselaje Download PDF

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Publication number
ES2585283R1
ES2585283R1 ES201531847A ES201531847A ES2585283R1 ES 2585283 R1 ES2585283 R1 ES 2585283R1 ES 201531847 A ES201531847 A ES 201531847A ES 201531847 A ES201531847 A ES 201531847A ES 2585283 R1 ES2585283 R1 ES 2585283R1
Authority
ES
Spain
Prior art keywords
fuselage
landing gear
connection frame
aircraft nose
gear housing
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
ES201531847A
Other languages
English (en)
Other versions
ES2585283B2 (es
ES2585283A2 (es
Inventor
Guillaume Gallant
Hervé BIENNES
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 SAS
Original Assignee
Airbus Operations SAS
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 SAS filed Critical Airbus Operations SAS
Publication of ES2585283A2 publication Critical patent/ES2585283A2/es
Publication of ES2585283R1 publication Critical patent/ES2585283R1/es
Application granted granted Critical
Publication of ES2585283B2 publication Critical patent/ES2585283B2/es
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/061—Frames
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/02—Undercarriages
    • B64C25/08—Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/16—Fairings movable in conjunction with undercarriage elements
    • 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
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/068—Fuselage sections
    • B64C1/0683—Nose cones
    • 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
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/10—Bulkheads
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/02—Undercarriages
    • B64C25/08—Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/02—Undercarriages
    • B64C25/08—Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/14—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like fore-and-aft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • 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
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/068—Fuselage sections

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Superstructure Of Vehicle (AREA)
  • Body Structure For Vehicles (AREA)
  • Automatic Assembly (AREA)

Abstract

Con el fin de ayudar a instalar las puertas en el alojamiento de tren de aterrizaje y ajustar su posición, la invención se refiere a un morro (1) de aeronave que comprende una cuaderna de conexión (50) entre el alojamiento (20) de tren de aterrizaje y el revestimiento exterior (16) del fuselaje, la cuaderna de conexión se extiende alrededor de una abertura (40) en el revestimiento exterior (16) y comprende:#- una falda (52) que se apoya contra el revestimiento exterior (16) del fuselaje y se conecta al mismo, la falda define un paso para el tren de aterrizaje (58) que está configurado para ser cerrado por puertas (62) cuando las últimas están en una posición de cierre; y#- medios (64) para soportar las puertas (62).
ES201531847A 2014-12-18 2015-12-18 Morro de aeronave provisto de una cuaderna de conexión entre el alojamiento del tren de aterrizaje y el revestimiento exterior del fuselaje Expired - Fee Related ES2585283B2 (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1462796A FR3030442B1 (fr) 2014-12-18 2014-12-18 Pointe avant d'aeronef equipee d'un cadre de jonction entre la case de train d'atterrissage et la peau exterieure du fuselage
FR1462796 2014-12-18

Publications (3)

Publication Number Publication Date
ES2585283A2 ES2585283A2 (es) 2016-10-04
ES2585283R1 true ES2585283R1 (es) 2017-02-08
ES2585283B2 ES2585283B2 (es) 2018-01-08

Family

ID=52684441

Family Applications (1)

Application Number Title Priority Date Filing Date
ES201531847A Expired - Fee Related ES2585283B2 (es) 2014-12-18 2015-12-18 Morro de aeronave provisto de una cuaderna de conexión entre el alojamiento del tren de aterrizaje y el revestimiento exterior del fuselaje

Country Status (4)

Country Link
US (1) US9840321B2 (es)
CN (1) CN105711803B (es)
ES (1) ES2585283B2 (es)
FR (1) FR3030442B1 (es)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2678729C1 (ru) * 2018-03-13 2019-01-31 Общество с ограниченной ответственностью "Конструкторское бюро "Современные авиационные технологии" Носовая часть фюзеляжа летательного аппарата
FR3086270A1 (fr) * 2018-09-20 2020-03-27 Airbus Operations Module de train d'atterrissage avant pour aeronef
CN112455647B (zh) * 2020-11-13 2023-08-22 中国航空工业集团公司沈阳飞机设计研究所 一种飞机起落架舱门悬挂结构
CN112357049A (zh) * 2020-11-30 2021-02-12 中国特种飞行器研究所 一种碳纤维增强铝合金层合板耐冲击无人机前罩结构
US11919624B2 (en) * 2022-03-15 2024-03-05 Safran Landing Systems Canada Inc. Landing gear door installation

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2459982A (en) * 1944-12-13 1949-01-25 Boeing Co Retractable shock absorbing strut
US20090078823A1 (en) * 2007-09-24 2009-03-26 The Boeing Company Aircraft nose landing gear enclosure
US20090146008A1 (en) * 2007-03-28 2009-06-11 Airbus Deutschland Gmbh Door Frame Compartment of Cast Titanium and Structural Fuselage Part
FR2954934A1 (fr) * 2010-01-07 2011-07-08 Eads Europ Aeronautic Defence Module de train d'atterrissage d'aeronef, aeronef le comportant et procede de fabrication d'un aeronef
US20120153078A1 (en) * 2010-12-17 2012-06-21 Airbus Operations (S.A.S.) Front part of an aircraft fuselage incorporating a bay for stowing landing gear
ES2400768A1 (es) * 2010-06-30 2013-04-12 Airbus Operations, S.L. Estructura interna de aeronave en material compuesto.
US20130134259A1 (en) * 2011-11-30 2013-05-30 Airbus Operations (Sas) Front structure of an aircraft fuselage comprising landing gear

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2661171A (en) * 1951-10-11 1953-12-01 Glenn L Martin Co Up and down lock mechanism for retractable landing gear for aircraft
US3198461A (en) * 1963-06-20 1965-08-03 Lockheed Aircraft Corp Retractable landing gear
JP3147539B2 (ja) * 1992-10-05 2001-03-19 本田技研工業株式会社 航空機の降着装置
US6047925A (en) * 1993-07-01 2000-04-11 The Boeing Company Nose gear door integral composite glide slope antenna
FR2782495B1 (fr) * 1998-08-19 2000-11-10 Aerospatiale Structure avant d'avion
FR2875475B1 (fr) * 2004-09-21 2008-02-08 Airbus France Sas Systeme de manoeuvre d'un train d'atterrissage pour aeronef et aeronef comportant un tel systeme
FR2910875B1 (fr) 2007-01-03 2009-10-09 Airbus France Sas Partie avant d'aeronef comprenant une cloison plane entre une zone pressurisee et une zone de logement de train non pressurisee.
FR2962410B1 (fr) * 2010-07-09 2013-07-12 Airbus Operations Sas Procede de reglage des trappes de case de train d'atterrissage et trappe de mise en oeuvre
FR2983826B1 (fr) * 2011-12-12 2013-12-20 Airbus Operations Sas Structure avant d'avion perfectionnee a compartiment pour train d'atterrissage.
FR2999524B1 (fr) * 2012-12-17 2015-02-20 Airbus Operations Sas Fond etanche avant d'aeronef comprenant des renfoncements pour le logement d'equipements de cockpit
FR3000016B1 (fr) * 2012-12-21 2016-01-15 Airbus Operations Sas Partie avant d'aeronef a case de train amelioree

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2459982A (en) * 1944-12-13 1949-01-25 Boeing Co Retractable shock absorbing strut
US20090146008A1 (en) * 2007-03-28 2009-06-11 Airbus Deutschland Gmbh Door Frame Compartment of Cast Titanium and Structural Fuselage Part
US20090078823A1 (en) * 2007-09-24 2009-03-26 The Boeing Company Aircraft nose landing gear enclosure
FR2954934A1 (fr) * 2010-01-07 2011-07-08 Eads Europ Aeronautic Defence Module de train d'atterrissage d'aeronef, aeronef le comportant et procede de fabrication d'un aeronef
ES2400768A1 (es) * 2010-06-30 2013-04-12 Airbus Operations, S.L. Estructura interna de aeronave en material compuesto.
US20120153078A1 (en) * 2010-12-17 2012-06-21 Airbus Operations (S.A.S.) Front part of an aircraft fuselage incorporating a bay for stowing landing gear
US20130134259A1 (en) * 2011-11-30 2013-05-30 Airbus Operations (Sas) Front structure of an aircraft fuselage comprising landing gear

Also Published As

Publication number Publication date
CN105711803B (zh) 2019-09-20
FR3030442A1 (fr) 2016-06-24
ES2585283B2 (es) 2018-01-08
ES2585283A2 (es) 2016-10-04
CN105711803A (zh) 2016-06-29
US20160176513A1 (en) 2016-06-23
FR3030442B1 (fr) 2017-01-27
US9840321B2 (en) 2017-12-12

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