WO2019224411A3 - Cono de cola y método de fabricación de un cono de cola - Google Patents

Cono de cola y método de fabricación de un cono de cola Download PDF

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Publication number
WO2019224411A3
WO2019224411A3 PCT/ES2019/070334 ES2019070334W WO2019224411A3 WO 2019224411 A3 WO2019224411 A3 WO 2019224411A3 ES 2019070334 W ES2019070334 W ES 2019070334W WO 2019224411 A3 WO2019224411 A3 WO 2019224411A3
Authority
WO
WIPO (PCT)
Prior art keywords
tail cone
interface
manufacturing
bearing structure
methof
Prior art date
Application number
PCT/ES2019/070334
Other languages
English (en)
French (fr)
Other versions
WO2019224411A2 (es
Inventor
Roberto GARCÍA PUENTE
Sergio GIL GONZÁLEZ
Rubén ESCALONA PEREIRO
José MARTÍN BRAVO
Roberto Jesús CERRATO MEDINA
Miguel ROUCO ZUFIAURRE
Original Assignee
Alestis Aerospace 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 Alestis Aerospace S.L. filed Critical Alestis Aerospace S.L.
Publication of WO2019224411A2 publication Critical patent/WO2019224411A2/es
Publication of WO2019224411A3 publication Critical patent/WO2019224411A3/es

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • 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
    • B64C1/069—Joining arrangements therefor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B64D29/04—Power-plant nacelles, fairings, or cowlings associated with fuselages
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D41/00—Power installations for auxiliary purposes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D41/00—Power installations for auxiliary purposes
    • B64D2041/002—Mounting arrangements for auxiliary power units (APU's)
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/50—Application for auxiliary power units (APU's)

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
  • Processing Of Terminals (AREA)

Abstract

La presente invención da a conocer un cono de cola del tipo que comprende:una interfaz a un cuerpo de una aeronave;una interfaz a una carena; yun revestimiento con forma tronco-conoidal entre dicha interfaz al cuerpo de la aeronave y la interfaz a la carena que define un alojamiento;en el que el alojamiento está destinado a recibir una unidad auxiliar de potencia y una estructura portante acoplada a la unidad auxiliar de potencia y porque la interfaz al cuerpo de la aeronave dispone de medios de conexión a la estructura portante estando la estructura portante conectada al cono de cola únicamente a través de los medios de conexión. Además, se da a conocer el método de fabricación de dicho cono de cola.
PCT/ES2019/070334 2018-05-21 2019-05-21 Cono de cola y método de fabricación de un cono de cola WO2019224411A2 (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ESP201830484 2018-05-21
ES201830484A ES2732306B2 (es) 2018-05-21 2018-05-21 Metodo de fabricacion de un cono de cola

Publications (2)

Publication Number Publication Date
WO2019224411A2 WO2019224411A2 (es) 2019-11-28
WO2019224411A3 true WO2019224411A3 (es) 2020-08-06

Family

ID=68580397

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/ES2019/070334 WO2019224411A2 (es) 2018-05-21 2019-05-21 Cono de cola y método de fabricación de un cono de cola

Country Status (2)

Country Link
ES (1) ES2732306B2 (es)
WO (1) WO2019224411A2 (es)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111746773B (zh) * 2020-07-10 2022-07-01 上海交通大学 一种刚柔一体结构飞艇尾锥

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005016748A2 (en) * 2003-07-22 2005-02-24 Honeywell International, Inc. Dual action inlet door and method for use thereof
US20080099611A1 (en) * 2006-10-31 2008-05-01 Esteban Martino Gonzalez Tail cone for aircraft with movable fairing and support structure for auxiliary power unit and the ancillary elements thereof
FR3014996A1 (fr) * 2013-12-16 2015-06-19 Microturbo Suspension d'un element tubulaire dans un compartiment d'aeronef
EP3103725A1 (en) * 2015-06-12 2016-12-14 Airbus Operations, S.L. Aircraft with an auxiliary power unit attached to the aircraft fuselage by means of an attachment system

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB724052A (en) * 1951-11-17 1955-02-16 Sncase Improvements in aeroplanes propelled by several jet engines
FR2928137B1 (fr) * 2008-02-29 2010-08-20 Airbus France Systeme de propulsion arriere d'avion fixe par poutres et avion comportant un tel systeme.
ES2350429B1 (es) * 2009-05-28 2011-11-18 Airbus Operations, S.L. Cono de cola de una aeronave con carena movil abatible
EP3040263B1 (en) * 2014-12-29 2017-12-20 Airbus Operations S.L. Tail cone of an aircraft
EP3040264B1 (en) * 2014-12-30 2018-07-11 Airbus Operations S.L. Fuselage rear end of an aircraft
ES2763875T3 (es) * 2015-12-15 2020-06-01 Airbus Operations Sl Sistema de suspensión para una unidad de potencia auxiliar

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005016748A2 (en) * 2003-07-22 2005-02-24 Honeywell International, Inc. Dual action inlet door and method for use thereof
US20080099611A1 (en) * 2006-10-31 2008-05-01 Esteban Martino Gonzalez Tail cone for aircraft with movable fairing and support structure for auxiliary power unit and the ancillary elements thereof
FR3014996A1 (fr) * 2013-12-16 2015-06-19 Microturbo Suspension d'un element tubulaire dans un compartiment d'aeronef
EP3103725A1 (en) * 2015-06-12 2016-12-14 Airbus Operations, S.L. Aircraft with an auxiliary power unit attached to the aircraft fuselage by means of an attachment system

Also Published As

Publication number Publication date
WO2019224411A2 (es) 2019-11-28
ES2732306A1 (es) 2019-11-21
ES2732306B2 (es) 2021-06-18

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