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ATE535444T1 - Anlage für eine flugzeuggondelführungssystem - Google Patents

Anlage für eine flugzeuggondelführungssystem

Info

Publication number
ATE535444T1
ATE535444T1 AT08864291T AT08864291T ATE535444T1 AT E535444 T1 ATE535444 T1 AT E535444T1 AT 08864291 T AT08864291 T AT 08864291T AT 08864291 T AT08864291 T AT 08864291T AT E535444 T1 ATE535444 T1 AT E535444T1
Authority
AT
Austria
Prior art keywords
nacelle
air intake
outer panel
attached
central structure
Prior art date
Application number
AT08864291T
Other languages
English (en)
Inventor
Guy Vauchel
Jean-Philippe Dauguet
Stephane Beilliard
Original Assignee
Aircelle Sa
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 Aircelle Sa filed Critical Aircelle Sa
Application granted granted Critical
Publication of ATE535444T1 publication Critical patent/ATE535444T1/de

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
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • 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
    • B64D29/06—Attaching of nacelles, fairings or cowlings
    • 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
    • B64D29/08—Inspection panels for power plants
    • 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
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • 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
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0206—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising noise reduction means, e.g. acoustic liners
    • 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
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0233—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising de-icing means
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/70—Disassembly methods

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Wind Motors (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Jib Cranes (AREA)
AT08864291T 2007-12-26 2008-09-10 Anlage für eine flugzeuggondelführungssystem ATE535444T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0709105A FR2925877B1 (fr) 2007-12-26 2007-12-26 Installation de systeme de guidage sur une nacelle d'aeronef.
PCT/FR2008/001262 WO2009080904A1 (fr) 2007-12-26 2008-09-10 Installation de systeme de guidage sur une nacelle d'aeronef

Publications (1)

Publication Number Publication Date
ATE535444T1 true ATE535444T1 (de) 2011-12-15

Family

ID=39577240

Family Applications (1)

Application Number Title Priority Date Filing Date
AT08864291T ATE535444T1 (de) 2007-12-26 2008-09-10 Anlage für eine flugzeuggondelführungssystem

Country Status (10)

Country Link
US (1) US8333344B2 (de)
EP (1) EP2222560B1 (de)
CN (1) CN101909998B (de)
AT (1) ATE535444T1 (de)
BR (1) BRPI0821023A2 (de)
CA (1) CA2705598A1 (de)
ES (1) ES2376701T3 (de)
FR (1) FR2925877B1 (de)
RU (1) RU2470839C2 (de)
WO (1) WO2009080904A1 (de)

Families Citing this family (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2906568B1 (fr) * 2006-10-02 2012-01-06 Aircelle Sa Structure d'entree d'air deposable pour nacelle de turboreacteur.
FR2914363B1 (fr) * 2007-03-26 2012-07-27 Aircelle Sa Systeme de guidage verrouillable pour partie mobile d'une nacelle
FR2938237B1 (fr) * 2008-11-13 2011-05-20 Aircelle Sa Nacelle pour turboreacteur a capot amont translatable
US9010084B2 (en) * 2009-02-02 2015-04-21 Airbus Operations Sas Aircraft nacelle including an optimised acoustic processing system
FR2965859B1 (fr) * 2010-10-07 2012-11-02 Snecma Dispositif de traitement acoustique du bruit emis par un turboreacteur
FR2966433B1 (fr) * 2010-10-26 2012-12-07 Airbus Operations Sas Capot d'aeronef incorporant des moyens pour limiter les phenomenes d'ecope de type pneumatique
FR2970513B1 (fr) * 2011-01-14 2015-07-31 Aircelle Sa Dispositif de liaison d'un cadre avant a un carter de soufflante
FR2970465B1 (fr) * 2011-01-19 2013-10-11 Aircelle Sa Nacelle pour un turboreacteur d'aeronef double flux.
GB201117079D0 (en) * 2011-10-05 2011-11-16 Rolls Royce Plc A propulsive unit for an aircraft
US9783315B2 (en) * 2012-02-24 2017-10-10 Rohr, Inc. Nacelle with longitudinal translating cowling and rotatable sleeves
FR2987601A1 (fr) * 2012-09-20 2013-09-06 Aircelle Sa Nacelle laminaire
FR2998545B1 (fr) * 2012-11-23 2016-10-28 Airbus Operations Sas Nacelle d'aeronef comprenant une liaison renforcee entre une entree d'air et une motorisation
FR3005100B1 (fr) * 2013-04-26 2015-05-01 Snecma Carter de turbomachine
US9708072B2 (en) 2014-04-30 2017-07-18 The Boeing Company Aircraft engine nacelle bulkheads and methods of assembling the same
US9604438B2 (en) 2014-04-30 2017-03-28 The Boeing Company Methods and apparatus for noise attenuation in an engine nacelle
US9656761B2 (en) * 2014-04-30 2017-05-23 The Boeing Company Lipskin for a nacelle and methods of making the same
US9938852B2 (en) 2014-04-30 2018-04-10 The Boeing Company Noise attenuating lipskin assembly and methods of assembling the same
US9874228B2 (en) * 2015-05-15 2018-01-23 Rohr, Inc. Nacelle inlet with extended outer barrel
FR3045570B1 (fr) * 2015-12-16 2017-12-22 Airbus Operations Sas Ensemble moteur pour aeronef, comprenant un dispositif d'accrochage du moteur equipe d'une enveloppe structurale fixee sur un caisson central
US10436112B2 (en) * 2017-06-26 2019-10-08 The Boeing Company Translating turning vanes for a nacelle inlet
US11125157B2 (en) * 2017-09-22 2021-09-21 The Boeing Company Advanced inlet design
FR3075761A1 (fr) * 2017-12-21 2019-06-28 Airbus Operations Partie anterieure de nacelle d'un ensemble propulsif comportant un cadre de rigidification incline
FR3086338B1 (fr) * 2018-09-20 2020-12-25 Safran Aircraft Engines Procede de preparation d'un support et de gestion acoustique, sur une turbomachine ou une nacelle
FR3087489B1 (fr) * 2018-10-18 2022-12-09 Airbus Operations Sas Partie anterieure de nacelle de groupe propulsif d'aeronef comportant une voie principale de propagation d'efforts entre une levre d'entree d'air et une peau arriere d'un panneau acoustique
FR3094698B1 (fr) 2019-04-02 2022-09-09 Safran Aircraft Engines Manche d’entree d’air pour une nacelle d’un ensemble propulsif d’aeronef
US11390393B2 (en) * 2019-06-04 2022-07-19 Rohr, Inc. Nacelle with a translatable inlet for an aircraft propulsion system
US11441482B2 (en) 2019-06-04 2022-09-13 Rohr, Inc. Single track translating inlet
FR3114849A1 (fr) * 2020-10-02 2022-04-08 Airbus Operations Turboreacteur double flux d’un aeronef comportant un capot articule en rotation et un systeme de deploiement dudit capot
FR3118481B1 (fr) * 2020-12-28 2023-04-21 Safran Nacelles Entrée d’air d’ensemble propulsif d’aéronef comprenant un organe de déplacement d’une partie amont mobile et procédé d’utilisation d’une telle entrée d’air
BR102022003769A2 (pt) 2021-05-04 2022-11-16 The Boeing Company Estrutura de entrada de nacele de um conjunto de motor
US11852022B2 (en) * 2021-06-10 2023-12-26 William Maxwell Retaining ejected gas turbine blades
US11346242B1 (en) * 2021-06-10 2022-05-31 William Maxwell Retaining ejected gas turbine blades
FR3128444A1 (fr) * 2021-10-26 2023-04-28 Airbus Operations (S.A.S.) Nacelle d’aéronef comprenant une liaison entre des conduits comportant des collerettes orientées vers l’intérieur et aéronef comprenant au moins une telle nacelle
US11878808B2 (en) * 2022-04-05 2024-01-23 Rohr, Inc. Nacelle inlet structure fitting with locator clip and hoist bracket

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR608599A (fr) 1925-03-31 1926-07-29 Perfectionnements aux machines automatiques à fabriquer les bouteilles et autres objets creux en verre
SU1320997A1 (ru) * 1985-04-01 2004-12-20 В.Ф. Гордеев Створка гондолы летательного аппарата
US4688757A (en) * 1986-08-11 1987-08-25 Dresser Industries, Inc. Soft seat Y pattern globe valve
GB9301457D0 (en) * 1993-01-26 1993-03-17 Short Brothers Plc An aircraft propulsuve power unit
CN1078663C (zh) * 1996-08-22 2002-01-30 波音公司 燃气涡轮发动机装置释压门的气流调节装置
FR2757823B1 (fr) * 1996-12-26 1999-03-12 Aerospatiale Nacelle de turboreacteur a ecoulement laminaire
US6340135B1 (en) * 2000-05-30 2002-01-22 Rohr, Inc. Translating independently mounted air inlet system for aircraft turbofan jet engine
US7588212B2 (en) 2003-07-08 2009-09-15 Rohr Inc. Method and apparatus for noise abatement and ice protection of an aircraft engine nacelle inlet lip
FR2862045B1 (fr) * 2003-11-12 2006-05-05 Snecma Moteurs Turboreacteur destine a etre fixe sur le fuselage d'un avion et en particulier sur sa partie arriere

Also Published As

Publication number Publication date
CN101909998B (zh) 2013-04-24
CA2705598A1 (fr) 2009-07-02
ES2376701T3 (es) 2012-03-16
WO2009080904A1 (fr) 2009-07-02
FR2925877A1 (fr) 2009-07-03
EP2222560A1 (de) 2010-09-01
FR2925877B1 (fr) 2009-12-04
BRPI0821023A2 (pt) 2015-06-16
US20100252689A1 (en) 2010-10-07
RU2470839C2 (ru) 2012-12-27
EP2222560B1 (de) 2011-11-30
US8333344B2 (en) 2012-12-18
CN101909998A (zh) 2010-12-08
RU2010129995A (ru) 2012-02-10

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