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FR2978731B1 - Nacelle d'aeronef incorporant un anneau de renfort. - Google Patents

Nacelle d'aeronef incorporant un anneau de renfort.

Info

Publication number
FR2978731B1
FR2978731B1 FR1157188A FR1157188A FR2978731B1 FR 2978731 B1 FR2978731 B1 FR 2978731B1 FR 1157188 A FR1157188 A FR 1157188A FR 1157188 A FR1157188 A FR 1157188A FR 2978731 B1 FR2978731 B1 FR 2978731B1
Authority
FR
France
Prior art keywords
reinforcement ring
aircraft nacelle
nacelle incorporating
incorporating
aircraft
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.)
Active
Application number
FR1157188A
Other languages
English (en)
Other versions
FR2978731A1 (fr
Inventor
Alain Porte
Frederic Chelin
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
Priority to FR1157188A priority Critical patent/FR2978731B1/fr
Publication of FR2978731A1 publication Critical patent/FR2978731A1/fr
Application granted granted Critical
Publication of FR2978731B1 publication Critical patent/FR2978731B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/04Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/05Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0206Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising noise reduction means, e.g. acoustic liners
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0266Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
    • B64D2033/0286Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for turbofan engines
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1157188A 2011-08-05 2011-08-05 Nacelle d'aeronef incorporant un anneau de renfort. Active FR2978731B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1157188A FR2978731B1 (fr) 2011-08-05 2011-08-05 Nacelle d'aeronef incorporant un anneau de renfort.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1157188A FR2978731B1 (fr) 2011-08-05 2011-08-05 Nacelle d'aeronef incorporant un anneau de renfort.

Publications (2)

Publication Number Publication Date
FR2978731A1 FR2978731A1 (fr) 2013-02-08
FR2978731B1 true FR2978731B1 (fr) 2014-05-02

Family

ID=44681326

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1157188A Active FR2978731B1 (fr) 2011-08-05 2011-08-05 Nacelle d'aeronef incorporant un anneau de renfort.

Country Status (1)

Country Link
FR (1) FR2978731B1 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3075761A1 (fr) * 2017-12-21 2019-06-28 Airbus Operations Partie anterieure de nacelle d'un ensemble propulsif comportant un cadre de rigidification incline
FR3086785B1 (fr) * 2018-09-28 2022-01-21 Airbus Operations Sas Ensemble comportant deux panneaux acoustiques juxtaposes dans lequel les panneaux comportent une face resistive qui s'etend jusqu'a une paroi d'extremite
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
EP4470920A1 (fr) * 2023-05-29 2024-12-04 Airbus Operations (S.A.S.) Ensemble de propulsion d'aéronef comportant au moins un panneau aérodynamique supporté par au moins un support radial intermédiaire, aéronef comprenant au moins un tel ensemble de propulsion

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2840647B1 (fr) * 2002-06-05 2004-10-29 Airbus France Dispositif pour le raccordement de deux pieces tubulaires de turboreacteur d'aeronef
FR2903732B1 (fr) * 2006-07-12 2008-09-12 Airbus France Sas Entree d'air pour turbomoteur d'aeronef.
FR2904604B1 (fr) * 2006-08-04 2009-02-27 Airbus France Sas Element de structure d'un aeronef
US7503425B2 (en) * 2006-10-02 2009-03-17 Spirit Aerosystems, Inc. Integrated inlet attachment

Also Published As

Publication number Publication date
FR2978731A1 (fr) 2013-02-08

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