FR3055885B1 - Nacelle d'aeronef comprenant une liaison entre une entree d'air et une motorisation qui comporte une bride - Google Patents

Nacelle d'aeronef comprenant une liaison entre une entree d'air et une motorisation qui comporte une bride Download PDF

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Publication number
FR3055885B1
FR3055885B1 FR1658497A FR1658497A FR3055885B1 FR 3055885 B1 FR3055885 B1 FR 3055885B1 FR 1658497 A FR1658497 A FR 1658497A FR 1658497 A FR1658497 A FR 1658497A FR 3055885 B1 FR3055885 B1 FR 3055885B1
Authority
FR
France
Prior art keywords
flange
engine
connection
air intake
aircraft nacelle
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
FR1658497A
Other languages
English (en)
Other versions
FR3055885A1 (fr
Inventor
Alain Porte
Arnaud Bourhis
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 FR1658497A priority Critical patent/FR3055885B1/fr
Publication of FR3055885A1 publication Critical patent/FR3055885A1/fr
Application granted granted Critical
Publication of FR3055885B1 publication Critical patent/FR3055885B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/243—Flange connections; Bolting arrangements
    • 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
    • F02C7/045—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for noise suppression
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1658497A 2016-09-13 2016-09-13 Nacelle d'aeronef comprenant une liaison entre une entree d'air et une motorisation qui comporte une bride Active FR3055885B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1658497A FR3055885B1 (fr) 2016-09-13 2016-09-13 Nacelle d'aeronef comprenant une liaison entre une entree d'air et une motorisation qui comporte une bride

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1658497 2016-09-13
FR1658497A FR3055885B1 (fr) 2016-09-13 2016-09-13 Nacelle d'aeronef comprenant une liaison entre une entree d'air et une motorisation qui comporte une bride

Publications (2)

Publication Number Publication Date
FR3055885A1 FR3055885A1 (fr) 2018-03-16
FR3055885B1 true FR3055885B1 (fr) 2022-06-03

Family

ID=57396628

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1658497A Active FR3055885B1 (fr) 2016-09-13 2016-09-13 Nacelle d'aeronef comprenant une liaison entre une entree d'air et une motorisation qui comporte une bride

Country Status (1)

Country Link
FR (1) FR3055885B1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3083214A1 (fr) * 2018-06-28 2020-01-03 Airbus Operations Nacelle d'un ensemble propulsif d'aeronef comportant une pluralite d'elements amortisseurs entre une partie avant et une partie principale, et ensemble propulsif d'aeronef associe

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6920958B2 (en) * 2003-10-17 2005-07-26 The Boeing Company Annular acoustic panel
FR2903732B1 (fr) * 2006-07-12 2008-09-12 Airbus France Sas Entree d'air pour turbomoteur d'aeronef.
US7871486B2 (en) * 2006-11-21 2011-01-18 General Electric Company Methods for making structures having mounting flanges
FR2998547B1 (fr) * 2012-11-23 2016-01-29 Airbus Operations Sas Nacelle d'aeronef comprenant une liaison deformable entre une entree d'air et une motorisation

Also Published As

Publication number Publication date
FR3055885A1 (fr) 2018-03-16

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