FR2991969B1 - TURBOREACTOR BLOWER NACELLE - Google Patents

TURBOREACTOR BLOWER NACELLE

Info

Publication number
FR2991969B1
FR2991969B1 FR1255588A FR1255588A FR2991969B1 FR 2991969 B1 FR2991969 B1 FR 2991969B1 FR 1255588 A FR1255588 A FR 1255588A FR 1255588 A FR1255588 A FR 1255588A FR 2991969 B1 FR2991969 B1 FR 2991969B1
Authority
FR
France
Prior art keywords
turboreactor
nacelle
blower
turboreactor blower
blower 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
FR1255588A
Other languages
French (fr)
Other versions
FR2991969A1 (en
Inventor
Philippe Gerard Chanez
Matthieu Leyko
Jean Bertucchi
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA 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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR1255588A priority Critical patent/FR2991969B1/en
Publication of FR2991969A1 publication Critical patent/FR2991969A1/en
Application granted granted Critical
Publication of FR2991969B1 publication Critical patent/FR2991969B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C7/00Structures or fairings not otherwise provided for
    • B64C7/02Nacelles
    • 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
    • B64D29/00Power-plant nacelles, fairings, or cowlings
    • B64D29/06Attaching of nacelles, fairings or cowlings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78Other construction of jet pipes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/70Shape

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1255588A 2012-06-14 2012-06-14 TURBOREACTOR BLOWER NACELLE Active FR2991969B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1255588A FR2991969B1 (en) 2012-06-14 2012-06-14 TURBOREACTOR BLOWER NACELLE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1255588A FR2991969B1 (en) 2012-06-14 2012-06-14 TURBOREACTOR BLOWER NACELLE

Publications (2)

Publication Number Publication Date
FR2991969A1 FR2991969A1 (en) 2013-12-20
FR2991969B1 true FR2991969B1 (en) 2014-09-05

Family

ID=46826733

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1255588A Active FR2991969B1 (en) 2012-06-14 2012-06-14 TURBOREACTOR BLOWER NACELLE

Country Status (1)

Country Link
FR (1) FR2991969B1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3000721B1 (en) * 2013-01-09 2016-10-14 Airbus Operations Sas AIRCRAFT PROPULSIVE ASSEMBLY COMPRISING AERODYNAMIC AERODYNAMIC REAR FITTING FOR SIDEWALLS WITH PROFILED WALLS FOR THE INJECTION OF FRESH AIR ALONG A THERMAL PROTECTION FLOOR
US10450898B2 (en) 2015-02-13 2019-10-22 United Technologies Corporation Track fairing assembly for a turbine engine nacelle

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2278147B1 (en) * 2009-06-16 2014-06-25 Rohr, Inc. Translating variable area fan nozzle providing an upstream bypass flow exit

Also Published As

Publication number Publication date
FR2991969A1 (en) 2013-12-20

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