FR3023260B1 - Ensemble propulsif d'aeronef - Google Patents

Ensemble propulsif d'aeronef

Info

Publication number
FR3023260B1
FR3023260B1 FR1456408A FR1456408A FR3023260B1 FR 3023260 B1 FR3023260 B1 FR 3023260B1 FR 1456408 A FR1456408 A FR 1456408A FR 1456408 A FR1456408 A FR 1456408A FR 3023260 B1 FR3023260 B1 FR 3023260B1
Authority
FR
France
Prior art keywords
aircraft assembly
propellant
propellant aircraft
assembly
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
FR1456408A
Other languages
English (en)
Other versions
FR3023260A1 (fr
Inventor
Francois Bellet
Cedric Renault
Jeremie Rabineau
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 Nacelles SAS
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
Priority to FR1456408A priority Critical patent/FR3023260B1/fr
Priority to PCT/FR2015/051806 priority patent/WO2016001581A1/fr
Publication of FR3023260A1 publication Critical patent/FR3023260A1/fr
Application granted granted Critical
Publication of FR3023260B1 publication Critical patent/FR3023260B1/fr
Priority to US15/386,954 priority patent/US9963999B2/en
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; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02Aircraft characterised by the type or position of power plant
    • B64D27/16Aircraft characterised by the type or position of power plant of jet type
    • B64D27/18Aircraft characterised by the type or position of power plant of jet type within or attached to wing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24Casings; Casing parts, e.g. diaphragms, casing fastenings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02Aircraft characterised by the type or position of power plant
    • B64D27/16Aircraft characterised by the type or position of power plant of jet type
    • B64D27/40
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00Power-plant nacelles, fairings, or cowlings
    • B64D29/02Power-plant nacelles, fairings, or cowlings associated with wings
    • 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
    • F02C9/00Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16Control of working fluid flow
    • F02C9/18Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages
    • 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
    • F05D2220/00Application
    • F05D2220/30Application in turbines
    • F05D2220/32Application in turbines in gas turbines
    • F05D2220/323Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines
FR1456408A 2014-07-03 2014-07-03 Ensemble propulsif d'aeronef Active FR3023260B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1456408A FR3023260B1 (fr) 2014-07-03 2014-07-03 Ensemble propulsif d'aeronef
PCT/FR2015/051806 WO2016001581A1 (fr) 2014-07-03 2015-07-01 Ensemble propulsif d'aéronef
US15/386,954 US9963999B2 (en) 2014-07-03 2016-12-21 Aircraft propulsion assembly

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1456408A FR3023260B1 (fr) 2014-07-03 2014-07-03 Ensemble propulsif d'aeronef

Publications (2)

Publication Number Publication Date
FR3023260A1 FR3023260A1 (fr) 2016-01-08
FR3023260B1 true FR3023260B1 (fr) 2016-07-15

Family

ID=51352677

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1456408A Active FR3023260B1 (fr) 2014-07-03 2014-07-03 Ensemble propulsif d'aeronef

Country Status (3)

Country Link
US (1) US9963999B2 (fr)
FR (1) FR3023260B1 (fr)
WO (1) WO2016001581A1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3060532B1 (fr) * 2016-12-20 2019-05-31 Airbus Operations Ensemble moteur pour aeronef, comprenant des dispositifs elastiques souples de transmission d'efforts entre des capots de nacelle et une structure annulaire reliee au carter moteur par des bielles
US11697506B2 (en) * 2020-05-15 2023-07-11 General Electric Company Methods and apparatus for gas turbine bending isolation

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3542826A1 (de) * 1985-12-04 1987-06-11 Mtu Muenchen Gmbh Wellendichtungseinrichtung fuer turbomaschinen, insbesondere gasturbinentriebwerke
GB9602130D0 (en) * 1996-02-02 1996-04-03 Rolls Royce Plc Improved method of combining ducted fan gas turbine engine modules and aircraft structure
US6821085B2 (en) * 2002-09-30 2004-11-23 General Electric Company Turbine engine axially sealing assembly including an axially floating shroud, and assembly method
FR2866070B1 (fr) * 2004-02-05 2008-12-05 Snecma Moteurs Turboreacteur a fort taux de dilution
FR2905991B1 (fr) * 2006-09-20 2012-01-13 Snecma Systeme propulsif integre comportant un moteur a turboreacteur a double flux.
FR2933070B1 (fr) * 2008-06-25 2010-08-20 Snecma Systeme propulsif d'aeronef
GB2525179B (en) * 2014-04-14 2016-09-07 Rolls Royce Plc A panel connection system and a method of using the same

Also Published As

Publication number Publication date
US20170101895A1 (en) 2017-04-13
WO2016001581A1 (fr) 2016-01-07
FR3023260A1 (fr) 2016-01-08
US9963999B2 (en) 2018-05-08

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