FR2986212B1 - AIRCRAFT NACELLE WITH A SLIDING REAR PART TO FORM A PUSH INVERTER. - Google Patents

AIRCRAFT NACELLE WITH A SLIDING REAR PART TO FORM A PUSH INVERTER.

Info

Publication number
FR2986212B1
FR2986212B1 FR1250739A FR1250739A FR2986212B1 FR 2986212 B1 FR2986212 B1 FR 2986212B1 FR 1250739 A FR1250739 A FR 1250739A FR 1250739 A FR1250739 A FR 1250739A FR 2986212 B1 FR2986212 B1 FR 2986212B1
Authority
FR
France
Prior art keywords
rear part
aircraft nacelle
sliding rear
push inverter
inverter
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
FR1250739A
Other languages
French (fr)
Other versions
FR2986212A1 (en
Inventor
Emmanuel Patsouris
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 FR1250739A priority Critical patent/FR2986212B1/en
Publication of FR2986212A1 publication Critical patent/FR2986212A1/en
Application granted granted Critical
Publication of FR2986212B1 publication Critical patent/FR2986212B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/64—Reversing fan flow
    • F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
    • F02K1/72—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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
    • B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/76—Control or regulation of thrust reversers
    • F02K1/763—Control or regulation of thrust reversers with actuating systems or actuating devices; Arrangement of actuators for thrust reversers
    • 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
    • F05D2260/00—Function
    • F05D2260/50—Kinematic linkage, i.e. transmission of position
    • 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
FR1250739A 2012-01-26 2012-01-26 AIRCRAFT NACELLE WITH A SLIDING REAR PART TO FORM A PUSH INVERTER. Active FR2986212B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1250739A FR2986212B1 (en) 2012-01-26 2012-01-26 AIRCRAFT NACELLE WITH A SLIDING REAR PART TO FORM A PUSH INVERTER.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1250739A FR2986212B1 (en) 2012-01-26 2012-01-26 AIRCRAFT NACELLE WITH A SLIDING REAR PART TO FORM A PUSH INVERTER.

Publications (2)

Publication Number Publication Date
FR2986212A1 FR2986212A1 (en) 2013-08-02
FR2986212B1 true FR2986212B1 (en) 2014-10-10

Family

ID=45894554

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1250739A Active FR2986212B1 (en) 2012-01-26 2012-01-26 AIRCRAFT NACELLE WITH A SLIDING REAR PART TO FORM A PUSH INVERTER.

Country Status (1)

Country Link
FR (1) FR2986212B1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3023210B1 (en) * 2014-07-07 2017-02-24 Safran PROCESS FOR MANUFACTURING A COMPOSITE MATERIAL PART COMPRISING AT LEAST ONE PORTION FORMING AN EFFORT INTRODUCTION OR LOCAL OUTPUT PORTION
FR3078112B1 (en) * 2018-02-22 2020-01-17 Airbus Operations NACELLE OF A TURBOREACTOR HAVING AN INVERTER SHUTTER

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1386232A (en) * 1971-03-31 1975-03-05 Short Brothers & Harland Ltd Fluid propulsion systems
FR2379705A1 (en) * 1977-02-08 1978-09-01 Snecma Thrust reversing mechanism for aircraft engine - has blades linked to sliding and moving parts of outer housing only
DE3844188C1 (en) * 1988-12-29 1990-05-17 Mtu Muenchen Gmbh
US5309711A (en) * 1991-08-21 1994-05-10 Rohr, Inc. Cascade type thrust reverser for fan jet engines
FR2786532B1 (en) * 1998-11-26 2001-09-07 Snecma OVERHEAD GRID TURBOREACTOR DRIVE INVERTER
US7559507B2 (en) * 2005-06-27 2009-07-14 The Boeing Company Thrust reversers including locking assemblies for inhibiting deflection

Also Published As

Publication number Publication date
FR2986212A1 (en) 2013-08-02

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