FR3010144B1 - Ensemble turbomachine d'aeronef pourvu d'un prelevement de fluide controle dans un flux secondaire. - Google Patents

Ensemble turbomachine d'aeronef pourvu d'un prelevement de fluide controle dans un flux secondaire. Download PDF

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Publication number
FR3010144B1
FR3010144B1 FR1358329A FR1358329A FR3010144B1 FR 3010144 B1 FR3010144 B1 FR 3010144B1 FR 1358329 A FR1358329 A FR 1358329A FR 1358329 A FR1358329 A FR 1358329A FR 3010144 B1 FR3010144 B1 FR 3010144B1
Authority
FR
France
Prior art keywords
secondary flow
fluid collection
controlled fluid
aircraft turbomachine
turbomachine assembly
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.)
Expired - Fee Related
Application number
FR1358329A
Other languages
English (en)
Other versions
FR3010144A1 (fr
Inventor
Jerome HUBER
Arnaud Hormiere
Loic DUSSOL
Clemence Barthomeuf
Dax Au
Florent Bonneau
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 FR1358329A priority Critical patent/FR3010144B1/fr
Publication of FR3010144A1 publication Critical patent/FR3010144A1/fr
Application granted granted Critical
Publication of FR3010144B1 publication Critical patent/FR3010144B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • 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
    • F02K1/28—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
    • F02K1/34—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow for attenuating noise
FR1358329A 2013-08-30 2013-08-30 Ensemble turbomachine d'aeronef pourvu d'un prelevement de fluide controle dans un flux secondaire. Expired - Fee Related FR3010144B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1358329A FR3010144B1 (fr) 2013-08-30 2013-08-30 Ensemble turbomachine d'aeronef pourvu d'un prelevement de fluide controle dans un flux secondaire.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1358329 2013-08-30
FR1358329A FR3010144B1 (fr) 2013-08-30 2013-08-30 Ensemble turbomachine d'aeronef pourvu d'un prelevement de fluide controle dans un flux secondaire.

Publications (2)

Publication Number Publication Date
FR3010144A1 FR3010144A1 (fr) 2015-03-06
FR3010144B1 true FR3010144B1 (fr) 2018-01-19

Family

ID=49667356

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1358329A Expired - Fee Related FR3010144B1 (fr) 2013-08-30 2013-08-30 Ensemble turbomachine d'aeronef pourvu d'un prelevement de fluide controle dans un flux secondaire.

Country Status (1)

Country Link
FR (1) FR3010144B1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3062371B1 (fr) 2017-01-31 2019-03-29 Airbus Nacelle d'un turboreacteur comportant un volet inverseur

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4291782A (en) * 1979-10-30 1981-09-29 The Boeing Company Simplified method and apparatus for hot-shield jet noise suppression
US7127880B2 (en) * 2003-08-29 2006-10-31 The Nordam Group, Inc. Induction coupled variable nozzle
FR2901321B1 (fr) * 2006-05-18 2011-08-12 Aircelle Sa Procede d'homogeneisation de l'air en sortie de turboreacteur pour abaisser le bruit genere

Also Published As

Publication number Publication date
FR3010144A1 (fr) 2015-03-06

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