FR2992347B1 - Recepteur de turbomachine d'aeronef a doublet d'helices contrarotatives non carenees, comprenant une turbine libre exterieure a maintien renforce - Google Patents

Recepteur de turbomachine d'aeronef a doublet d'helices contrarotatives non carenees, comprenant une turbine libre exterieure a maintien renforce

Info

Publication number
FR2992347B1
FR2992347B1 FR1255904A FR1255904A FR2992347B1 FR 2992347 B1 FR2992347 B1 FR 2992347B1 FR 1255904 A FR1255904 A FR 1255904A FR 1255904 A FR1255904 A FR 1255904A FR 2992347 B1 FR2992347 B1 FR 2992347B1
Authority
FR
France
Prior art keywords
carinated
doublet
free turbine
aircraft turbomachine
extended free
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
FR1255904A
Other languages
English (en)
Other versions
FR2992347A1 (fr
Inventor
Sarah Chartier
Dominik Igel
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 FR1255904A priority Critical patent/FR2992347B1/fr
Publication of FR2992347A1 publication Critical patent/FR2992347A1/fr
Application granted granted Critical
Publication of FR2992347B1 publication Critical patent/FR2992347B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/02—Hub construction
    • B64C11/04—Blade mountings
    • B64C11/06—Blade mountings for variable-pitch blades
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/46—Arrangements of, or constructional features peculiar to, multiple propellers
    • B64C11/48—Units of two or more coaxial propellers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D2027/005—Aircraft with an unducted turbofan comprising contra-rotating rotors, e.g. contra-rotating open rotors [CROR]
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1255904A 2012-06-22 2012-06-22 Recepteur de turbomachine d'aeronef a doublet d'helices contrarotatives non carenees, comprenant une turbine libre exterieure a maintien renforce Active FR2992347B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1255904A FR2992347B1 (fr) 2012-06-22 2012-06-22 Recepteur de turbomachine d'aeronef a doublet d'helices contrarotatives non carenees, comprenant une turbine libre exterieure a maintien renforce

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1255904A FR2992347B1 (fr) 2012-06-22 2012-06-22 Recepteur de turbomachine d'aeronef a doublet d'helices contrarotatives non carenees, comprenant une turbine libre exterieure a maintien renforce

Publications (2)

Publication Number Publication Date
FR2992347A1 FR2992347A1 (fr) 2013-12-27
FR2992347B1 true FR2992347B1 (fr) 2014-07-18

Family

ID=46754683

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1255904A Active FR2992347B1 (fr) 2012-06-22 2012-06-22 Recepteur de turbomachine d'aeronef a doublet d'helices contrarotatives non carenees, comprenant une turbine libre exterieure a maintien renforce

Country Status (1)

Country Link
FR (1) FR2992347B1 (fr)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3111161B1 (fr) 2020-06-05 2022-05-06 Safran Aircraft Engines Systeme de verrouillage d'aubes de soufflante a calage variable
FR3115342B1 (fr) 2020-10-16 2022-10-21 Safran Aircraft Engines Dispositif d'étanchéité extensible, notamment pour une soufflante à aubes à calage variable
FR3115817B1 (fr) 2020-10-29 2022-10-07 Safran Aircraft Engines Bride de verrouillage d'aubes de soufflante à calage variable
FR3117154B1 (fr) 2020-12-04 2023-06-09 Safran Aircraft Engines Systeme de fixation de plateforme aérodynamique pour une soufflante à aubes à calage variable
FR3136547B1 (fr) 2022-06-14 2024-04-26 Safran Aircraft Engines Système de verrouillage d'aubes d'un module de soufflante de type baïonnette
FR3136851B1 (fr) 2022-06-15 2024-05-03 Safran Aircraft Engines Système de verrouillage d'aubes d'un module de soufflante muni d'un dispositif de maintien d'une bride de pivot
FR3136853B1 (fr) 2022-06-17 2024-05-10 Safran Aircraft Engines Système de verrouillage d'aubes d'un module de soufflante à double crabots
FR3137412A1 (fr) 2022-07-01 2024-01-05 Safran Aircraft Engines Système de verrouillage d'aubes d'un module de soufflante par double noix de serrage
FR3137410B1 (fr) 2022-07-04 2024-05-17 Safran Aircraft Engines Système de verrouillage d'aube d'un module de soufflante muni d'un doigt de verrouilage
FR3137715A1 (fr) 2022-07-11 2024-01-12 Safran Aircraft Engines Système de verrouillage d'une aube d'un module de soufflante par levier de serrage

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4732538A (en) * 1984-03-02 1988-03-22 General Electric Company Blade hub air scoop
DE10361653B4 (de) * 2003-12-30 2008-08-07 Airbus Deutschland Gmbh Kühleinrichtung zum Abführen von Wärme von einer im Innenraum eines Flugzeuges angeordneten Wärmequelle
FR2963054B1 (fr) * 2010-07-22 2012-07-27 Snecma Anneau de retention

Also Published As

Publication number Publication date
FR2992347A1 (fr) 2013-12-27

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