FR3006713B1 - Dispositif de decouplage pour turbomachine comportant une piece intermediaire - Google Patents

Dispositif de decouplage pour turbomachine comportant une piece intermediaire

Info

Publication number
FR3006713B1
FR3006713B1 FR1355379A FR1355379A FR3006713B1 FR 3006713 B1 FR3006713 B1 FR 3006713B1 FR 1355379 A FR1355379 A FR 1355379A FR 1355379 A FR1355379 A FR 1355379A FR 3006713 B1 FR3006713 B1 FR 3006713B1
Authority
FR
France
Prior art keywords
turbomachine
intermediate piece
decoupling device
decoupling
piece
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
FR1355379A
Other languages
English (en)
Other versions
FR3006713A1 (fr
Inventor
Francois Gallet
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 FR1355379A priority Critical patent/FR3006713B1/fr
Publication of FR3006713A1 publication Critical patent/FR3006713A1/fr
Application granted granted Critical
Publication of FR3006713B1 publication Critical patent/FR3006713B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
    • F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
    • F01D25/162—Bearing supports
    • 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)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1355379A 2013-06-11 2013-06-11 Dispositif de decouplage pour turbomachine comportant une piece intermediaire Active FR3006713B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1355379A FR3006713B1 (fr) 2013-06-11 2013-06-11 Dispositif de decouplage pour turbomachine comportant une piece intermediaire

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1355379A FR3006713B1 (fr) 2013-06-11 2013-06-11 Dispositif de decouplage pour turbomachine comportant une piece intermediaire

Publications (2)

Publication Number Publication Date
FR3006713A1 FR3006713A1 (fr) 2014-12-12
FR3006713B1 true FR3006713B1 (fr) 2016-10-14

Family

ID=48795836

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1355379A Active FR3006713B1 (fr) 2013-06-11 2013-06-11 Dispositif de decouplage pour turbomachine comportant une piece intermediaire

Country Status (1)

Country Link
FR (1) FR3006713B1 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10830099B2 (en) 2017-11-20 2020-11-10 Raytheon Technologies Corporation Fuse joint with fenestrated fuse pin
US11371432B2 (en) * 2017-02-28 2022-06-28 Safran Aircraft Engines Aircraft engine intake arrangement comprising a mechanical decoupler

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3081523B1 (fr) 2018-05-28 2021-01-08 Safran Aircraft Engines Turbomachine d'aeronef comportant des moyens de decouplage
FR3118785B1 (fr) * 2021-01-12 2023-05-19 Safran Aircraft Engines Piece de blocage pour assemblage d’elements de turbomachine comprenant des moyens fusibles et turbomachine correspondante

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6240719B1 (en) * 1998-12-09 2001-06-05 General Electric Company Fan decoupler system for a gas turbine engine
DE10157576C2 (de) * 2001-11-23 2003-11-06 Mtu Aero Engines Gmbh Drehlagerung mit einer Sollbruchstelle
FR2976623B1 (fr) * 2011-06-20 2013-06-28 Snecma Dispositif de decouplage pour turbomoteur a double flux

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11371432B2 (en) * 2017-02-28 2022-06-28 Safran Aircraft Engines Aircraft engine intake arrangement comprising a mechanical decoupler
US10830099B2 (en) 2017-11-20 2020-11-10 Raytheon Technologies Corporation Fuse joint with fenestrated fuse pin

Also Published As

Publication number Publication date
FR3006713A1 (fr) 2014-12-12

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