DE602005000185D1 - Turbomaschine mit einem Blockiersystem für die Haupttriebwerkswelle mit Lager-Sollbruchstelle - Google Patents

Turbomaschine mit einem Blockiersystem für die Haupttriebwerkswelle mit Lager-Sollbruchstelle

Info

Publication number
DE602005000185D1
DE602005000185D1 DE602005000185T DE602005000185T DE602005000185D1 DE 602005000185 D1 DE602005000185 D1 DE 602005000185D1 DE 602005000185 T DE602005000185 T DE 602005000185T DE 602005000185 T DE602005000185 T DE 602005000185T DE 602005000185 D1 DE602005000185 D1 DE 602005000185D1
Authority
DE
Germany
Prior art keywords
turbomachine
main engine
break point
engine shaft
blocking system
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
DE602005000185T
Other languages
English (en)
Other versions
DE602005000185T2 (de
Inventor
Aymeric Hugonie
Claude Mons
Jean-Luc Soupizon
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
Publication of DE602005000185D1 publication Critical patent/DE602005000185D1/de
Application granted granted Critical
Publication of DE602005000185T2 publication Critical patent/DE602005000185T2/de
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
    • 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
    • F01D21/06—Shutting-down
    • 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)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
DE602005000185T 2004-04-14 2005-04-08 Turbomaschine mit einem Blockiersystem für die Haupttriebwerkswelle mit Lager-Sollbruchstelle Active DE602005000185T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0403910A FR2869073B1 (fr) 2004-04-14 2004-04-14 Systeme de blocage d'un arbre principal de moteur a palier fusible
FR0403910 2004-04-14

Publications (2)

Publication Number Publication Date
DE602005000185D1 true DE602005000185D1 (de) 2006-11-30
DE602005000185T2 DE602005000185T2 (de) 2007-08-30

Family

ID=34942093

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005000185T Active DE602005000185T2 (de) 2004-04-14 2005-04-08 Turbomaschine mit einem Blockiersystem für die Haupttriebwerkswelle mit Lager-Sollbruchstelle

Country Status (8)

Country Link
US (1) US7360986B2 (de)
EP (1) EP1593816B1 (de)
JP (1) JP4459853B2 (de)
CA (1) CA2500986C (de)
DE (1) DE602005000185T2 (de)
ES (1) ES2274505T3 (de)
FR (1) FR2869073B1 (de)
RU (1) RU2368791C2 (de)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8167531B2 (en) * 2008-05-16 2012-05-01 General Electric Company Method and apparatus for supporting rotor assemblies during unbalances
GB201003588D0 (en) * 2010-03-04 2010-04-21 Rolls Royce Plc Improvements relating to layered composite components
WO2014081500A2 (en) * 2012-09-28 2014-05-30 United Technologies Corporation Auxiliary component mounts
US9631517B2 (en) 2012-12-29 2017-04-25 United Technologies Corporation Multi-piece fairing for monolithic turbine exhaust case
EP3575561B1 (de) * 2013-03-13 2022-04-13 Raytheon Technologies Corporation Turbofan-triebwerk und verfahren zur reduktion der last auf eine untersetzungsvorrichtung
RU2536655C1 (ru) * 2013-10-04 2014-12-27 Открытое акционерное общество "Авиадвигатель" Газотурбинный двигатель
FR3026774B1 (fr) * 2014-10-07 2020-07-17 Safran Aircraft Engines Turbomachine comportant un dispositif de freinage du rotor de soufflante.
CN107237655B (zh) * 2016-03-28 2019-03-15 中国航发商用航空发动机有限责任公司 航空发动机及其风扇叶片飞脱载荷下熔断方法
FR3062681B1 (fr) * 2017-02-07 2020-11-20 Safran Aircraft Engines Turboreacteur a architecture de paliers optimisee pour le support d'un arbre basse pression
CN113047959B (zh) * 2019-12-27 2022-07-12 中国航发商用航空发动机有限责任公司 航空发动机制动装置和航空发动机

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3880479A (en) * 1973-09-04 1975-04-29 Curtiss Wright Corp Emergency bearings for rotating shaft systems
GB2323637B (en) * 1997-03-25 2000-12-13 Rolls Royce Plc Ducted fan gas turbine engine
FR2773586B1 (fr) * 1998-01-09 2000-02-11 Snecma Turbomachine a freinage mutuel d'arbres concentriques
US6312215B1 (en) * 2000-02-15 2001-11-06 United Technologies Corporation Turbine engine windmilling brake
US6491497B1 (en) * 2000-09-22 2002-12-10 General Electric Company Method and apparatus for supporting rotor assemblies during unbalances

Also Published As

Publication number Publication date
CA2500986A1 (fr) 2005-10-14
JP2005299661A (ja) 2005-10-27
RU2005110988A (ru) 2006-11-20
FR2869073A1 (fr) 2005-10-21
DE602005000185T2 (de) 2007-08-30
EP1593816A1 (de) 2005-11-09
JP4459853B2 (ja) 2010-04-28
FR2869073B1 (fr) 2006-07-21
RU2368791C2 (ru) 2009-09-27
CA2500986C (fr) 2012-10-30
EP1593816B1 (de) 2006-10-18
US20050232755A1 (en) 2005-10-20
US7360986B2 (en) 2008-04-22
ES2274505T3 (es) 2007-05-16

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