FR2384111A1 - Dispositif de securite pour turbine - Google Patents

Dispositif de securite pour turbine

Info

Publication number
FR2384111A1
FR2384111A1 FR7805970A FR7805970A FR2384111A1 FR 2384111 A1 FR2384111 A1 FR 2384111A1 FR 7805970 A FR7805970 A FR 7805970A FR 7805970 A FR7805970 A FR 7805970A FR 2384111 A1 FR2384111 A1 FR 2384111A1
Authority
FR
France
Prior art keywords
blades
safety device
blade
ring
turbine safety
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.)
Granted
Application number
FR7805970A
Other languages
English (en)
Other versions
FR2384111B1 (fr
Inventor
Henry Tubbs
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Publication of FR2384111A1 publication Critical patent/FR2384111A1/fr
Application granted granted Critical
Publication of FR2384111B1 publication Critical patent/FR2384111B1/fr
Granted legal-status Critical Current

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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/16—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means
    • F01D11/18—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means using stator or rotor components with predetermined thermal response, e.g. selective insulation, thermal inertia, differential expansion
    • 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
    • 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
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/208—Heat transfer, e.g. cooling using heat pipes

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Control Of Turbines (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Abstract

L'invention concerne un dispositif de sécurité destiné à éviter les avaries causées, dans les moteurs à turbine à gaz, par le détachement accidentel des aubes mobiles. Les aubes mobiles 16 sont entourées d'une couronne creuse 21 dont la paroi 22 contiguë aux aubes est assez mince pour qu'une aube ou fragment d'aube détaché la traverse et vienne s'immobiliser dans la couronne. Cette dernière constitue un conduit thermique dont la cavité 23 est remplie d'une vapeur condensable, de préférence de la vapeur de mercure, de façon à améliorer les échanges thermiques et réduire la déformation de la couronne.
FR7805970A 1977-03-17 1978-03-02 Dispositif de securite pour turbine Granted FR2384111A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB11267/77A GB1548836A (en) 1977-03-17 1977-03-17 Gasturbine engine

Publications (2)

Publication Number Publication Date
FR2384111A1 true FR2384111A1 (fr) 1978-10-13
FR2384111B1 FR2384111B1 (fr) 1983-05-06

Family

ID=9983070

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7805970A Granted FR2384111A1 (fr) 1977-03-17 1978-03-02 Dispositif de securite pour turbine

Country Status (6)

Country Link
US (1) US4199300A (fr)
JP (1) JPS53131313A (fr)
DE (1) DE2811478C3 (fr)
FR (1) FR2384111A1 (fr)
GB (1) GB1548836A (fr)
IT (1) IT7821288A0 (fr)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2502696A1 (fr) * 1981-03-25 1982-10-01 Rolls Royce Moteur a turbine a gaz presentant une immunite accrue aux dommages causes par l'ingestion de corps etrangers
EP0205559A1 (fr) * 1984-12-04 1986-12-30 Sundstrand Corporation Enceinte de protection d'une roue de turbine
EP0806547A1 (fr) * 1996-05-08 1997-11-12 Asea Brown Boveri AG Turbine axiale pour turbocompresseurs
EP3650658B1 (fr) * 2015-05-06 2022-11-23 Raytheon Technologies Corporation Anneau de contrôle

Families Citing this family (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5252088A (en) * 1975-10-24 1977-04-26 Hitachi Ltd Nucelar plant
GB2053367B (en) * 1979-07-12 1983-01-26 Rolls Royce Cooled shroud for a gas turbine engine
DE3018621C2 (de) * 1980-05-16 1982-06-03 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Außengehäuse für Axialverdichter oder -turbinen von Strömungsmaschinen, insbesondere Gasturbinentriebwerken
US5192186A (en) * 1980-10-03 1993-03-09 Rolls-Royce Plc Gas turbine engine
GB2251895B (en) * 1980-10-03 1992-12-09 Rolls Royce Gas turbine engine
GB2090333B (en) * 1980-12-18 1984-04-26 Rolls Royce Gas turbine engine shroud/blade tip control
GB2254378B (en) * 1981-12-30 1993-03-31 Rolls Royce Gas turbine engine ring shroud ring mounting
GB2316134B (en) * 1982-02-12 1998-07-01 Rolls Royce Improvements in or relating to gas turbine engines
GB2257754B (en) * 1983-02-26 1993-09-29 Rolls Royce Improvements in or relating to axial flow gas turbines
US4547122A (en) * 1983-10-14 1985-10-15 Aeronautical Research Associates Of Princeton, Inc. Method of containing fractured turbine blade fragments
DE3407946A1 (de) * 1984-03-03 1985-09-05 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Einrichtung zur verhinderung der ausbreitung von titanfeuer bei turbomaschinen, insbesondere gasturbinen- bzw. gasturbinenstrahltriebwerken
DE3407945A1 (de) * 1984-03-03 1985-09-05 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Verfahren und mittel zur vermeidung der entstehung von titanfeuer
US5188505A (en) * 1991-10-07 1993-02-23 General Electric Company Structural ring mechanism for containment housing of turbofan
DE10108559A1 (de) * 2001-02-22 2002-09-05 Alstom Switzerland Ltd Adaptive Spitzendichtung für eine axial durchströmte Turbomaschine
US7900438B2 (en) * 2006-07-28 2011-03-08 General Electric Company Heat transfer system and method for turbine engine using heat pipes
US7900437B2 (en) * 2006-07-28 2011-03-08 General Electric Company Heat transfer system and method for turbine engine using heat pipes
US7823374B2 (en) * 2006-08-31 2010-11-02 General Electric Company Heat transfer system and method for turbine engine using heat pipes
US7845159B2 (en) * 2006-08-31 2010-12-07 General Electric Company Heat pipe-based cooling apparatus and method for turbine engine
US8015788B2 (en) * 2006-12-27 2011-09-13 General Electric Company Heat transfer system for turbine engine using heat pipes
EP2159377A1 (fr) * 2008-08-27 2010-03-03 Siemens Aktiengesellschaft Support d'aubes statoriques pour une turbine à gaz et installation à turbine à gaz associée
EP2194235A1 (fr) * 2008-12-05 2010-06-09 Siemens Aktiengesellschaft Composant de boîtier pour une turbomachine axiale doté d'un contrôle d'intervalle passif, turbine à gaz dotée du composant de boîtier et procédé destiné au rééquipement d'un composant de boîtier existant
US10329940B2 (en) 2013-10-04 2019-06-25 General Electric Company Method and system for passive clearance control in a gas turbine engine
US9963994B2 (en) 2014-04-08 2018-05-08 General Electric Company Method and apparatus for clearance control utilizing fuel heating
GB201517171D0 (en) * 2015-09-29 2015-11-11 Rolls Royce Plc A casing for a gas turbine engine and a method of manufacturing such a casing
US10309242B2 (en) * 2016-08-10 2019-06-04 General Electric Company Ceramic matrix composite component cooling
FR3062169B1 (fr) * 2017-01-20 2019-04-19 Safran Aircraft Engines Carter de module de turbomachine d'aeronef, comprenant un caloduc associe a un anneau d'etancheite entourant une roue mobile aubagee du module
US10487684B2 (en) 2017-03-31 2019-11-26 The Boeing Company Gas turbine engine fan blade containment systems
US10550718B2 (en) 2017-03-31 2020-02-04 The Boeing Company Gas turbine engine fan blade containment systems
EP3632896A1 (fr) 2018-10-01 2020-04-08 Evonik Operations GmbH Production d'acides aminés à partir de leurs aminonitriles
EP3632895A1 (fr) 2018-10-01 2020-04-08 Evonik Operations GmbH Production sans sel d'acides aminés à partir de leurs aminonitriles
EP3632894A1 (fr) 2018-10-01 2020-04-08 Evonik Operations GmbH Production de méthionine pauvre en sous-produits à partir du nitrile de méthionine

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2879936A (en) * 1955-12-16 1959-03-31 Westinghouse Electric Corp Elastic fluid apparatus
US2935294A (en) * 1957-01-22 1960-05-03 Thompson Ramo Wooldridge Inc Double wall turbine shroud
FR1234350A (fr) * 1958-07-07 1960-10-17 Bristol Siddeley Engines Perfectionnements aux moteurs
DE1426808A1 (de) * 1964-01-21 1969-03-13 Garrett Corp Fangvorrichtung fuer ein Turbinenrad

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2073605A (en) * 1935-02-21 1937-03-16 Belluzzo Giuseppe Construction of internal combustion turbines
NL71631C (fr) * 1946-07-30
FR996476A (fr) * 1949-10-01 1951-12-19 Cem Comp Electro Mec Cylindre pour turbines à gaz
US3402767A (en) * 1964-11-23 1968-09-24 Euratom Heat pipes
US3287906A (en) * 1965-07-20 1966-11-29 Gen Motors Corp Cooled gas turbine vanes
US3493177A (en) * 1967-07-26 1970-02-03 Trw Inc Method of and means for cooling the throat wall of rocket engine nozzle
US3537713A (en) * 1968-02-21 1970-11-03 Garrett Corp Wear-resistant labyrinth seal
US3627444A (en) * 1969-11-24 1971-12-14 Gen Motors Corp Wick lined vanes and their manufacture
US3719365A (en) * 1971-10-18 1973-03-06 Gen Motors Corp Seal structure

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2879936A (en) * 1955-12-16 1959-03-31 Westinghouse Electric Corp Elastic fluid apparatus
US2935294A (en) * 1957-01-22 1960-05-03 Thompson Ramo Wooldridge Inc Double wall turbine shroud
FR1234350A (fr) * 1958-07-07 1960-10-17 Bristol Siddeley Engines Perfectionnements aux moteurs
DE1426808A1 (de) * 1964-01-21 1969-03-13 Garrett Corp Fangvorrichtung fuer ein Turbinenrad

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
EXBK/72 *

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2502696A1 (fr) * 1981-03-25 1982-10-01 Rolls Royce Moteur a turbine a gaz presentant une immunite accrue aux dommages causes par l'ingestion de corps etrangers
EP0205559A1 (fr) * 1984-12-04 1986-12-30 Sundstrand Corporation Enceinte de protection d'une roue de turbine
EP0205559A4 (fr) * 1984-12-04 1988-10-20 Sundstrand Corp Enceinte de protection d'une roue de turbine.
EP0806547A1 (fr) * 1996-05-08 1997-11-12 Asea Brown Boveri AG Turbine axiale pour turbocompresseurs
EP3650658B1 (fr) * 2015-05-06 2022-11-23 Raytheon Technologies Corporation Anneau de contrôle

Also Published As

Publication number Publication date
FR2384111B1 (fr) 1983-05-06
IT1093366B (fr) 1985-07-19
JPS5613162B2 (fr) 1981-03-26
DE2811478B2 (de) 1979-11-08
DE2811478A1 (de) 1978-09-21
IT7821288A0 (it) 1978-03-16
GB1548836A (en) 1979-07-18
JPS53131313A (en) 1978-11-16
DE2811478C3 (de) 1980-07-24
US4199300A (en) 1980-04-22

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