[go: up one dir, main page]

EP2071136A3 - Braking device for a turbine in a gas turbine motor in the event of shaft breakage - Google Patents

Braking device for a turbine in a gas turbine motor in the event of shaft breakage Download PDF

Info

Publication number
EP2071136A3
EP2071136A3 EP08156698A EP08156698A EP2071136A3 EP 2071136 A3 EP2071136 A3 EP 2071136A3 EP 08156698 A EP08156698 A EP 08156698A EP 08156698 A EP08156698 A EP 08156698A EP 2071136 A3 EP2071136 A3 EP 2071136A3
Authority
EP
European Patent Office
Prior art keywords
event
turbine
braking device
braking
shaft
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
EP08156698A
Other languages
German (de)
French (fr)
Other versions
EP2071136B1 (en
EP2071136A2 (en
Inventor
Jacques René Bart
Didier René André Escure
Claude Marcel Mons
Stéphane Rousselin
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 EP2071136A2 publication Critical patent/EP2071136A2/en
Publication of EP2071136A3 publication Critical patent/EP2071136A3/en
Application granted granted Critical
Publication of EP2071136B1 publication Critical patent/EP2071136B1/en
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
    • F01D21/006—Arrangements of brakes
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/90—Coating; Surface treatment
    • 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
    • F05D2260/90—Braking
    • F05D2260/902—Braking using frictional mechanical forces
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/20—Oxide or non-oxide ceramics
    • F05D2300/21—Oxide ceramics
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/20—Oxide or non-oxide ceramics
    • F05D2300/21—Oxide ceramics
    • F05D2300/2102—Glass
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/20—Oxide or non-oxide ceramics
    • F05D2300/21—Oxide ceramics
    • F05D2300/2118—Zirconium oxides
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/40—Organic materials
    • F05D2300/44—Resins
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/601—Fabrics
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/611—Coating
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/614—Fibres or filaments

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Braking Arrangements (AREA)

Abstract

On présente un dispositif de freinage, dans un moteur à turbine à gaz, d'une turbine comprenant un rotor entraînant un arbre mobile en rotation par rapport à un stator, en cas de rupture dudit arbre. Le dispositif est caractérisé par le fait qu'il comprend un premier organe de freinage (110) pourvu d'au moins un élément abrasif (110A) et un second organe de freinage (120) comprenant un élément en forme d'anneau (120A) réalisé en un matériau susceptible d'être érodé par l'élément abrasif (110A), les deux organes de freinage étant solidaires l'un du rotor, l'autre du stator et venant en contact par déplacement axial du rotor après rupture de l'arbre, l'élément abrasif (110A) du premier organe de freinage (110) érodant l'élément en forme d'anneau (120) du second organe de freinage (120).

Figure imgaf001
A braking device is presented in a gas turbine engine of a turbine comprising a rotor driving a shaft movable in rotation with respect to a stator, in the event of rupture of said shaft. The device is characterized in that it comprises a first braking member (110) provided with at least one abrasive element (110A) and a second braking member (120) comprising a ring-shaped element (120A). made of a material that can be eroded by the abrasive element (110A), the two braking members being secured to one of the rotor, the other of the stator and coming into contact by axial displacement of the rotor after breaking the shaft, the abrasive element (110A) of the first braking member (110) eroding the ring-shaped member (120) of the second braking member (120).
Figure imgaf001
EP08156698.6A 2007-05-25 2008-05-21 Gas turbine motor with a braking device in the event of shaft breakage Active EP2071136B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0703758A FR2916482B1 (en) 2007-05-25 2007-05-25 BRAKE SYSTEM IN CASE OF TURBINE SHAFT RUPTURE IN A GAS TURBINE ENGINE

Publications (3)

Publication Number Publication Date
EP2071136A2 EP2071136A2 (en) 2009-06-17
EP2071136A3 true EP2071136A3 (en) 2010-03-10
EP2071136B1 EP2071136B1 (en) 2018-07-25

Family

ID=39099813

Family Applications (1)

Application Number Title Priority Date Filing Date
EP08156698.6A Active EP2071136B1 (en) 2007-05-25 2008-05-21 Gas turbine motor with a braking device in the event of shaft breakage

Country Status (3)

Country Link
US (1) US8161727B2 (en)
EP (1) EP2071136B1 (en)
FR (1) FR2916482B1 (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2916483B1 (en) * 2007-05-25 2013-03-01 Snecma SYSTEM FOR DISSIPATING ENERGY IN THE EVENT OF TURBINE SHAFT BREAKAGE IN A GAS TURBINE ENGINE
DE102011086775A1 (en) 2011-07-20 2013-01-24 Mtu Aero Engines Gmbh Method for producing an inlet lining, inlet system, turbomachine and vane
US9062560B2 (en) 2012-03-13 2015-06-23 United Technologies Corporation Gas turbine engine variable stator vane assembly
FR3026774B1 (en) * 2014-10-07 2020-07-17 Safran Aircraft Engines TURBOMACHINE COMPRISING A BLOWER ROTOR BRAKING DEVICE.
US10190440B2 (en) 2015-06-10 2019-01-29 Rolls-Royce North American Technologies, Inc. Emergency shut-down detection system for a gas turbine
FR3049646B1 (en) * 2016-03-31 2019-04-12 Safran Aircraft Engines DEVICE FOR LIMITING THE OVERVIEW OF A TURBINE ROTOR ROTOR
US10815824B2 (en) * 2017-04-04 2020-10-27 General Electric Method and system for rotor overspeed protection
FR3113922B1 (en) 2020-09-08 2023-03-31 Safran Aircraft Engines Turbine brake
EP4006316A1 (en) 2020-11-27 2022-06-01 Rolls-Royce Deutschland Ltd & Co KG Shaft breakage protection system

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2050550A5 (en) * 1969-06-17 1971-04-02 Commissariat Energie Atomique Governor for turbine rotors
US4498291A (en) * 1982-10-06 1985-02-12 Rolls-Royce Limited Turbine overspeed limiter for turbomachines
EP0374003A1 (en) * 1988-12-15 1990-06-20 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Turbo machine with a braking device between rotor and exhaust sump
EP0928881A1 (en) * 1998-01-09 1999-07-14 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Turbomachine with concentric shafts which in case of a shaft rupture have a braking action on each other
US20060042226A1 (en) * 2004-08-27 2006-03-02 Ronald Trumper Gas turbine braking apparatus & method

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3490748A (en) * 1968-05-14 1970-01-20 Gen Motors Corp Fragmentation brake for turbines
JPS6213479A (en) * 1985-07-10 1987-01-22 Sumitomo Electric Ind Ltd Friction material
GB2199900B (en) * 1987-01-15 1991-06-19 Rolls Royce Plc A turbopropeller or turbofan gas turbine engine
DE19857552A1 (en) 1998-12-14 2000-06-15 Rolls Royce Deutschland Method for detecting a shaft break in a fluid flow machine
US6312215B1 (en) * 2000-02-15 2001-11-06 United Technologies Corporation Turbine engine windmilling brake
DE10218459B3 (en) * 2002-04-25 2004-01-15 Mtu Aero Engines Gmbh Multi-stage axial compressor
FR2875842B1 (en) 2004-09-28 2010-09-24 Snecma Moteurs DEVICE FOR LIMITING TURBINE OVERVIEW IN A TURBOMACHINE

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2050550A5 (en) * 1969-06-17 1971-04-02 Commissariat Energie Atomique Governor for turbine rotors
US4498291A (en) * 1982-10-06 1985-02-12 Rolls-Royce Limited Turbine overspeed limiter for turbomachines
EP0374003A1 (en) * 1988-12-15 1990-06-20 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Turbo machine with a braking device between rotor and exhaust sump
EP0928881A1 (en) * 1998-01-09 1999-07-14 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Turbomachine with concentric shafts which in case of a shaft rupture have a braking action on each other
US20060042226A1 (en) * 2004-08-27 2006-03-02 Ronald Trumper Gas turbine braking apparatus & method

Also Published As

Publication number Publication date
EP2071136B1 (en) 2018-07-25
US20090126336A1 (en) 2009-05-21
FR2916482A1 (en) 2008-11-28
US8161727B2 (en) 2012-04-24
FR2916482B1 (en) 2009-09-04
EP2071136A2 (en) 2009-06-17

Similar Documents

Publication Publication Date Title
EP2071136A3 (en) Braking device for a turbine in a gas turbine motor in the event of shaft breakage
FR2907495B1 (en) TURBOMACHINE
EP1930553A3 (en) Centrifugal compressor
EP1908635A3 (en) Vehicle outside mirror device
FR2928979A1 (en) DEVICE FOR CONTROLLING AUBES WITH VARIABLE TIMING IN A TURBOMACHINE.
FR2847086A1 (en) ROTARY ELECTRIC MACHINE FOR VEHICLE
FR3049025B1 (en) CLUTCH MECHANISM AND METHOD FOR ASSEMBLING SUCH A MECHANISM ON A TRANSMISSION CHAIN
UA89021C2 (en) Turbomachine with means for axial retention of the rotor
EP1880172B1 (en) Actuator for measurement indicators
US20080148833A1 (en) Sensing rotation of an engine component relative to an engine body using a starter ring
EP1741959A4 (en) MOUNTING STRUCTURE FOR ROTATING ELEMENT
FR2859323A1 (en) UNIVERSAL ACTUATOR, IN PARTICULAR FOR APPLICATION TO DASHBOARDS
FR2803954A1 (en) GEAR GEAR FOR FUNCTIONAL EQUIPMENT OF VEHICLES, PROVIDED WITH A MAGNETIC RING FOR MEASURING THE ROTATION SPEED OF ITS ARMATURE SHAFT
EP2577234A2 (en) Indicator device of an instrument panel with a complex planar movement
FR2831624A1 (en) Frangible coupling for aircraft turbofan drive shaft has annular array of shear bolts between bearing and carrier
WO2010043202A3 (en) Vacuum pump with a sealed accommodation of lubricant
FR3064134B1 (en) ELECTRICAL POWER COMPRESSOR WITH MAGNET HOLDER
EP3913779A1 (en) Gear motor comprising a stator with double diameter
FR2794196A1 (en) Measurement and continuous display of actuator rod position utilizes cable connected at end to rod and wound round rotating drum
FR3112319B1 (en) Protective device for an optical sensor and corresponding driving assistance system
FR3092354B1 (en) Electromechanical device for actuating a lock with vibratory decoupling
EP0467750A1 (en) Driving arm mounting arrangement, in particular for windshield wiper
FR3001782B1 (en) ACTUATOR AND CABIN SEAT COMPRISING SUCH ACTUATOR
EP1845546A3 (en) Bistable manoeuvring device of a mobile shaft and battery cutout comprising such a device
JP2005076463A5 (en)

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20080521

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MT NL NO PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA MK RS

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MT NL NO PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA MK RS

17Q First examination report despatched

Effective date: 20101014

AKX Designation fees paid

Designated state(s): DE FR GB

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: SNECMA

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: SAFRAN AIRCRAFT ENGINES

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

INTG Intention to grant announced

Effective date: 20180404

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): DE FR GB

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602008056125

Country of ref document: DE

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602008056125

Country of ref document: DE

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20190426

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20240419

Year of fee payment: 17

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20240418

Year of fee payment: 17

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20240418

Year of fee payment: 17