FR3096072B1 - Turbomachine comprising a variable viscance shaft bearing damper - Google Patents

Turbomachine comprising a variable viscance shaft bearing damper Download PDF

Info

Publication number
FR3096072B1
FR3096072B1 FR1905025A FR1905025A FR3096072B1 FR 3096072 B1 FR3096072 B1 FR 3096072B1 FR 1905025 A FR1905025 A FR 1905025A FR 1905025 A FR1905025 A FR 1905025A FR 3096072 B1 FR3096072 B1 FR 3096072B1
Authority
FR
France
Prior art keywords
bearing
variable
turbomachine
seal
viscance
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
FR1905025A
Other languages
French (fr)
Other versions
FR3096072A1 (en
Inventor
Julien Fabien Patrick Becoulet
Alexandre Jean-Marie Tan-Kim
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
Safran Aircraft Engines 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 Safran Aircraft Engines SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1905025A priority Critical patent/FR3096072B1/en
Publication of FR3096072A1 publication Critical patent/FR3096072A1/en
Application granted granted Critical
Publication of FR3096072B1 publication Critical patent/FR3096072B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/16Arrangement of bearings; Supporting or mounting bearings in casings
    • F01D25/162Bearing supports
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/16Arrangement of bearings; Supporting or mounting bearings in casings
    • F01D25/162Bearing supports
    • F01D25/164Flexible supports; Vibration damping means associated with the bearing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/18Lubricating arrangements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/60Assembly methods
    • F05D2230/64Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • F05D2230/644Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins for adjusting the position or the alignment, e.g. wedges or eccenters
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/50Bearings
    • F05D2240/53Hydrodynamic or hydrostatic bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/30Retaining components in desired mutual position
    • F05D2260/32Retaining components in desired mutual position by means of magnetic or electromagnetic forces

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Support Of The Bearing (AREA)

Abstract

Turbomachine (10) comportant un arbre rotatif (16), un palier (18) soutenant l’arbre rotatif (16), un support de palier (20) soutenant le palier (18), et une bague intermédiaire (24) disposée entre le palier (18) et le support de palier (20), la bague intermédiaire (24) étant configurée pour coulisser axialement par rapport au palier (18), un premier joint (36) couplé axialement avec le palier (18) et un deuxième joint (38) couplé axialement avec la bague intermédiaire (24), le premier joint (36), le deuxième joint (38), le palier (18) et la bague intermédiaire (24) définissant une chambre (40) à longueur axiale (L) variable et formant, lorsqu’elle est remplie d’huile, un amortisseur à raideur variable. Figure pour l’abrégé : Fig. 2.Turbomachine (10) comprising a rotating shaft (16), a bearing (18) supporting the rotating shaft (16), a bearing support (20) supporting the bearing (18), and an intermediate ring (24) disposed between the bearing (18) and the bearing support (20), the intermediate ring (24) being configured to slide axially relative to the bearing (18), a first seal (36) axially coupled with the bearing (18) and a second seal (38) axially coupled with the intermediate ring (24), the first seal (36), the second seal (38), the bearing (18) and the intermediate ring (24) defining an axial length chamber (40) (L ) variable and forming, when filled with oil, a variable stiffness damper. Figure for the abstract: Fig. 2.

FR1905025A 2019-05-14 2019-05-14 Turbomachine comprising a variable viscance shaft bearing damper Active FR3096072B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1905025A FR3096072B1 (en) 2019-05-14 2019-05-14 Turbomachine comprising a variable viscance shaft bearing damper

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1905025 2019-05-14
FR1905025A FR3096072B1 (en) 2019-05-14 2019-05-14 Turbomachine comprising a variable viscance shaft bearing damper

Publications (2)

Publication Number Publication Date
FR3096072A1 FR3096072A1 (en) 2020-11-20
FR3096072B1 true FR3096072B1 (en) 2021-04-30

Family

ID=68072623

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1905025A Active FR3096072B1 (en) 2019-05-14 2019-05-14 Turbomachine comprising a variable viscance shaft bearing damper

Country Status (1)

Country Link
FR (1) FR3096072B1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3120904B1 (en) * 2021-03-18 2023-03-24 Safran Aircraft Engines CENTERING AND GUIDE DEVICE FOR AN AIRCRAFT TURBOMACHINE SHAFT

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2629537B1 (en) 1988-03-30 1990-11-30 Snecma MULTI-BODY TURBOMACHINE INTER-SHAFT BEARING PROVIDED WITH A GAMING CONTROL DEVICE
FR2845138B1 (en) * 2002-10-01 2004-12-17 Snecma Moteurs BEARING BEARING AMORTIZED WITH OIL
US7574854B2 (en) * 2006-01-06 2009-08-18 General Electric Company Gas turbine engine assembly and methods of assembling same
FR2979681B1 (en) 2011-09-05 2014-05-16 Snecma TURBOMACHINE COMPRISING A FLUID FILM FOR DAMPING A TURBOMACHINE SHAFT GUIDE BEARING AND METHOD FOR ADJUSTING THE THICKNESS OF SUCH A DAMPING FLUID FILM

Also Published As

Publication number Publication date
FR3096072A1 (en) 2020-11-20

Similar Documents

Publication Publication Date Title
JP5297190B2 (en) Vacuum pump
FR3034460A1 (en) ROTOR AND ROTOR TURBOMACHINE ASSEMBLY AT VERY HIGH SPEEDS INCLUDING SUCH A ROTOR ASSEMBLY
RU2008107337A (en) BEARING DAMPING ELEMENT, BEARING AND GAS TURBINE ENGINE
JP6783534B2 (en) Radial bearing equipment and rotating machinery
JP2009257445A (en) Tilting pad thrust bearing
FR3096072B1 (en) Turbomachine comprising a variable viscance shaft bearing damper
JP2010121779A (en) Rolling bearing
FR3081185B1 (en) TURBOMACHINE STATOR ELEMENT
FR3094425B1 (en) Hydraulic machine with advanced bearing
FR2496169A1 (en) VISCOUS SHOCK ABSORBER WITH ROTOR CENTERING ELEMENT
WO2020085122A1 (en) Sliding member
FR3103096B1 (en) EXTENDED FLEXIBLE MEDICAL DEVICE SUPPORT ARTICULATED ARM
JPS5933426B2 (en) extrusion centrifuge
FR3098239B1 (en) Damping device for a rolling bearing, comprising a rigid support passing through a flexible cage
JP6949200B2 (en) Rotating machines and turbochargers
KR101710173B1 (en) High speed press with hydrostatic bearing
FR3120568B1 (en) Suspension stop provided with a ring for retaining a cover in relation to a support
FR3104206B1 (en) LUBRICATION ENCLOSURE FOR AN AIRCRAFT TURBOMACHINE
JP2009167805A (en) Crankshaft and lubricating device of internal combustion engine
JPH09317820A (en) Damper device for rotating machine
BE1027876B1 (en) TURBOMACHINE MODULE
FR3085752B1 (en) PROCESS FOR MEASURING CLEARANCE OF A TURBOCHARGER
FR3082907B1 (en) AIRCRAFT TURBOMACHINE HAVING PIVOT LINKS AT EACH END OF A SHAFT AND A SLIDING LINK BETWEEN SAID PIVOT LINKS
FR3096733B1 (en) Turbomachine kit
JP2019007541A (en) Trust bearing and turbocharger

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 2

PLSC Publication of the preliminary search report

Effective date: 20201120

PLFP Fee payment

Year of fee payment: 3

PLFP Fee payment

Year of fee payment: 4

PLFP Fee payment

Year of fee payment: 5

PLFP Fee payment

Year of fee payment: 6