FR3016392B1 - Procede d'identification de la configuration d'equilibrage installee sur un rotor de turbomachine - Google Patents

Procede d'identification de la configuration d'equilibrage installee sur un rotor de turbomachine

Info

Publication number
FR3016392B1
FR3016392B1 FR1450250A FR1450250A FR3016392B1 FR 3016392 B1 FR3016392 B1 FR 3016392B1 FR 1450250 A FR1450250 A FR 1450250A FR 1450250 A FR1450250 A FR 1450250A FR 3016392 B1 FR3016392 B1 FR 3016392B1
Authority
FR
France
Prior art keywords
identifying
turbomachine rotor
balancing configuration
configuration installed
balancing
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
FR1450250A
Other languages
English (en)
Other versions
FR3016392A1 (fr
Inventor
Valerio Gerez
Francois Prost
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 FR1450250A priority Critical patent/FR3016392B1/fr
Priority to GB1612315.0A priority patent/GB2536592B/en
Priority to US15/111,414 priority patent/US10598017B2/en
Priority to PCT/FR2015/050007 priority patent/WO2015104488A1/fr
Publication of FR3016392A1 publication Critical patent/FR3016392A1/fr
Application granted granted Critical
Publication of FR3016392B1 publication Critical patent/FR3016392B1/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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/027—Arrangements for balancing
    • 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
    • F05D2230/72—Maintenance
    • 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
    • F05D2240/00—Components
    • F05D2240/20—Rotors
    • F05D2240/24—Rotors for turbines
    • 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
    • F05D2270/00—Control
    • F05D2270/80—Devices generating input signals, e.g. transducers, sensors, cameras or strain gauges
    • F05D2270/804—Optical devices
    • F05D2270/8041—Cameras

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Testing Of Balance (AREA)
FR1450250A 2014-01-13 2014-01-13 Procede d'identification de la configuration d'equilibrage installee sur un rotor de turbomachine Active FR3016392B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR1450250A FR3016392B1 (fr) 2014-01-13 2014-01-13 Procede d'identification de la configuration d'equilibrage installee sur un rotor de turbomachine
GB1612315.0A GB2536592B (en) 2014-01-13 2015-01-05 Method for identifying the balancing configuration installed on a turbomachine rotor
US15/111,414 US10598017B2 (en) 2014-01-13 2015-01-05 Method of identifying the balancing configuration installed on a turbine engine rotor
PCT/FR2015/050007 WO2015104488A1 (fr) 2014-01-13 2015-01-05 Procede d'identification de la configuration d'equilibrage installee sur un rotor de turbomachine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1450250A FR3016392B1 (fr) 2014-01-13 2014-01-13 Procede d'identification de la configuration d'equilibrage installee sur un rotor de turbomachine

Publications (2)

Publication Number Publication Date
FR3016392A1 FR3016392A1 (fr) 2015-07-17
FR3016392B1 true FR3016392B1 (fr) 2016-02-05

Family

ID=50483122

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1450250A Active FR3016392B1 (fr) 2014-01-13 2014-01-13 Procede d'identification de la configuration d'equilibrage installee sur un rotor de turbomachine

Country Status (4)

Country Link
US (1) US10598017B2 (fr)
FR (1) FR3016392B1 (fr)
GB (1) GB2536592B (fr)
WO (1) WO2015104488A1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11732585B2 (en) 2021-01-28 2023-08-22 General Electric Company Trapped rotatable weights to improve rotor balance
US20230349297A1 (en) * 2022-04-29 2023-11-02 Pratt & Whitney Canada Corp. Method of manufacturing a mistuned rotor

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1261830A (fr) 1960-07-07 1961-05-19 Wilfley & Sons Inc A Procédé de centrage de l'enveloppe des pompes centrifuges
US7303377B2 (en) * 2004-04-14 2007-12-04 Pratt & Whitney Canada Corp. Apparatus and method of balancing a shaft
US7957851B2 (en) * 2005-05-09 2011-06-07 American Airlines, Inc. System and method for utilization of transmitted digital flight data acquisition information to accomplish vibration balance solutions
GB0514149D0 (en) * 2005-07-09 2005-08-17 Rolls Royce Plc In-situ component monitoring
US20070110543A1 (en) * 2005-11-12 2007-05-17 Christopher Milton Fitch Tail-driven screw fastener for use in tamper-resistant and decorative applications
US7412898B1 (en) * 2006-07-28 2008-08-19 Disney Enterprises, Inc. Load sensing system including RFID tagged fasteners
FR2920187B1 (fr) * 2007-08-24 2014-07-04 Snecma Soufflante pour turbomachine d'aeronef comprenant une bride d'equilibrage masqueee par le cone d'entree.
US8434216B2 (en) * 2008-01-08 2013-05-07 General Electric Company Methods and systems for in-situ machine maintenance
FR2939470B1 (fr) * 2008-12-10 2011-01-07 Snecma Soufflante pour turbomachine comprenant un systeme d'equilibrage a trous borgnes de logement de masses
US8322991B2 (en) * 2009-04-10 2012-12-04 Rolls-Royce Corporation Balance weight
GB0908502D0 (en) * 2009-05-19 2009-06-24 Rolls Royce Plc A balanced rotor for a turbine engine
FR2977029B1 (fr) * 2011-06-22 2013-07-12 Airbus Operations Sas Procede d'equilibrage pour systeme propulsif a helices contrarotatives non carenees
GB201210870D0 (en) * 2012-06-20 2012-08-01 Rolls Royce Plc Rotor balancing method
FR2999227B1 (fr) * 2012-12-10 2015-02-06 Snecma Procede d'equilibrage d'un rotor de turbomachine et rotor equilibre par un tel procede
FR3001291B1 (fr) * 2013-01-18 2015-02-27 Snecma Dispositif d'equilibrage moteur pour capot d'entree de turbomachine
US9016560B2 (en) * 2013-04-15 2015-04-28 General Electric Company Component identification system
US10030534B2 (en) * 2016-02-24 2018-07-24 General Electric Company Detectable datum markers for gas turbine engine components for measuring distortion

Also Published As

Publication number Publication date
FR3016392A1 (fr) 2015-07-17
US10598017B2 (en) 2020-03-24
WO2015104488A1 (fr) 2015-07-16
GB201612315D0 (en) 2016-08-31
GB2536592B (en) 2020-07-01
GB2536592A (en) 2016-09-21
US20160333695A1 (en) 2016-11-17

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