CA2766534C - Pale de rotor et procede de reduction de la charge de friction des extremites - Google Patents

Pale de rotor et procede de reduction de la charge de friction des extremites Download PDF

Info

Publication number: CA2766534C
Authority: CA; Canada
Prior art keywords: tip; airfoil; cutter; leading edge; blade
Prior art date: 2009-06-30
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.): Expired - Fee Related

Application number

CA2766534A

Other languages

English (en)

Other versions

CA2766534A1 (fr

Inventor

Nicholas Joseph Kray

David W. Crall

Daniel E. Mollmann

Donald Lee Gardner

Marcia Boyle Johnson

Howard P. Weaver

Max Robert Farson

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.)

General Electric Co

Original Assignee

General Electric Co

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.)

2009-06-30

Filing date

2010-06-02

Publication date

2017-12-12

2009-06-30 Priority claimed from US12/494,610 external-priority patent/US8662834B2/en

2009-06-30 Priority claimed from US12/494,595 external-priority patent/US8657570B2/en

2010-06-02 Application filed by General Electric Co filed Critical General Electric Co

2011-01-06 Publication of CA2766534A1 publication Critical patent/CA2766534A1/fr

2017-12-12 Application granted granted Critical

2017-12-12 Publication of CA2766534C publication Critical patent/CA2766534C/fr

Status Expired - Fee Related legal-status Critical Current

2030-06-02 Anticipated expiration legal-status Critical

Links

238000000034 method Methods 0.000 title claims abstract description 49
239000000463 material Substances 0.000 claims abstract description 75
230000003068 static effect Effects 0.000 claims abstract description 10
238000003754 machining Methods 0.000 claims description 10
238000005219 brazing Methods 0.000 claims description 7
229910052751 metal Inorganic materials 0.000 claims description 7
239000002184 metal Substances 0.000 claims description 7
230000008878 coupling Effects 0.000 claims description 4
238000010168 coupling process Methods 0.000 claims description 4
238000005859 coupling reaction Methods 0.000 claims description 4
239000011888 foil Substances 0.000 abstract 1
239000007789 gas Substances 0.000 description 14
239000003082 abrasive agent Substances 0.000 description 8
239000000567 combustion gas Substances 0.000 description 3
239000000203 mixture Substances 0.000 description 3
239000007787 solid Substances 0.000 description 3
238000003466 welding Methods 0.000 description 3
RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 2
239000000853 adhesive Substances 0.000 description 2
230000001070 adhesive effect Effects 0.000 description 2
230000000712 assembly Effects 0.000 description 2
238000000429 assembly Methods 0.000 description 2
239000000919 ceramic Substances 0.000 description 2
239000003795 chemical substances by application Substances 0.000 description 2
238000005336 cracking Methods 0.000 description 2
238000005520 cutting process Methods 0.000 description 2
229910003460 diamond Inorganic materials 0.000 description 2
239000010432 diamond Substances 0.000 description 2
230000001788 irregular Effects 0.000 description 2
238000004519 manufacturing process Methods 0.000 description 2
TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 2
239000002245 particle Substances 0.000 description 2
HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 2
229910010271 silicon carbide Inorganic materials 0.000 description 2
239000007921 spray Substances 0.000 description 2
239000010936 titanium Substances 0.000 description 2
229910052719 titanium Inorganic materials 0.000 description 2
241001508687 Mustela erminea Species 0.000 description 1
229910001069 Ti alloy Inorganic materials 0.000 description 1
238000004026 adhesive bonding Methods 0.000 description 1
229910045601 alloy Inorganic materials 0.000 description 1
239000000956 alloy Substances 0.000 description 1
239000002131 composite material Substances 0.000 description 1
239000000284 extract Substances 0.000 description 1
239000000446 fuel Substances 0.000 description 1
239000007769 metal material Substances 0.000 description 1
230000004048 modification Effects 0.000 description 1
238000012986 modification Methods 0.000 description 1
230000002265 prevention Effects 0.000 description 1
230000001052 transient effect Effects 0.000 description 1

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
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/20—Specially-shaped blade tips to seal space between tips and stator
- 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
- F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
- F01D11/122—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with erodable or abradable material
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/08—Sealings
- F04D29/16—Sealings between pressure and suction sides
- F04D29/161—Sealings between pressure and suction sides especially adapted for elastic fluid pumps
- F04D29/164—Sealings between pressure and suction sides especially adapted for elastic fluid pumps of an axial flow wheel
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
- F04D29/324—Blades
- 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
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/36—Application in turbines specially adapted for the fan of turbofan engines
- 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)

CA2766534A 2009-06-30 2010-06-02 Pale de rotor et procede de reduction de la charge de friction des extremites Expired - Fee Related CA2766534C (fr)

Applications Claiming Priority (5)

Application Number	Priority Date	Filing Date	Title
US12/494,610 US8662834B2 (en)	2009-06-30	2009-06-30	Method for reducing tip rub loading
US12/494,595 US8657570B2 (en)	2009-06-30	2009-06-30	Rotor blade with reduced rub loading
US12/494,595		2009-06-30
US12/494,610		2009-06-30
PCT/US2010/036996 WO2011002570A1 (fr)	2009-06-30	2010-06-02	Pale de rotor et procédé de réduction de la charge de friction des extrémités

Publications (2)

Publication Number	Publication Date
CA2766534A1 CA2766534A1 (fr)	2011-01-06
CA2766534C true CA2766534C (fr)	2017-12-12

Family

ID=42543343

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
CA2766534A Expired - Fee Related CA2766534C (fr)	2009-06-30	2010-06-02	Pale de rotor et procede de reduction de la charge de friction des extremites

Country Status (4)

Country	Link
EP (1)	EP2449216A1 (fr)
JP (1)	JP5628307B2 (fr)
CA (1)	CA2766534C (fr)
WO (1)	WO2011002570A1 (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US10221698B2 (en)	2014-02-14	2019-03-05	United Technologies Corporation	Polymer-coated blade with abrasive tip
DE102014212652A1 (de)	2014-06-30	2016-01-14	MTU Aero Engines AG	Strömungsmaschine
US10060273B2 (en)	2015-04-15	2018-08-28	United Technologies Corporation	System and method for manufacture of abrasive coating
US10794394B2 (en)	2015-04-15	2020-10-06	Raytheon Technologies Corporation	Abrasive tip for composite fan blades
US11268183B2 (en)	2015-05-06	2022-03-08	Raytheon Technologies Corporation	Method of forming an abrasive coating on a fan blade tip
GB201900961D0 (en)	2019-01-24	2019-03-13	Rolls Royce Plc	Fan blade
IT202000003853A1 (it) *	2020-02-25	2021-08-25	Nobili S P A	Apparecchiatura, in particolare un atomizzatore, per cospargere un fluido, o liquido, di trattamento

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US3096930A (en) *	1961-06-26	1963-07-09	Meyerhoff Leonard	Propeller design
FR2615254A1 (fr) *	1987-05-13	1988-11-18	Snecma	Aube mobile de soufflante comportant une depouille en extremite
US4884820A (en) *	1987-05-19	1989-12-05	Union Carbide Corporation	Wear resistant, abrasive laser-engraved ceramic or metallic carbide surfaces for rotary labyrinth seal members
US5275531A (en) *	1993-04-30	1994-01-04	Teleflex, Incorporated	Area ruled fan blade ends for turbofan jet engine
US5476363A (en) *	1993-10-15	1995-12-19	Charles E. Sohl	Method and apparatus for reducing stress on the tips of turbine or compressor blades
GB9325135D0 (en) *	1993-12-08	1994-02-09	Rolls Royce Plc	Manufacture of wear resistant components
US5456576A (en) *	1994-08-31	1995-10-10	United Technologies Corporation	Dynamic control of tip clearance
IL120137A0 (en) *	1997-02-03	1997-06-10	Iscar Ltd	Cutting insert
US6338609B1 (en) *	2000-02-18	2002-01-15	General Electric Company	Convex compressor casing
EP1391537B1 (fr) *	2001-05-31	2012-02-22	Mitsubishi Heavy Industries, Ltd.	Procede et materiau de formage de revetement, et feuille de formage de revetement abrasif
US6843928B2 (en) *	2001-10-12	2005-01-18	General Electric Company	Method for removing metal cladding from airfoil substrate
GB0216952D0 (en) *	2002-07-20	2002-08-28	Rolls Royce Plc	Gas turbine engine casing and rotor blade arrangement
EP1820938A1 (fr) *	2006-02-20	2007-08-22	ABB Turbo Systems AG	Eléments de nettoyage sur les extrémités des aubes d' une turbine
JP4830812B2 (ja) *	2006-11-24	2011-12-07	株式会社Ｉｈｉ	圧縮機動翼
US8172518B2 (en) *	2006-12-29	2012-05-08	General Electric Company	Methods and apparatus for fabricating a rotor assembly

2010
- 2010-06-02 JP JP2012517542A patent/JP5628307B2/ja not_active Expired - Fee Related
- 2010-06-02 WO PCT/US2010/036996 patent/WO2011002570A1/fr not_active Ceased
- 2010-06-02 EP EP10727571A patent/EP2449216A1/fr not_active Withdrawn
- 2010-06-02 CA CA2766534A patent/CA2766534C/fr not_active Expired - Fee Related

Also Published As

Publication number	Publication date
JP2012532268A (ja)	2012-12-13
EP2449216A1 (fr)	2012-05-09
JP5628307B2 (ja)	2014-11-19
WO2011002570A1 (fr)	2011-01-06
CA2766534A1 (fr)	2011-01-06

Legal Events

Date	Code	Title	Description
2015-04-15	EEER	Examination request	Effective date: 20150327
2019-07-15	MKLA	Lapsed	Effective date: 20190603

Publication	Publication Date	Title
US8657570B2 (en)	2014-02-25	Rotor blade with reduced rub loading
US8662834B2 (en)	2014-03-04	Method for reducing tip rub loading
US7780410B2 (en)	2010-08-24	Method and apparatus for gas turbine engines
JP3948926B2 (ja)	2007-07-25	ロータ組立体の円周方向リム応力を減少させる方法及び装置
CA2615625C (fr)	2015-12-01	Methodes et appareillage de fabrication d'un rotor
CA2766534C (fr)	2017-12-12	Pale de rotor et procede de reduction de la charge de friction des extremites
US7887299B2 (en)	2011-02-15	Rotary body for turbo machinery with mistuned blades
JP5450997B2 (ja)	2014-03-26	ロータブレード
US20120021243A1 (en)	2012-01-26	Components with bonded edges
CA2880602C (fr)	2022-05-31	Aube renforcee pour une turbine a gaz
EP1965025A2 (fr)	2008-09-03	Aube de turbine
US20080292466A1 (en)	2008-11-27	Method to center locate cutter teeth on shrouded turbine blades
EP4130430B1 (fr)	2025-05-14	Rotor à aubage intégral
US20200157953A1 (en)	2020-05-21	Composite fan blade with abrasive tip
US20060280610A1 (en)	2006-12-14	Turbine blade and method of fabricating same
EP3095959A1 (fr)	2016-11-23	Procédé de conception et de fabrication de pale de rotor
US12385400B2 (en)	2025-08-12	Method of manufacturing a mistuned rotor
WO2014096840A1 (fr)	2014-06-26	Structure de profil aérodynamique ayant des bords de coupe de partie pointe
US20260103987A1 (en)	2026-04-16	Turbine engine with a blade assembly having a dovetail
US20260103988A1 (en)	2026-04-16	Turbine engine with a blade assembly having a dovetail
US20260103989A1 (en)	2026-04-16	Turbine engine with a blade assembly having a dovetail