FR2960463B1 - Procede de reparation d'une bride d'un carter - Google Patents
Procede de reparation d'une bride d'un carterInfo
- Publication number
- FR2960463B1 FR2960463B1 FR1054260A FR1054260A FR2960463B1 FR 2960463 B1 FR2960463 B1 FR 2960463B1 FR 1054260 A FR1054260 A FR 1054260A FR 1054260 A FR1054260 A FR 1054260A FR 2960463 B1 FR2960463 B1 FR 2960463B1
- Authority
- FR
- France
- Prior art keywords
- flange
- face
- repairing
- hole
- worn
- 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
Links
- 238000000034 method Methods 0.000 title abstract 3
- 238000004026 adhesive bonding Methods 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P6/00—Restoring or reconditioning objects
- B23P6/002—Repairing turbine components, e.g. moving or stationary blades, rotors
- B23P6/005—Repairing turbine components, e.g. moving or stationary blades, rotors using only replacement pieces of a particular form
-
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
- F01D25/243—Flange connections; Bolting arrangements
-
- 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
- F01D5/005—Repairing methods or devices
-
- 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
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49229—Prime mover or fluid pump making
- Y10T29/49231—I.C. [internal combustion] engine making
- Y10T29/49233—Repairing, converting, servicing or salvaging
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/49318—Repairing or disassembling
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49718—Repairing
- Y10T29/49721—Repairing with disassembling
- Y10T29/49723—Repairing with disassembling including reconditioning of part
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49718—Repairing
- Y10T29/49732—Repairing by attaching repair preform, e.g., remaking, restoring, or patching
- Y10T29/49734—Repairing by attaching repair preform, e.g., remaking, restoring, or patching and removing damaged material
- Y10T29/49735—Mechanically attaching preform with separate fastener
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Mounting Of Bearings Or Others (AREA)
Abstract
L'invention concerne un procédé de réparation d'une bride de carter pour un turboréacteur ou un turbopropulseur d'avion, la bride (1) comportant au moins un trou de passage (4) d'une vis de fixation d'un équipement, débouchant sur une face de la bride (1) usée par frottement de l'équipement. Le procédé consiste à monter sur la bride (1) un organe d'appui (7) comportant une paroi (13) radiale recouvrant la face usée de la bride (1), cette paroi (13) comprenant un trou venant en regard du trou (4) de la bride (1) et ayant une épaisseur destinée à compenser l'usure de la face de la bride (1), ledit organe (7) comportant en outre une butée (16, 17) d'appui sur la périphérie de la bride (1) et étant fixé sur la bride par collage.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1054260A FR2960463B1 (fr) | 2010-06-01 | 2010-06-01 | Procede de reparation d'une bride d'un carter |
US13/149,133 US8734103B2 (en) | 2010-06-01 | 2011-05-31 | Method of repairing a flange of a casing |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1054260A FR2960463B1 (fr) | 2010-06-01 | 2010-06-01 | Procede de reparation d'une bride d'un carter |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2960463A1 FR2960463A1 (fr) | 2011-12-02 |
FR2960463B1 true FR2960463B1 (fr) | 2013-03-29 |
Family
ID=43302173
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1054260A Active FR2960463B1 (fr) | 2010-06-01 | 2010-06-01 | Procede de reparation d'une bride d'un carter |
Country Status (2)
Country | Link |
---|---|
US (1) | US8734103B2 (fr) |
FR (1) | FR2960463B1 (fr) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20130051990A1 (en) * | 2011-08-29 | 2013-02-28 | Leonard Paul Palmisano | Bushing to repair circumferential flanged ring |
US10233780B2 (en) | 2013-07-11 | 2019-03-19 | United Technologies Corporation | Flange partial section replacement repair |
FR3054800B1 (fr) * | 2016-08-05 | 2019-05-17 | Safran Aircraft Engines | Procede de reparation d'une aube de turbomachine et ensemble obtenu par ce procede |
CN111571113B (zh) * | 2020-05-28 | 2021-05-18 | 三一重机有限公司 | 轴瓦座修复方法 |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB8904988D0 (en) * | 1989-03-04 | 1989-04-19 | Refurbished Turbine Components | Turbine blade repair |
US5203066A (en) * | 1991-10-18 | 1993-04-20 | Svedala, Inc. | Method of repairing large rotating machines in which parts are bolted together through radially extending flanges |
US7858897B2 (en) | 2006-10-27 | 2010-12-28 | United Technologies Corporation | Insert weld repair |
US7722318B2 (en) | 2007-02-13 | 2010-05-25 | United Technologies Corporation | Hole liners for repair of vane counterbore holes |
US9643286B2 (en) * | 2007-04-05 | 2017-05-09 | United Technologies Corporation | Method of repairing a turbine engine component |
-
2010
- 2010-06-01 FR FR1054260A patent/FR2960463B1/fr active Active
-
2011
- 2011-05-31 US US13/149,133 patent/US8734103B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
US8734103B2 (en) | 2014-05-27 |
US20110293409A1 (en) | 2011-12-01 |
FR2960463A1 (fr) | 2011-12-02 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 7 |
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PLFP | Fee payment |
Year of fee payment: 8 |
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CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170707 |
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PLFP | Fee payment |
Year of fee payment: 9 |
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PLFP | Fee payment |
Year of fee payment: 10 |
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PLFP | Fee payment |
Year of fee payment: 11 |
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PLFP | Fee payment |
Year of fee payment: 12 |
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PLFP | Fee payment |
Year of fee payment: 13 |
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PLFP | Fee payment |
Year of fee payment: 14 |
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PLFP | Fee payment |
Year of fee payment: 15 |