FR3117390B1 - TOOLS FOR MACHINING AN ABRADABLE ANNULAR LAYER OF A FAN CASING OF AN AIRCRAFT TURBOMACHINE AND METHOD FOR MACHINING USING SUCH TOOLS - Google Patents
TOOLS FOR MACHINING AN ABRADABLE ANNULAR LAYER OF A FAN CASING OF AN AIRCRAFT TURBOMACHINE AND METHOD FOR MACHINING USING SUCH TOOLS Download PDFInfo
- Publication number
- FR3117390B1 FR3117390B1 FR2013066A FR2013066A FR3117390B1 FR 3117390 B1 FR3117390 B1 FR 3117390B1 FR 2013066 A FR2013066 A FR 2013066A FR 2013066 A FR2013066 A FR 2013066A FR 3117390 B1 FR3117390 B1 FR 3117390B1
- Authority
- FR
- France
- Prior art keywords
- machining
- tools
- annular layer
- aircraft turbomachine
- tool
- 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
- 238000003754 machining Methods 0.000 title abstract 6
- 238000000034 method Methods 0.000 title abstract 2
Classifications
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- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23B—TURNING; BORING
- B23B3/00—General-purpose turning-machines or devices, e.g. centre lathes with feed rod and lead screw; Sets of turning-machines
- B23B3/22—Turning-machines or devices with rotary tool heads
- B23B3/26—Turning-machines or devices with rotary tool heads the tools of which perform a radial movement; Rotary tool heads thereof
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23C—MILLING
- B23C3/00—Milling particular work; Special milling operations; Machines therefor
- B23C3/02—Milling surfaces of revolution
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23Q—DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
- B23Q9/00—Arrangements for supporting or guiding portable metal-working machines or apparatus
- B23Q9/0014—Portable machines provided with or cooperating with guide means supported directly by the workpiece during action
- B23Q9/0042—Portable machines provided with or cooperating with guide means supported directly by the workpiece during action the guide means being fixed only on the workpiece
- B23Q9/0057—Portable machines provided with or cooperating with guide means supported directly by the workpiece during action the guide means being fixed only on the workpiece and being capable of guiding the tool in a circular path
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B24—GRINDING; POLISHING
- B24B—MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
- B24B19/00—Single-purpose machines or devices for particular grinding operations not covered by any other main group
- B24B19/26—Single-purpose machines or devices for particular grinding operations not covered by any other main group for grinding workpieces with arcuate surfaces, e.g. parts of car bodies, bumpers or magnetic recording heads
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B24—GRINDING; POLISHING
- B24B—MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
- B24B23/00—Portable grinding machines, e.g. hand-guided; Accessories therefor
- B24B23/08—Portable grinding machines designed for fastening on workpieces or other parts of particular section, e.g. for grinding commutators
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- 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
- F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
- F01D25/285—Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such structures
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23B—TURNING; BORING
- B23B2215/00—Details of workpieces
- B23B2215/76—Components for turbines
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23C—MILLING
- B23C2215/00—Details of workpieces
- B23C2215/04—Aircraft components
-
- 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
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- 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
- F05D2230/10—Manufacture by removing material
- F05D2230/14—Micromachining
-
- 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)
- Drilling And Boring (AREA)
Abstract
L’invention concerne un outillage (20) d’usinage d’une couche annulaire abradable (10b) d’un carter (3) de soufflante (1) d’une turbomachine d’aéronef, cet outillage (20) étant configuré pour être au moins en partie logé dans ledit carter (3) et comportant un corps central (30) de centrage et de fixation sur un disque (2) de soufflante de la turbomachine, un outil de mesure (40), un outil (50) d’usinage, et un premier moteur (52) d’entraînement en rotation de l’outil d’usinage. L’invention concerne aussi un procédé d’usinage d’une couche annulaire abradable (10b) d’un carter (3) de soufflante (1) d’une turbomachine d’aéronef, au moyen d’un tel outillage (20). Figure pour l'abrégé : Fig. 6The invention relates to a tool (20) for machining an abradable annular layer (10b) of a casing (3) of a fan (1) of an aircraft turbomachine, this tool (20) being configured to be at least partly housed in said casing (3) and comprising: a central body (30) for centering and fixing on a fan disk (2) of the turbomachine, a measuring tool (40), a tool (50) d machining, and a first motor (52) for rotating the machining tool. The invention also relates to a method for machining an abradable annular layer (10b) of a casing (3) of a fan (1) of an aircraft turbomachine, by means of such tooling (20). Figure for abstract: Fig. 6
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2013066A FR3117390B1 (en) | 2020-12-11 | 2020-12-11 | TOOLS FOR MACHINING AN ABRADABLE ANNULAR LAYER OF A FAN CASING OF AN AIRCRAFT TURBOMACHINE AND METHOD FOR MACHINING USING SUCH TOOLS |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2013066 | 2020-12-11 | ||
FR2013066A FR3117390B1 (en) | 2020-12-11 | 2020-12-11 | TOOLS FOR MACHINING AN ABRADABLE ANNULAR LAYER OF A FAN CASING OF AN AIRCRAFT TURBOMACHINE AND METHOD FOR MACHINING USING SUCH TOOLS |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3117390A1 FR3117390A1 (en) | 2022-06-17 |
FR3117390B1 true FR3117390B1 (en) | 2024-01-19 |
Family
ID=74669047
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR2013066A Active FR3117390B1 (en) | 2020-12-11 | 2020-12-11 | TOOLS FOR MACHINING AN ABRADABLE ANNULAR LAYER OF A FAN CASING OF AN AIRCRAFT TURBOMACHINE AND METHOD FOR MACHINING USING SUCH TOOLS |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR3117390B1 (en) |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2240735A (en) * | 1990-02-13 | 1991-08-14 | Rolls Royce Plc | Portable machine tool |
US8888418B2 (en) * | 2006-10-19 | 2014-11-18 | United Technologies Corporation | Fan rub strip in situ machining system and method |
GB201419695D0 (en) * | 2014-11-05 | 2014-12-17 | Rolls Royce Plc | Machining Tool |
US10815783B2 (en) * | 2018-05-24 | 2020-10-27 | General Electric Company | In situ engine component repair |
US11338461B2 (en) * | 2019-04-26 | 2022-05-24 | General Electric Company | System for machining the abradable material of a turbofan engine |
-
2020
- 2020-12-11 FR FR2013066A patent/FR3117390B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR3117390A1 (en) | 2022-06-17 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 2 |
|
PLSC | Publication of the preliminary search report |
Effective date: 20220617 |
|
PLFP | Fee payment |
Year of fee payment: 3 |
|
PLFP | Fee payment |
Year of fee payment: 4 |