CA963497A - Powder metal honeycomb - Google Patents
Powder metal honeycombInfo
- Publication number
- CA963497A CA963497A CA122,379A CA122379A CA963497A CA 963497 A CA963497 A CA 963497A CA 122379 A CA122379 A CA 122379A CA 963497 A CA963497 A CA 963497A
- Authority
- CA
- Canada
- Prior art keywords
- powder metal
- metal honeycomb
- honeycomb
- powder
- metal
- 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.)
- Expired
Links
- 239000002184 metal Substances 0.000 title 1
- 239000000843 powder Substances 0.000 title 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/006—Pressing and sintering powders, granules or fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
- B22F7/06—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
-
- 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
- F01D11/125—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 with a reinforcing structure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D69/00—Friction linings; Attachment thereof; Selection of coacting friction substances or surfaces
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D69/00—Friction linings; Attachment thereof; Selection of coacting friction substances or surfaces
- F16D69/02—Composition of linings ; Methods of manufacturing
- F16D69/027—Compositions based on metals or inorganic oxides
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/02—Sealings between relatively-stationary surfaces
- F16J15/14—Sealings between relatively-stationary surfaces by means of granular or plastic material, or fluid
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
-
- 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
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/28—Three-dimensional patterned
- F05D2250/283—Three-dimensional patterned honeycomb
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D69/00—Friction linings; Attachment thereof; Selection of coacting friction substances or surfaces
- F16D2069/002—Combination of different friction materials
-
- 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)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Inorganic Chemistry (AREA)
- Composite Materials (AREA)
- Manufacturing & Machinery (AREA)
- Materials Engineering (AREA)
- Powder Metallurgy (AREA)
- Laminated Bodies (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10014070A | 1970-12-21 | 1970-12-21 |
Publications (1)
Publication Number | Publication Date |
---|---|
CA963497A true CA963497A (en) | 1975-02-25 |
Family
ID=22278288
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA122,379A Expired CA963497A (en) | 1970-12-21 | 1971-09-08 | Powder metal honeycomb |
Country Status (5)
Country | Link |
---|---|
JP (1) | JPS553402B1 (de) |
CA (1) | CA963497A (de) |
DE (1) | DE2163068C3 (de) |
FR (1) | FR2119460A5 (de) |
GB (1) | GB1361814A (de) |
Families Citing this family (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3964877A (en) * | 1975-08-22 | 1976-06-22 | General Electric Company | Porous high temperature seal abradable member |
US4150998A (en) * | 1976-12-09 | 1979-04-24 | General Electric Company | Rotary sealant abradable material and method for making |
FR2431896A1 (fr) * | 1978-07-25 | 1980-02-22 | Snecma | Procede pour la fabrication de pieces comportant au moins une partie en un materiau poreux susceptible d'etre use par abrasion |
DE8013163U1 (de) * | 1980-05-16 | 1988-10-13 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Gehäuse für eine thermische Turbomaschine mit einer wärmedämmenden Auskleidung |
GB2081817B (en) * | 1980-08-08 | 1984-02-15 | Rolls Royce | Turbine blade shrouding |
US4433845A (en) * | 1981-09-29 | 1984-02-28 | United Technologies Corporation | Insulated honeycomb seal |
DE3413534A1 (de) * | 1984-04-10 | 1985-10-24 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Gehaeuse einer stroemungsmaschine |
JPS6110092U (ja) * | 1984-06-20 | 1986-01-21 | ソニー株式会社 | モータの回転制御回路 |
FR2583493B1 (fr) * | 1985-06-14 | 1989-06-30 | Alsthom Atlantique | Produit alveole pour garniture d'etancheite de turbomachine |
DE4341216C2 (de) * | 1993-12-03 | 1997-01-16 | Mtu Muenchen Gmbh | Dichtungsbauteil für Spalt- oder Labyrinthdichtungen und Verfahren zu seiner Herstellung |
EP0661415A1 (de) * | 1993-12-17 | 1995-07-05 | Sulzer Innotec Ag | Einrichtung mit rotierfähigem Körper, Gehäuse und dazwischen liegendem Dichtspalt |
DE19945581B4 (de) | 1999-09-23 | 2014-04-03 | Alstom Technology Ltd. | Turbomaschine |
GB0008892D0 (en) | 2000-04-12 | 2000-05-31 | Rolls Royce Plc | Abradable seals |
DE10140742B4 (de) * | 2000-12-16 | 2015-02-12 | Alstom Technology Ltd. | Vorrichtung zur Dichtspaltreduzierung zwischen einer rotierenden und einer stationären Komponente innerhalb einer axial durchströmten Strömungsmaschine |
DE10259963B4 (de) * | 2002-12-20 | 2010-04-01 | Mtu Aero Engines Gmbh | Wabendichtung |
GB0304546D0 (en) * | 2003-02-27 | 2003-04-02 | Rolls Royce Plc | Abradable seals |
DE102004057360B4 (de) * | 2004-11-27 | 2007-11-29 | Mtu Aero Engines Gmbh | Verfahren zum Herstellen einer Wabendichtung |
DE102005040184B4 (de) * | 2005-08-25 | 2011-05-12 | Mtu Aero Engines Gmbh | Mantelringsegment einer Gasturbine und Verfahren zur Herstellung derselben |
DE102006009860A1 (de) * | 2006-03-03 | 2007-09-06 | Mtu Aero Engines Gmbh | Verfahren zur Herstellung eines Dichtsegments und Dichtsegment zur Verwendung in Verdichter- und Turbinenkomponenten |
US20080260523A1 (en) * | 2007-04-18 | 2008-10-23 | Ioannis Alvanos | Gas turbine engine with integrated abradable seal |
US20080260522A1 (en) * | 2007-04-18 | 2008-10-23 | Ioannis Alvanos | Gas turbine engine with integrated abradable seal and mount plate |
US20150354392A1 (en) * | 2014-06-10 | 2015-12-10 | General Electric Company | Abradable coatings |
US20150354393A1 (en) * | 2014-06-10 | 2015-12-10 | General Electric Company | Methods of manufacturing a shroud abradable coating |
FR3044946B1 (fr) | 2015-12-14 | 2018-01-12 | Safran Aircraft Engines | Revetement abradable a densite variable |
GB201614070D0 (en) * | 2016-08-17 | 2016-09-28 | Rolls Royce Plc | A component for a gas turbine engine and method of manufacture |
GB201916958D0 (en) * | 2019-11-21 | 2020-01-08 | Rolls Royce Plc | Abradable sealing element |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1527763A (fr) * | 1966-10-06 | 1968-06-07 | Hispano Suiza Lallemant Soc | Perfectionnements apportés aux dispositifs à disques de friction, notamment aux freins |
-
1971
- 1971-09-08 CA CA122,379A patent/CA963497A/en not_active Expired
- 1971-12-17 FR FR7145550A patent/FR2119460A5/fr not_active Expired
- 1971-12-17 GB GB5863671A patent/GB1361814A/en not_active Expired
- 1971-12-18 DE DE2163068A patent/DE2163068C3/de not_active Expired
- 1971-12-20 JP JP10406971A patent/JPS553402B1/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
GB1361814A (en) | 1974-07-30 |
DE2163068B2 (de) | 1980-04-10 |
JPS553402B1 (de) | 1980-01-25 |
DE2163068C3 (de) | 1980-12-04 |
DE2163068A1 (de) | 1972-07-13 |
FR2119460A5 (de) | 1972-08-04 |
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