GB201120338D0 - Abradable liner - Google Patents
Abradable linerInfo
- Publication number
- GB201120338D0 GB201120338D0 GBGB1120338.7A GB201120338A GB201120338D0 GB 201120338 D0 GB201120338 D0 GB 201120338D0 GB 201120338 A GB201120338 A GB 201120338A GB 201120338 D0 GB201120338 D0 GB 201120338D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- abradable liner
- abradable
- liner
- 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.)
- Withdrawn
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
- F01D5/12—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
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/522—Casings; Connections of working fluid for axial pumps especially adapted for elastic fluid pumps
- F04D29/526—Details of the casing section radially opposing blade tips
-
- 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
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/05—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
- F02K9/32—Constructional parts; Details not otherwise provided for
- F02K9/34—Casings; Combustion chambers; Liners thereof
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
- F02K9/32—Constructional parts; Details not otherwise provided for
- F02K9/34—Casings; Combustion chambers; Liners thereof
- F02K9/346—Liners, e.g. inhibitors
-
- 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
- F04D29/02—Selection of particular materials
- F04D29/023—Selection of particular materials especially adapted for elastic fluid pumps
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/20—Oxide or non-oxide ceramics
- F05D2300/22—Non-oxide ceramics
- F05D2300/224—Carbon, e.g. graphite
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/20—Oxide or non-oxide ceramics
- F05D2300/22—Non-oxide ceramics
- F05D2300/228—Nitrides
- F05D2300/2282—Nitrides of boron
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/20—Oxide or non-oxide ceramics
- F05D2300/22—Non-oxide ceramics
- F05D2300/229—Sulfides
- F05D2300/2291—Sulfides of molybdenum
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/40—Organic materials
- F05D2300/43—Synthetic polymers, e.g. plastics; Rubber
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/40—Organic materials
- F05D2300/43—Synthetic polymers, e.g. plastics; Rubber
- F05D2300/432—PTFE [PolyTetraFluorEthylene]
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/40—Organic materials
- F05D2300/44—Resins
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/50—Intrinsic material properties or characteristics
- F05D2300/509—Self lubricating materials; Solid lubricants
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1120338.7A GB2496887A (en) | 2011-11-25 | 2011-11-25 | Gas turbine engine abradable liner |
| PCT/EP2012/072228 WO2013075954A1 (en) | 2011-11-25 | 2012-11-09 | Abradable liner for a gas turbine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1120338.7A GB2496887A (en) | 2011-11-25 | 2011-11-25 | Gas turbine engine abradable liner |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| GB201120338D0 true GB201120338D0 (en) | 2012-01-04 |
| GB2496887A GB2496887A (en) | 2013-05-29 |
Family
ID=45475706
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1120338.7A Withdrawn GB2496887A (en) | 2011-11-25 | 2011-11-25 | Gas turbine engine abradable liner |
Country Status (2)
| Country | Link |
|---|---|
| GB (1) | GB2496887A (en) |
| WO (1) | WO2013075954A1 (en) |
Families Citing this family (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2951241A4 (en) * | 2013-01-29 | 2016-08-24 | United Technologies Corp | Blade rub material |
| DE102013223585A1 (en) | 2013-11-19 | 2015-06-03 | MTU Aero Engines AG | Inlet lining based on metal fibers |
| US9957819B2 (en) | 2014-03-28 | 2018-05-01 | United Technologies Corporation | Abrasive tip blade manufacture methods |
| GB201405704D0 (en) * | 2014-03-31 | 2014-05-14 | Rolls Royce Plc | Gas turbine engine |
| GB2525410B (en) * | 2014-04-24 | 2018-01-17 | Rolls Royce Plc | A boroscope and a method of processing a component within an assembled apparatus using a boroscope |
| JP2016102493A (en) * | 2014-11-17 | 2016-06-02 | 一夫 有▲吉▼ | Anti-bird strike net |
| US9950788B2 (en) * | 2015-07-14 | 2018-04-24 | Northrop Grumman Systems Corporation | Magrail, bleed air driven lift fan |
| US10670045B2 (en) | 2016-04-29 | 2020-06-02 | Raytheon Technologies Corporation | Abrasive blade tips with additive layer resistant to clogging |
| US10655492B2 (en) | 2016-04-29 | 2020-05-19 | United Technologies Corporation | Abrasive blade tips with additive resistant to clogging by organic matrix abradable |
| US10422242B2 (en) | 2016-04-29 | 2019-09-24 | United Technologies Corporation | Abrasive blade tips with additive resistant to clogging by organic matrix abradable |
| US10233938B2 (en) | 2016-04-29 | 2019-03-19 | United Technologies Corporation | Organic matrix abradable coating resistant to clogging of abrasive blade tips |
| CN116641910A (en) * | 2022-02-16 | 2023-08-25 | 中国航发商用航空发动机有限责任公司 | A fan contains casing and aero-engine |
| US11939871B1 (en) * | 2022-10-28 | 2024-03-26 | Rtx Corporation | Abradable material and design for jet engine applications |
| US12384139B2 (en) * | 2022-10-28 | 2025-08-12 | Rtx Corporation | Abradable material and design for jet engine applications |
Family Cites Families (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB791568A (en) * | 1956-03-26 | 1958-03-05 | Gen Motors Corp | Improvements in axial flow compressors |
| US4139376A (en) * | 1974-02-28 | 1979-02-13 | Brunswick Corporation | Abradable seal material and composition thereof |
| US4336276A (en) * | 1980-03-30 | 1982-06-22 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Fully plasma-sprayed compliant backed ceramic turbine seal |
| US5196471A (en) * | 1990-11-19 | 1993-03-23 | Sulzer Plasma Technik, Inc. | Thermal spray powders for abradable coatings, abradable coatings containing solid lubricants and methods of fabricating abradable coatings |
| US5304032A (en) * | 1991-07-22 | 1994-04-19 | Bosna Alexander A | Abradable non-metallic seal for rotating turbine engines |
| US5472315A (en) * | 1993-11-09 | 1995-12-05 | Sundstrand Corporation | Abradable coating in a gas turbine engine |
| US5704759A (en) * | 1996-10-21 | 1998-01-06 | Alliedsignal Inc. | Abrasive tip/abradable shroud system and method for gas turbine compressor clearance control |
| SG88799A1 (en) * | 1999-12-17 | 2002-05-21 | United Technologies Corp | Abradable seal having improved properties |
| US20010055652A1 (en) * | 1999-12-17 | 2001-12-27 | William John Dalzell | Method of making abradable seal having improved properties |
| EP1328574B1 (en) * | 2000-08-29 | 2018-04-11 | Andrew W. Suman | Abradable dry powder coatings, methods for making and coating, and coated articles therefrom |
| US6660405B2 (en) * | 2001-05-24 | 2003-12-09 | General Electric Co. | High temperature abradable coating for turbine shrouds without bucket tipping |
| US6887530B2 (en) * | 2002-06-07 | 2005-05-03 | Sulzer Metco (Canada) Inc. | Thermal spray compositions for abradable seals |
| US6969231B2 (en) * | 2002-12-31 | 2005-11-29 | General Electric Company | Rotary machine sealing assembly |
| DE10353810A1 (en) * | 2003-11-17 | 2005-06-23 | Rolls-Royce Deutschland Ltd & Co Kg | Inner cover tape for the stator blades of the compressor of a gas turbine |
| US20070134411A1 (en) * | 2005-12-14 | 2007-06-14 | General Electric Company | Method for making compositions containing microcapsules and compositions made thereof |
-
2011
- 2011-11-25 GB GB1120338.7A patent/GB2496887A/en not_active Withdrawn
-
2012
- 2012-11-09 WO PCT/EP2012/072228 patent/WO2013075954A1/en not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| GB2496887A (en) | 2013-05-29 |
| WO2013075954A1 (en) | 2013-05-30 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |