GB201002250D0 - Compressor casing - Google Patents
Compressor casingInfo
- Publication number
- GB201002250D0 GB201002250D0 GBGB1002250.7A GB201002250A GB201002250D0 GB 201002250 D0 GB201002250 D0 GB 201002250D0 GB 201002250 A GB201002250 A GB 201002250A GB 201002250 D0 GB201002250 D0 GB 201002250D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- compressor casing
- compressor
- casing
- 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- Withdrawn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
- 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
- F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
-
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/02—Surge control
-
- 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
-
- 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
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/68—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers
- F04D29/681—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps
- F04D29/685—Inducing localised fluid recirculation in the stator-rotor interface
-
- 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
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/14—Casings or housings protecting or supporting assemblies within
-
- 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
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
- F05D2270/10—Purpose of the control system to cope with, or avoid, compressor flow instabilities
- F05D2270/101—Compressor surge or stall
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1002250A GB2477745A (en) | 2010-02-11 | 2010-02-11 | Compressor Casing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1002250A GB2477745A (en) | 2010-02-11 | 2010-02-11 | Compressor Casing |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| GB201002250D0 true GB201002250D0 (en) | 2010-03-31 |
| GB2477745A GB2477745A (en) | 2011-08-17 |
Family
ID=42110513
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1002250A Withdrawn GB2477745A (en) | 2010-02-11 | 2010-02-11 | Compressor Casing |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB2477745A (en) |
Families Citing this family (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2607715B1 (en) * | 2011-12-22 | 2017-03-29 | MTU Aero Engines GmbH | Housing for a bladed rotor of a flow engine |
| US20160153465A1 (en) * | 2014-12-01 | 2016-06-02 | General Electric Company | Axial compressor endwall treatment for controlling leakage flow therein |
| DE102018116062A1 (en) * | 2018-07-03 | 2020-01-09 | Rolls-Royce Deutschland Ltd & Co Kg | Structure assembly for a compressor of a turbomachine |
| US10914318B2 (en) | 2019-01-10 | 2021-02-09 | General Electric Company | Engine casing treatment for reducing circumferentially variable distortion |
| US12258870B1 (en) | 2024-03-08 | 2025-03-25 | Rolls-Royce North American Technologies Inc. | Adjustable fan track liner with slotted array active fan tip treatment for distortion tolerance |
| US12215712B1 (en) | 2024-05-09 | 2025-02-04 | Rolls-Royce North American Technologies Inc. | Adjustable fan track liner with dual grooved array active fan tip treatment for distortion tolerance |
| US12209541B1 (en) | 2024-05-09 | 2025-01-28 | Rolls-Royce North American Technologies Inc. | Adjustable fan track liner with dual slotted array active fan tip treatment for distortion tolerance |
| US12286936B1 (en) | 2024-05-09 | 2025-04-29 | Rolls-Royce North American Technologies Inc. | Adjustable fan track liner with groove array active fan tip treatment for distortion tolerance |
| US12168983B1 (en) | 2024-06-28 | 2024-12-17 | Rolls-Royce North American Technologies Inc. | Active fan tip treatment using rotating drum array in fan track liner with axial and circumferential channels for distortion tolerance |
| US12209502B1 (en) | 2024-06-28 | 2025-01-28 | Rolls-Royce North American Technologies Inc. | Active fan tip treatment using rotating drum array with axial channels in fan track liner for distortion tolerance |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2017228B (en) * | 1977-07-14 | 1982-05-06 | Pratt & Witney Aircraft Of Can | Shroud for a turbine rotor |
| FR2558900B1 (en) * | 1984-02-01 | 1988-05-27 | Snecma | DEVICE FOR PERIPHERAL SEALING OF AXIAL COMPRESSOR BLADES |
| WO1995034745A1 (en) * | 1994-06-14 | 1995-12-21 | United Technologies Corporation | Interrupted circumferential groove stator structure |
| DE69909120T2 (en) * | 1998-11-13 | 2003-12-24 | Pratt & Whitney Canada Inc., Longueuil | HOUSING CONFIGURATION FOR A COMPRESSOR |
-
2010
- 2010-02-11 GB GB1002250A patent/GB2477745A/en not_active Withdrawn
Also Published As
| Publication number | Publication date |
|---|---|
| GB2477745A (en) | 2011-08-17 |
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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) |