GB201222974D0 - An aerofoil structure - Google Patents
An aerofoil structureInfo
- Publication number
- GB201222974D0 GB201222974D0 GBGB1222974.6A GB201222974A GB201222974D0 GB 201222974 D0 GB201222974 D0 GB 201222974D0 GB 201222974 A GB201222974 A GB 201222974A GB 201222974 D0 GB201222974 D0 GB 201222974D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- aerofoil structure
- aerofoil
- 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.)
- Ceased
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
- 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
- F01D11/127—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 a deformable or crushable structure, e.g. honeycomb
-
- 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
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
-
- 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
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/288—Protective coatings for blades
-
- 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
- F05D2230/90—Coating; Surface treatment
-
- 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)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Composite Materials (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GBGB1222974.6A GB201222974D0 (en) | 2012-12-19 | 2012-12-19 | An aerofoil structure |
| PCT/GB2013/053370 WO2014096839A1 (en) | 2012-12-19 | 2013-12-19 | An aerofoil structure with collapsible tip portion |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GBGB1222974.6A GB201222974D0 (en) | 2012-12-19 | 2012-12-19 | An aerofoil structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB201222974D0 true GB201222974D0 (en) | 2013-01-30 |
Family
ID=47631054
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GBGB1222974.6A Ceased GB201222974D0 (en) | 2012-12-19 | 2012-12-19 | An aerofoil structure |
Country Status (2)
| Country | Link |
|---|---|
| GB (1) | GB201222974D0 (en) |
| WO (1) | WO2014096839A1 (en) |
Families Citing this family (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9850767B2 (en) | 2014-08-08 | 2017-12-26 | United Technologies Corporation | Aluminum fan blade tip with thermal barrier |
| US11168702B2 (en) | 2017-08-10 | 2021-11-09 | Raytheon Technologies Corporation | Rotating airfoil with tip pocket |
| US10533575B2 (en) | 2017-09-06 | 2020-01-14 | United Technologies Corporation | Fan blade tip with frangible strip |
| US12365453B2 (en) | 2018-10-12 | 2025-07-22 | Textron Innovations Inc. | Multi-material ducted rotor blade tip extension |
| US11286037B2 (en) | 2018-10-12 | 2022-03-29 | Textron Innovations Inc. | Ducted rotor blade tip extension |
| US11286036B2 (en) * | 2018-10-12 | 2022-03-29 | Textron Innovations Inc. | Ducted rotor blade tip extension |
| US11215061B2 (en) * | 2020-02-04 | 2022-01-04 | Raytheon Technologies Corporation | Blade with wearable tip-rub-portions above squealer pocket |
| US11565799B2 (en) | 2020-06-12 | 2023-01-31 | Textron Innovations Inc. | Adjustable ducted rotor blade tip extension |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6135715A (en) * | 1999-07-29 | 2000-10-24 | General Electric Company | Tip insulated airfoil |
| GB0911330D0 (en) * | 2009-07-01 | 2009-08-12 | Rolls Royce Plc | Actuatable seal for aerofoil blade tip |
| EP2309098A1 (en) * | 2009-09-30 | 2011-04-13 | Siemens Aktiengesellschaft | Airfoil and corresponding guide vane, blade, gas turbine and turbomachine |
| DE102010062087A1 (en) * | 2010-11-29 | 2012-05-31 | Siemens Aktiengesellschaft | Turbomachine with sealing structure between rotating and stationary parts and method for producing this sealing structure |
-
2012
- 2012-12-19 GB GBGB1222974.6A patent/GB201222974D0/en not_active Ceased
-
2013
- 2013-12-19 WO PCT/GB2013/053370 patent/WO2014096839A1/en not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| WO2014096839A1 (en) | 2014-06-26 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AT | Applications terminated before publication under section 16(1) |