CA2972805A1 - A frangible composite airfoil - Google Patents
A frangible composite airfoil Download PDFInfo
- Publication number
- CA2972805A1 CA2972805A1 CA2972805A CA2972805A CA2972805A1 CA 2972805 A1 CA2972805 A1 CA 2972805A1 CA 2972805 A CA2972805 A CA 2972805A CA 2972805 A CA2972805 A CA 2972805A CA 2972805 A1 CA2972805 A1 CA 2972805A1
- Authority
- CA
- Canada
- Prior art keywords
- energy dissipating
- blade
- dissipating member
- composite blade
- airfoil
- 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.)
- Abandoned
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
- F01D5/28—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
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
- F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
-
- 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
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
- F04D29/324—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
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/603—Composites; e.g. fibre-reinforced
-
- 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)
- Reinforced Plastic Materials (AREA)
Applications Claiming Priority (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US14/596,841 US9878501B2 (en) | 2015-01-14 | 2015-01-14 | Method of manufacturing a frangible blade |
US14/596,841 | 2015-01-14 | ||
US14/596,815 US9243512B1 (en) | 2015-01-14 | 2015-01-14 | Rotary machine with a frangible composite blade |
US14/596,804 US9828862B2 (en) | 2015-01-14 | 2015-01-14 | Frangible airfoil |
US14/596,804 | 2015-01-14 | ||
US14/596,815 | 2015-01-14 | ||
PCT/US2016/013419 WO2016115352A1 (en) | 2015-01-14 | 2016-01-14 | A frangible composite airfoil |
Publications (1)
Publication Number | Publication Date |
---|---|
CA2972805A1 true CA2972805A1 (en) | 2016-07-21 |
Family
ID=55272690
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA2972805A Abandoned CA2972805A1 (en) | 2015-01-14 | 2016-01-14 | A frangible composite airfoil |
Country Status (5)
Country | Link |
---|---|
EP (1) | EP3245387A1 (zh) |
JP (1) | JP2018508684A (zh) |
CN (1) | CN107407154B (zh) |
CA (1) | CA2972805A1 (zh) |
WO (1) | WO2016115352A1 (zh) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20190242399A1 (en) * | 2018-02-08 | 2019-08-08 | General Electric Company | Turbine engine with composite blade |
US10746045B2 (en) * | 2018-10-16 | 2020-08-18 | General Electric Company | Frangible gas turbine engine airfoil including a retaining member |
US20200141268A1 (en) * | 2018-11-01 | 2020-05-07 | General Electric Company | Frangible Gas Turbine Engine Airfoil |
US10815795B2 (en) * | 2018-12-20 | 2020-10-27 | General Electric Company | Pre-tension and retention structure for composite fan blade |
WO2024154386A1 (ja) * | 2023-01-16 | 2024-07-25 | 株式会社Ihi | 複合材翼 |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3551070A (en) * | 1968-05-08 | 1970-12-29 | Dov Z Glucksman | Axial fan |
CA2042218A1 (en) * | 1990-07-20 | 1992-01-21 | Jan C. Schilling | Composite airfoil with increased shear capability |
US6290895B1 (en) * | 1997-10-14 | 2001-09-18 | General Electric Company | Selectively flexible caul and method of use |
GB0516036D0 (en) * | 2005-08-04 | 2005-09-14 | Rolls Royce Plc | Aerofoil |
GB0815483D0 (en) * | 2008-08-27 | 2008-10-01 | Rolls Royce Plc | Blade arrangement |
GB201003588D0 (en) * | 2010-03-04 | 2010-04-21 | Rolls Royce Plc | Improvements relating to layered composite components |
GB201003592D0 (en) * | 2010-03-04 | 2010-04-21 | Rolls Royce Plc | A component comprising a resin matrix |
-
2016
- 2016-01-14 WO PCT/US2016/013419 patent/WO2016115352A1/en active Application Filing
- 2016-01-14 CN CN201680005933.7A patent/CN107407154B/zh active Active
- 2016-01-14 CA CA2972805A patent/CA2972805A1/en not_active Abandoned
- 2016-01-14 JP JP2017535663A patent/JP2018508684A/ja active Pending
- 2016-01-14 EP EP16702283.9A patent/EP3245387A1/en not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
EP3245387A1 (en) | 2017-11-22 |
CN107407154A (zh) | 2017-11-28 |
WO2016115352A1 (en) | 2016-07-21 |
JP2018508684A (ja) | 2018-03-29 |
CN107407154B (zh) | 2019-12-24 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FZDE | Dead |
Effective date: 20190115 |