CA927751A - Turbomachine rotor - Google Patents
Turbomachine rotorInfo
- Publication number
- CA927751A CA927751A CA092763A CA92763A CA927751A CA 927751 A CA927751 A CA 927751A CA 092763 A CA092763 A CA 092763A CA 92763 A CA92763 A CA 92763A CA 927751 A CA927751 A CA 927751A
- Authority
- CA
- Canada
- Prior art keywords
- turbomachine rotor
- turbomachine
- rotor
- 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
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
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
-
- 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
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US88392069A | 1969-12-10 | 1969-12-10 |
Publications (1)
Publication Number | Publication Date |
---|---|
CA927751A true CA927751A (en) | 1973-06-05 |
Family
ID=25383588
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA092763A Expired CA927751A (en) | 1969-12-10 | 1970-09-10 | Turbomachine rotor |
Country Status (3)
Country | Link |
---|---|
US (1) | US3625634A (en) |
CA (1) | CA927751A (en) |
GB (1) | GB1272200A (en) |
Families Citing this family (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2143561B1 (en) * | 1971-06-29 | 1974-03-08 | Snecma | |
DE2150741C3 (en) * | 1971-10-12 | 1973-11-22 | Messerschmitt Boelkow Blohm | The rotor blades of a rotary wing aircraft are suspended from the rotor head without flapping or pivot joints |
US3904316A (en) * | 1974-08-16 | 1975-09-09 | Gen Motors Corp | Turbine rotor with slot loaded blades and composite bands |
GB1553038A (en) * | 1977-04-28 | 1979-09-19 | Snecma | Drum for an axial flow compressor rotor and process for its manufacture |
FR2453294A1 (en) * | 1979-04-04 | 1980-10-31 | Snecma | DEVICE FOR FIXING BLADES ON A COMPRESSOR ROTOR FOR A TURBO-REACTOR |
IT1135752B (en) * | 1981-04-17 | 1986-08-27 | Nuovo Pignone Spa | IMPROVEMENTS IN THE POWER STAGE OF A GAS TURBINE |
US4566700A (en) * | 1982-08-09 | 1986-01-28 | United Technologies Corporation | Abrasive/abradable gas path seal system |
US4483054A (en) * | 1982-11-12 | 1984-11-20 | United Technologies Corporation | Method for making a drum rotor |
DE3316535A1 (en) * | 1983-05-06 | 1984-11-08 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | TURBO COMPRESSOR WITH INLET COVER |
US4648802A (en) * | 1984-09-06 | 1987-03-10 | Pda Engineering | Radial flow rotor with inserts and turbine utilizing the same |
US4919594A (en) * | 1987-05-15 | 1990-04-24 | Allied-Signal Inc. | Composite member, unitary rotor member including same, and method of making |
US4867644A (en) * | 1987-05-15 | 1989-09-19 | Allied-Signal Inc. | Composite member, unitary rotor member including same, and method of making |
US5632600A (en) * | 1995-12-22 | 1997-05-27 | General Electric Company | Reinforced rotor disk assembly |
DE19650260A1 (en) * | 1996-12-04 | 1998-06-10 | Asea Brown Boveri | Rotor for turbomachinery |
GB2456637B (en) * | 1997-06-03 | 2010-01-13 | Rolls Royce Plc | A fibre reinforced metal rotor |
US6217283B1 (en) * | 1999-04-20 | 2001-04-17 | General Electric Company | Composite fan platform |
US6213720B1 (en) | 1999-06-11 | 2001-04-10 | Alliedsignal, Inc. | High strength composite reinforced turbomachinery disk |
DE10259822B4 (en) * | 2002-12-19 | 2009-01-02 | Siemens Ag | Electric machine with bandaged, deep-cooling winding |
DE10358421A1 (en) * | 2003-12-13 | 2005-07-07 | Mtu Aero Engines Gmbh | Rotor for a turbomachine |
DE102006011513A1 (en) | 2006-03-10 | 2007-09-13 | Rolls-Royce Deutschland Ltd & Co Kg | Inlet cone of a fiber composite material for a gas turbine engine and method for its production |
DE102006015838A1 (en) * | 2006-04-03 | 2007-10-04 | Rolls-Royce Deutschland Ltd & Co Kg | Axial compressor e.g. high pressure compressor, for gas turbine engine, has rotor drum that is formed from rotor rings with fiber belts and is made from high temperature resistant fibers that are bedded with polymer e.g. polyamide |
US8011877B2 (en) | 2008-11-24 | 2011-09-06 | General Electric Company | Fiber composite reinforced aircraft gas turbine engine drums with radially inwardly extending blades |
EP2204541B1 (en) * | 2008-12-24 | 2012-03-07 | Techspace Aero S.A. | Rotor stage of an integral bladed compressor drum of an axial turbomachine and corresponding manufacturing method. |
EP2287445A1 (en) | 2009-07-16 | 2011-02-23 | Techspace Aero S.A. | Axial compressor rotor drum with composite web |
RU2013146686A (en) * | 2011-07-19 | 2015-08-27 | Эллиотт Компани | ASSEMBLY AND METHOD OF ATTACHING THE SUPPORT JAXLE TO THE DRUM SHAFT OF THE AXIAL COMPRESSOR ROTOR |
US8777576B2 (en) | 2011-08-22 | 2014-07-15 | General Electric Company | Metallic fan blade platform |
GB201611674D0 (en) * | 2016-07-05 | 2016-08-17 | Rolls Royce Plc | A turbine arrangement |
CN111550435A (en) * | 2020-05-25 | 2020-08-18 | 中国航发沈阳发动机研究所 | Multistage rotor disk connection structure |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR980131A (en) * | 1951-05-08 | |||
US2143466A (en) * | 1937-12-31 | 1939-01-10 | Westinghouse Electric & Mfg Co | Turbine apparatus |
FR907059A (en) * | 1946-09-20 | 1946-02-28 | High temperature gas turbine | |
US2803397A (en) * | 1952-05-20 | 1957-08-20 | Gen Motors Corp | Compressor wheel |
GB1170592A (en) * | 1966-11-29 | 1969-11-12 | Rolls Royce | Aerofoil-Shaped Blades and Blade Assemblies, for use in a Fluid Flow Machine |
US3403844A (en) * | 1967-10-02 | 1968-10-01 | Gen Electric | Bladed member and method for making |
US3519368A (en) * | 1968-09-03 | 1970-07-07 | Gen Electric | Composite turbomachinery rotors |
-
1969
- 1969-12-10 US US883920A patent/US3625634A/en not_active Expired - Lifetime
-
1970
- 1970-09-10 CA CA092763A patent/CA927751A/en not_active Expired
- 1970-11-26 GB GB56216/70A patent/GB1272200A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
GB1272200A (en) | 1972-04-26 |
US3625634A (en) | 1971-12-07 |
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