GB9016445D0 - A rotor particularly for compressors or turbines of gas turbine propulsion units - Google Patents
A rotor particularly for compressors or turbines of gas turbine propulsion unitsInfo
- Publication number
- GB9016445D0 GB9016445D0 GB909016445A GB9016445A GB9016445D0 GB 9016445 D0 GB9016445 D0 GB 9016445D0 GB 909016445 A GB909016445 A GB 909016445A GB 9016445 A GB9016445 A GB 9016445A GB 9016445 D0 GB9016445 D0 GB 9016445D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- compressors
- turbines
- gas turbine
- propulsion units
- turbine propulsion
- 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.)
- Granted
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
- F01D5/066—Connecting means for joining rotor-discs or rotor-elements together, e.g. by a central bolt, by clamps
-
- 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
- F01D5/141—Shape, i.e. outer, aerodynamic form
- F01D5/142—Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows
-
- 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
- F01D5/141—Shape, i.e. outer, aerodynamic form
- F01D5/146—Shape, i.e. outer, aerodynamic form of blades with tandem configuration, split blades or slotted blades
-
- 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
-
- 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)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE3924829A DE3924829A1 (en) | 1989-07-27 | 1989-07-27 | COMPRESSOR OR TURBINE RUNNER, ESPECIALLY FOR GAS TURBINE ENGINES |
Publications (3)
Publication Number | Publication Date |
---|---|
GB9016445D0 true GB9016445D0 (en) | 1990-09-12 |
GB2235734A GB2235734A (en) | 1991-03-13 |
GB2235734B GB2235734B (en) | 1993-08-25 |
Family
ID=6385939
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9016445A Expired - Fee Related GB2235734B (en) | 1989-07-27 | 1990-07-26 | Turbo-rotor construction. |
Country Status (4)
Country | Link |
---|---|
DE (1) | DE3924829A1 (en) |
FR (1) | FR2650338B1 (en) |
GB (1) | GB2235734B (en) |
IT (1) | IT1242978B (en) |
Families Citing this family (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2712037B1 (en) * | 1993-11-03 | 1995-12-08 | Snecma | Compressor turbomachine, the rotor of which has a removable upstream stage. |
GB2303188B (en) * | 1995-07-13 | 1999-04-28 | Bmw Rolls Royce Gmbh | An assembly of two turbine rotor discs |
DE19525699A1 (en) * | 1995-07-14 | 1997-01-16 | Bmw Rolls Royce Gmbh | Tandem vane grille |
JPH11311130A (en) * | 1998-04-27 | 1999-11-09 | Kawasaki Heavy Ind Ltd | Booster structure for jet engine |
EP1077310A1 (en) * | 1999-08-18 | 2001-02-21 | Siemens Aktiengesellschaft | Vaned stator |
US6572337B1 (en) * | 1999-11-30 | 2003-06-03 | General Electric Co. | Turbine rotor torque transmission |
FR2869374B1 (en) * | 2004-04-23 | 2009-01-30 | Snecma Moteurs Sa | SYSTEM FOR FASTENING WORKPIECES THROUGH STUDDERS |
DE102007035726A1 (en) | 2007-07-30 | 2009-02-05 | Mtu Aero Engines Gmbh | Tandem stage has integral bladed, axially adjacent rotors where each of two bladed rotors has transfer elements, which are separated from connection area on shaft |
US8047768B2 (en) * | 2009-01-12 | 2011-11-01 | General Electric Company | Split impeller configuration for synchronizing thermal response between turbine wheels |
DE102009023100A1 (en) * | 2009-05-28 | 2010-12-02 | Rolls-Royce Deutschland Ltd & Co Kg | Turbomachine with a blade row group with meridionalem edge distance |
DE102011084125A1 (en) * | 2011-10-07 | 2013-04-11 | Mtu Aero Engines Gmbh | Blade segment for turbomachine e.g. gas turbine for aircraft engine, has upper shroud which interconnects blades to each other, and lower shroud is divided into several portions which are firmly connected to the blades |
EP2626512B1 (en) * | 2012-02-10 | 2017-04-12 | MTU Aero Engines GmbH | Flow engine |
DE102014203607A1 (en) | 2014-02-27 | 2015-08-27 | Rolls-Royce Deutschland Ltd & Co Kg | Blade row group |
DE102014203604A1 (en) | 2014-02-27 | 2015-08-27 | Rolls-Royce Deutschland Ltd & Co Kg | Blade row group |
DE102014204346A1 (en) | 2014-03-10 | 2015-09-10 | Rolls-Royce Deutschland Ltd & Co Kg | Method for producing a double-row paddle wheel for a turbomachine and double-row paddle wheel |
DE102014205226A1 (en) * | 2014-03-20 | 2015-09-24 | Rolls-Royce Deutschland Ltd & Co Kg | Blade row group |
US20190010956A1 (en) * | 2017-07-06 | 2019-01-10 | United Technologies Corporation | Tandem blade rotor disk |
US20200248560A1 (en) * | 2019-02-05 | 2020-08-06 | United Technologies Corporation | Tandem fan for boundary layer ingestion systems |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE390486C (en) * | 1922-07-14 | 1924-02-20 | Rudolf Wagner Dr | Blade, especially for steam and gas turbines |
GB628263A (en) * | 1943-06-01 | 1949-08-25 | Louis Breguet | Improvements in or relating to axial flow compressors |
DE1503647A1 (en) * | 1965-06-19 | 1969-03-13 | Meissen Turbowerke | Spaltflegelrad for axial flow machines, especially for fans and blowers |
GB1277881A (en) * | 1968-05-09 | 1972-06-14 | Stone Manganese Marine Ltd | Improvements relating to marine propellers |
GB1432875A (en) * | 1973-07-11 | 1976-04-22 | Rolls Royce | Gas rotor assemblies |
US3916495A (en) * | 1974-02-25 | 1975-11-04 | Gen Electric | Method and means for balancing a gas turbine engine |
-
1989
- 1989-07-27 DE DE3924829A patent/DE3924829A1/en active Granted
-
1990
- 1990-07-17 IT IT02096390A patent/IT1242978B/en active IP Right Grant
- 1990-07-18 FR FR9009154A patent/FR2650338B1/en not_active Expired - Fee Related
- 1990-07-26 GB GB9016445A patent/GB2235734B/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
IT1242978B (en) | 1994-05-18 |
FR2650338A1 (en) | 1991-02-01 |
GB2235734B (en) | 1993-08-25 |
IT9020963A0 (en) | 1990-07-17 |
DE3924829C2 (en) | 1991-07-11 |
FR2650338B1 (en) | 1993-05-14 |
IT9020963A1 (en) | 1992-01-17 |
DE3924829A1 (en) | 1991-02-07 |
GB2235734A (en) | 1991-03-13 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19960726 |