GB1438702A - Gas turbine components - Google Patents
Gas turbine componentsInfo
- Publication number
- GB1438702A GB1438702A GB5334073A GB5334073A GB1438702A GB 1438702 A GB1438702 A GB 1438702A GB 5334073 A GB5334073 A GB 5334073A GB 5334073 A GB5334073 A GB 5334073A GB 1438702 A GB1438702 A GB 1438702A
- Authority
- GB
- United Kingdom
- Prior art keywords
- slot
- gas turbine
- bonding
- nov
- laminations
- 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
- F01D5/34—Rotor-blade aggregates of unitary construction, e.g. formed of sheet laminae
-
- 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
- F01D5/04—Blade-carrying members, e.g. rotors for radial-flow machines or engines
- F01D5/043—Blade-carrying members, e.g. rotors for radial-flow machines or engines of the axial inlet- radial outlet, or vice versa, type
- F01D5/046—Heating, heat insulation or cooling means
-
- 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
- F01D5/04—Blade-carrying members, e.g. rotors for radial-flow machines or engines
- F01D5/043—Blade-carrying members, e.g. rotors for radial-flow machines or engines of the axial inlet- radial outlet, or vice versa, type
- F01D5/048—Form or construction
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/4932—Turbomachine making
- Y10T29/49325—Shaping integrally bladed rotor
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Motor Or Generator Cooling System (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US308188A US3927952A (en) | 1972-11-20 | 1972-11-20 | Cooled turbine components and method of making the same |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1438702A true GB1438702A (en) | 1976-06-09 |
Family
ID=23192929
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB5334073A Expired GB1438702A (en) | 1972-11-20 | 1973-11-16 | Gas turbine components |
Country Status (4)
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2734507A1 (de) * | 1976-08-11 | 1978-02-16 | Jan Mowill | Laufradelement |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4416581A (en) * | 1982-02-16 | 1983-11-22 | Elliott Turbomachinery Co., Inc. | Method and apparatus for cooling an expander |
GB2130509B (en) * | 1982-11-16 | 1986-03-05 | Rolls Royce | A method for eliminating or minimising the effects of defects in materials |
US4587700A (en) * | 1984-06-08 | 1986-05-13 | The Garrett Corporation | Method for manufacturing a dual alloy cooled turbine wheel |
US4664598A (en) * | 1984-10-05 | 1987-05-12 | Reliance Electric Company | Unitized quick-assembly fan |
US4659288A (en) * | 1984-12-10 | 1987-04-21 | The Garrett Corporation | Dual alloy radial turbine rotor with hub material exposed in saddle regions of blade ring |
DE3802763A1 (de) * | 1988-01-30 | 1989-08-10 | Kloeckner Humboldt Deutz Ag | Radialturbine |
US5832715A (en) * | 1990-02-28 | 1998-11-10 | Dev; Sudarshan Paul | Small gas turbine engine having enhanced fuel economy |
US5253472A (en) * | 1990-02-28 | 1993-10-19 | Dev Sudarshan P | Small gas turbine having enhanced fuel economy |
US5215439A (en) * | 1991-01-15 | 1993-06-01 | Northern Research & Engineering Corp. | Arbitrary hub for centrifugal impellers |
US6042879A (en) * | 1997-07-02 | 2000-03-28 | United Technologies Corporation | Method for preparing an apertured article to be recoated |
US6511294B1 (en) | 1999-09-23 | 2003-01-28 | General Electric Company | Reduced-stress compressor blisk flowpath |
US6524070B1 (en) | 2000-08-21 | 2003-02-25 | General Electric Company | Method and apparatus for reducing rotor assembly circumferential rim stress |
US6499953B1 (en) * | 2000-09-29 | 2002-12-31 | Pratt & Whitney Canada Corp. | Dual flow impeller |
US6471474B1 (en) | 2000-10-20 | 2002-10-29 | General Electric Company | Method and apparatus for reducing rotor assembly circumferential rim stress |
CN101338766B (zh) * | 2007-07-04 | 2011-11-30 | 富准精密工业(深圳)有限公司 | 离心风扇及采用该离心风扇的散热模组 |
CN101514711A (zh) * | 2008-02-22 | 2009-08-26 | 赵明慧 | 涡轮叶片和涡轮机 |
FR2944060B1 (fr) * | 2009-04-06 | 2013-07-19 | Turbomeca | Systeme d'air secondaire pour compresseur centrifuge ou mixte |
US8678771B2 (en) * | 2009-12-14 | 2014-03-25 | Siemens Energy, Inc. | Process for manufacturing a component |
WO2011106780A1 (en) * | 2010-02-26 | 2011-09-01 | Ventions, Llc | Small scale high speed turbomachinery |
DE102011009028A1 (de) * | 2011-01-20 | 2012-07-26 | Daimler Ag | Turbinenrad für eine Radialturbine sowie Abgasturbolader mit einer Radialturbine |
US9714577B2 (en) | 2013-10-24 | 2017-07-25 | Honeywell International Inc. | Gas turbine engine rotors including intra-hub stress relief features and methods for the manufacture thereof |
US10040122B2 (en) | 2014-09-22 | 2018-08-07 | Honeywell International Inc. | Methods for producing gas turbine engine rotors and other powdered metal articles having shaped internal cavities |
US20230012375A1 (en) * | 2021-07-09 | 2023-01-12 | Raytheon Technologies Corporation | Radial flow turbine rotor with internal fluid cooling |
US11761632B2 (en) * | 2021-08-05 | 2023-09-19 | General Electric Company | Combustor swirler with vanes incorporating open area |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2407531A (en) * | 1942-05-02 | 1946-09-10 | Fed Reserve Bank | Elastic fluid mechanism |
US2613058A (en) * | 1945-11-30 | 1952-10-07 | Atkinson Joseph | Cooled bladed rotor |
US2618462A (en) * | 1948-12-30 | 1952-11-18 | Kane Saul Allan | Turbine rotor formed of laminated plates with aperture overlap |
US2801792A (en) * | 1949-09-15 | 1957-08-06 | Svenska Rotor Maskiner Ab | Cooling of machine structures |
FR1208163A (fr) * | 1957-12-11 | 1960-02-22 | Standard Motor Co Ltd | Rotor à aubage pour turbines et compresseurs |
US3074151A (en) * | 1959-10-19 | 1963-01-22 | Viber Company | Laminated air turbine rotor and method of making the same |
US3515499A (en) * | 1968-04-22 | 1970-06-02 | Aerojet General Co | Blades and blade assemblies for turbine engines,compressors and the like |
US3778183A (en) * | 1968-04-22 | 1973-12-11 | Aerojet General Co | Cooling passages wafer blade assemblies for turbine engines, compressors and the like |
GB1175816A (en) * | 1968-06-24 | 1969-12-23 | Rolls Royce | Improvements relating to the Cooling of Aerofoil Shaped Blades |
US3781130A (en) * | 1972-06-27 | 1973-12-25 | Us Air Force | Turbine blade manufactured of self-carrying laminates |
-
1972
- 1972-11-20 US US308188A patent/US3927952A/en not_active Expired - Lifetime
-
1973
- 1973-11-15 FR FR7340637A patent/FR2207245B1/fr not_active Expired
- 1973-11-16 GB GB5334073A patent/GB1438702A/en not_active Expired
- 1973-11-20 CA CA186,270A patent/CA997272A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2734507A1 (de) * | 1976-08-11 | 1978-02-16 | Jan Mowill | Laufradelement |
Also Published As
Publication number | Publication date |
---|---|
FR2207245B1 (US20110158925A1-20110630-C00042.png) | 1976-06-25 |
CA997272A (en) | 1976-09-21 |
FR2207245A1 (US20110158925A1-20110630-C00042.png) | 1974-06-14 |
US3927952A (en) | 1975-12-23 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PCNP | Patent ceased through non-payment of renewal fee |