GB1161298A - Turbomachine Rotors - Google Patents
Turbomachine RotorsInfo
- Publication number
- GB1161298A GB1161298A GB3972/67A GB397267A GB1161298A GB 1161298 A GB1161298 A GB 1161298A GB 3972/67 A GB3972/67 A GB 3972/67A GB 397267 A GB397267 A GB 397267A GB 1161298 A GB1161298 A GB 1161298A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbomachine rotors
- rotors
- turbomachine
- heading
- aug
- 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
- F01D5/08—Heating, heat-insulating or cooling means
- F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
-
- 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
- F01D5/08—Heating, heat-insulating 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
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/187—Convection cooling
-
- 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
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
-
- 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
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3023—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2240/00—Components
- F05B2240/80—Platforms for stationary or moving blades
- F05B2240/801—Platforms for stationary or moving blades cooled platforms
-
- 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
- F05D2240/00—Components
- F05D2240/80—Platforms for stationary or moving blades
- F05D2240/81—Cooled platforms
Abstract
1,161,298. Turbine rotors. GENERAL MOTORS CORP. Aug.24, 1967 [Dec. 19, 1966], No.38972/67. Heading F1T. The subject matter of this Specification is the same as that disclosed in Specification 1,161,297 but the claims are concerned with the cooling passages formed between the rotor rim (10) and the sheet metal ring (62).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US60279566A | 1966-12-19 | 1966-12-19 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1161298A true GB1161298A (en) | 1969-08-13 |
Family
ID=24412840
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3972/67A Expired GB1161298A (en) | 1966-12-19 | 1967-08-24 | Turbomachine Rotors |
GB38971/67A Expired GB1161297A (en) | 1966-12-19 | 1967-08-24 | Turbomachine Rotors |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB38971/67A Expired GB1161297A (en) | 1966-12-19 | 1967-08-24 | Turbomachine Rotors |
Country Status (3)
Country | Link |
---|---|
US (1) | US3446480A (en) |
DE (1) | DE1601568A1 (en) |
GB (2) | GB1161298A (en) |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1801475B2 (en) * | 1968-10-05 | 1971-08-12 | Daimler Benz Ag, 7000 Stuttgart | AIR-COOLED TURBINE BLADE |
US3619076A (en) * | 1970-02-02 | 1971-11-09 | Gen Electric | Liquid-cooled turbine bucket |
US3747182A (en) * | 1970-05-07 | 1973-07-24 | United Aircraft Corp | Method of fabricating a hollow turbine blade having an insert therein |
US3697192A (en) * | 1970-05-07 | 1972-10-10 | United Aircraft Corp | Hollow turbine blade |
US3709632A (en) * | 1971-02-12 | 1973-01-09 | Gen Motors Corp | Blade tip closure |
US3709631A (en) * | 1971-03-18 | 1973-01-09 | Caterpillar Tractor Co | Turbine blade seal arrangement |
US3846041A (en) * | 1972-10-31 | 1974-11-05 | Avco Corp | Impingement cooled turbine blades and method of making same |
US3858290A (en) * | 1972-11-21 | 1975-01-07 | Avco Corp | Method of making inserts for cooled turbine blades |
GB1550368A (en) * | 1975-07-16 | 1979-08-15 | Rolls Royce | Laminated materials |
JP3811502B2 (en) * | 1994-08-24 | 2006-08-23 | ウエスチングハウス・エレクトリック・コーポレイション | Gas turbine blades with cooling platform |
WO1999060253A1 (en) * | 1998-05-18 | 1999-11-25 | Siemens Aktiengesellschaft | Cooled turbine blade platform |
EP1923536A1 (en) * | 2006-11-17 | 2008-05-21 | Siemens Aktiengesellschaft | Liner in a cooling channel of a turbine blade |
EP2706242A1 (en) * | 2012-09-11 | 2014-03-12 | Techspace Aero S.A. | Fixing of blades on an axial compressor drum |
EP2735707B1 (en) * | 2012-11-27 | 2017-04-05 | Safran Aero Boosters SA | Axial turbomachine guide nozzle with segmented inner shroud and corresponding compressor |
EP3232001A1 (en) * | 2016-04-15 | 2017-10-18 | Siemens Aktiengesellschaft | Rotor blade for a turbine |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2601969A (en) * | 1946-01-25 | 1952-07-01 | United Specialties Co | Turbine wheel |
US2779565A (en) * | 1948-01-05 | 1957-01-29 | Bruno W Bruckmann | Air cooling of turbine blades |
US2840299A (en) * | 1952-09-22 | 1958-06-24 | Thompson Prod Inc | Axial flow compressor rotor |
BE551145A (en) * | 1955-09-26 | |||
US2888243A (en) * | 1956-10-22 | 1959-05-26 | Pollock Robert Stephen | Cooled turbine blade |
-
1966
- 1966-12-19 US US602795A patent/US3446480A/en not_active Expired - Lifetime
-
1967
- 1967-08-24 GB GB3972/67A patent/GB1161298A/en not_active Expired
- 1967-08-24 GB GB38971/67A patent/GB1161297A/en not_active Expired
- 1967-09-19 DE DE19671601568 patent/DE1601568A1/en active Pending
Also Published As
Publication number | Publication date |
---|---|
US3446480A (en) | 1969-05-27 |
GB1161297A (en) | 1969-08-13 |
DE1601568A1 (en) | 1970-08-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] |