GB750597A - Rotors for gas turbine installations and exhaust gas turboblower installations - Google Patents
Rotors for gas turbine installations and exhaust gas turboblower installationsInfo
- Publication number
- GB750597A GB750597A GB3113/55A GB311355A GB750597A GB 750597 A GB750597 A GB 750597A GB 3113/55 A GB3113/55 A GB 3113/55A GB 311355 A GB311355 A GB 311355A GB 750597 A GB750597 A GB 750597A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rotor
- blower
- turbine
- installations
- rotor shaft
- 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
- F01D5/04—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
-
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
- F01D25/166—Sliding contact bearing
-
- 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
- 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
- F05D2220/00—Application
- F05D2220/40—Application in turbochargers
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
750,597. Gas turbine plant; centrifugal blowers. KLOCKNER - HUMBOLDT - DEUTZ AKT.-GES. June 26, 1953 [June 27, 1952], No. 3113/55. Divided out of 750,508. Drawings to Specification. Classes 110(1) and 110(3) In a rotor assembly for a gas turbine plant or an exhaust-gas turbo-blower, a hollow cup-like member carries the turbine rotor on the exterior of its base and carries the blower rotor on its peripheral surface, and a tubular support for the rotor shaft bearings projects into the cuplike member, the rotor shaft being connected to the interior of the said base; the cross-section of the base in the direction of heat conduction to the blower is larger than the cross-section of the points of contact of its interior with the rotor shaft. This arrangement limits the flow of heat from the turbine rotor to the rotor shaft and bearings. A screen situated between the turbine and blower rotors limits radiation of heat from the turbine rotor and is cooled by air leaking from the blower rotor and passing along one or both sides of the screen. The subject-matter is substantially the same as that of Specification 750,508, but the claims differ.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE750597X | 1952-06-27 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB750597A true GB750597A (en) | 1956-06-20 |
Family
ID=6650481
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3113/55A Expired GB750597A (en) | 1952-06-27 | 1953-06-26 | Rotors for gas turbine installations and exhaust gas turboblower installations |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB750597A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3300043A1 (en) * | 1982-01-06 | 1983-08-04 | Hitachi, Ltd., Tokyo | TURBOCHARGER |
US5125228A (en) * | 1990-12-13 | 1992-06-30 | Sundstrand Corporation | Diaphragm seal plate |
US5161945A (en) * | 1990-10-10 | 1992-11-10 | Allied-Signal Inc. | Turbine engine interstage seal |
-
1953
- 1953-06-26 GB GB3113/55A patent/GB750597A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3300043A1 (en) * | 1982-01-06 | 1983-08-04 | Hitachi, Ltd., Tokyo | TURBOCHARGER |
US5161945A (en) * | 1990-10-10 | 1992-11-10 | Allied-Signal Inc. | Turbine engine interstage seal |
US5125228A (en) * | 1990-12-13 | 1992-06-30 | Sundstrand Corporation | Diaphragm seal plate |
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