GB622869A - Improvements in internal combustion and other high-speed, high-temperature turbines - Google Patents
Improvements in internal combustion and other high-speed, high-temperature turbinesInfo
- Publication number
- GB622869A GB622869A GB947047A GB947047A GB622869A GB 622869 A GB622869 A GB 622869A GB 947047 A GB947047 A GB 947047A GB 947047 A GB947047 A GB 947047A GB 622869 A GB622869 A GB 622869A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rings
- discs
- rotor
- pins
- disc
- 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
- F01D5/066—Connecting means for joining rotor-discs or rotor-elements together, e.g. by a central bolt, by clamps
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
622,869. Turbine rotors. BAUMANN, K., and METROPOLITANVICKERS ELECTRICAL CO.. Ltd. April 9, 1947, No. 9470. Addition to 585,086. [Class 110(iii] In a means for securing together two or more blade-carrying discs of a turbine rotor, adjacent faces of adjacent discs are formed with axially extending rings; the rings are secured together by a connecting member having annular grooves which receive projecting portions of the rings, or alternatively one ring is annularly grooved to receive the other ring. The parts are held together by radially disposed taper pins. In the construction shown in Fig. 1, the rings 5 on adjacent rotor discs 1 extend into grooves defined by the inner and outer flanges 6, 7 of a connecting member. The latter is conveniently made in two halves which are welded together along a peripheral joint 12 after the taper pins 8 have been inserted. The taper pins are held in place by forked locking collars 9. The end discs are secured to extensions 2 of the main shaft by connecting rings 10. Concentricity of the rotor discs and shaft extensions is maintained by spigots 3. To permit thermal expansion, axial and radial clearances are provided between the disc ,rings and the connecting members. In an alternative construction, Fig. 2 (not shown), separate connecting members are eliminated; one disc of a two-stage rotor has an axially extending ring which projects into an annular groove defined by inner 'and outer flanges formed on the other disc. An annular ledge on the latter disc prevents inward movement of the taper pins. Outward movement of the pins is prevented by plugs which overlie the pins and are screwed into a ring attached to the outer flange. The rotor is attached to the rotor shaft at one end only, the method of attachment being similar to that shown in Fig. 3 of the drawings of the parent Specification. There may be more than two discs. Specification 603,996 is referred to
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB947047A GB622869A (en) | 1947-04-09 | 1947-04-09 | Improvements in internal combustion and other high-speed, high-temperature turbines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB947047A GB622869A (en) | 1947-04-09 | 1947-04-09 | Improvements in internal combustion and other high-speed, high-temperature turbines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB622869A true GB622869A (en) | 1949-05-09 |
Family
ID=9872590
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB947047A Expired GB622869A (en) | 1947-04-09 | 1947-04-09 | Improvements in internal combustion and other high-speed, high-temperature turbines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB622869A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1046956B (en) * | 1956-07-19 | 1958-12-18 | Daimler Benz Ag | Attachment of runners for flow machines, preferably gas turbines |
DE1284689B (en) * | 1962-05-10 | 1968-12-05 | Licentia Gmbh | Faceplate stack, e.g. B. composed of face plates and axially clamped runners of a thermal axial turbine, in particular gas turbine |
FR2577992A1 (en) * | 1985-02-25 | 1986-08-29 | Gen Electric | REMOVABLE STIFFENING ELEMENT, IN PARTICULAR FOR A GAS TURBINE ENGINE CASING |
WO2001040631A1 (en) * | 1999-12-03 | 2001-06-07 | Siemens Westinghouse Power Corporation | Shear pin with locking cam |
RU2623618C1 (en) * | 2016-07-08 | 2017-06-28 | Публичное акционерное общество "Уфимское моторостроительное производственное объединение" ПАО "УМПО" | Joint of compressor rotors and gas turbine engine turbine |
CN113606000A (en) * | 2021-07-28 | 2021-11-05 | 中国科学院工程热物理研究所 | Disc rotor system with vibration damping and weight reducing functions |
-
1947
- 1947-04-09 GB GB947047A patent/GB622869A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1046956B (en) * | 1956-07-19 | 1958-12-18 | Daimler Benz Ag | Attachment of runners for flow machines, preferably gas turbines |
DE1284689B (en) * | 1962-05-10 | 1968-12-05 | Licentia Gmbh | Faceplate stack, e.g. B. composed of face plates and axially clamped runners of a thermal axial turbine, in particular gas turbine |
FR2577992A1 (en) * | 1985-02-25 | 1986-08-29 | Gen Electric | REMOVABLE STIFFENING ELEMENT, IN PARTICULAR FOR A GAS TURBINE ENGINE CASING |
WO2001040631A1 (en) * | 1999-12-03 | 2001-06-07 | Siemens Westinghouse Power Corporation | Shear pin with locking cam |
RU2623618C1 (en) * | 2016-07-08 | 2017-06-28 | Публичное акционерное общество "Уфимское моторостроительное производственное объединение" ПАО "УМПО" | Joint of compressor rotors and gas turbine engine turbine |
CN113606000A (en) * | 2021-07-28 | 2021-11-05 | 中国科学院工程热物理研究所 | Disc rotor system with vibration damping and weight reducing functions |
CN113606000B (en) * | 2021-07-28 | 2023-03-14 | 中国科学院工程热物理研究所 | Disc rotor system with vibration damping and weight reducing functions |
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