JPS57210103A - Stacked rotor - Google Patents
Stacked rotorInfo
- Publication number
- JPS57210103A JPS57210103A JP9233781A JP9233781A JPS57210103A JP S57210103 A JPS57210103 A JP S57210103A JP 9233781 A JP9233781 A JP 9233781A JP 9233781 A JP9233781 A JP 9233781A JP S57210103 A JPS57210103 A JP S57210103A
- Authority
- JP
- Japan
- Prior art keywords
- bolt
- discs
- fitted
- sleeve
- bolt holes
- 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.)
- Pending
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)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
PURPOSE:To prevent the damage of the coupling bolt of a stacked rotor in which plural discs having moving vanes are piled up, by fitting sleeves in the bolt holes of the discs so that the sleeves bear the centrifugal force which acts to the coupling bolt. CONSTITUTION:To construct a rotor for an axial-flow compressor or the like, plural discs 2 (2a-2c) fitted with moving vanes in grooves provided on the peripheral portions of the discs are piled up in the axial direction and conjoined to each other by a stacking bolt 3. The bolt holes 4a, 4c of the discs 2a, 2c are finished with high accuracy by reaming. The bolt hole 4b of the other disc 2b is drilled to a larger diameter than the former bolt holes 4a, 4c. A sleeve 6, in which the bolt 3 is to be movably fitted, is provided in the bolt hole 4b. Both the ends 6a of the sleeve 6 are tightly fitted in the bolt holes 4a, 4c but the expanded intermediate part of the sleeve is fitted with a clearance in the bolt hole 4b.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP9233781A JPS57210103A (en) | 1981-06-17 | 1981-06-17 | Stacked rotor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP9233781A JPS57210103A (en) | 1981-06-17 | 1981-06-17 | Stacked rotor |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS57210103A true JPS57210103A (en) | 1982-12-23 |
Family
ID=14051574
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP9233781A Pending JPS57210103A (en) | 1981-06-17 | 1981-06-17 | Stacked rotor |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS57210103A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6095751A (en) * | 1997-09-11 | 2000-08-01 | Mitsubishi Heavy Industries, Ltd. | Seal device between fastening bolt and bolthole in gas turbine disc |
JP2009063000A (en) * | 2008-12-19 | 2009-03-26 | Mitsubishi Heavy Ind Ltd | Structure for attaching spindle bolt of compressor |
JP2013215088A (en) * | 2012-03-30 | 2013-10-17 | General Electric Co <Ge> | System and method for coupling rotor components |
WO2016060686A1 (en) * | 2014-10-17 | 2016-04-21 | Siemens Aktiengesellschaft | Gas turbine spindle bolt with shrink fitted sleeve |
WO2021230874A1 (en) * | 2020-05-14 | 2021-11-18 | Dresser-Rand Company | Compressor rotor structure |
-
1981
- 1981-06-17 JP JP9233781A patent/JPS57210103A/en active Pending
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6095751A (en) * | 1997-09-11 | 2000-08-01 | Mitsubishi Heavy Industries, Ltd. | Seal device between fastening bolt and bolthole in gas turbine disc |
JP2009063000A (en) * | 2008-12-19 | 2009-03-26 | Mitsubishi Heavy Ind Ltd | Structure for attaching spindle bolt of compressor |
JP2013215088A (en) * | 2012-03-30 | 2013-10-17 | General Electric Co <Ge> | System and method for coupling rotor components |
WO2016060686A1 (en) * | 2014-10-17 | 2016-04-21 | Siemens Aktiengesellschaft | Gas turbine spindle bolt with shrink fitted sleeve |
WO2021230874A1 (en) * | 2020-05-14 | 2021-11-18 | Dresser-Rand Company | Compressor rotor structure |
US11885340B2 (en) | 2020-05-14 | 2024-01-30 | Siemens Energy Global GmbH & Co. KG | Compressor rotor structure |
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