JPS56162300A - Manufacture of casing for gas-turbine compressor - Google Patents
Manufacture of casing for gas-turbine compressorInfo
- Publication number
- JPS56162300A JPS56162300A JP6390680A JP6390680A JPS56162300A JP S56162300 A JPS56162300 A JP S56162300A JP 6390680 A JP6390680 A JP 6390680A JP 6390680 A JP6390680 A JP 6390680A JP S56162300 A JPS56162300 A JP S56162300A
- Authority
- JP
- Japan
- Prior art keywords
- casing
- groove part
- shaped member
- casings
- manufacture
- 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
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
PURPOSE: To make it possible to largely reduce the number of processes needed for manufacture of a casing for a gas-turbine compressor, by integrally casting a casing having a groove part, fixing a half ring-shaped member to the step part formed in a portion of the groove part in order to form a bleeder hole, and assembling thus formed upper and lower casings together.
CONSTITUTION: A casing 14 having a groove part 16 is cast. Into a step part 17 formed in a portion of said groove part 16 by machining, a half ring-shaped member 15, which has been machined separately, is fitted in order to form a bleeding hole having an opening of given width. The half surface of the ring-shaped member 15 is secured by using, e.g., bolts 19 as shown in the figure. Thus, the upper and lower half casings 14 and 14 in which the half ring-shaped members 15 and 15 have been secured to the respective grooves 16 having the step parts 17 are assembled together. According, formation of the bleeder hole is made possible by using the casings 14 of integral structure, and the number of the necessary processes can be largely reduced by facilitating the assembly thereof.
COPYRIGHT: (C)1981,JPO&Japio
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6390680A JPS56162300A (en) | 1980-05-16 | 1980-05-16 | Manufacture of casing for gas-turbine compressor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6390680A JPS56162300A (en) | 1980-05-16 | 1980-05-16 | Manufacture of casing for gas-turbine compressor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS56162300A true JPS56162300A (en) | 1981-12-14 |
Family
ID=13242827
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP6390680A Pending JPS56162300A (en) | 1980-05-16 | 1980-05-16 | Manufacture of casing for gas-turbine compressor |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS56162300A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1431516A2 (en) | 2002-12-17 | 2004-06-23 | Rolls Royce Plc | Diffuser arrangement |
| JP2012202405A (en) * | 2011-03-23 | 2012-10-22 | General Electric Co <Ge> | Cast turbine casing and nozzle diaphragm preform |
| CN107962354A (en) * | 2017-11-24 | 2018-04-27 | 中国航发沈阳黎明航空发动机有限责任公司 | A kind of processing technology of opposite opened casing |
-
1980
- 1980-05-16 JP JP6390680A patent/JPS56162300A/en active Pending
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1431516A2 (en) | 2002-12-17 | 2004-06-23 | Rolls Royce Plc | Diffuser arrangement |
| EP1431516A3 (en) * | 2002-12-17 | 2005-03-30 | Rolls Royce Plc | Diffuser arrangement |
| US7062918B2 (en) | 2002-12-17 | 2006-06-20 | Rolls-Royce Plc | Diffuser arrangement |
| JP2012202405A (en) * | 2011-03-23 | 2012-10-22 | General Electric Co <Ge> | Cast turbine casing and nozzle diaphragm preform |
| EP2503108A3 (en) * | 2011-03-23 | 2017-06-07 | General Electric Company | Cast turbine casing and nozzle diaphragm preforms |
| CN107962354A (en) * | 2017-11-24 | 2018-04-27 | 中国航发沈阳黎明航空发动机有限责任公司 | A kind of processing technology of opposite opened casing |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| FR2502529B1 (en) | METHOD FOR MANUFACTURING THE AERODYNAMICALLY PROFILED PART OF A VANE OF A GAS TURBINE ENGINE | |
| JPS56132497A (en) | Axial thrust equalizer | |
| CA2087761A1 (en) | High pressure turbine component interference fit up | |
| GB2050524B (en) | Turbine stator shroud assembly | |
| JPS5791328A (en) | Axial flow gas turbine engine | |
| GB1518076A (en) | Ceramic rotor blade assembly for a gas turbine engine | |
| EP0372275A3 (en) | Method of modifying turbine rotor discs | |
| DE3377925D1 (en) | Rotor blade form for the first stage of a combustion turbine | |
| JPS5710714A (en) | External casing for axial flow compressor or axial flow turbine of jet engine | |
| GB2397102B (en) | Turbine shroud assembly | |
| JPS56162300A (en) | Manufacture of casing for gas-turbine compressor | |
| GB2144492B (en) | Stator assembly for bounding the flow path of a gas turbine engine | |
| JPS5534812A (en) | Rotor of magnetic generator and its manufacturing method | |
| ZA862770B (en) | Armature rotors for electromagnetic retarders | |
| US5102296A (en) | Turbine nozzle, and a method of varying the power of same | |
| US4177003A (en) | Installation for centering the inner housing of a steam turbine | |
| ATE15161T1 (en) | MOLDED METAL PART AND ITS MANUFACTURING PROCESS. | |
| JPS56162298A (en) | Diaphragm for centrifugal compressor | |
| JPS56148648A (en) | Manufacturing method of cast covered ceramic piston | |
| JPS5632005A (en) | Steam turbine nozzle diaphragm | |
| JPS57171005A (en) | Manufacture of impeller | |
| JPS55151103A (en) | Manufacture of turbine nozzle | |
| ATE131427T1 (en) | METHOD FOR PRODUCING A PARTIAL JOINT IN TURBINE CONSTRUCTION | |
| JPS5656992A (en) | Vane type compressor | |
| DE3509193A1 (en) | FLOWING MACHINE WITH INNER HOUSING |