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JPS56162300A - Manufacture of casing for gas-turbine compressor - Google Patents

Manufacture of casing for gas-turbine compressor

Info

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
Application number
JP6390680A
Other languages
Japanese (ja)
Inventor
Takeo Hirochi
Katsuo Wada
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hitachi Ltd
Original Assignee
Hitachi Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Hitachi Ltd filed Critical Hitachi Ltd
Priority to JP6390680A priority Critical patent/JPS56162300A/en
Publication of JPS56162300A publication Critical patent/JPS56162300A/en
Pending legal-status Critical Current

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
JP6390680A 1980-05-16 1980-05-16 Manufacture of casing for gas-turbine compressor Pending JPS56162300A (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (6)

* Cited by examiner, † Cited by third party
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

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