JPS53104020A - Gas turbine combustor - Google Patents

Gas turbine combustor

Info

Publication number
JPS53104020A
JPS53104020A JP1811777A JP1811777A JPS53104020A JP S53104020 A JPS53104020 A JP S53104020A JP 1811777 A JP1811777 A JP 1811777A JP 1811777 A JP1811777 A JP 1811777A JP S53104020 A JPS53104020 A JP S53104020A
Authority
JP
Japan
Prior art keywords
gas turbine
turbine combustor
transition
transition pieces
interlinking
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
JP1811777A
Other languages
Japanese (ja)
Inventor
Soichi Kurosawa
Nobuyuki Iizuka
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 JP1811777A priority Critical patent/JPS53104020A/en
Publication of JPS53104020A publication Critical patent/JPS53104020A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE: To prevent clamps and transition pieces from breakage by means of interlinking between each transition piece for suppressing vibration of the transition pieces.
COPYRIGHT: (C)1978,JPO&Japio
JP1811777A 1977-02-23 1977-02-23 Gas turbine combustor Pending JPS53104020A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1811777A JPS53104020A (en) 1977-02-23 1977-02-23 Gas turbine combustor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1811777A JPS53104020A (en) 1977-02-23 1977-02-23 Gas turbine combustor

Publications (1)

Publication Number Publication Date
JPS53104020A true JPS53104020A (en) 1978-09-09

Family

ID=11962655

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1811777A Pending JPS53104020A (en) 1977-02-23 1977-02-23 Gas turbine combustor

Country Status (1)

Country Link
JP (1) JPS53104020A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110779043A (en) * 2019-10-09 2020-02-11 东方电气集团东方汽轮机有限公司 Combustor tail cylinder structure and outlet lateral connection method

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4218649Y1 (en) * 1965-10-14 1967-10-28
US3609968A (en) * 1970-04-29 1971-10-05 Westinghouse Electric Corp Self-adjusting seal structure
US3670497A (en) * 1970-09-02 1972-06-20 United Aircraft Corp Combustion chamber support
JPS5112763A (en) * 1974-07-22 1976-01-31 Funai Electric Co
JPS5194009A (en) * 1975-01-29 1976-08-18

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4218649Y1 (en) * 1965-10-14 1967-10-28
US3609968A (en) * 1970-04-29 1971-10-05 Westinghouse Electric Corp Self-adjusting seal structure
US3670497A (en) * 1970-09-02 1972-06-20 United Aircraft Corp Combustion chamber support
JPS5112763A (en) * 1974-07-22 1976-01-31 Funai Electric Co
JPS5194009A (en) * 1975-01-29 1976-08-18

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110779043A (en) * 2019-10-09 2020-02-11 东方电气集团东方汽轮机有限公司 Combustor tail cylinder structure and outlet lateral connection method
CN110779043B (en) * 2019-10-09 2020-11-24 东方电气集团东方汽轮机有限公司 Combustor tail cylinder structure and outlet lateral connection method

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