JPS5246215A - Intermediate transfer annular structure for 22shaft gas turbine engine - Google Patents

Intermediate transfer annular structure for 22shaft gas turbine engine

Info

Publication number
JPS5246215A
JPS5246215A JP11991076A JP11991076A JPS5246215A JP S5246215 A JPS5246215 A JP S5246215A JP 11991076 A JP11991076 A JP 11991076A JP 11991076 A JP11991076 A JP 11991076A JP S5246215 A JPS5246215 A JP S5246215A
Authority
JP
Japan
Prior art keywords
22shaft
gas turbine
intermediate transfer
turbine engine
annular structure
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.)
Granted
Application number
JP11991076A
Other languages
Japanese (ja)
Other versions
JPS5536813B2 (en
Inventor
David J Amos
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.)
CBS Corp
Original Assignee
Westinghouse Electric Corp
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
Priority claimed from US05/620,608 external-priority patent/US4013377A/en
Application filed by Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Priority to JP11991076A priority Critical patent/JPS5246215A/en
Publication of JPS5246215A publication Critical patent/JPS5246215A/en
Publication of JPS5536813B2 publication Critical patent/JPS5536813B2/ja
Granted legal-status Critical Current

Links

Landscapes

  • Turbine Rotor Nozzle Sealing (AREA)
JP11991076A 1975-10-08 1976-10-07 Intermediate transfer annular structure for 22shaft gas turbine engine Granted JPS5246215A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11991076A JPS5246215A (en) 1975-10-08 1976-10-07 Intermediate transfer annular structure for 22shaft gas turbine engine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US05/620,608 US4013377A (en) 1975-10-08 1975-10-08 Intermediate transition annulus for a two shaft gas turbine engine
JP11991076A JPS5246215A (en) 1975-10-08 1976-10-07 Intermediate transfer annular structure for 22shaft gas turbine engine

Publications (2)

Publication Number Publication Date
JPS5246215A true JPS5246215A (en) 1977-04-12
JPS5536813B2 JPS5536813B2 (en) 1980-09-24

Family

ID=26457562

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11991076A Granted JPS5246215A (en) 1975-10-08 1976-10-07 Intermediate transfer annular structure for 22shaft gas turbine engine

Country Status (1)

Country Link
JP (1) JPS5246215A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5596327A (en) * 1978-12-04 1980-07-22 Gen Electric Apparatus for maintaining gap between variable vanes
JPS60112601U (en) * 1983-12-29 1985-07-30 株式会社新潟鐵工所 turbine nozzle
JPH01136631U (en) * 1988-03-15 1989-09-19
JP2010007669A (en) * 2002-02-28 2010-01-14 General Electric Co <Ge> Device for varying inlet air flow of gas turbine engine
EP3339572A1 (en) * 2016-12-20 2018-06-27 Rolls-Royce plc Variable guide vane device
EP3832145A1 (en) * 2019-12-06 2021-06-09 Pratt & Whitney Canada Corp. Assembly for a compressor section of a gas turbine engine
US11952943B2 (en) 2019-12-06 2024-04-09 Pratt & Whitney Canada Corp. Assembly for a compressor section of a gas turbine engine

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5596327A (en) * 1978-12-04 1980-07-22 Gen Electric Apparatus for maintaining gap between variable vanes
JPS6365811B2 (en) * 1978-12-04 1988-12-16 Gen Electric
JPS60112601U (en) * 1983-12-29 1985-07-30 株式会社新潟鐵工所 turbine nozzle
JPH0122881Y2 (en) * 1983-12-29 1989-07-12
JPH01136631U (en) * 1988-03-15 1989-09-19
JP2010007669A (en) * 2002-02-28 2010-01-14 General Electric Co <Ge> Device for varying inlet air flow of gas turbine engine
EP3339572A1 (en) * 2016-12-20 2018-06-27 Rolls-Royce plc Variable guide vane device
EP3832145A1 (en) * 2019-12-06 2021-06-09 Pratt & Whitney Canada Corp. Assembly for a compressor section of a gas turbine engine
US11952943B2 (en) 2019-12-06 2024-04-09 Pratt & Whitney Canada Corp. Assembly for a compressor section of a gas turbine engine

Also Published As

Publication number Publication date
JPS5536813B2 (en) 1980-09-24

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