JPS5536813B2 - - Google Patents
Info
- Publication number
- JPS5536813B2 JPS5536813B2 JP11991076A JP11991076A JPS5536813B2 JP S5536813 B2 JPS5536813 B2 JP S5536813B2 JP 11991076 A JP11991076 A JP 11991076A JP 11991076 A JP11991076 A JP 11991076A JP S5536813 B2 JPS5536813 B2 JP S5536813B2
- Authority
- JP
- Japan
- 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.)
- Expired
Links
Landscapes
- Turbine Rotor Nozzle Sealing (AREA)
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 JPS5246215A (en) | 1977-04-12 |
| JPS5536813B2 true JPS5536813B2 (enExample) | 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 (enExample) |
Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4278398A (en) * | 1978-12-04 | 1981-07-14 | General Electric Company | Apparatus for maintaining variable vane clearance |
| JPS60112601U (ja) * | 1983-12-29 | 1985-07-30 | 株式会社新潟鐵工所 | タ−ビンノズル |
| JPH01136631U (enExample) * | 1988-03-15 | 1989-09-19 | ||
| US6619916B1 (en) * | 2002-02-28 | 2003-09-16 | General Electric Company | Methods and apparatus for varying gas turbine engine inlet air flow |
| FR3027053B1 (fr) * | 2014-10-10 | 2019-09-13 | Safran Aircraft Engines | Stator de turbomachine d'aeronef |
| GB201621739D0 (en) * | 2016-12-20 | 2017-02-01 | Rolls Royce Plc | Variable guide vane device |
| US10711632B2 (en) * | 2018-08-29 | 2020-07-14 | General Electric Company | Variable nozzles in turbine engines and methods related thereto |
| US11952943B2 (en) | 2019-12-06 | 2024-04-09 | Pratt & Whitney Canada Corp. | Assembly for a compressor section of a gas turbine engine |
| US20210172373A1 (en) * | 2019-12-06 | 2021-06-10 | Pratt & Whitney Canada Corp. | Assembly for a compressor section of a gas turbine engine |
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1976
- 1976-10-07 JP JP11991076A patent/JPS5246215A/ja active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5246215A (en) | 1977-04-12 |