JPS5268611A - Sealing device for nozzle-wing supporting unit in turbo-fan engine - Google Patents
Sealing device for nozzle-wing supporting unit in turbo-fan engineInfo
- Publication number
- JPS5268611A JPS5268611A JP14329975A JP14329975A JPS5268611A JP S5268611 A JPS5268611 A JP S5268611A JP 14329975 A JP14329975 A JP 14329975A JP 14329975 A JP14329975 A JP 14329975A JP S5268611 A JPS5268611 A JP S5268611A
- Authority
- JP
- Japan
- Prior art keywords
- nozzle
- supporting unit
- turbo
- sealing device
- fan engine
- 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
Links
Landscapes
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
PURPOSE: In order to set the clearance of the sealed surface fixed, devised is to organize the sealed surface of the supporting unit for the external radius side of the flange of a nozzle-wing so as to be in parallel with the relative displacement which is created during the operation of the engine.
COPYRIGHT: (C)1977,JPO&Japio
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP14329975A JPS5268611A (en) | 1975-12-04 | 1975-12-04 | Sealing device for nozzle-wing supporting unit in turbo-fan engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP14329975A JPS5268611A (en) | 1975-12-04 | 1975-12-04 | Sealing device for nozzle-wing supporting unit in turbo-fan engine |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS5268611A true JPS5268611A (en) | 1977-06-07 |
JPS558642B2 JPS558642B2 (en) | 1980-03-05 |
Family
ID=15335508
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP14329975A Granted JPS5268611A (en) | 1975-12-04 | 1975-12-04 | Sealing device for nozzle-wing supporting unit in turbo-fan engine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS5268611A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5575507A (en) * | 1978-11-25 | 1980-06-06 | Rolls Royce | Nozzle guide vane assembly for gas turbine engine |
US4640092A (en) * | 1986-03-03 | 1987-02-03 | United Technologies Corporation | Combustion chamber rear outer seal |
US4725199A (en) * | 1985-12-23 | 1988-02-16 | United Technologies Corporation | Snap ring construction |
US6305899B1 (en) * | 1998-09-18 | 2001-10-23 | Rolls-Royce Plc | Gas turbine engine |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS4110001Y1 (en) * | 1965-06-15 | 1966-05-13 |
-
1975
- 1975-12-04 JP JP14329975A patent/JPS5268611A/en active Granted
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS4110001Y1 (en) * | 1965-06-15 | 1966-05-13 |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5575507A (en) * | 1978-11-25 | 1980-06-06 | Rolls Royce | Nozzle guide vane assembly for gas turbine engine |
JPS6125883B2 (en) * | 1978-11-25 | 1986-06-18 | Rolls Royce 1971 Ltd | |
US4725199A (en) * | 1985-12-23 | 1988-02-16 | United Technologies Corporation | Snap ring construction |
US4640092A (en) * | 1986-03-03 | 1987-02-03 | United Technologies Corporation | Combustion chamber rear outer seal |
US6305899B1 (en) * | 1998-09-18 | 2001-10-23 | Rolls-Royce Plc | Gas turbine engine |
Also Published As
Publication number | Publication date |
---|---|
JPS558642B2 (en) | 1980-03-05 |
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