SU1064702A1 - NOISE PROTECTOR OF THE EXHAUST AIR OF THE AVIATION GAS TURBINE ENGINE - Google Patents
NOISE PROTECTOR OF THE EXHAUST AIR OF THE AVIATION GAS TURBINE ENGINEInfo
- Publication number
- SU1064702A1 SU1064702A1 SU3470183/06A SU3470183A SU1064702A1 SU 1064702 A1 SU1064702 A1 SU 1064702A1 SU 3470183/06 A SU3470183/06 A SU 3470183/06A SU 3470183 A SU3470183 A SU 3470183A SU 1064702 A1 SU1064702 A1 SU 1064702A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- gas turbine
- turbine engine
- exhaust air
- aviation gas
- dividers
- Prior art date
Links
Landscapes
- Exhaust Silencers (AREA)
Abstract
Глушитель шума выхлопной струи авиационного газотурбинного двигателя, содержащий установленные на срезе сопла выдвижные рассекатели, отличающийся тем, что, с целью повышения эффективности шумоглушения, рассекатели установлены под углом 45-60° к плоскости среза, а концы рассекателей размещены на расстоянии, равном 0,15-0,2 диаметра сопла от его внутренней поверхности.A silencer for an exhaust jet of an aviation gas turbine engine containing retractable dividers installed at the nozzle section, characterized in that, in order to increase the efficiency of sound attenuation, the dividers are installed at an angle of 45-60 ° to the cut plane, and the ends of the dividers are placed at a distance of 0.15 -0.2 diameter of the nozzle from its inner surface.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU3470183/06A SU1064702A1 (en) | 1982-07-12 | 1982-07-12 | NOISE PROTECTOR OF THE EXHAUST AIR OF THE AVIATION GAS TURBINE ENGINE |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU3470183/06A SU1064702A1 (en) | 1982-07-12 | 1982-07-12 | NOISE PROTECTOR OF THE EXHAUST AIR OF THE AVIATION GAS TURBINE ENGINE |
Publications (1)
Publication Number | Publication Date |
---|---|
SU1064702A1 true SU1064702A1 (en) | 2005-12-10 |
Family
ID=60526368
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU3470183/06A SU1064702A1 (en) | 1982-07-12 | 1982-07-12 | NOISE PROTECTOR OF THE EXHAUST AIR OF THE AVIATION GAS TURBINE ENGINE |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU1064702A1 (en) |
-
1982
- 1982-07-12 SU SU3470183/06A patent/SU1064702A1/en active
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JPS5720539A (en) | Exhaust nozzle for gas turbine engine | |
GB2066354B (en) | Sound absorbing structure for use in gas turbine engines | |
GB2044358B (en) | Gas turbine jet engine mounting | |
IT1131162B (en) | CURVED AXIS DHARIA SOCKET FOR GAS TURBO ENGINE | |
GB2073325B (en) | Gas turbine aircraft engine air intake | |
GB2065766B (en) | Sound absorbing structure for use in gas turbine engines | |
GB2132278B (en) | Gas turbine engine exhaust nozzle assembly | |
IT8723250A0 (en) | COMBINATION OF VORTEX GENERATOR FOR GAS TURBO ENGINE COMBUSTION. | |
DE3371927D1 (en) | DIFFUSER FOR GAS TURBINE ENGINE | |
GB1541066A (en) | Aircraft gas turbine engine flight manoeuverable exhaust nozzle | |
IT1131298B (en) | DIFFUSER PARTICULARLY SUITABLE FOR GAS TURBO ENGINES | |
GB1335724A (en) | Gas turbine engine exhaust nozzles | |
GB2036875B (en) | Suppressing gas turbine engines noise | |
IT8321087A1 (en) | DIFFUSER STRUCTURE FOR A GAS TURBINE ENGINE | |
SU1064702A1 (en) | NOISE PROTECTOR OF THE EXHAUST AIR OF THE AVIATION GAS TURBINE ENGINE | |
DE69006868D1 (en) | Gas turbine air jet engine. | |
GB2076893B (en) | I c engine exhaust gas silencer | |
IT1060613B (en) | SOUND ATTENUATION INLET DUCT PARTICULARLY FOR A GAS TURBINE ENGINE | |
IT8123606A0 (en) | FUEL NOZZLE FOR GAS TURBO ENGINE. | |
GB1470146A (en) | Aircraft with an encased pusher propeller | |
GB881974A (en) | Improvements in noise suppression jet propulsion nozzle | |
JPS5537591A (en) | Assembly of jet pipe with variableearea final nozzle for gas turbine engine | |
GB746702A (en) | Improvements in or relating to gas turbine engines | |
AT346131B (en) | SILENCER ARRANGEMENT IN THE EXHAUST FLOW OF A GAS TURBINE SYSTEM | |
SU270397A1 (en) | DEVICE FOR REDUCING THE NOISE OF A JET MOTOR WITH A CENTRAL BODY IN THE AREA OF A NOZZLE |