FIELD: mechanical and power engineering. SUBSTANCE: rotary axially symmetric nozzle has spherical tip of housing and bracket on which rotary member is secured by axles. Bracket is L-shaped. bracket attachment flanges are mounted on spherical tip. Distance between bracket attachment flange to axle of rotation of rotary member is L=0.08-0.12D where D is diameter of sphere of spherical tip over its outer surface. EFFECT: improved reliability of nozzle owing to decrease of difference in linear temperature expansion of bracket and spherical tip. 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| DEVICE FOR TURBOJET JET NOZZLE ROTATION | 2018 |
|
RU2702325C1 |
| ROTARY AXIALLY SYMMETRIC NOZZLE | 1999 |
|
RU2162956C2 |
| AXISYMMETRIC SWIVEL NOZZLE COOLING SYSTEM | 1987 |
|
RU2095605C1 |
| TURBOJET ADJUSTABLE NOZZLE | 2013 |
|
RU2529283C1 |
| ROTARY AXISYMMETRIC NOZZLE OF TURBOJET ENGINE | 2016 |
|
RU2641425C1 |
| SWIVEL AXISYMMETRIC NOZZLE FOR TURBO-JET ENGINE | 2003 |
|
RU2250385C2 |
| METHOD OF OPERATION OF ROTATING ROUND SUPERSONIC REACTION NOZZLE OF TURBOJET ENGINE AND DEVICE FOR IMPLEMENTING THIS METHOD | 1998 |
|
RU2145670C1 |
| EXHAUST SYSTEM OF TURBOPROP ENGINE | 2001 |
|
RU2216487C2 |
| GEAR MEASURING RADIUS OF SPHERICAL POLISHED SURFACES | 2001 |
|
RU2215987C2 |
| AXISYMMETRIC SWIVEL NOZZLE FOR TURBO-JET ENGINE | 2003 |
|
RU2250384C2 |
