FIELD: machine building.
SUBSTANCE: radial ring flange on its outer or inner periphery comprises alternating projections with holes for fastening tightening bolts and hollows as well as tools to prevent faulty angle joint by preventing bolts from entering a hollow. The tools to prevent faulty angle joint are formed by the bottom of at least one hollow of the inner or, respectively, outer periphery with its radius in relation to the turbomachine axis being less or, respectively, greater than the radius of the circle externally or, respectively, internally tangent to the holes for the bolts to pass through the projections. The other invention of the group relates to the connection of gas-turbine engine elements comprising the above said flange fixed by the bolts with ring clamps. The bolts are placed between the clamps' holes and in the flange projections' holes; the bottom of smaller or, respectively, greater radius is placed between the two flange projections and two projections of at least one of the clamps. One more invention of the group refers to a gas-turbine engine comprising the above connection.
EFFECT: invention eliminates risk of faulty ring flange installation.
8 cl, 6 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| RADIAL RING FLANGE, LOW-PRESSURE TURBINE FOR GAS TURBINE ENGINE AND GAS TURBINE ENGINE | 2009 |
|
RU2514462C2 |
| TOOL FOR FITTING INNER BEARING RACE CARRYING BEARING CAGE AND SCREWS FOR RETAINING IN TURBOMACHINE | 2014 |
|
RU2660548C2 |
| ROTOR SHAFT BEARING OF LOW-PRESSURE COMPRESSOR OF TURBOJET ENGINE (VERSIONS), CASING OF ROTOR SHAFT REAR BEARING, ROTOR SHAFT COMPONENT, POLYFUNCTIONAL EXTERNAL TIGHTENING COMPONENT OF ROTOR SHAFT, CONNECTION COMPONENT OF ROTOR SHAFT, CASING OF BEARING OF ROTOR SHAFT REAR BEARING | 2016 |
|
RU2614029C1 |
| ROTOR SHAFT BEARING OF LOW-PRESSURE COMPRESSOR OF TURBOJET ENGINE (VERSIONS), CYLINDER CONSTITUENT OF ROTOR SHAFT, EXTERNAL TIGHTENING COMPONENT OF ROTOR SHAFT | 2016 |
|
RU2614018C1 |
| SINGLE-SCREW ECCENTRIC PUMP (VERSIONS) | 2011 |
|
RU2557792C2 |
| ROTOR SHAFT BEARING OF LOW-PRESSURE COMPRESSOR OF TURBOJET ENGINE (VERSIONS), SEALING SPOOL OF ROTOR SHAFT BEARING, ROTOR SHAFT BEARING BLOCK, CONTACT HUB OF ROTOR SHAFT BRACELET SEALING, OIL-CONTROL RING OF ROTOR SHAFT | 2016 |
|
RU2614017C1 |
| SUPPORT OF SHAFT ROTOR OF LOW-PRESSURE COMPRESSOR OF GAS TURBINE ENGINE (VERSIONS), BODY OF SHAFT SUPPORT AND BODY OF BALL-BEARING ROTOR SHAFT SUPPORT | 2016 |
|
RU2614020C1 |
| GAS TURBINE ENGINE DISTRIBUTOR, GAS TURBINE ENGINE TURBINE AND GAS TURBINE ENGINE | 2009 |
|
RU2506431C2 |
| FLANGE OF ROTOR DISK CARRYING BLADES AND ITS ARRANGEMENT IN GAS-TURBINE ENGINE | 2001 |
|
RU2282727C2 |
| LOW-PRESSURE COMPRESSOR OF GAS TURBINE ENGINE OF AVIATION TYPE | 2016 |
|
RU2614708C1 |
