FIELD: engines and pumps.
SUBSTANCE: turbomachine high-pressure turbine stator comprises annular housing, sector webs and air circulation casing angular sectors. The latter are arranged to make continuous circular chamber surrounding turbine rotor blades. Air circulation casing angular sectors feed air onto casing to allow adjusting the gap nearby turbine rotor blade faces. Proposed method comprises setting stator elements angular distribution pattern for preset angular sector to rule out coherence of angular positions of zones arranged between adjacent webs and casing intersector zones between adjacent casings. It includes also extending the pattern above to entire circumference of stator. Other invention of the set relates to turbomachine high-pressure turbine stator assembled as specified above.
EFFECT: higher efficiency and longer life.
10 cl, 4 dwg
Title | Year | Author | Number |
---|---|---|---|
DEVICE TO ADJUST GAS TURBINE RADIAL GAPS WITH EQUALISATION OF AIRFLOWS | 2005 |
|
RU2379522C2 |
DEVICE FOR AXIAL FIXING SECTOR OF RING SEAL IN HIGH-PRESSURE TURBINE OF TURBOMACHINE | 2005 |
|
RU2365767C2 |
GAS TURBINE ENGINE GUIDE VANES SEALING DEVICE | 2012 |
|
RU2604777C2 |
SECTOR OF STATOR BLADES, AXIAL TURBOMACHINE STATOR, AXIAL TURBOMACHINE | 2014 |
|
RU2619914C2 |
SEALING DEVICE BETWEEN ROTOR AND STATOR OF GAS TURBINE ENGINE | 2018 |
|
RU2762016C2 |
METHOD OF AIRCRAFT LANDING GEAR WHEELS DRIVING AND AIRCRAFT LANDING GEAR WITH DRIVEN WHEELS | 2011 |
|
RU2495792C2 |
TURBO-MACHINE STATOR AND METHOD OF ITS ASSEMBLY/DISASSEMBLY | 2003 |
|
RU2335637C2 |
STATOR OF AXIAL TURBINE MACHINE , METHOD OF ITS MANUFACTURING AND TURBINE MACHINE CONTAINING THIS STATOR | 2013 |
|
RU2568353C2 |
AXIAL TURBINE MACHINE STATOR BLADES RETAINING RING AND AXIAL TURBOMACHINE | 2015 |
|
RU2614302C2 |
AXIAL TURBOMACHINE | 2015 |
|
RU2696177C2 |
Authors
Dates
2009-11-27—Published
2005-03-14—Filed