FIELD: turbine and compressor manufacture, namely processes for making large-size housings of compressors and turbines.
SUBSTANCE: method comprises steps of using as housing blank standard housing with parting portions having stator, rotor and working blades and worked out its resource in working modes whose power is no less than power for making article with stabilized crystalline structure of metal and stress zones; measuring errors from predetermined geometry size of turnings of mounting surface for inserts, size determining radial mutual arrangement of rotor and stator and gaps between working blades and housing; grinding parting portions of housing by value exceeding predetermined errors and turning diameters of housing at providing designed parameters of article and proper relation of said parameters and gap between working blades of rotor and housing.
EFFECT: enhanced operational reliability, technological effectiveness of construction.
1 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF MAKING ROTOR OF BLADE MACHINE | 1991 |
|
RU2047464C1 |
METHOD TO PRODUCE GAS TURBINE AXIAL COMPRESSOR DIFFUSER VANES | 2008 |
|
RU2383421C1 |
METHOD FOR NON-DESTRUCTIVE TESTING OF METAL OF TURBINE BLADES SUBJECTED TO PERMANENT AND VARIABLE OPERATING LOADS FOR PROLONGED PERIODS AT HIGH TEMPERATURES | 2019 |
|
RU2706814C1 |
METHOD AND SYSTEM OF TOP MACHINING | 2017 |
|
RU2726303C1 |
METHOD OF TURBOMACHINE MANUFACTURE AND GRINDING MACHINE FOR ITS EMBODIMENT | 1996 |
|
RU2162782C2 |
METHOD OF PRODUCING ROTOR OR BLADED MACHINE, MACHINE TOOL FOR GRINDING AND DEVICE FOR AUTOMATIC CONTROL | 1996 |
|
RU2179502C2 |
TURBOMACHINE | 2003 |
|
RU2232276C1 |
METHOD OF BUILDING UP RADIAL CLEARANCES IN END DIAPHRAGM SEALS OF STEAM TURBINE | 0 |
|
SU1724901A1 |
METHOD AND DEVICE FOR STAMPING BLINGS | 2021 |
|
RU2769333C1 |
METHOD OF AIRCRAFT LANDING GEAR WHEELS DRIVING AND AIRCRAFT LANDING GEAR WITH DRIVEN WHEELS | 2011 |
|
RU2495792C2 |
Authors
Dates
2004-11-27—Published
2003-09-03—Filed