FIELD: gas-turbine engine engineering. SUBSTANCE: method comprises adjusting and balancing reserve vanes in manufacturing an engine. EFFECT: simplified replacement. 3 cl
Title | Year | Author | Number |
---|---|---|---|
METHOD OF REPLACEMENT OF AXIAL-FLOW COMPRESSOR MOVING BLADES | 1992 |
|
RU2013568C1 |
METHOD OF REPLACEMENT OF DAMAGED BLADES OF GAS-TURBINE ENGINE FAN | 1992 |
|
RU2034177C1 |
METHOD OF ASSEMBLING AND BALANCING HIGH-SPEED ROTORS AND SHAFT LINES OF AIRCRAFT GAS TURBINE ENGINES AND GAS COMPRESSOR UNITS | 2022 |
|
RU2822671C2 |
HIGH-PRESSURE TURBINE ROTOR OF A GAS TURBINE ENGINE (VERSIONS) | 2018 |
|
RU2691868C1 |
GAS TURBINE ENGINE LOW-PRESSURE TURBINE (LPT) (VERSIONS), ROTOR SHAFT CONNECTION UNIT WITH LPT DISC, LPT ROTOR AIR COOLING PATH AND AIR FEEDING APPARATUS FOR COOLING LPT ROTOR BLADES | 2018 |
|
RU2684355C1 |
TURBINE PART CONVECTIVE COOLING DEVICE | 1990 |
|
RU2009331C1 |
GAS TURBINE ENGINE OVERHAUL METHOD (VERSIONS) AND GAS TURBINE ENGINE REPAIRED ACCORDING TO THIS METHOD (VERSIONS), OVERHAUL OF BATCH, RESUPPLIED GROUP OF GAS TURBINE ENGINES AND GAS TURBINE ENGINE REPAIRED BY THIS METHOD | 2013 |
|
RU2555932C2 |
TURBINE NOZZLE BLOCK | 1991 |
|
RU1825021C |
GAS TURBINE ENGINE LOW-PRESSURE COMPRESSOR ROTOR LAST STAGE DISC | 2015 |
|
RU2603220C1 |
DISPERSIVE REINFORCED NICKEL BASED ALLOY | 1992 |
|
RU2016119C1 |
Authors
Dates
1997-12-20—Published
1995-01-30—Filed