FIELD: engines and pumps.
SUBSTANCE: turbine support relates to aircraft engine production. Gas turbine support comprises inner housing with bearing, radial spokes attached to inner housing and passing through turbine nozzle vane inner spaces, flexible elements and outer support made integral from closed hollow ring with brackets arranged along turbine lengthwise axis. Note here that aforesaid brackets are pivoted to aforesaid spokes via adjusting elements.
EFFECT: more or less equal tightening of spokes in turbine assembly.
2 cl, 1 dwg
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RU2691202C1 |
| COOLED TURBINE OF GAS TURBINE ENGINE | 2001 |
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