FIELD: engines and pumps.
SUBSTANCE: enhanced dual-flow turbo jet engine with the fan driven via a simple aligned reduction gear, the reduction gear idlers running in plain bearings, the said bearing fixed sleeve inner space outlet communicating, via channels, with the slot space between the aforesaid bearing working surfaces, while its inlet communicates with the oil feed jet and, via perforated walls, with the reduction gear air chamber. Note here, that the said inner space and channels are filled with a sponge or open-pore capillary material, or with carbon (synthetic) fibres, or in the case of higher temperatures, with metal compacted basket.
EFFECT: higher engine reliability provided for by feeding lubricant onto the idlers plain bearings in change-over operating conditions.
2 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ENHANCED DUAL-FLOW TURBO JET ENGINE | 2006 |
|
RU2330171C2 |
| BYPASS GAS TURBINE ENGINE WITH FAN DRIVEN BY SIMPLE COAXIAL INNER GEARING REDUCTION GEAR | 2007 |
|
RU2346176C1 |
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|
RU2311554C2 |
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|
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| GAS TURBINE ENGINE SINGLE-ROW BLOWER REDUCTION GEAR DRIVE | 2007 |
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RU2347928C1 |
| SUPER-BYPASS GAS TURBINE ENGINE WITH BIROTARY BLOWER. | 2007 |
|
RU2347929C2 |
| BYPASS GAS-TURBINE ENGINE | 2006 |
|
RU2349784C2 |
| CYCLOIDAL REDUCER, FAN MODULE OF DUAL-FLOW TURBOJET ENGINE AND DUAL-FLOW TURBOJET ENGINE | 2013 |
|
RU2627990C2 |
| FRONT PART OF AIRCRAFT DOUBLE-FLOW GAS TURBINE ENGINE AND AIRCRAFT DOUBLE-FLOW GAS TURBINE ENGINE | 2015 |
|
RU2686248C2 |
| BIROTATING BYPASS GAS TURBINE ENGINE | 2023 |
|
RU2803681C1 |
