FIELD: machine building.
SUBSTANCE: group of inventions relates a turbine engine gearbox. Said gearbox comprises casing (30) and two gear lines (40a, 40b) arranged in a V shape. Casing (30) comprises two arms (30a, 30b), each of which has one of two gear lines (40a, 40b) placed therein, lubricant tank (35) placed between said two gear lines (40a, 40b). Turbomachine comprises a gearbox.
EFFECT: freeing up space in the fan zone, which enables to increase the diameter of the fan and improve the performance of the engine.
10 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| DEVICE FOR TURBOPROP FAN BLADE ORIENTATION CONTROL | 2010 |
|
RU2525101C2 |
| DENTAL MATERIAL CONTAINER | 2018 |
|
RU2752586C1 |
| TURBOMACHINE BLADE REINFORCEMENT WITH METAL ELEMENT | 2010 |
|
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| CLOSURE PLATE, AND SLIDING CLOSURE ON SPOUT OF CONTAINER CONTAINING MOLTEN METAL | 2012 |
|
RU2598422C2 |
| POWER UNIT TO DRIVE HIGH-PRESSURE PUMP | 2006 |
|
RU2315190C1 |
| AIR SUPPLY UNIT | 2010 |
|
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| CLAMPING DEVICE OF HAND-HELD MACHINE AND HAND-HELD MACHINE | 2011 |
|
RU2588909C2 |
| TURBINE MACHINE WITH DEVICE FOR SEALING JOINTS | 2002 |
|
RU2296865C2 |
| FRONT PART OF AIRCRAFT DOUBLE-FLOW GAS TURBINE ENGINE AND AIRCRAFT DOUBLE-FLOW GAS TURBINE ENGINE | 2015 |
|
RU2686248C2 |
| BURNER WITH LOW TEMPERATURE LID | 2020 |
|
RU2800464C2 |
