FIELD: aviation.
SUBSTANCE: both block bearings are located on one side of the impeller from the side of a driving shaft and located in a single barrel concentrically installed above the shaft the open side of it is unfolded along the gas-oil mix supply channels, and the bottom through the annular slot formed in it is interconnected with the root part of inter-blade channels of the impeller.
EFFECT: invention allows to improve reliability of breather operation and to simplify his design.
4 cl, 2 dwg
| Title | Year | Author | Number |
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RU2596903C1 |
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| CENTRIFUGAL BREATHER | 2014 |
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RU2548228C1 |
| CENTRIFUGAL BREATHER | 2004 |
|
RU2277177C1 |
