FIELD: engines and pumps.
SUBSTANCE: invention relates to a fan disk for a turbojet engine through which a gas flows in one flow direction. Disk has a radial section shaped as a pin, comprising a first branch, adapted to be secured to a drive shaft of the turbojet engine, a second branch extending opposite the first branch and adapted to support a plurality of fan blades, and a curved connecting wall extending between the first branch and the second branch.
EFFECT: invention is aimed at increasing the reliability of turbojet engines.
18 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| FAN DISK OF TURBOJET ENGINE AND TURBOJET ENGINE | 2014 |
|
RU2761506C2 |
| MODULAR ENGINE, SUCH AS JET ENGINE, WITH SPEED REDUCTION GEAR | 2014 |
|
RU2674098C1 |
| METHOD OF DISMOUNTING TURBOJET ENGINE, DEVICE FOR HEATING | 2013 |
|
RU2635741C2 |
| IMPELLER FOR TURBOJET AND TURBOJET INCLUDING SAID IMPELLER | 2008 |
|
RU2487248C2 |
| CYCLOIDAL REDUCER, FAN MODULE OF DUAL-FLOW TURBOJET ENGINE AND DUAL-FLOW TURBOJET ENGINE | 2013 |
|
RU2627990C2 |
| TURBO-JET ENGINE | 1991 |
|
RU2027054C1 |
| DOUBLE-FLOW TURBINE JET ENGINE | 2019 |
|
RU2730565C1 |
| FAN ROTOR AND TURBOJET ENGINE | 2012 |
|
RU2594037C2 |
| INNER HOUSING OF INTERMEDIATE HOUSING FOR AIRCRAFT TURBOJET ENGINE, INTERMEDIATE HOUSING, INCLUDING SUCH INNER HOUSING, AND TURBOJET ENGINE, INCLUDING SUCH INTERMEDIATE HOUSING | 2016 |
|
RU2714388C2 |
| TURBOMACHINE ROTOR AND TURBOJET ENGINE | 2012 |
|
RU2607986C2 |
