FIELD: non-displacement compressors and pumps.
SUBSTANCE: invention relates to a fan, in particular, for a small turbine engine, such as a jet engine, having a hub ratio corresponding to the ratio of the diameter of the inner limit of air intake section 26 at the radially internal ends of the leading edges of fan blades 10, divided by the diameter of the circle through which the outer ends of the fan blades pass, which has a value of 0.25 to 0.27.
EFFECT: present invention provides for a selection of particular dimensions of a fan for a turbine engine, and thus a significant improvement of performances and saving in weight.
16 cl, 10 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| FAN FOR TURBOMACHINE | 2014 |
|
RU2683343C1 |
| HIGH-PRESSURE TURBINE ROTOR OF A GAS TURBINE ENGINE (VERSIONS) | 2018 |
|
RU2691868C1 |
| GAS TURBINE ENGINE LOW-PRESSURE TURBINE (LPT) (VERSIONS), ROTOR SHAFT CONNECTION UNIT WITH LPT DISC, LPT ROTOR AIR COOLING PATH AND AIR FEEDING APPARATUS FOR COOLING LPT ROTOR BLADES | 2018 |
|
RU2684355C1 |
| FIRST STAGE DISC OF TURBOJET ENGINE LOW-PRESSURE COMPRESSOR ROTOR SHAFT (VERSIONS) | 2015 |
|
RU2603217C1 |
| TURBOMACHINE ROTOR AND TURBOJET ENGINE | 2012 |
|
RU2607986C2 |
| ROTOR SHAFT OF LOW PRESSURE COMPRESSOR OF TURBOJET ENGINE, CONNECTION ASSEMBLY OF ROTOR SHAFT DISKS OF LOW PRESSURE COMPRESSOR OF TURBOJET ENGINE, SPACER OF CONNECTION ASSEMBLY OF ROTOR SHAFT DISKS OF LOW PRESSURE COMPRESSOR OF TURBOJET ENGINE | 2014 |
|
RU2565133C1 |
| FAN ROTOR AND TURBOJET ENGINE | 2012 |
|
RU2594037C2 |
| TURBINE MODULE FOR GAS TURBINE ENGINE, COMPRESSOR JOINTED WITH SAID MODULE AND GAS TURBINE ENGINE | 2006 |
|
RU2403401C2 |
| ROTOR SHAFT OF LOW PRESSURE COMPRESSOR OF TURBOJET ENGINE, CONNECTION ASSEMBLY OF ROTOR SHAFT DISKS OF LOW PRESSURE COMPRESSOR OF TURBOJET ENGINE, SPACER OF CONNECTION ASSEMBLY OF ROTOR SHAFT DISKS OF LOW PRESSURE COMPRESSOR OF TURBOJET ENGINE | 2014 |
|
RU2565141C1 |
| TURBOJET ENGINE LOW-PRESSURE COMPRESSOR FIRST STAGE ROTOR IMPELLER (VERSIONS) | 2015 |
|
RU2603382C1 |
