FIELD: gas-turbine engine engineering.
SUBSTANCE: blade (10) comprises metallic shaped part (14) provided with recess (34) on its first side (16) which receives filler (38). The recess has a number of cells (34b) separated by ribs (36) which are submerged into the filler.
EFFECT: improved design.
20 cl, 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| COMPOSITE BLADE OF GAS TURBINE ENGINE WITH REINFORCING METAL ELEMENT | 2007 |
|
RU2445465C2 |
| INNER NOZZLE FOR TEEMING OF FUSED METAL FROM METAL VESSEL AND METHOD OF ITS FABRICATION | 2011 |
|
RU2562870C2 |
| FAN BLADE OF GAS TURBINE ENGINE | 2017 |
|
RU2661433C1 |
| FAN BLADE OF GAS TURBINE ENGINE | 2017 |
|
RU2667220C1 |
| ENGINE WITH COMPOUND TURBINE COOLING | 2007 |
|
RU2447302C2 |
| GAS TURBINE ENGINE FAN BLADE | 2017 |
|
RU2675161C1 |
| FAN BLADE OF GAS TURBINE ENGINE | 2017 |
|
RU2661439C1 |
| TURBINE BLADE | 1993 |
|
RU2088764C1 |
| FAN FOR TURBOMACHINE | 2014 |
|
RU2683343C1 |
| LONG HOLLOW WIDE-CHORD FAN OF AIRCRAFT TRDD FAN AND METHOD OF ITS MANUFACTURING | 2019 |
|
RU2726955C1 |
