FIELD: engines and pumps.
SUBSTANCE: turbine wheel comprises turbine blades (20) shaped aerodynamic part (102). Said aerodynamic shape has rated profile corresponding to data cited in the tables 1 through 11 wherein distances X, Y, Z and R are given in inches and the tables 1' through 11' wherein said distances are given in centimetres. Magnitudes if coordinates X and Y are smoothly connected by arc with radius R to make profile cross-section of said shaped part at every distance Z. Profile cross-section at distances Z are smoothly interconnected to produce a complete aerodynamic shape.
EFFECT: higher efficiency and bearing capacity of the blade of aerodynamic part and the blade on the whole.
10 cl, 3 dwg, 22 tbl
| Title | Year | Author | Number |
|---|---|---|---|
| TURBINE BLADE AERODYNAMIC PROFILE (VERSIONS) AND TURBINE (VERSIONS) | 2004 |
|
RU2350756C2 |
| TURBINE BLADE WITH AERODYNAMIC PROFILE (VERSIONS) AND TURBINE | 2004 |
|
RU2342538C2 |
| STEAM TURBINE WORKING BLADE | 2023 |
|
RU2815341C1 |
| TURBINE NOZZLE VANE (VERSIONS) AND TURBINE WITH NOZZLE VANES | 2012 |
|
RU2606736C2 |
| ROTOR BLADE (VERSIONS) AND TURBINE UNIT | 2011 |
|
RU2581501C2 |
| WORKING BLADE OF HIGH-LOAD STAGE OF STEAM TURBINE | 2023 |
|
RU2813717C1 |
| METHOD OF MODIFICATION OF STEAM TURBINE ROTOR BLADE, STEAM TURBINE ROTOR BLADE AND MULTISTAGE STEAM TURBINE | 2003 |
|
RU2264541C2 |
| GAS TURBINE BLADE | 2000 |
|
RU2178086C2 |
| BLADE WITH AIRFOIL AND AXIAL TURBOMACHINE | 2012 |
|
RU2549387C2 |
| TURBINE BLADE END RETAINING ELEMENT | 2007 |
|
RU2351769C1 |
