Turbine rotor blade of a gas turbine
US9593584B2 · kind B2 · utility
4Cited by
18References
20Claims
0Family size
Assignees
Inventors
Key dates
| Filing date | Oct 24, 2013 |
| Grant date | Mar 14, 2017 |
| Priority date | — |
| Expiry date | Jun 10, 2035 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2240/307
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
The present invention relates to a turbine rotor blade of a gas turbine with a blade tip, said blade tip having at least on its suction side, extending from a stagnation point on the blade leading edge to an intersection point of the suction-side profile line of the blade with a trailing-edge circle, an overhang which is substantially zero at the stagnation point and at the intersection point and which has a maximum value at around 40% of the running length of the suction-side overhang.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.