| People | Locations | Statistics |
|---|---|---|
| Naji, M. |
| |
| Motta, Antonella |
| |
| Aletan, Dirar |
| |
| Mohamed, Tarek |
| |
| Ertürk, Emre |
| |
| Taccardi, Nicola |
| |
| Kononenko, Denys |
| |
| Petrov, R. H. | Madrid |
|
| Alshaaer, Mazen | Brussels |
|
| Bih, L. |
| |
| Casati, R. |
| |
| Muller, Hermance |
| |
| Kočí, Jan | Prague |
|
| Šuljagić, Marija |
| |
| Kalteremidou, Kalliopi-Artemi | Brussels |
|
| Azam, Siraj |
| |
| Ospanova, Alyiya |
| |
| Blanpain, Bart |
| |
| Ali, M. A. |
| |
| Popa, V. |
| |
| Rančić, M. |
| |
| Ollier, Nadège |
| |
| Azevedo, Nuno Monteiro |
| |
| Landes, Michael |
| |
| Rignanese, Gian-Marco |
|
Haje, Detlef
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (4/4 displayed)
- 2011Thermoplastic last-stage blade
- 2011Turbinenschaufel, Turbinenwelle, Turbinenanlage und Verfahren zur Montage der Turbinenschaufel
- 2010Verfahren zum Anbringen bzw. Herstellen eines geschlossenen Deckbandes für eine Laufbeschaufelung einer Turbinenstufe sowie Laufbeschaufelung einer Turbinenstufe für eine Turbine
- 2010Verfahren zum Anbringen bzw. Herstellen eines geschlossenen Deckbandes für eine Laufbeschaufelung einer Turbinenstufe sowie Laufbeschaufelung einer Turbinenstufe für eine Turbine
Places of action
| Organizations | Location | People |
|---|
patent
Turbinenschaufel, Turbinenwelle, Turbinenanlage und Verfahren zur Montage der Turbinenschaufel
Abstract
The invention relates to a turbine blade (1), a turbine shaft (2) having such a turbine blade (1), a turbine system comprising a turbine shaft (2) having such a turbine blade (1), and a method for installing the turbine blade (1), resulting in that the turbine blade (1) is made of a fiber composite material and, at the same time, the bearing strength of the turbine blade (1) or the blade root (3) of the turbine blade (1) is increased relative to metal turbine blades by reducing stress concentrations at locations of the blade root (3) at which the blade root (3) is supported by corresponding wall segments (6) of a groove (4) of the turbine shaft (2), thus extending the service life of the turbine blade (1) and thus the turbine shaft (2) and the turbine system having such turbine blades (1). The aim is achieved by a particularly fine fit of the blade root (3) of the turbine blade (1) in the shape of the groove (4) of the turbine shaft (2), due to the effect of heating on the blade root (3) brought about by precautionary heating (8) during assembly to the turbine shaft (2), and consequently of auto-adaptation of the shape to the shape of the groove (4) of the turbine shaft (2).