AT291677T
Turbine blade with a hot gas suporting platform and a mechanical load suporting platform
Abstract
The invention claims a turbine blade (1), wherein a integrally formed; the blade of the blade axis (4) extended (2). To be is a high heat high-load mechanical and load at the same time, wherein the edges are ensure consumption of the coolant economic; based on the invention, (8) is formed with in a blade (2) is transversely (12) and hot working medium platform (12) on the hot working medium platform of the blade axis (4) of the bearing platform (14); the bearing platform (14) (12) is (2) and solderless joint through the blade between the hot working medium bed.
Term
No projected expiry on record.
- Priority and filed
- Granted
- Today
11 members in 6 offices
Members11
| Document | Office | Kind | |
|---|---|---|---|
| US2003133802A1 | United States of America | A1 | |
| EP1329593A1 | European Patent Office (EPO) | A1 | |
| JP2003214109A | Japan | A | |
| CN1436920A | China | A | |
| EP1329593B1 | European Patent Office (EPO) | B1 | |
| AT291677TThis record | Austria | T | |
| ATE291677T1 | Austria | T1 | |
| DE50202538D1 | Germany | D1 | |
| US6887040B2 | United States of America | B2 | |
| CN1313707C | China | C | |
| JP4249990B2 | Japan | B2 |
1 legal event, as the office reported them to INPADOC
Events
| Event | Code | |
|---|---|---|
| Ceased due to non-payment of the annual feeCeasedREN | REN |
Numbers
- Application
- 2001267
Titles2
- German
- TURBINENSCHAUFEL MIT EINER HEISSGASPLATTFORM UND EINER LASTPLATTFORM
- English
- TURBINE BUCKET WITH A HOT GAS PLATFORM AND A LOAD PLATFORM
Classification
- CPC, 4
- F01D9/042
- F01D5/147
- F01D9/04
- F05D2240/80
- IPC, 3
- F01D5 14
- F01D9 02
- F01D9 04