Method and apparatus for cooling gas turbine engine rotor blade
Abstract
A rotor blade (40) for a gas turbine engine, includes a platform (62) including a radially outer surface (152) and a radially inner surface (144). An airfoil (60) extends radially outward from the platform. A shank (64) extends radially inward from the platform. A dovetail (66) extends from the shank such that an internal cavity is defined at least partially by the airfoil, the platform, the shank, and the dovetail. A cooling circuit extends through a portion of the shank for supplying cooling air from the cavity for impingement cooling of the platform radially inner surface.

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Every citation, both ways
| Document | Relation | Office | Category | Cited during | Relevant claims |
|---|---|---|---|---|---|
| EP0801208A2 | Cites | European Patent Office (EPO) | Y | Search report | 8 |
| EP1178181A2 | Cites | European Patent Office (EPO) | XYI | Search report | 1,3 |
| EP1205636A2 | Cites | European Patent Office (EPO) | X | Search report | 1,3 |
| US2912223A | Cites | United States of America | Y | Search report | 9,10 |
| US2915279A | Cites | United States of America | A | Search report | 4,5 |
| JPS6463605A | Cites | Japan | Y | Search report | 2,4-6 |
14 members in 4 offices; this record represents the family
Priority claims2
| Document | Office | Kind | Date |
|---|---|---|---|
| 699060 | United States of America | – | |
| 69906003 | United States of America | A |
Members14
| Document | Office | Kind | |
|---|---|---|---|
| CN1611748A | China | A | |
| EP1528224A2 | European Patent Office (EPO) | A2 | |
| US2005095128A1 | United States of America | A1 | |
| US2005095129A1 | United States of America | A1 | |
| JP2005133726A | Japan | A | |
| EP1589193A2 | European Patent Office (EPO) | A2 | |
| CN1690365A | China | A | |
| JP2005307981A | Japan | A | |
| US7147440B2 | United States of America | B2 | |
| US7600972B2 | United States of America | B2 | |
| CN1611748B | China | B | |
| JP4762524B2 | Japan | B2 | |
| EP1528224A3This record | European Patent Office (EPO) | A3 | |
| EP1528224B1 | European Patent Office (EPO) | B1 |
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| Expiry of rightR071 | R071 | DE | |
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Numbers
- Publication
- 1528224
- Application
- 42566463
Titles3
- German
- Methode und Einrichtung zur Kühlung einer Gasturbinenschaufel
- English
- Method and apparatus for cooling gas turbine engine rotor blade
- French
- Méthode et dispositif de refroidissement d'une aube de turbine
Classification
- CPC, 4
- F01D5/187
- F05D2260/201
- F05D2240/81
- Y10T29/49321
- IPC, 3
- F01D5 18
- F01D5 30
- F02C7 18
Designated states33
- Contracting states, 28
- Austria
- Belgium
- Bulgaria
- Switzerland
- Cyprus
- Czechia
- Germany
- Denmark
- Estonia
- Spain
- Finland
- France
- United Kingdom
- Greece
- Hungary
- Ireland
- Italy
- Liechtenstein
- Luxembourg
- Monaco
- Netherlands (Kingdom of the)
- Poland
- Portugal
- Romania
and 4 moreShow fewer
- Sweden
- Slovenia
- Slovakia
- Türkiye
- Extension states, 5
- Albania
- Croatia
- Lithuania
- Latvia
- North Macedonia