Methods and apparatus to reduce seal rubbing within gas turbine engines
Abstract
A seal assembly for a gas turbine engine (10) includes a first stage disk (30) and a second stage disk (32), a disk retainer (53), and an interstage seal assembly (50) extending between the first and second stage disks. The interstage seal assembly includes a radially outer shell (54) extending radially outwardly from a web portion (58). The outer shell includes an upstream arm (60) and a downstream arm (62) extending outwardly from the outer shell, the disk retainer between the outer shell upstream arm and the first stage disk, the downstream arm coupled to the second stage disk.

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| Document | Relation | Office | Cited during |
|---|---|---|---|
| EP0202188A1 | Cites | European Patent Office (EPO) | Search report |
| US2002187046A1 | Cites | United States of America | Search report |
| US3842595A | Cites | United States of America | Search report |
| US4582467A | Cites | United States of America | Search report |
| US5217348A | Cites | United States of America | Search report |
| US5288210A | Cites | United States of America | Search report |
| US6267553B1 | Cites | United States of America | Search report |
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Priority claims2
| Document | Office | Kind | Date |
|---|---|---|---|
| 653337 | United States of America | – | |
| 65333703 | United States of America | A |
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| Document | Office | Kind | |
|---|---|---|---|
| US2005047910A1 | United States of America | A1 | |
| EP1512841A2 | European Patent Office (EPO) | A2 | |
| JP2005098297A | Japan | A | |
| CN1611754A | China | A | |
| US6899520B2 | United States of America | B2 | |
| CN100404818C | China | C | |
| EP1512841A3This record | European Patent Office (EPO) | A3 | |
| EP1512841B1 | European Patent Office (EPO) | B1 |
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Numbers
- Publication
- 1512841
- Application
- 42552810
Titles3
- German
- Gasturbinendichtungen mit verringerter Reibung
- English
- Methods and apparatus to reduce seal rubbing within gas turbine engines
- French
- Réduction de frottement de joints d'étanchéité pour turbines à gaz
Classification
- CPC, 2
- F01D11/001
- F01D5/06
- IPC, 6
- F01D11 02
- F01D5 06
- F01D11 00
- F01D25 00
- F02C7 28
- F16J15 54
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