Ablative seal
Abstract
Abstract A composite sealing structure for sealing the gap between stationary and moving surfaces of a gas impelling device, for example a turbine. Preferably, the sealing structure is on the surface of the stationary member. The sealing structure is adapted, in the event of a rub, to melt immediately at the rubbed surface whereby the metal is molten and readily displaced to allow free passage of the rubbing surface of the other member. The sealing structure includes an outer sealing layer as the proximate surface of one member and an intermediate bonding layer bonding the sealing layer to the surface of the member. The sealing layer is of a metal alloy having a melting point close to, but above the operating temperature in the impelling device and below the melting point of the surface of the one member. The bonding layer is of an alloy compatible with the sealing layer alloy and with the base metal, forms a firm bond with both the sealing layer and the base metal surface, is adapted to melt initially at a temperature lower than that of either, has a remelt temperature above the operating temperature of the impelling device, and good strength at the operating temperature. Preferably, the alloys used for the sealing and bonding layers are brazing alloys.
Inventors
- 👤 H Dunthorne
Bibliographic Details
Claims Analysis
Total Claims: 7References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1977-09-16 | 1978-03-18 | 1978-09-17 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1981-09-16 | 1982-03-18 | 1982-09-17 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1985-09-16 | 1986-03-18 | 1986-09-17 | $7700.00 | Window Closed / Lapsed |