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Seal accommodating thermal expansion between adjacent casings in gas turbine engine
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1992 |
| Description | A casing around a turbine and a casing around discharge nozzles have a concentrically arranged shell portion. The seal contains internal pressure while accommodating eccentric, expansion and axial travel. Arcuate seal segments have one leg sealing against a radial surface extending from the inner shell and the other leg against the outer shell. A linkage guides travel of the segments. |
| File Size | 353828 |
| Page Count | 8 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20080004315 |
| Archival Resource Key | ark:/13960/t83j8cr8r |
| Language | English |
| Publisher Date | 1992-08-25 |
| Access Restriction | Open |
| Subject Keyword | Mechanical Engineering Seals Stoppers Patents Thermal Expansion Gas Turbine Engines Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Patent |