High temperature turbine engine structure
Patent
·
OSTI ID:5266293
A high temperature ceramic/metallic turbine engine includes a metallic housing which journals a rotor member of the turbine engine. A ceramic disk-like shroud portion of the engine is supported on the metallic housing portion and maintains a close running clearance with the rotor member. A ceramic spacer assembly maintains the close running clearance of the shroud portion and rotor member despite differential thermal movements between the shroud portion and metallic housing portion. 5 figures.
- Assignee:
- Allied Signal Inc., Morris Township, NJ ()
- Patent Number(s):
- US 5279031; A
- Application Number:
- PPN: US 7-843874
- OSTI ID:
- 5266293
- Resource Relation:
- Patent File Date: 27 Feb 1992
- Country of Publication:
- United States
- Language:
- English
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