High temperature turbine engine structure
Patent
·
OSTI ID:868860
- Mesa, AZ
- Tempe, AZ
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.
- DOE Contract Number:
- DEN3-167
- Assignee:
- Allied-Signal Inc. (Morris Township, Morris County, NJ)
- Patent Number(s):
- US 5228284
- OSTI ID:
- 868860
- Country of Publication:
- United States
- Language:
- English
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High temperature turbine engine structure
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Related Subjects
temperature
turbine
engine
structure
ceramic
metallic
housing
journals
rotor
disk-like
shroud
portion
supported
maintains
close
running
clearance
spacer
assembly
despite
differential
thermal
movements
running clearance
close running
engine structure
housing portion
differential thermal
metallic housing
turbine engine
shroud portion
temperature turbine
temperature ceramic
thermal movements
spacer assembly
assembly maintains
metallic turbine
ceramic spacer
ceramic disk-like
despite differential
disk-like shroud
thermal movement
/60/415/
turbine
engine
structure
ceramic
metallic
housing
journals
rotor
disk-like
shroud
portion
supported
maintains
close
running
clearance
spacer
assembly
despite
differential
thermal
movements
running clearance
close running
engine structure
housing portion
differential thermal
metallic housing
turbine engine
shroud portion
temperature turbine
temperature ceramic
thermal movements
spacer assembly
assembly maintains
metallic turbine
ceramic spacer
ceramic disk-like
despite differential
disk-like shroud
thermal movement
/60/415/