Rolling contact mounting arrangement for a ceramic combustor
Patent
·
OSTI ID:870115
- 328 Sneath Way, Alpine, CA 91901
- 1780 Geronimo Tr., Maitland, FL 32751
A combustor assembly having a preestablished rate of thermal expansion is mounted within a gas turbine engine housing having a preestablished rate of thermal expansion being greater than the preestablished rate of thermal expansion of the combustor assembly. The combustor assembly is constructed of a inlet end portion, a outlet end portion and a plurality of combustor ring segments positioned between the end portions. A mounting assembly is positioned between the combustor assembly and the gas turbine engine housing to allow for the difference in the rate of thermal expansion while maintaining axially compressive force on the combustor assembly to maintain contact between the separate components.
- Research Organization:
- Solar Turbines Inc
- DOE Contract Number:
- AC02-92CE40960
- Assignee:
- Boyd, Gary L. (328 Sneath Way, Alpine, CA 91901);Shaffer, James E. (1780 Geronimo Tr., Maitland, FL 32751)
- Patent Number(s):
- US 5457954
- OSTI ID:
- 870115
- Country of Publication:
- United States
- Language:
- English
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Related Subjects
rolling
contact
mounting
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ceramic
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preestablished
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mounted
gas
turbine
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inlet
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outlet
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segments
positioned
portions
allow
difference
maintaining
axially
compressive
force
maintain
separate
components
separate components
compressive force
rolling contact
combustor assembly
preestablished rate
turbine engine
thermal expansion
gas turbine
engine housing
mounting assembly
ceramic combustor
mounting arrangement
maintain contact
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/60/
contact
mounting
arrangement
ceramic
combustor
assembly
preestablished
rate
thermal
expansion
mounted
gas
turbine
engine
housing
constructed
inlet
portion
outlet
plurality
segments
positioned
portions
allow
difference
maintaining
axially
compressive
force
maintain
separate
components
separate components
compressive force
rolling contact
combustor assembly
preestablished rate
turbine engine
thermal expansion
gas turbine
engine housing
mounting assembly
ceramic combustor
mounting arrangement
maintain contact
separate component
/60/