Airfoil nozzle and shroud assembly
Abstract
An airfoil and nozzle assembly including an outer shroud having a plurality of vane members attached to an inner surface and having a cantilevered end. The assembly further includes a inner shroud being formed by a plurality of segments. Each of the segments having a first end and a second end and having a recess positioned in each of the ends. The cantilevered end of the vane member being positioned in the recess. The airfoil and nozzle assembly being made from a material having a lower rate of thermal expansion than that of the components to which the airfoil and nozzle assembly is attached.
- Inventors:
-
- Maitland, FL
- San Diego, CA
- Issue Date:
- Research Org.:
- Solar Turbines Inc
- OSTI Identifier:
- 870975
- Patent Number(s):
- 5634768
- Assignee:
- Solar Turbines Incorporated (San Diego, CA)
- Patent Classifications (CPCs):
-
F - MECHANICAL ENGINEERING F01 - MACHINES OR ENGINES IN GENERAL F01D - NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- DOE Contract Number:
- AC02-92CE40960
- Resource Type:
- Patent
- Country of Publication:
- United States
- Language:
- English
- Subject:
- airfoil; nozzle; shroud; assembly; including; outer; plurality; vane; attached; inner; surface; cantilevered; formed; segments; recess; positioned; material; rate; thermal; expansion; components; outer shroud; nozzle assembly; thermal expansion; inner surface; assembly including; inner shroud; shroud assembly; /415/
Citation Formats
Shaffer, James E, and Norton, Paul F. Airfoil nozzle and shroud assembly. United States: N. p., 1997.
Web.
Shaffer, James E, & Norton, Paul F. Airfoil nozzle and shroud assembly. United States.
Shaffer, James E, and Norton, Paul F. Wed .
"Airfoil nozzle and shroud assembly". United States. https://www.osti.gov/servlets/purl/870975.
@article{osti_870975,
title = {Airfoil nozzle and shroud assembly},
author = {Shaffer, James E and Norton, Paul F},
abstractNote = {An airfoil and nozzle assembly including an outer shroud having a plurality of vane members attached to an inner surface and having a cantilevered end. The assembly further includes a inner shroud being formed by a plurality of segments. Each of the segments having a first end and a second end and having a recess positioned in each of the ends. The cantilevered end of the vane member being positioned in the recess. The airfoil and nozzle assembly being made from a material having a lower rate of thermal expansion than that of the components to which the airfoil and nozzle assembly is attached.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {1997},
month = {1}
}
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