Multi-spool CO2 aircraft power system for operating multiple generators
Abstract
A CO2 bottoming cycle system includes a first compressor operatively connected to a first turbine through a first shaft. A first generator is operatively connected to the first shaft. A second compressor is fluidically connected to the first compressor. The second compressor is operatively connected to a second turbine through a second shaft. A second generator is operatively connected to the second shaft. The first turbine is fluidically connected to the second turbine.
- Inventors:
- Issue Date:
- Research Org.:
- Hamilton Sundstrand Corporation, Charlotte, NC (United States)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 1998328
- Patent Number(s):
- 11635023
- Application Number:
- 17/715,156
- Assignee:
- Hamilton Sundstrand Corporation (Charlotte, NC)
- DOE Contract Number:
- AR0001342
- Resource Type:
- Patent
- Resource Relation:
- Patent File Date: 04/07/2022
- Country of Publication:
- United States
- Language:
- English
Citation Formats
Taylor, Stephen H., and MacDonald, Malcolm P. Multi-spool CO2 aircraft power system for operating multiple generators. United States: N. p., 2023.
Web.
Taylor, Stephen H., & MacDonald, Malcolm P. Multi-spool CO2 aircraft power system for operating multiple generators. United States.
Taylor, Stephen H., and MacDonald, Malcolm P. Tue .
"Multi-spool CO2 aircraft power system for operating multiple generators". United States. https://www.osti.gov/servlets/purl/1998328.
@article{osti_1998328,
title = {Multi-spool CO2 aircraft power system for operating multiple generators},
author = {Taylor, Stephen H. and MacDonald, Malcolm P.},
abstractNote = {A CO2 bottoming cycle system includes a first compressor operatively connected to a first turbine through a first shaft. A first generator is operatively connected to the first shaft. A second compressor is fluidically connected to the first compressor. The second compressor is operatively connected to a second turbine through a second shaft. A second generator is operatively connected to the second shaft. The first turbine is fluidically connected to the second turbine.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2023},
month = {4}
}
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