Fuel and air injection handling system for a combustor of a rotating detonation engine
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United States of America Patent
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Dec 27, 2022
Grant Date -
Apr 25, 2019
app pub date -
Oct 18, 2018
filing date -
Oct 24, 2017
priority date (Note) -
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Abstract
A fuel and air injection handling system for a rotating detonation engine is provided. The system includes a compressor configured to compress air received via a compressor inlet and configured to output the air that is compressed as swirling, compressed air through a compressor outlet. The system also includes an annular rotating detonation combustor fluidly coupled with the compressor outlet. The annular rotating detonation combustor has a detonation cavity that extends around an annular axis, the annular rotating detonation combustor configured to combust the compressed air from the compressor in detonations that rotate within the detonation cavity around the annular axis of the annular rotating detonation combustor. The annular rotating detonation combustor is fluidly and directly coupled with the compressor outlet.
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