Aircraft engine with opposed piston engine
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United States of America Patent
Stats
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Jun 11, 2024
Grant Date -
Dec 8, 2022
app pub date -
Sep 3, 2020
filing date -
Sep 3, 2020
priority date (Note) -
In Force
status (Latency Note)
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Abstract
An aircraft engine has a hollow driveshaft with a spool coaxial with the driveshaft and extending through the driveshaft to rotate independently of the driveshaft. A first harmonic cam is mounted on the driveshaft and a second spaced apart harmonic cam is mounted on the spool. At least one combustion cylinder is positioned between the cams along a combustion cylinder axis that is parallel with but radially spaced apart from the driveshaft. A piston assembly is disposed in each end of the combustion cylinder, with each piston assembly engaging a separate cam. A high-pressure compressor turbine is mounted on the driveshaft and driven by movement of a piston assembly, compressing air for the combustion cylinder. A rotating component is mounted on the spool and driven by movement of the other piston assembly. The rotating component may be another compressor turbine, a drive turbine, a fan or a propeller.

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Patent Owner(s)
Patent Owner | Address | |
---|---|---|
HTS LLC | 11515 SUMMERHILL LANE HOUSTON TX 77024 |
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- [Patents Count]
Inventor(s)
Inventor Name | Address | # of filed Patents | Total Citations |
---|---|---|---|
Schneider, Gustavo Ludwig | Rio de Janeiro, BR | 9 | 7 |
Todeschini, Hilgert Carlos Marcelo | Bento Goncalves, BR | 6 | 3 |
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