GAS TURBINE APPARATUS WITH COUNTER-ROTATING BLADES
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United States of America Patent
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Issued Date -
Jun 9, 2022
app pub date -
Dec 7, 2020
filing date -
Dec 7, 2020
priority date (Note) -
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status (Latency Note)
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Abstract
A gas turbine apparatus has a main shaft, a first plurality of blades mounted to the main shaft, a second plurality of blades each interposed between blades of the first plurality of blades, a barrel affixed to the second set of blades, a fuel line opening to an interior of the barrel, and an igniter cooperative with the interior of the barrel and adapted to selectively ignite fuel in the barrel. The first plurality of blades rotate in a direction opposite to a direction of rotation of the second plurality of blades. The fuel line passes a fuel into the interior of the barrel.
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