Combustor of a turbomachine including multiple tubular radial pathways arranged at multiple circumferential and axial locations
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United States of America Patent
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Sep 15, 2015
Grant Date -
Jul 4, 2013
app pub date -
Jan 4, 2012
filing date -
Jan 4, 2012
priority date (Note) -
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Abstract
A combustor of a turbomachine is provided and includes an assembly defining an interior and being configured to direct air to flow along an annulus in a first direction about the interior and in a second direction toward the interior, the first and second directions being substantially opposed, a manifold configured to be supplied with fuel and a tubular body defining a pathway along which the air is transmittable in a third direction from the annulus to the interior, the third direction being transverse to the first and second directions. The tubular body includes a sidewall extendible through the manifold. The sidewall defines an injection hole within the manifold by which transmitted air is mixable with the fuel.
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