Combustor of a turbomachine
A combustor (11) of a turbomachine is provided and includes an assembly defining an interior (220) and being configured to direct air to flow along an annulus (30) in a first direction (D1) about the interior and in a second direction (D2) toward the interior, the first and second directions being s...
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Main Author | |
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Format | Patent |
Language | English French German |
Published |
10.07.2013
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Subjects | |
Online Access | Get full text |
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Summary: | A combustor (11) of a turbomachine is provided and includes an assembly defining an interior (220) and being configured to direct air to flow along an annulus (30) in a first direction (D1) about the interior and in a second direction (D2) toward the interior, the first and second directions being substantially opposed, a manifold (40) configured to be supplied with fuel and a tubular body (60) 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 (60) 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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Bibliography: | Application Number: EP20120198795 |