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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Bibliographic Details
Main Author Nadkarni, Vaibhav
Format Patent
LanguageEnglish
French
German
Published 19.08.2020
Subjects
BLASTING
COMBUSTION APPARATUS
COMBUSTION PROCESSES
GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
HEATING
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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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.
Bibliography:Application Number: EP20120198795