Transition Piece Aft Frame

A transition piece aft frame (20) for a turbomachine is provided and includes a manifold (21) having an interior that is receptive of fuel and formed to define fuel injection holes (22) configured to inject the received fuel from the manifold interior toward a main flow of products of combustion flo...

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Bibliographic Details
Main Authors DICINTIO, RICHARD MARTIN, MELTON, PATRICK BENEDICT
Format Patent
LanguageEnglish
French
German
Published 08.05.2013
Subjects
AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
ENGINE PLANTS IN GENERAL
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
STEAM ENGINES
WEAPONS
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Summary:A transition piece aft frame (20) for a turbomachine is provided and includes a manifold (21) having an interior that is receptive of fuel and formed to define fuel injection holes (22) configured to inject the received fuel from the manifold interior toward a main flow of products of combustion flowing through the manifold. The manifold includes a main body having an interior facing surface (31) that faces the main flow of the products of the combustion and along which the fuel injection holes are defined.
Bibliography:Application Number: EP20120190991