FUEL INJECTION FOR INTEGRAL COMBUSTOR AND TURBINE VANE

A system includes a combustor (102). The combustor (102) has a combustor wall (104) with a combustor dome (106) at an upstream end (114) of the combustor wall (104), and an outlet (108) at a downstream end (116) of the combustor wall (104) opposite the upstream end (114). The combustor wall (104) in...

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Bibliographic Details
Main Authors PROCIW, Lev A, RYON, Jason
Format Patent
LanguageEnglish
French
German
Published 02.06.2021
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 system includes a combustor (102). The combustor (102) has a combustor wall (104) with a combustor dome (106) at an upstream end (114) of the combustor wall (104), and an outlet (108) at a downstream end (116) of the combustor wall (104) opposite the upstream end (114). The combustor wall (104) includes an inner wall portion (120) and an outer wall portion (122) defining an interior of the combustor therebetween. Each of the inner wall portion (120) and outer wall portion (122) extends from the combustor dome (106) to the downstream end (116) of the combustor wall (104). The combustor wall (104) includes an air cooling passage (112) embedded inside at least one of the inner wall portion (120) and the outer wall portion (122). The air cooling passage (112) extends from the upstream end (114) of the combustor wall (104) to the downstream end (116) of the combustor wall (104).
Bibliography:Application Number: EP20200206634