SYSTEME DE FOURNITURE DE COMBUSTIBLE
A fuel delivery system for the combustor 14 of a gas turbine engine comprises a combustor support pin 26, a fuel atomizer 22, and a tube 30 for delivering fuel to the atomizer. The combustor support pin provides axial support for the combustor and includes a duct 28 in which the fuel delivery tube i...
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Main Author | |
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Format | Patent |
Language | French |
Published |
25.10.1991
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Edition | 4 |
Subjects | |
Online Access | Get full text |
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Summary: | A fuel delivery system for the combustor 14 of a gas turbine engine comprises a combustor support pin 26, a fuel atomizer 22, and a tube 30 for delivering fuel to the atomizer. The combustor support pin provides axial support for the combustor and includes a duct 28 in which the fuel delivery tube is removably located. Fuel is delivered into an annular duct 36 by the tube via a circumferential groove 56 of progressively reducing depth. Swirl vanes 50 control air flow at the entry to the duct 36. |
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Bibliography: | Application Number: FR19850018187 |