Axially staged combustion system for a gas turbine engine

Power plants – Combustion products used as motive fluid – Combustion products generator

Reexamination Certificate

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C060S740000, C431S278000

Reexamination Certificate

active

07631499

ABSTRACT:
An axially staged combustion system is provided for a gas turbine engine comprising a main body structure having a plurality of first and second injectors. First structure provides fuel to at least one of the first injectors. The fuel provided to the one first injector is adapted to mix with air and ignite to produce a flame such that the flame associated with the one first injector defines a flame front having an average length when measured from a reference surface of the main body structure. Each of the second injectors comprising a section extending from the reference surface of the main body structure through the flame front and having a length greater than the average length of the flame front. Second structure provides fuel to at least one of the second injectors. The fuel passes through the one second injector and exits the one second injector at a location axially spaced from the flame front.

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Norman Chigier, The Future of Atomization and Sprays, Department of Mechanical Engineering, Carnegie Mellon University, Pittsburgh, Pennsylvania, USA, Sep. 2005.

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