Methods and apparatus for generating gas turbine engine...

Power plants – Reaction motor – Method of operation

Reexamination Certificate

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C060S226100, C060S248000, C060S224000

Reexamination Certificate

active

10895585

ABSTRACT:
Methods and apparatus for generating thrust from a gas turbine engine using a pulse detonation system is provided. The gas turbine engine includes a fan assembly, and a bypass duct channeling air to a core engine and the pulse detonation system. The method includes injecting a charge of fuel into a pulse detonation tube that is coupled radially outward from the core engine, and controlling a supply of air from the fan into the pulse detonation tube through an opening in the inlet end of the pulse detonation tube using a rotary valve that is positioned radially outward from the core engine.

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International Search Report;London Patent Office; Dated Oct. 12, 2005; Reference 13DV-145502/10676; Application No. GB0510168.8; 3 pgs.

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