Modular chevron exhaust nozzle

Power plants – Reaction motor – Particular exhaust nozzle feature

Reexamination Certificate

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C239S265390

Reexamination Certificate

active

07926285

ABSTRACT:
An exhaust nozzle for a gas turbine engine includes a modular chevron. The chevron includes dual skins fixedly joined together at a base flange, and at a rim extending along the trailing edge of the chevron between the base and apex thereof.

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U.S. Appl. No. 11/751,174, filed May 21, 2007, Renggli.
General Electric Company, “CF6-80C2 Conic Nozzle,” in public use in USA more than one year before Jun. 1, 2007, single page.

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