Gas turbine engine with fan variable area nozzle having a...

Power plants – Reaction motor – Particular exhaust nozzle feature

Reexamination Certificate

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C060S785000

Reexamination Certificate

active

07966827

ABSTRACT:
A turbofan engine includes a fan variable area nozzle having a multiple of vents through a fan nacelle and rotatable elements rotatable within the vents by an actuator system. Rotation of the rotatable element within each vent changes the effective area of the fan nozzle exit area to permit efficient operation at a multiple of flight conditions.

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PCT Patent Application No. PCT/2006/39049, Fan Variable Area Nozzle With Cable Actuator System, filed Oct. 12, 2006.
PCT Patent Application No. PCT/2006/39794, Gas Turbine Engine With Axial Movable Fan Variable Area Nozzle, filed Oct. 12, 2006.
PCT Patent Application No. PCT/2006/39796, Gas Turbine Engine With Louvered Fan Variable Area Nozzle, filed Oct. 12, 2006.
PCT Patent Application No. PCT/2006/39948, Fan Variable Area Nozzle With Adaptive Structure, filed Oct. 12, 2006.
PCT Patent Application No. PCT/2006/39953, Fan Variable Area Nozzle With Electromechanical Actuator, filed Oct. 12, 2006.
PCT Patent Application No. PCT/2006/39989, Gas Turbine Engine With Circumferential Sleeved Fan Variable Area Nozzle, filed Oct. 12, 2006.
PCT Patent Application No. PCT/2006/40248, Gas Turbine Engine With Rotationally Overlapped Fan Variable Area Nozzle, filed Oct. 12, 2006.
PCT Patent Application No. PCT/2006/40249, Gas Turbine Engine Fan Variable Area Nozzle With Swivalable Insert System, filed Oct. 12, 2006.
PCT Patent Application No. PCT/2006/40250, Fan Variable Area Nozzle Positional Measurement System, filed Oct. 12, 2006.
PCT Patent Application No. PCT/2006/40251, Gas Turbine Engine Bifurcation Located Fan Variable Area Nozzle, filed Oct. 12, 2006.
PCT Patent Application No. PCT/2007/63255, Fan Variable Area Nozzle for a Gas Turbine Engine Fan Nacelle With Drive Ring Actuation System, filed Mar. 5, 2007.
PCT Patent Application No. PCT/2006/39936, Fan Variable Area Nozzle for a Gas Turbine Engine Fan Nacelle With Sliding Actuation System, filed Oct. 12, 2006.

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