Actuation mechanism for a convertible gas turbine propulsion...

Power plants – Reaction motor – With thrust direction modifying means

Reexamination Certificate

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C060S785000, C251S063500

Reexamination Certificate

active

08061119

ABSTRACT:
An actuation mechanism for use in a convertible gas turbine propulsion system comprises a plenum, a pneumatically powered drive body and a spring system. The plenum receives pressurized air from the convertible gas turbine propulsion system. The pneumatically powered drive body is connected to the plenum to receive pressurized air to axially move the drive body in a first direction. The spring system is connected to the drive body to axially move the drive body in a second direction.

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