Exit area control mechanism for convergent divergent nozzles

F - Mech Eng,Light,Heat,Weapons – 02 – K

Patent

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F02K 1/12 (2006.01) F02K 1/15 (2006.01)

Patent

CA 2308131

A mechanism for controlling the exit area of convergent-divergent nozzles comprises a synchronizing ring concentric with the nozzle axis, joined to a group of angled lever arms that pivot around a preferably radial axis around the nozzle structure, determining the position of a group of compression struts which are joined at one side to the mentioned angled lever arms by a pivot joint and on their opposite ends to a group of divergent petals, such that for every circumferential position of the synchronizing ring, the exhaust area of the nozzle is determined.

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