Nozzles for gas turbine engines
AssigneeRolls-Royce (1971) Limited
InventorDouglas John Nightingale
Life of this patent
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Abstract
A variable area convergent/divergent iris nozzle for a gas turbine engine has a plurality of interdigitated master and slave petals. Each master petal has a pair of axially spaced rollers which run on guide tracks mounted on the engine jet pipe. A pivotable link connects the upstream end of each master petal to a unison ring which is axially movable to translate the petals thereby varying the area of the nozzle.
Claims7
A variable area nozzle for a gas turbine engine comprising fixed structure including a jet pipe, a circumferential array of nozzle petals, including certain master petals arranged about the discharge opening of the jet pipe and means supporting the petals for nozzle area varying movement relative to the jet pipe, said means including in respect of at least said master nozzle petals respective pairs of axially spaced apart rollers which engage guide track surfaces supported from said structure, there being, in respect of the upstream roller of each said pair, a radially outwardly facing guide track surface and in respect of the downstream roller of each said pair a radially inwardly facing guide track surface, the radially inwardly and outwardly facing guide track surfaces being mutually inclined for changing the relative petal inclinations on operation of means for simultaneously moving all the said petals along said guide track surfaces, there being further provided structure interconnecting the radially inwardly facing guide track surfaces whereby in operation radially outward loads from the said downstream rollers are borne at least partially by tension in said structure.
Dependencies are inferred from the claim text.