초록 ▼

In a jet pipe and variable area final nozzle assembly, the jet pipe 12 is necked at a region upstream of the final nozzle to reduce the diameter of the remainder of the jet pipe downstream of the neck to a diameter more nearly equal to but not less than the maximum throat area of the nozzle. The noz

In a jet pipe and variable area final nozzle assembly, the jet pipe 12 is necked at a region upstream of the final nozzle to reduce the diameter of the remainder of the jet pipe downstream of the neck to a diameter more nearly equal to but not less than the maximum throat area of the nozzle. The nozzle flaps are pivoted to the end of the jet pipe, although they could alternatively be translatable, and have an upstream portion 20 which overlies the jet pipe. An actuating mechanism preferably in the form of a unison ring 30 operated by jacks is mounted around the reduced diameter portion of the jet pipe and operates on the upstream portions of the nozzle flaps via a roller and cam arrangement 26, 24 to vary the area of the nozzle. An outer fairing 14 which now need be of no greater diameter than the maximum diameter of the jet pipe surrounds the jet pipe and the actuating mechanism (see FIG. 1).

대표청구항 ▼

A jet pipe and variable area final nozzle assembly for a gas turbine engine, comprising: a jet pipe having a downstream end; a plurality of nozzle flaps each connected by means of a fixed pivot to substantially the downstream end of the jet pipe for pivoting movement to vary the outlet area of the n

A jet pipe and variable area final nozzle assembly for a gas turbine engine, comprising: a jet pipe having a downstream end; a plurality of nozzle flaps each connected by means of a fixed pivot to substantially the downstream end of the jet pipe for pivoting movement to vary the outlet area of the nozzle, a portion of each flap extending upstream of said pivot and overlying said jet pipe; an outer fairing having a maximum diameter substantially equal to the maximum jet pipe diameter, fixed to said jet pipe and surrounding the downstream end of said jet pipe and said nozzle flaps, said jet pipe being necked downstream of its connection to the fairing to a diameter more nearly equal to but not less than the maximum throat area of the nozzle; an annular space defined by the necked portion of said jet pipe and portions downstream therefrom, and the corresponding portions of said outer fairing; and an actuation system disposed in said annular space, comprising: a translatable ring disposed around said jet pipe; an actuating mechanism connected to said fairing for translating said translatable ring; and interconnecting means for interconnecting said translatable ring and said nozzle flaps, to operate said flaps, said ring being interconnected to said flaps upstream of said pivot and being located upstream of said pivot, said actuating mechanism being connected to said fairing on the downstream side of said translatable ring, the translation of said ring causing the pivoting of said flaps.