초록 ▼

A nozzle/valve device for a ducted rocket motor is provided. The nozzle/valve device employs a design in which a nozzle throat blockage element can be moved by translational motion within the nozzle throat section of the device. The blockage element is designed so that in the closed position the noz

A nozzle/valve device for a ducted rocket motor is provided. The nozzle/valve device employs a design in which a nozzle throat blockage element can be moved by translational motion within the nozzle throat section of the device. The blockage element is designed so that in the closed position the nozzle throat has a minimum cross-sectional flow area and therefore the nozzle throat is never fully closed. The seals employed in the nozzle/valve device are isolated from contact with reaction products of the gas generator and effective use of minimum amounts of erosion resistant materials is achieved.

대표청구항 ▼

A nozzle/valve device for controlling flow of high temperature gases from a fuel generator to a secondary combustion chamber of a ducted rocket motor, said nozzle/valve comprising, in combination, a valve body having a stem section and two flow sections intersecting and attached to the ends of said

A nozzle/valve device for controlling flow of high temperature gases from a fuel generator to a secondary combustion chamber of a ducted rocket motor, said nozzle/valve comprising, in combination, a valve body having a stem section and two flow sections intersecting and attached to the ends of said stem section, said stem section comprising an outer stem member and a stem insulator for said outer stem member housed with said outer stem member and extending throughout the length of the outer stem member, the interior surface of said stem insulator defining a central longitudinal stem cavity extending throughout the length of the stem insulator and containing openings in registration extending transversely through the side walls of said outer stem member and stem insulator; flow sections respectively comprising a tubular flow insulator contiguous with the upper and lower ends of said stem insulator and defining flow ports in registration with said transversely extended openings in said stem insulator, to form flow channels and transversely intersecting said central longitudinal cavity; a guillotine rod having two end positioned flow blockage elements joined by a heat insulator portion, said blockage elements being mounted within said central longitudinal stem cavity in slidable contact with the interior surface of said stem insulator and intersecting said flow channels, each flow blockage element having a hole spaced with respect to the other hole to individually complete the definition of said flow channels, said guillotine rod being endwise linked to an actuator device means for positioning the guillotine rod, as desired, within said central longitudinal stem cavity to effect a position in which the spaced holes of said flow blockage elements are in desired registration with the remainder of each flow channel, to provide the desired amount of interference with flow of gases through said flow channels from said generator to said secondary combustion chamber.