Pintle-controlled propulsion system with external ring actuator
View Patent ↗A propulsion system with a divergent-convergent nozzle is provided with variable thrust by a pintle whose position relative to the nozzle throat is controlled by an actuator that includes a rotor that external to, and encircling, the nozzle, and that is coupled to either the pintle or to the nozzle shell by a linkage that translates the rotary movement of the rotor into linear movement of either the pintle or the shell.
1. A pintle-controlled propulsion nozzle comprising:
(a) a shell shaped forming a propulsion gas flow passage including a throat;
(b) a pintle positioned inside said throat to define a gap around said pintle for flow of propulsion gas through said throat, said pintle and said shell joined by a movable mounting that allows variation in positions of said pintle and said shell relative to each other and consequently in width of said gap; and
(c) an actuator external to said shell, said actuator operatively joined to either said pintle or said shell to cause movement thereof and consequently variation in said width of said gap, said actuator comprising a rotor encircling said shell and a linkage to translate rotational movement of said rotor into linear movement.
2. The pintle-controlled propulsion nozzle of claim 1 wherein said actuator is operatively joined to said pintle.
3. The pintle-controlled propulsion nozzle of claim 1 wherein said actuator is upstream of said throat.
4. The pintle-controlled propulsion nozzle of claim 1 wherein said actuator is downstream of said throat.
5. The pintle-controlled propulsion nozzle of claim 1 wherein said shell has a longitudinal axis, said nozzle further comprising an inlet to said throat that is coaxial with said shell.
6. The pintle-controlled propulsion nozzle of claim 1 wherein said shell has a longitudinal axis, said nozzle further comprising an inlet to said throat that is lateral to said shell.