Jet nozzle plug with varying, non-circular cross sections
View Patent ↗In a jet engine having a plug nozzle and a plug extending rearwardly from the nozzle exit, the improvement comprising a plug having successive cross sections spaced apart rearwardly of the nozzle exit, the cross sections transitioning from circular or near circular at the exit plane defined at the nozzle exit, to progressively non-circular, rearwardly.
1. In a jet engine having a plug nozzle and a plug extending rearwardly from the nozzle exit, the improvement comprising
a) said plug having successive cross sections spaced apart rearwardly of the nozzle exit,
b) said cross sections changing from circular or near circular at the exit plane defined at the nozzle exit, to progressively non-circular, rearwardly,
c) each cross section defining a median line minor axis and a major axis bi-secting said minor axis, and longer than said minor axis,
d) the minor axes of successive cross-sections in a rearward direction progressively decreasing in length, beyond a mid-portion of the plug length protruding from the nozzle exit,
e) said cross-sections at ends of said major axes having convex surface outlines directed from and protruding away from said major axes at distal ends thereof,
f) the major axes of successive cross-sections in a rearward direction substantially between the nozzle exit and said plug length mid-portion remaining substantially the same.
2. The improvement of claim 1 wherein said cross-sections define ellipses having progressively relatively decreasing minor axes.
3. The improvement of claim 1 wherein said cross sections have boundary curvature that progressively increases in said rearward direction.
4. The improvement of claim 1 wherein said cross sections have upper and lower portions, said lower portions progressively reducing in width, and said upper portions progressively increasing in width to a maximum locus.
5. The improvement of claim 4 wherein said upper portions progressively decrease in width above said locus.
6. The improvement of claim 1 wherein the nozzle is a two exit co-annular nozzle, wherein the second aft nozzle is comprised of a shaped plug nozzle.
7. The improvement of claim 6 wherein the plug nozzle has a forward exit portion and a rearward exit portion located rearwardly of the forward exit portion, the plug nozzle protruding from and rearwardly of the rearward exit portion.
8. The improvement of claim 7 wherein the rearward exit portion has an exit diameter less than the exit diameter of the forward exit portion.