Exhaust nozzle construction

Claim 2

In combination with an aircraft engine exhaust duct, a peripheral housing positioned around said exhaust duct forming a peripheral chamber, nozzle means being movable to control exhaust flow through said exhaust duct to provide a primary flow path, inlet openings located through said peripheral housing into said peripheral chamber for receiving exhaust flow from said exhaust duct, said nozzle means being movable to direct exhaust flow from said exhaust duct into said peripheral chamber through said inlet openings, outlet openings positioned in said peripheral housing to direct exhaust flow therefrom to provide a secondary flow path.

Claim 3

A combination as set forth in claim 1 wherein each of said outlet openings has a ring mounted therein for rotation, each ring having vanes for flow directing, said rings being movable to provide a variable forward thrust and a rearward thrust.

Claim 4

A combination as set forth in claim 2 wherein said nozzle means provides a variable exit area for controlling thrust, and said outlet openings provide a constant exit area for controlling thrust.

Claim 5

A combination as set forth in claim 1 wherein said peripheral housing has a rear wall, said rear wall containing said inlet openings, said nozzle means having seal means which cooperates with said rear wall to cover and uncover said inlet openings, control means for moving said nozzle means to cover and uncover said inlet openings.

Claim 6

A combination as set forth in claim 4 wherein said nozzle means has upper and lower flaps with forward edges which cooperate with the upper and lower curved sections, said seal means blocking flow out of the peripheral chamber through the inlet openings outwardly around the forward edges of the flaps as the forward edges move across the inlet openings.

Claim 7

A combination as set forth in claim 4 wherein the total area of both inlet openings is made slightly larger than the minimum area of said nozzle means.

Claim 8

A combination as set forth in claim 1 wherein the forward part of said exhaust duct is circular and said exhaust duct has an end transition section which contours a circular duct to a rectangular duct at its end, said rectangular end having an upper edge and a lower edge, said nozzle means being a two-dimensional flap nozzle means connected to the rectangular end of the transition section, said peripheral housing having a rear wall, said rear wall including an upper curved section extending upwardly from the upper edge of said rectangular end and a lower curved section extending downwardly from the lower edge of said rectangular end, said inlet openings being located in said upper and lower curved sections, said two-dimensional flap nozzle means having upper and lower flaps with forward edges which cooperate with the upper and lower curved sections, respectively, of said rear wall.

Claim 9

A combination as set forth in claim 7 wherein each of said forward edges of said upper and lower flaps has an outwardly extending curved seal portion for providing a sealing action with said upper and lower curved sections of said rear wall, said curved seal portions blocking flow out of the peripheral chamber through the inlet openings outwardly around the forward edges of the flaps as the forward edges move across the inlet openings.

Claim 10

A combination as set forth in claim 7 wherein each of said outlet openings has a ring mounted therein for rotation, each ring having vanes for flow directing, said rings being movable to provide a variable forward thrust, said variable forward thrust being obtained while the engine is at a high R.P.M.

Claim 11

A combination as set forth in claim 9 wherein said peripheral housing has sides curved outwardly, four rings having fixed vanes for flow directing, a ring being mounted for rotation at the upper and lower corner of each side wall facing outwardly at an angle.

Claim 12

A combination as set forth in claim 1 wherein said peripheral housing extends entirely around said exhaust duct, said peripheral housing having a front wall connected to said exhaust duct, said peripheral housing having a rear wall connected to said exhaust duct, said peripheral chamber extending entirely around said exhaust duct, said inlet openings being located in the rear wall of said peripheral housing and opening into said peripheral chamber, said outlet openings directing exhaust flow out of said peripheral chamber.

Claim 13

In combination with an aircraft engine exhaust duct, a peripheral housing positioned around said exhaust duct forming a peripheral chamber therewith, said peripheral chamber extending entirely around said exhaust duct, said peripheral housing having a front wall extending outwardly from said exhaust duct forming the forward end of said peripheral chamber and a rear wall extending outwardly from said exhaust duct forming the rearward end of said peripheral chamber, nozzle means at the end of said aircraft engine exhaust duct being movable to variably control exhaust flow through said exhaust duct to provide a primary flow path for direct forward propulsion, inlet openings located through the rear wall of said peripheral housing opening into said peripheral chamber for receiving exhaust flow from said exhaust duct and directing it into said peripheral chamber, said inlet openings being positioned outwardly of said exhaust duct, said nozzle means being movable to direct exhaust flow from said exhaust duct forwardly into said peripheral chamber thorugh said inlet openings, outlet openings positioned in said peripheral housing to direct exhaust flow from said peripheral chamber to provide a secondary flow path.

Claim 14

In combination with an aircraft engine exhaust duct, a peripheral housing positioned around said exhaust duct forming a peripheral chamber therewith, said peripheral chamber extending entirely around said exhaust duct, said peripheral housing having a front wall extending outwardly from said exhaust duct forming the forward end of said peripheral chamber and a rear wall extending outwardly from said exhaust duct forming the rearward end of said peripheral chamber, nozzle means at the end of said aircraft engine exhaust duct being movable to variably control exhaust flow through said exhaust duct to provide a primary flow path for direct forward propulsion, inlet openings located through the rear wall of said peripheral housing opening into said peripheral chamber for receiving exhaust flow from said exhaust duct and directing it into said peripheral chamber, said inlet openings being positioned outwardly of said exhaust duct, said nozzle means being movable to direct exhaust flow from said exhaust duct forwardly into said peripheral chamber thorugh said inlet openings, outlet openings positioned in said peripheral housing to direct exhaust flow from said peripheral chamber to provide a secondary flow path.