Gas turbine engine gas flow ducts

Claim 2

An exhaust flow duct for receiving fan air and exhaust gases from a ducted fan gas turbine engine power plant, said exhaust flow duct comprising: an augmenter air intake positioned within the length of the exhaust flow duct and through which ambient air may flow into the exhaust flow duct; a flow mixing device comprising a generally annular shaped member mounted coaxially within said exhaust flow duct in radially spaced apart relationship therewith, said generally annular shaped member having its upstream end positioned downstream of said augmenter air intake and having lobes formed at least in its downstream end portion with a converging exterior surface for causing flow exterior of said annular shaped member to converge in a downstream direction and a diverging interior surface for causing flow interior of said annular shaped member to diverge in a downstream direction and to mix with the converging exterior flow downstream of said annular shaped member; and flap means for selectively opening and closing said augmenter air intake, said flap means being movable between a first position closing said augmenter air intake and permitting fan air and exhaust gases to respectively flow over the exterior and interior of said annularly shaped member and a second position wherein said augmenter air intake is opened to permit only ambieint air to flow over the exterior of said annular shaped member and to direct fan air and exhaust gases to flow through the interior of said annular shaped member.

Claim 3

An exhaust flow duct as claimed in claim 1 in which said flap means is pivoted at its upstream end and which extends from said exhaust flow duct to the upstream end of said annular shaped member when said flap means is moved to the second position.

Claim 4

An exhaust flow duct as claimed in claim 2 in which said flap means includes at least a pair of flap members, each pivotally connected at its upstream end with one being pivotally connected downstream of the other, said flap members being arranged to overlap one another when said flap members are moved to said second position.

Claim 5

An exhaust flow duct as claimed in claim 1 including a variable area propulsion nozzle at the extreme downstream end thereof, said variable area propulsion nozzle including a plurality of flaps each pivotally mounted between its respective upstream and downstream ends.

Claim 6

A ducted fan gas turbine engine power plant comprising: a core gas generator having a fan at its upstream end; an elongated casing surrounding said core gas generator and said fan and defining with said core gas generator a duct for fan air, said casing having a portion extending downstream of said core gas generator and defining an exhaust flow duct; said exhaust flow duct including an augmenter air intake positioned within its length and through which ambient air may flow into the exhaust flow duct; a flow mixing device comprising a generally annular shaped member mounted coaxially within said exhaust flow duct in a radially spaced apart relationship therewith, said annular shaped member having its upstream end positioned downstream of said augmenter air intake and having lobes formed at least in its downstream end portion with a converging exterior surface for causing flow exterior of said annular shaped member to converge in a downstream direction and a diverging interior surface for causing flow interior of said annular shaped member to diverge in a downstream direction and to mix with the converging exterior flow downstream of said annular shaped member; and flap means for selectively opening and closing said augmenter air intake, said flap means being movable between a first position closing said augmenter air intake and permitting fan air and exhaust gases to respectively flow over the exterior and interior of said annularly shaped member and a second position wherein said augmenter air intake is opened to permit only ambient air to flow over the exterior of said annular shaped member and to direct fan air and exhaust gases to flow through the interior of said annular shaped member.

Claim 7

A ducted fan gas turbine engine power plant comprising: a core gas generator having a fan at its upstream end; an elongated casing surrounding said core gas generator and said fan and defining with said core gas generator a duct for fan air, said casing having a portion extending downstream of said core gas generator and defining an exhaust flow duct; said exhaust flow duct including an augmenter air intake positioned within its length and through which ambient air may flow into the exhaust flow duct; a flow mixing device comprising a generally annular shaped member mounted coaxially within said exhaust flow duct in a radially spaced apart relationship therewith, said annular shaped member having its upstream end positioned downstream of said augmenter air intake and having lobes formed at least in its downstream end portion with a converging exterior surface for causing flow exterior of said annular shaped member to converge in a downstream direction and a diverging interior surface for causing flow interior of said annular shaped member to diverge in a downstream direction and to mix with the converging exterior flow downstream of said annular shaped member; and flap means for selectively opening and closing said augmenter air intake, said flap means being movable between a first position closing said augmenter air intake and permitting fan air and exhaust gases to respectively flow over the exterior and interior of said annularly shaped member and a second position wherein said augmenter air intake is opened to permit only ambient air to flow over the exterior of said annular shaped member and to direct fan air and exhaust gases to flow through the interior of said annular shaped member.

Claim 8

A ducted fan gas turbine engine power plant as claimed in claim 5 in which said annular shaped member has its upstream end spaced axially downstream of said core gas generator's downstream end.

Claim 9

A ducted fan gas turbine engine power plant as claimed in claim 6 in which said augmenter air intake is positioned generally radially outwardly of the core gas generator's downstream end.

Claim 10

A ducted fan gas turbine engine power plant as claimed in claim 7 in which said flap means is pivoted at its upstream end and which extends from said exhaust flow duct to the upstream end of said annular shaped member when said flap means is moved to the second position.

Claim 11

A ducted fan gas turbine engine power plant as claimed in claim 8 in which said flap means includes at least a pair of flap members, each pivotally connected at its upstream end with one being pivotally connected downstream of the other, said flap members being arranged to overlap one another when said flap members are moved to said second position.

Claim 12

A ducted fan gan turbine engine power plant as claimed in claim 5 including a variable area propulsion nozzle at the extreme downstream end of said exhaust flow duct, said variable propulsion nozzle including a plurality of flaps each pivotally mounted between its respective upstream and downstream ends.