POWER TURBINE INLET DUCT LIP
A power turbine section for a gas turbine engine includes an inlet duct upstream of a first power turbine vane array, the inlet duct including a lip.
1 . A power turbine section for a gas turbine engine comprising:
a first power turbine vane array; and
an inlet duct upstream of said first power turbine vane array, said inlet duct including an annular inner duct wall spaced from an annular outer duct wall, said annular inner duct wall including a lip.
2 . The power turbine section as recited in claim 1 , wherein said lip extends from a gas path surface of said annular inner duct wall.
3 . The power turbine section as recited in claim 1 , wherein said lip defines a ramp.
4 . The power turbine section as recited in claim 3 , wherein said ramp defines an angle of about ten (10) degrees with respect to a gas path surface.
5 . The power turbine section as recited in claim 1 , wherein said lip defines a downstream edge of said annular inner duct wall.
6 . The power turbine section as recited in claim 5 , wherein said downstream edge of said annular inner duct wall at least partially axially overlaps a mount lug of said first power turbine vane array, said mount lug receivable into a bearing support.
7 . The power turbine section as recited in claim 1 , wherein said inlet duct generally forms a frustoconical shape.
8 . The power turbine section as recited in claim 7 , wherein an upstream edge of said annular inner duct wall and said annular outer duct wall are radially inboard of a respective downstream edge of said annular inner duct wall and said annular outer duct wall.
9 . The power turbine section as recited in claim 1 , further comprising an inlet case that supports said first power turbine vane array and said inlet duct upstream.
10 . The power turbine section as recited in claim 9 , further comprising an air strut that extends through said inlet case and said inlet duct.
11 . The power turbine section as recited in claim 10 , wherein said air strut extends through said inlet duct aft of an upstream edge and forward of a downstream edge of said inlet duct.
12 . A gas turbine engine comprising:
a gas generator section; and
a power turbine section driven by said gas generator section, said power turbine section including an inlet duct, said inlet duct including an annular inner duct wall spaced from an annular outer duct wall, said annular inner duct wall including a lip.
13 . The gas turbine engine as recited in claim 12 , further comprising a first power turbine vane array, said inlet duct upstream of said first power turbine vane array.
14 . The gas turbine engine as recited in claim 12 , wherein said lip extends from a gas path surface of said annular inner duct wall.
15 . The gas turbine engine as recited in claim 14 , wherein said lip defines a ramp.
16 . The gas turbine engine as recited in claim 15 , wherein said ramp defines an angle of about ten (10) degrees with respect to said gas path surface.
17 . The gas turbine engine as recited in claim 14 , wherein said lip defines a downstream edge of said annular inner duct wall
18 . The gas turbine engine as recited in claim 17 , wherein said downstream edge of said annular inner duct wall at least partially axially overlaps a mount lug of a first power turbine vane array, said mount lug receivable into a bearing support.
19 . The gas turbine engine as recited in claim 18 , wherein said bearing support is a #7 bearing support.
20 . The gas turbine engine as recited in claim 18 , wherein said gas turbine engine is an industrial gas turbine engine within a ground mounted enclosure.