Transition duct support and method to provide a tuned level of support stiffness
A transition duct support apparatus and a method to support an exit frame in a transition duct in a gas turbine engine are provided. A stiffener ( 24 ) may be arranged to provide support to an outer edge ( 27 ) of an exit frame ( 12 ) in a transition duct ( 14 ). Stiffener ( 24 ) may be configured to circumferentially extend between mutually opposed corners ( 30 ) of the exit frame of the transition duct. A brace ( 26 ) may be connected to a centrally-disposed section ( 20 ) and may extend to support respective end portions ( 32 ) of the stiffener. The support apparatus is effective to provide a respective tuned level of stiffness support with respect to one or more axes of the exit frame in the transition duct. The apparatus and method may be effective for distributing mechanical stresses on the exit frame of the transition duct and/or neighboring regions in the transition duct.
1. A transition duct support apparatus comprising:
a centrally-disposed section circumferentially extending along an exit frame in a transition duct from a combustor to a turbine;
a single continuous stiffener connected to the centrally-disposed section and disposed radially inwardly relative to the centrally-disposed section in a direction toward the exit frame, the single continuous stiffener circumferentially extending between mutually opposed corners of the exit frame of the transition duct, the single continuous stiffener arranged to provide support to an outer edge of the exit frame in the transition duct; and
a brace connected to the centrally-disposed section and disposed radially outwardly relative to the single continuous stiffener in a direction outward the exit frame, the support apparatus effective to provide a respective tuned level of stiffness support with respect to one or more axes of the exit frame in the transition duct,
wherein the brace is configured to circumferentially extend at an incline with respect to the single continuous stiffener towards the mutually opposed corners of the exit frame of the transition duct to support respective end portions of the single continuous stiffener, and
wherein the centrally-disposed section connects the brace to the single continuous stiffener to form an integral structure being a plate, the plate having a flat surface extending along a radial plane along a radial direction of the exit frame, wherein the centrally-disposed section, the brace, and the single continuous stiffener are disposed entirely on the radial plane.
2. The transition duct support apparatus of claim 1 , comprising at least one access opening.
3. The transition duct support apparatus of claim 1 , further comprising at least one notch and/or at least one hinge effective to attain the respective tuned level of stiffness support with respect to the one or more axes of the exit frame in the transition duct.
4. The transition duct support apparatus of claim 3 , wherein the at least one notch and/or the at least one hinge are arranged to provide bending flexibility about a circumferential axis.
5. The transition duct support apparatus of claim 1 , wherein the integral structure comprises a composite structure.
6. The transition duct support apparatus of claim 1 , wherein the centrally-disposed section and the single continuous stiffener comprise an integral structure affixable to the brace.
7. The transition duct support apparatus of claim 6 , further comprising at least one hinge arranged between the integral structure and the brace.
8. The transition duct support apparatus of claim 1 , wherein the integral structure comprises a varying three-dimensional profile configured to attain the respective tuned level of stiffness support with respect to the one or more axes of the exit frame in the transition duct.
9. A combustor system comprising the transition duct support apparatus of claim 1 .