A centerbody for the exhaust system of a gas turbine engine having an upstream end mounted within an exhaust duct casing of the exhaust system. The centerbody includes a plurality of ventilation openings defined in a centerbody wall which provide fluid flow communication between an internal cavity a
A centerbody for the exhaust system of a gas turbine engine having an upstream end mounted within an exhaust duct casing of the exhaust system. The centerbody includes a plurality of ventilation openings defined in a centerbody wall which provide fluid flow communication between an internal cavity and exhaust gas flow surrounding the centerbody, such that ventilating air from within the cavity can exit into the exhaust gas flow.
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The invention claimed is: 1. An exhaust centerbody of a gas turbine engine disposed within an exhaust duct casing, exhaust gas flow passing through an annular exhaust duct passage defined between the exhaust centerbody and the surrounding exhaust duct casing, the exhaust centerbody comprising: a fo
The invention claimed is: 1. An exhaust centerbody of a gas turbine engine disposed within an exhaust duct casing, exhaust gas flow passing through an annular exhaust duct passage defined between the exhaust centerbody and the surrounding exhaust duct casing, the exhaust centerbody comprising: a forward centerbody portion defining a first outer wall over which exhaust gas flows and having an annular :flange at a downstream end thereof, the annular flange including a first flange portion and a second flange portion downstream of the first flange portion, the second flange portion being substantially parallel to a central axis of the centerbody and the first flange portion being disposed between the first outer wall and the second flange portion at an angle relative to said second flange portion; a tailcone portion defining a second outer wall, the tailcone portion having a closed downstream end and an open upstream end, said open upstream end of the tailcone portion being mated to the second flange portion of the forward centerbody portion about the circumference of the annular flange thereof; a centerbody cavity defined within the first and second outer walls and the closed downstream end; and a plurality of ventilation openings defined in said first flange portion of the forward centerbody portion, said ventilation openings permitting fluid to flow from the centerbody cavity within the exhaust centerbody into the exhaust gas flow outside the centerbody cavity, thereby ventilating the centerbody cavity. 2. The exhaust centerbody as defined in claim 1, wherein the open upstream end of the tailcone portion is a continuous axisymmetric rim. 3. The exhaust centerbody as defined in claim 2, wherein the rim extends in a direction generally parallel to the central axis and to the second flange portion of the forward centerbody portion. 4. The exhaust centerbody as defined in claim 1, wherein the open upstream end of the tailcone portion is fastened to the second flange portion of the forward centerbody portion by a plurality of fasteners disposed about the circumference of the annular flange. 5. The exhaust centerbody as defined in claim 1, wherein the angle of the first flange portion is obtuse. 6. The exhaust centerbody as defined in claim 1, wherein the angle of the first flange portion is at least 90 degrees. 7. The exhaust centerbody as defined in claim 1, wherein each of said plurality of ventilation openings is substantially circular. 8. The exhaust centerbody as defined in claim 1, wherein said plurality of ventilation openings are circumferentially evenly distributed about said first flange portion of the annular flange. 9. The exhaust centerbody as defined in claim 1, wherein the exhaust centerbody is supported within the exhaust duct casing by a series of struts radially extending through said exhaust duct passage between said forward centerbody portion of the exhaust centerbody and the exhaust duct. 10. The exhaust centerbody as defined in claim 9, wherein said struts are hollow and each define an airflow passage therethrough, said airflow passages providing fluid flow communication between the centerbody cavity and a source of ventilation airflow. 11. An exhaust centerbody of a gas turbine engine disposed within an exhaust duct casing of an exhaust system, the centerbody having a central longitudinal axis coincident with that of the gas turbine engine, the centerbody comprising: an upstream end mounted within the exhaust duct casing of the exhaust system, a closed downstream end. and an annular centerbody wall extending between the upstream and downstream ends, a cavity defined within the centerbody and being in communication with a source of ventilation airflow; and a plurality of ventilation openings defined in said centerbody wall, said ventilation openings providing fluid flow communication between the cavity and exhaust gas flow of the gas turbine engine, such that ventilating air from within the cavity exits into the exhaust gas flow via said plurality of ventilation openings, said plurality of ventilation openings being circumferentially evenly disposed about the centerbody wall within an annular flange wall thereof, said annular flange wall being located between said upstream end and said closed downstream end and disposed at an obtuse angle relative to the central longitudinal axis of the centerbody. 12. The exhaust centerbody as defined in claim 11, wherein the centerbody wall comprises a first centerbody portion and a second centerbody portion serially connected together. 13. The exhaust centerbody as defined in claim 12, wherein the first and second centerbody portions are mated together proximate said annular flange wall. 14. The exhaust centerbody as defined in claim 13, wherein the first centerbody portion comprises a first wall portion at an upstream end thereof, a second wall portion at a downstream end thereof and a radially extending flange wall between the first and second wall portions, the second wall portion being substantially parallel to the central longitudinal axis of the centerbody and the radially extending flange wall being disposed between the first wall portion and the second wall portion at said obtuse angle. 15. The exhaust centerbody as defined in claim 14, wherein the second centerbody portion has an open upstream end which is mated to the second wall portion about the circumference thereof. 16. The exhaust centerbody as defined in claim 15, wherein the open upstream end of the second centerbody portion is a continuous axisymmetric rim. 17. The exhaust centerbody as defined in claim 16, wherein the rim extends in a direction generally parallel to the central longitudinal axis and to the second wall portion. 18. The exhaust centerbody as defined in claim 13, wherein the first and second centerbody portions are fastened together proximate said radially extending flange wall by a plurality of fasteners disposed about the circumference of the second wall portion. 19. The exhaust centerbody as defined in claim 11, wherein each of said plurality of ventilation openings is substantially circular.
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이 특허에 인용된 특허 (23)
Cicon Dennis E. (Manchester CT), Acoustic treated exhaust plug for turbine engine.
Johnson Joseph M. (Bothell WA) Thornock Russell L. (Seattle WA), Method of positioning an aircraft jet engine noise suppressor in a convergent jet engine nozzle.
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