Afterburner heat shield
AssigneeGeneral Electric Company
InventorsJohn Herman Mueller, Mark Leonard Vossman, William Ralph Maskiell
Life of this patent
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AssigneeGeneral Electric Company
InventorsJohn Herman Mueller, Mark Leonard Vossman, William Ralph Maskiell
Estimating the term…
A heat shield and support strut for a turbine engine afterburner. The heat shield can be replaced without moving or disconnecting the fuel tube. The heat shield includes a housing that may be telescoped over the fuel injection tube and is attachable to the strut without moving the housing transverse to a longitudinal axis of the fuel injection tube. The support strut includes a body having an outer end for attachment to an outer wall of the afterburner section, an inner end, and a passage extending through the body from its outer end to its inner end for receiving the fuel injection tube. The inner end has a cavity for receiving the head of the heat shield. The cavity is shaped for a close fit on the head in the cavity. The body has a flat mounting surface in the cavity for engagement by the flat mounting surface of the head.
A heat shield for protecting a fuel injection tube of a turbine engine afterburner section, the afterburner section having a cylindrical outer wall, a liner positioned in spaced relation from the outer wall and generally defining a boundary between a core duct for flow of turbine exhaust gas and an annular bypass duct for flow of cooling air, at least one fuel injection tube extending from the outer wall inwardly to the core duct, the fuel injection tube having a longitudinal axis, a first portion of the fuel injection tube in the bypass duct and a second portion of the fuel injection tube in the core duct, and a strut positioned generally between the outer wall and the liner and enclosing the first portion of the fuel injection tube, the heat shield comprising:
A support strut for supporting a heat shield in a turbine engine afterburner section, the afterburner section having a cylindrical outer wall, a liner positioned in spaced relation from the outer wall and generally defining a boundary between a core duct for flow of turbine exhaust gas and an annular bypass duct for flow of cooling air, at least one fuel injection tube extending from the outer wall inwardly to the core duct, the fuel injection tube having a first portion in the bypass duct and a second portion in the core duct, the heat shield having a housing for enclosing said second portion of the fuel injection tube and having a head with a generally flat mounting surface, the support strut comprising:
Dependencies are inferred from the claim text.