Augmentor spray bars
First Claim
Patent Images
1. A turbine engine augmentor comprising:
- a centerbody within a gas flowpath from upstream to downstream and having a downstream tailcone; and
a plurality of vanes positioned in the gas flowpath outboard of the centerbody and having first and second sides;
an augmentor fueling system comprising;
a plurality of spray bars, each spray bar at least partially within an associated at least one of said vanes, comprising;
a conduit; and
a plurality of nozzles coupled to the conduit, each nozzle positioned to discharge an associated fuel stream from one of the sides of the associated vane; and
a plurality of blocks, each block mounted within the associated vane relative to an associated one of the nozzles for a range of motion relative thereto between an inward extreme and an outward extreme and movably cooperating with the associated vane, wherein there are nozzles along each of the first side and second side of each of the vanes and each said vane contains a plurality of said blocks, each said block mounted to the associated said nozzle.
3 Assignments
0 Petitions
Accused Products
Abstract
A gas turbine engine fueling system includes a number of spray bars having conduits extending through associated vanes. A number of fuel injector nozzles are along each conduit. Each of the nozzles are positioned to discharge an associated fuel stream from one of the sides of the associated vane. A number of wear members are each mounted relative to the associated one of the nozzles for a range of motion relative thereto. The wear members movably cooperate with the associated vane to accommodate operating deflection and/or tolerances of the spray bars and vanes.
28 Citations
22 Claims
-
1. A turbine engine augmentor comprising:
-
a centerbody within a gas flowpath from upstream to downstream and having a downstream tailcone; and a plurality of vanes positioned in the gas flowpath outboard of the centerbody and having first and second sides; an augmentor fueling system comprising; a plurality of spray bars, each spray bar at least partially within an associated at least one of said vanes, comprising; a conduit; and a plurality of nozzles coupled to the conduit, each nozzle positioned to discharge an associated fuel stream from one of the sides of the associated vane; and a plurality of blocks, each block mounted within the associated vane relative to an associated one of the nozzles for a range of motion relative thereto between an inward extreme and an outward extreme and movably cooperating with the associated vane, wherein there are nozzles along each of the first side and second side of each of the vanes and each said vane contains a plurality of said blocks, each said block mounted to the associated said nozzle. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13)
-
-
14. A turbine engine augmentor comprising:
-
a centerbody within a gas flowpath from upstream to downstream and having a downstream tailcone; and a plurality of vanes positioned in the gas flowpath outboard of the centerbody and having first and second sides; an augmentor fueling system comprising; a plurality of spray bars, each spray bar at least partially within an associated at least one of said vanes, comprising; a conduit; and a plurality of nozzles coupled to the conduit, each nozzle positioned to discharge an associated fuel stream from one of the sides of the associated vane; and means within the vanes movably intervening between both the spray bars and the vanes for accommodating operating deflection of at least one of the spray bars and vanes wherein the means are associated with the nozzles.
-
-
15. A turbine engine augmentor comprising:
-
a centerbody within a gas flowpath from upstream to downstream and having a downstream tailcone; and a plurality of vanes positioned in the gas flowpath outboard of the centerbody and having first and second sides; an augmentor fueling system comprising; a plurality of spray bars, each spray bar at least partially within an associated at least one of said vanes, comprising; a conduit; and a plurality of nozzles coupled to the conduit, each nozzle positioned to discharge an associated fuel stream from one of the sides of the associated vane; and a plurality of blocks, each block mounted within the associated vane relative to an associated one of the nozzles and movably cooperating with the associated vane, and comprising electro-graphitic carbon. - View Dependent Claims (16)
-
-
17. A turbine engine augmentor comprising:
-
a centerbody within a gas flowpath from upstream to downstream and having a downstream tailcone; and a plurality of vanes positioned in the gas flowpath outboard of the centerbody and having first and second sides; an augmentor fueling system comprising; a plurality of spray bars, each spray bar at least partially within an associated at least one of said vanes, comprising; a conduit; and a plurality of nozzles coupled to the conduit, each nozzle positioned to discharge an associated fuel stream from one of the sides of the associated vane; and a plurality of blocks, each block mounted within the associated vane relative to an associated one of the nozzles and removable from the associated nozzle nondestructively of said nozzle movably cooperating with the associated vane, and comprising a material that preferentially wears relative to an adjacent material of the associated vane, each of the plurality of blocks are secured to the associated nozzle by a retainer interfitting with said block and said nozzle. - View Dependent Claims (18, 19, 20, 21, 22)
-
Specification