Fuel distribution device, gas turbine engine and mounting method
A fuel distribution device is provided wherein an axis is defined. The device comprises a body housing a distribution path for fuel; the distribution path has one inlet and a plurality of outlets; the inlet is located on the external surface of the body at an end of an inlet branch of the distribution path; the plurality of outlets are located on the external surface of the body at ends of a corresponding plurality of outlet branches of the distribution path; the inlet branch and the outlet branches are fluidly connected to a distribution space; and the outlet branches are arranged radially.
1. A fuel distribution device comprising:
a defined axis;
a first body housing a first distribution path providing a pilot fuel supply to a combustion chamber coupled to the fuel distribution device, wherein the first distribution path has a first inlet and a first plurality of outlets;
a second body housing a second distribution path providing a main fuel supply to the combustion chamber, wherein the second distribution path has a second inlet and a second plurality of outlets; and
a fixing plate, wherein a plane of the fixing plate is perpendicular to the defined axis;
wherein the first inlet and the second inlet are respectively located on external surfaces of the first body housing and the second body housing, the first inlet located at a first end of a first inlet branch of the first distribution path and the second inlet located at a second end of a second inlet branch of the second distribution path;
wherein the first plurality of outlets and the second plurality of outlets are respectively located on external surfaces of the first body housing and the second body housing, the first plurality of outlets located at first ends of a corresponding first plurality of outlet branches of the first distribution path and the second plurality of outlets located at second ends of a corresponding second plurality of outlet branches of the second distribution path;
wherein the first inlet branch and the first plurality of outlet branches are fluidly connected to a first distribution space, and the second inlet branch and the second plurality of outlet branches are fluidly connected to a second distribution space, the first distribution space separate from the second distribution space;
wherein the first body, the second body and the fixing plate are axially aligned relative to each other with respect to the defined axis and are stacked such that the second body lies between the first body and the fixing plate; and
wherein the first plurality of outlet branches and the second plurality of outlet branches are arranged radially with respect to the first distribution space and the second distribution space.
2. The fuel distribution device of claim 1 , wherein the first inlet branch and the second inlet branch are arranged radially with respect to the first distribution space and the second distribution space.
3. The fuel distribution device of claim 1 , wherein the first distribution space includes a first ring conduit and the second distribution space includes a second ring conduit.
4. The fuel distribution device of claim 1 , wherein the first inlet branch is arranged axially.
5. The fuel distribution device of claim 4 , wherein the first inlet branch is arranged axially with respect to the first distribution space.
6. The fuel distribution device of claim 1 , wherein the first distribution space includes a first cylindrical cavity and the second distribution space includes a second cylindrical cavity.
7. The fuel distribution device of claim 1 , wherein the first body housing, the second body housing, and the fixing plate are axially aligned.
8. The fuel distribution device of claim 7 , wherein:
the first plurality of outlet branches are arranged axially with respect to the first distribution space; and
the second plurality of outlet branches are arranged axially with respect to the second distribution space.
9. A gas turbine engine comprising one or more fuel distribution devices, the fuel distribution device comprising:
a defined axis;
a first body housing a first distribution path providing a pilot fuel supply to a combustion chamber of the gas turbine engine, the combustion chamber coupled to the fuel distribution device, wherein the first distribution path has a first inlet and a first plurality of outlets;
a second body housing a second distribution path providing a main fuel supply to the combustion chamber, wherein the second distribution path has a second inlet and a second plurality of outlets; and
a fixing plate, wherein a plane of the fixing plate is perpendicular to the defined axis;
wherein the first inlet and the second inlet are respectively located on external surfaces of the first body housing and the second body housing, the first inlet located at a first end of a first inlet branch of the first distribution path and the second inlet located at a second end of a second inlet branch of the second distribution path;
wherein the first plurality of outlets and the second plurality of outlets are respectively located on external surfaces of the first body housing and the second body housing, the first plurality of outlets located at first ends of a corresponding first plurality of outlet branches of the first distribution path and the second plurality of outlets located at second ends of a corresponding second plurality of outlet branches of the second distribution path;
wherein the first inlet branch and the first plurality of outlet branches are fluidly connected to a first distribution space, and the second inlet branch and the second plurality of outlet branches are fluidically connected to a second distribution space, the first distribution space separate from the second distribution space;
wherein the first body the second body and the fixing plate are axially aligned relative to each other with respect to the defined axis and are stacked such that the second body lies between the first body and the fixing plate; and
wherein the first plurality of outlet branches and the second plurality of outlet branches are arranged radially with respect to the first distribution space and the second distribution space.
10. The gas turbine engine of claim 9 , wherein the combustion chamber includes an end cover plate, wherein said fuel distribution device is mounted on said end cover plate through one or two or three or four or five or more mounting columns.