Low loss oil accumulator assembly
An oil accumulator assembly may comprise a scavenge tube including an aperture defined by a break in the scavenge tube and/or an annular cylindrical structure concentrically situated about the scavenge tube. The aperture may be configured to receive oil flowing through the scavenge tube, and the annular cylindrical structure may be configured to accumulate oil flowing through the aperture. The oil accumulator assembly may further comprise a drainage outlet disposed in the annular cylindrical structure. Oil accumulated within the annular cylindrical structure may drain through the drainage outlet in response to an engine being shut down. The oil accumulated within the annular cylindrical structure may fill a portion of the scavenge tube situated within an engine fan case to prevent coking within the scavenge tube.
1. An oil accumulator assembly for a gas turbine engine, the oil accumulator assembly comprising:
a scavenge tube including an aperture defined by a break in a wall of the scavenge tube;
an annular generally cylindrical structure situated concentrically about the scavenge tube,
the annular generally cylindrical structure comprising:
a first radial surface extending radially from an exterior surface of the scavenge tube,
a second radial surface extending radially from the exterior surface of the scavenge tube, and
an exterior axially extending surface connecting the first radial surface and the second radial surface; and
an oil pump configured to draw oil through the scavenge tube in a first axial flow direction, the first axial flow direction corresponding to a direction extending from the first radial surface of the annular generally cylindrical structure toward the second radial surface of the annular generally cylindrical structure,
wherein the annular generally cylindrical structure is configured to accumulate oil flowing through the aperture of the scavenge tube and, in response to the oil pump being shut down, drain the accumulated oil into the scavenge tube such that the accumulated oil flows into
the scavenge tube in a radial flow direction and then flows through the scavenge tube in a second axial flow direction opposite the first axial flow direction.
2. The oil accumulator assembly of claim 1 , further comprising a drainage outlet disposed in the scavenge tube.
3. The oil accumulator assembly of claim 2 , wherein the annular cylindrical structure is configured to drain the accumulated oil through the drainage outlet in response to the oil pump being shut down.
4. The oil accumulator assembly of claim 1 , wherein the accumulated drained from the annular generally cylindrical structure fills a portion of the scavenge tube situated within an engine fan case to prevent coking within the scavenge tube.
5. The oil accumulator assembly of claim 1 , wherein the wall of the scavenge tube defining the aperture is disposed within the annular generally cylindrical structure, between the first radial surface and the second radial surface.
6. The oil accumulator assembly of claim 1 , wherein the scavenge tube extends through the first radial surface, terminates at the aperture, and resumes its course within the annular generally cylindrical structure to extend through the second radial surface.
7. The oil accumulator assembly of claim 1 , wherein the aperture is disposed in the scavenge tube such that air and oil are permitted to fill the annular generally cylindrical structure.
8. The oil accumulator assembly of claim 1 , wherein the oil accumulated in the annular generally cylindrical structure does not substantially interfere with the oil flowing through the scavenge tube.
9. A gas turbine engine propulsion system comprising:
a scavenge tube including an aperture defined by a break in a wall of the scavenge tube;
an oil pump configured to draw oil through the scavenge tube in a first axial flow direction;
an annular cylindrical structure situated concentrically about the scavenge tube,
wherein the annular cylindrical structure is configured to accumulate oil flowing through the aperture and, in response to the oil pump being shut down, drain the accumulated oil into the scavenge tube such that the accumulated oil travels through the scavenge tube in a second axial flow direction opposite the first axial flow direction, and
wherein the annular cylindrical structure comprises a first radially extending surface, a second radially extending surface, and an exterior axially extending surface connecting the first radially extending surface and the second radially extending surface.
10. The gas turbine engine propulsion system of claim 9 , further comprising a drainage outlet disposed in the scavenge tube.
11. The gas turbine engine propulsion system of claim 10 , wherein the annular cylindrical structure is configured to drain the accumulated oil through the drainage outlet in response to an engine being shut down.
12. The gas turbine engine propulsion system of claim 9 , wherein the annular cylindrical structure is configured to drain the accumulated oil to till a portion of the scavenge tube situated within an engine fan case to prevent coking within the scavenge tube.