Gas turbine lubrication systems
A casing for a fan drive gear system includes a cast body with an upper and a lower portion. The cast body defines an oil inlet and an oil outlet arranged below the oil outlet. An integrally cast oil channel extends between the inlet and outlet for conveying oil from the upper portion of the cast body portion to the lower portion of the cast body for providing a supply of lubrication to the gear system when oil pools in an upper portion of an auxiliary oil reservoir during negative-G flight events.
1. A casing for a fan drive gear system, comprising:
a cast body having upper and lower portions, defining:
an oil inlet;
an oil outlet arranged below the oil inlet; and
an integrally cast oil channel extending between the oil inlet and oil outlet;
wherein the integrally cast oil channel is configured to convey oil from the cast body upper portion to the cast body lower portion for lubricating the fan drive gear system of a geared turbofan engine when oil pools in an upper portion of an auxiliary oil reservoir during negative-G flight events.
2. A casing as recited in claim 1 , further including an inlet strainer coupled to the oil inlet.
3. A casing as recited in claim 2 , wherein the cast body defines an overflow port fluidly connected to the auxiliary oil reservoir.
4. A casing as recited in claim 3 , wherein the inlet strainer is arranged below the overflow port so as to draw in oil when an oil level in the auxiliary oil reservoir is below the overflow port for keeping air out of the oil inlet.
5. A casing as recited in claim 1 , wherein the cast body defines a gutter inlet fluidly coupled to the fan drive gear system for providing oil to the auxiliary oil reservoir.
6. A casing as recited in claim 5 , wherein the oil inlet is laterally offset and below the gutter inlet for limiting entrained air in oil entering the oil inlet.
7. A casing as recited in claim 1 , wherein at least one of the oil inlet and the oil outlet includes a machined axial surface.
8. A casing as recited in claim 7 , wherein the machined axial surface is orthogonal with respect to an axis of the cast body.
9. A casing as recited in claim 1 , wherein the oil inlet and the oil outlet are located on an interior face of the cast body.
10. A casing as recited in claim 1 , wherein the oil channel traces an arcuate path about an exterior face of the cast body.
11. A lubrication system for a fan drive gear system, comprising:
a casing, comprising:
a cast body having upper and lower portions, defining:
an oil inlet;
an oil outlet arranged below the oil inlet; and
an integrally cast oil channel extending between the oil inlet and oil outlet;
an auxiliary oil reservoir bounded by a circumferentially extending face of the casing, wherein the integrally cast oil channel is configured to convey oil from the cast body upper portion to the cast body lower portion for lubricating the fan drive gear system of a geared turbofan engine when oil pools in an upper portion of the auxiliary oil reservoir during negative-G flight events;
an auxiliary oil pump mounted to the face of the casing; and
a transfer tube fluidly connecting the oil outlet fluidly connecting the auxiliary oil pump with the auxiliary oil reservoir.
12. A lubrication system as recited in claim 11 , further comprising an inlet strainer coupled to the oil inlet and positioned in an area proximate to an inlet to the auxiliary oil reservoir so that entrained air in oil flowing through the oil channel is limited.
13. A lubrication system as recited in claim 11 , further comprising a main oil pump and a shuttle valve fluidly connected to the main oil pump and the auxiliary oil pump, the shuttle valve configured to fluidly couple the auxiliary oil pump to the fan drive gear system upon detecting low main oil pump pressure.
14. A geared turbofan engine, comprising:
a housing including a casing, the casing comprising:
a cast body having upper and lower portions, defining:
an oil inlet;
an oil outlet arranged below the oil inlet; and
an integrally cast oil channel extending between the oil inlet and oil outlet;
an auxiliary oil reservoir disposed in an upper portion of the housing;
a fan drive gear system operatively disposed within the housing;
a gutter for collecting oil arranged about the gear system; and
wherein the auxiliary oil reservoir is configured to supply oil from the cast body upper portion to the cast body lower portion for lubricating the fan drive gear system during negative-G flight events by flowing oil through the oil channel between the oil inlet and oil outlet.
15. An engine as recited in claim 14 , further including an inlet strainer coupled to the oil inlet.
16. An engine as recited in claim 15 , wherein the inlet strainer is positioned in an area proximate to an inlet to the auxiliary oil reservoir so that entrained air in oil flowing through the oil channel is limited.
17. An engine as recited in claim 15 , wherein the cast body defines an overflow port fluidly connected to the auxiliary oil reservoir.
18. An engine as recited in claim 17 , wherein the inlet strainer is arranged below the overflow port so as to draw in oil when the oil level in the auxiliary oil reservoir is below the overflow port for keeping air out of the oil inlet.
19. An engine as recited in claim 14 , wherein the cast body defines a gutter inlet fluidly coupled to the gutter for providing oil to the auxiliary oil reservoir.
20. An engine as recited in claim 19 , wherein the oil inlet is laterally offset and below the gutter inlet for limiting entrained air in oil entering the oil inlet.