Embedded auxiliary oil system for gearbox protection
A gearbox is provided for use in a gas turbine engine. The gearbox includes a plurality of gears, a casing surrounding the plurality of gears, and a lubricant re-circulation system. The casing defines a sump positioned beneath the plurality of gears to retain lubricant. The lubricant re-circulation system includes a re-circulation pump, a re-circulation inlet positioned within the sump, and a re-circulation outlet positioned to supply lubricant to the plurality of gears.
1. A lubrication system for a gas turbine engine comprising:
a gearbox comprising:
a plurality of gears; and
a casing surrounding the plurality of gears, the casing defining a sump positioned beneath the plurality of gears;
a primary lubrication system comprising:
a reservoir separated from the casing,
a primary pump configured to deliver lubricant from the reservoir to the plurality of gears through a primary supply line extending through the casing, and
a primary return line extending through the casing, the primary return line configured to return lubricant from the plurality of gears to the reservoir; and
a secondary lubrication system comprising a secondary pump, a secondary supply line, and a secondary return line, the secondary lubrication system contained entirely within the gearbox, wherein:
the secondary pump is configured to:
deliver lubricant to the plurality of gears through the secondary supply line, and
draw lubricant from the sump through the secondary return line.
2. The lubrication system of claim 1 , wherein the primary return line comprises a primary inlet positioned closer to the plurality of gears than a secondary inlet of the secondary return line.
3. The lubrication system of claim 2 , wherein the primary inlet is sized and positioned such that lubricant within the sump may not cross the primary inlet to reach the plurality of gears.
4. The lubrication system of claim 1 , wherein the secondary pump is mechanically linked to rotation of a shaft of the gas turbine engine.
5. The lubrication system of claim 4 , wherein the primary pump is mechanically linked to rotation of the shaft of the gas turbine engine.
6. The lubrication system of claim 1 , wherein the primary return line comprises a primary inlet configured to receive lubricant from a chamber within the casing in which the plurality of gears is arranged.
7. The lubrication system of claim 6 , wherein the primary inlet is positioned between the sump and the plurality of gears.
8. The lubrication system of claim 6 , wherein a cross-sectional area of the primary inlet is greater than a cross-sectional area of a secondary inlet of the secondary return line.
9. The lubrication system of claim 6 , wherein the primary inlet is positioned within the sump.
10. The lubrication system of claim 9 , wherein the primary inlet is separated from a secondary inlet of the secondary return line by a baffle.
11. The lubrication system of claim 6 , wherein the primary supply line comprises a primary outlet configured to supply lubricant into a chamber within the casing in which the plurality of gears is arranged.
12. The lubrication system of claim 1 , wherein the casing defines a choke point between the sump and the plurality of gears, wherein a maximum cross-sectional area of the sump is greater than a cross-sectional area of the choke point.
13. The lubrication system of claim 1 , wherein the secondary pump is positioned within the sump.
14. The lubrication system of claim 1 , wherein the secondary pump is positioned within a sidewall of the casing.