Lubrication system
A gearbox includes a housing defining an interior. The housing includes outer walls and inner walls defining other structure within the housing, and at least one wall of the housing includes a semi-hollow volume. A main lubricant reservoir is disposed within the interior of the housing, and at least one pump is arranged in the interior of the housing for pumping lubricant from the main lubricant reservoir and distributing the lubricant throughout the housing. The semi-hollow volume of the at least one wall stores lubricant during normal operation of the pump, and when a loss of lubricant occurs within the housing, lubricant seeps from the semi-hollow volume to distribute lubricant throughout the housing.
1. A gearbox comprising:
a housing defining an interior, the housing including outer walls and inner walls defining structure within the housing, wherein at least one wall of the housing includes a semi-hollow volume;
a main lubricant reservoir disposed within the interior of the housing; and
at least one pump arranged in the interior of the housing for pumping lubricant from the main lubricant reservoir and distributing the lubricant throughout the housing, lubricant is pumped through a first flow path to be directly distributed to a first location and a second flow path to be directly distributed to a second location different than the first location, wherein the first location is the interior of the housing and the second location is the semi-hollow volume of the at least one wall,
wherein the semi-hollow volume of the at least one wall is configured to store lubricant and function as an auxiliary lubricant reservoir during normal operation of the at least one pump, and further wherein when the main lubricant reservoir is damaged such that a loss of lubricant occurs within the housing, lubricant is configured to seep from the semi-hollow volume to distribute lubricant throughout the housing.
2. The gearbox of claim 1 , wherein the semi-hollow volume of the at least one wall at least partially comprises a lattice structure.
3. The gearbox of claim 2 , wherein the at least one wall and the lattice structure are integrally formed as a single structure.
4. The gearbox of claim 3 , wherein the single structure is a 3D printed structure.
5. The gearbox of claim 2 , wherein the lattice structure is a cubic lattice structure.
6. The gearbox of claim 1 , wherein at least two walls of the housing include a semi-hollow volume, and the at least two walls are interconnected via a channel.
7. The gearbox of claim 1 , wherein lubricant is configured to seep from the semi-hollow volume to distribute lubricant within the interior of the housing in the normal operation of the at least one pump.
8. The gearbox of claim 1 , further including at least one jet fluidly connected to the at least one pump and configured to spray lubricant from the main lubricant reservoir into the housing.
9. The gearbox of claim 8 , wherein the at least one jet sprays lubricant from the main lubricant reservoir into the housing in the normal operation of the at least one pump, and when the main lubricant reservoir is damaged such that loss of lubricant occurs, the at least one jet does not spray lubricant into the housing.
10. The gearbox of claim 8 , further including a conduit that couples the main lubricant reservoir to the at least one jet, the conduit being formed integrally with at least one wall of the housing.
11. A lubrication system for a gearbox assembly, the lubrication system comprising:
a gearbox housing defining an interior, the gearbox housing including outer walls and inner walls defining structure within the gearbox housing, wherein at least one wall of the gearbox housing includes a semi-hollow volume, the gearbox housing further including a sump that stores lubricant and function as a main lubricant reservoir;
a transmission element disposed within the interior of the gearbox housing that receives and is lubricated by the lubricant;
wherein during normal operation of the lubrication system, lubricant is configured to be pumped from the sump and through a first flow path to be directly distributed to the transmission element, and lubricant is configured to be pumped through a second flow path to be directly distributed and stored in the semi-hollow volume of the at least one wall such that the semi-hollow volume is configured to function as an auxiliary lubricant reservoir, and
wherein during emergency operation of the lubrication system, lubricant is configured to seep from the semi-hollow volume to distribute lubricant to the transmission element.
12. The lubrication system of claim 11 , wherein the semi-hollow volume includes an internal structure.
13. The lubrication system of claim 12 , wherein the internal structure at least partially comprises a lattice structure.
14. The lubrication system of claim 11 , wherein the at least one wall includes an aperture adjacent a hot spot of the transmission element, the aperture fluidly connected to the semi-hollow volume such that lubricant seeps through the aperture during emergency operation of the lubrication system.
15. The lubrication system of claim 11 , wherein during normal operation of the lubrication system, lubricant is configured to seep from the semi-hollow volume to distribute lubricant to the gearbox housing.
16. An aircraft comprising:
a body;
a prime mover supported by the body;
a rotary assembly supported by the body;
a gearbox mechanically connected between the prime mover and the rotary assembly, the gearbox including,
a housing defining an interior, the housing including a plurality of walls, wherein at least one of the plurality of walls includes a semi-hollow volume;
a main lubricant reservoir; and
at least one pump arranged in the interior of the housing for pumping lubricant from the main lubricant reservoir and distributing lubricant throughout the housing, lubricant is pumped through a first flow path to be directly distributed to a first location and a second flow path to be directly distributed to a second location different than the first location, wherein the first location is the interior of the housing and second location is the the semi-hollow volume of the at least one wall,
wherein the semi-hollow volume of the at least one wall is configured to store lubricant and function as an auxiliary lubricant reservoir during a normal operating condition of the at least one pump, and further wherein during an emergency operating condition, lubricant is configured to seep from the semi-hollow volume to distribute lubricant throughout the housing.
17. The aircraft of claim 16 , wherein the semi-hollow volume of the at least one of the plurality of walls at least partially comprises a lattice structure.
18. The aircraft of claim 16 , wherein the gearbox further includes at least one jet fluidly connected to the at least one pump and configured to spray lubricant from the main lubricant reservoir into the housing.
19. The aircraft of claim 16 , wherein the gearbox further includes at least one jet fluidly connected to the at least one pump and configured to fill the semi-hollow volume with lubricant.
20. The aircraft of claim 16 , wherein the main lubricant reservoir is damaged such that a loss of lubricant occurs within the housing in the emergency operating condition.