Machine and gearbox system and cooling therefor
A system includes a gearbox having an external surface; a fan or impeller constructed to generate a first cooling airflow when rotated; a shroud operative to guide and discharge the first cooling airflow over the external surface and cool the gearbox, wherein at least a portion of the shroud is spaced apart from the gearbox and disposed radially outward of the external surface; and a flow entrainment structure coupled to the gearbox and/or the shroud, wherein the flow entrainment structure is constructed to entrain a second cooling airflow and combine the second cooling airflow with the first cooling airflow to form a combined cooling airflow directed across the external surface to cool the gearbox.
1. A system, comprising:
a machine having an external surface;
a cooling airflow generator constructed to generate a cooling airflow when rotated;
a flow guide structure to guide the cooling airflow and discharge the cooling airflow over the external surface and cool the machine using the cooling airflow, wherein at least a portion of the flow guide structure is spaced apart from the machine and disposed radially outward of the external surface so the cooling airflow is guided between the machine and the flow guide structure; and
a flow inducer mounted to the flow guide structure so that the flow inducer is radially spaced outwardly of the flow guide structure, wherein the flow inducer includes an inlet to admit additional cooling airflow from an environment in which the machine is located and into a space between the flow guide structure and the flow inducer, and the flow inducer includes an outlet in which the additional cooling airflow exits the space and is entrained into the cooling airflow discharged from the flow guide structure to form a combined cooling airflow that is directed across the external surface of the machine.
2. The system of claim 1 , further comprising a plurality of standoffs constructed to space the flow inducer apart from the guide structure.
3. The system of claim 1 , wherein the flow inducer is operative to entrain the additional cooling airflow using the cooling airflow discharged from the flow guide structure, and to provide additional cooling to the machine using the additional cooling airflow.
4. The system of claim 1 , wherein the inlet includes a smooth transition portion constructed to reduce pressure losses in the additional cooling airflow.
5. The system of claim 1 , wherein the flow inducer is integral with the flow guide structure.
6. The system of claim 1 , wherein the flow inducer is a flat plate.
7. The system of claim 1 , wherein the flow inducer has an airfoil shape.
8. The system of claim 1 , wherein the flow inducer includes an outlet constructed to direct the additional cooling airflow toward the external surface.
9. The system of claim 1 , wherein the flow inducer is constructed to entrain the additional cooling airflow using the Coanda effect and/or the Bernoulli principle.
10. A system, comprising,
a gearbox having an external surface;
a fan or impeller constructed to generate a first cooling airflow when rotated;
a shroud to guide the first cooling airflow and discharge the first cooling airflow over the external surface, wherein at least a portion of the shroud is spaced apart from the gearbox and disposed radially outward of the external surface so the first cooling airflow is guided between the gearbox and the shroud; and
a flow entrainment structure mounted on the shroud so that the flow entrainment structure is radially spaced outwardly of the shroud, wherein the flow entrainment structure includes an inlet to admit a second cooling airflow from an environment in which the gearbox is located and into a space between the shroud and the flow entrainment structure, and the flow entrainment structure includes an outlet in which the second cooling airflow exits the space and is entrained into the first cooling airflow discharged from the shroud to combine the second cooling airflow with the first cooling airflow to form a combined cooling airflow,
wherein the combined cooling airflow is directed across the external surface to cool the gearbox.
11. The system of claim 10 , further comprising a plurality of standoffs constructed to space the flow entrainment structure apart from the shroud.
12. The system of claim 10 , wherein the inlet includes a smooth transition portion constructed to reduce pressure losses in the second cooling airflow.
13. The system of claim 10 , wherein the flow entrainment structure is integral with the shroud.
14. The system of claim 10 , wherein the flow entrainment structure is a flat plate.
15. The system of claim 10 , wherein the flow entrainment structure has an airfoil shape.
16. The system of claim 10 , wherein the flow entrainment structure includes an outlet constructed to direct the second cooling airflow toward the external surface.
17. The system of claim 10 , wherein the flow entrainment structure is constructed to entrain the second cooling airflow using the Coanda effect and/or the Bernoulli principle.