Patent Application
20140044524
Contemporary aircraft include fans used for various cooling purposes, which currently include a configuration having two grease-packed bearings that support a rotating shaft of the fan. Due to a harsh operational environment of high temperature and high rotational speeds, the grease forming the bearing lubricant deteriorates quickly, resulting in relatively frequent maintenance to keep the fan in operating condition. The maintenance is currently done by completely removing at least a portion of the fan from the aircraft.
In one embodiment, the invention relates to an impeller fan assembly including a housing having an inner peripheral wall defining a flow through opening, a stator located within the flow through opening and comprising an annular array of stationary blades provided along the inner peripheral wall, a rotor comprising a hub and an annular array of non-stationary blades extending from the hub, at least two spaced apart bearings mounted to the stator, a shaft having a hollow portion rotatably supported by the bearings for rotation about a rotational axis, a sump provided in the stator, and a screw pump provided within the hollow portion of the shaft and having a screw pump inlet fluidly coupled to the sump and a screw pump outlet in fluid communication with the bearings, whereby rotation of the screw pump pumps fluid from the sump to the bearings.
In the drawings:
A housing 12 including an inner peripheral wall 14 defining a flow through opening 16 may be included in the impeller fan assembly 10. In the illustrated example, the flow of air is left to right through the flow through opening 16. An impeller 18 may be moveably mounted within the housing 12 and a cooling air stream may be generated by the impeller 18 during operation of the impeller fan assembly 10.
At least two spaced apart bearings 30 may be operably mounted to the stator 20. More specifically, the stator 20 has been illustrated as including a recess 32 while a bearing housing 34 mounts the bearings 30 and the bearing housing 34 may be received within the recess 32 of the stator 20. In the illustrated example, two spaced apart bearings 30 have been shown although it will be understood that additional bearings 30 may be included.
A shaft 42 may be rotatably supported by the bearings 30 for rotation about a rotational axis 44. The rotor 24 may be operably coupled to the shaft 42 such that both the shaft 42 and rotor 24 may be co-rotated. The shaft 42 may include a hollow portion 46.
A sump 48 may be provided in the stator 20. In the illustrated example, the bearing housing 34 and a portion of the recess 32 of the stator 20 define the sump 48. A fluid such as oil may be introduced into the sump 48. The sump 48 may span the spaced apart bearings 30 such that when the shaft 42 is oriented such that the rotational axis 44 is horizontal, the bearings 30 are at least partially immersed within the fluid in the sump 48. Further, when the shaft 42 is oriented such that the rotational axis 44 is vertical, at least one of the bearings 30 may not be immersed in the fluid within the sump 48.
The fluid may be circulated by a screw pump 50 to lubricate the bearings 30. More specifically, the screw pump 50 has been illustrated as being provided within the hollow portion 46 of the shaft 42. The screw pump 50 may be coupled to the shaft 42 such that the screw pump 50 co-rotates with the shaft 42.
A screw pump inlet 52 of the screw pump 50 fluidly couples to the sump 48. The screw pump inlet 52 may be located such that when the rotational axis is horizontal, the screw pump inlet 52 is not immersed in the fluid in the sump 48. The screw pump inlet 52 may be located such that when the rotational axis is vertical, the screw pump inlet 52 is immersed in the fluid in the sump 48.
A screw pump outlet 54 may also be in fluid communication with the bearings 30. Several screw pump outlets 54 have been illustrated in the exemplary embodiment. The screw pump outlet 54 may be located such that when the rotational axis 44 is vertical, fluid emitted from the screw pump outlet 54 flows by gravity onto at least one of the bearings 30. In the illustrated example, the screw pump outlet 54 is located above both of the spaced apart bearings 30 such that when the rotational axis 44 is vertical, fluid emitted from the screw pump outlet 54 flows by gravity onto both of the bearings 30.
A fluid access port 60 may be formed in the stator 20 and fluidly coupled to the sump 48. The fluid in the sump 48 may be drained through the fluid access port 60. A plug 62 may be used to close the fluid accesses port 60. Any suitable plug 62 may be used. Further, a second access port 63 may be formed in the bearing housing 34 and fluidly coupled to the sump 48. Fluid may be filled in the sump 48 through the second access port 63. A plug 65 may be included to close the second access port 63.
As more clearly illustrated in
During operation, rotation of the shaft 42 is utilized to operate the screw pump 50. A quantity of fluid in the sump 48 may be adjusted for both horizontal and vertical orientations of the impeller fan assembly 10. Referring to
The embodiments described above provide for a variety of benefits including that they have higher efficiency, high reliability, less maintenance, all-attitude operation, and lower weight. The embodiments described above use a fluid such as oil, in place of grease, for bearing lubrication, and allow the fluid to be changed without removing the impeller fan assembly from the aircraft. This results in a reduced frequency of the removal of the impeller fan assembly and greatly prolongs the service life of the impeller fan assembly, which will result in cost savings, as well as much improved aircraft utilization. The embodiments described above result in easier maintenance and improved fan service life, which results in commercial advantages including reduced maintenance cost and reduced down time of the aircraft on which the impeller fan assembly is installed.
This written description uses examples to disclose the invention, including the best mode, and also to enable any person skilled in the art to practice the invention, including making and using any devices or systems and performing any incorporated methods. The patentable scope of the invention is defined by the claims, and may include other examples that occur to those skilled in the art. Such other examples are intended to be within the scope of the claims if they have structural elements that do not differ from the literal language of the claims, or if they include equivalent structural elements with insubstantial differences from the literal languages of the claims.
