The present invention relates to a hydraulic pump and, more particularly, to a seal assembly for use on an output shaft of a hydraulic pump.
A gas turbine engine may include a hydraulic pump for powering certain engine components. In one example, a hydraulic pump may be used to hydraulically power actuators that control an afterburner exhaust nozzle. The hydraulic pump includes a shaft that extends to an aircraft engine gearbox and that extends the length of the pump to communicate with a plurality of hydraulic pump components, such as pistons, gears, or vanes. A portion of the shaft, the hydraulic pump components, and hydraulic fluid are disposed within a housing.
When the aircraft engine gearbox drives the shaft, the shaft rotates within the hydraulic pump to thereby provide power to the pistons, gears, or vanes to force hydraulic fluid through the pump. As a result, power is provided to the aforementioned actuators.
To prevent leakage of the hydraulic fluid from the area along the shaft where the shaft extends through the housing, a magnetic seal has typically been used. In this regard, one section of the magnetic seal is mounted to a stator of the pump, which is typically coupled to the housing, and another section of the magnetic seal is mounted to a rotor of the pump, which is typically coupled to the shaft. The two sections of the magnetic seal attract one another to provide a leak-tight seal between the shaft and the housing.
In some cases, however, the magnetic seal may not effectively seal the hydraulic pump. For example, if the stator and rotor experience a relatively large amount of axial travel therebetween, the magnetic seal may separate which may result in loss of oil. Additionally, if metal chips are inadvertently generated inside the pump, the metal chips may interfere with the magnetic seal and separation may occur.
Accordingly, there is a need for seal assembly that is effective even when a hydraulic pump stator and a rotor experience axial travel therebetween. In addition, there is a need for seal assembly that continues to be operational, in the event metal chips are generated inside the pump. Furthermore, other desirable features and characteristics of the present invention will become apparent from the subsequent detailed description and the appended claims, taken in conjunction with the accompanying drawings and the foregoing technical field and background.
The present invention provides a seal assembly for a hydraulic pump. The assembly includes a spacer ring, a rotor having a first side and a second side, the first side engaging the spacer ring, and a spring-loaded face seal having a face in contact with the rotor second side, where the face seal is configured to supply a force against the rotor sufficient to cause the face seal face to sealingly engage the rotor second side.
In another embodiment, and by way of example only, a hydraulic pump is provided that includes a housing, a shaft rotationally mounted at least partially within the housing, a spacer ring mounted to the shaft, a rotor mounted to the shaft and having a first side and a second side, where the rotor first side engages the spacer ring, and a spring-loaded face seal coupled to the housing and having a face in contact with the rotor second side, the face seal configured to supply a force against the rotor sufficient to cause the face seal face to sealingly engage the rotor second side.
In still another embodiment, a seal-assembly for a hydraulic pump includes a spacer ring, a rotor having a first side and a second side, the first side engaging the spacer ring, a stator having a face in contact with the rotor second side, a seal case within which the stator is disposed, and a spring disposed within the seal case, the spring configured to supply a force against the rotor that is sufficient to cause the stator face to sealingly engage the rotor second side.
Other independent features and advantages of the preferred seal assembly will become apparent from the following detailed description, taken in conjunction with the accompanying drawings which illustrate, by way of example, the principles of the invention.
Before proceeding with the detailed description, it should be appreciated that the present invention is not limited to use in conjunction with a specific type of rotating machine. Thus, although the present invention is, for convenience of explanation, depicted and described as being implemented in a turbine starter, it should be appreciated that it can be implemented in numerous other machines including, but not limited to, a gas turbine engine, a hydraulic pump, a water pump, or various other chemical and industrial pumps.
Turning now to the description, a cross sectional view of a conventional hydraulic pump 100 is provided in
The shaft 104 is rotationally mounted within the housing 102 and extends through the cover plate opening 114. The shaft 104 has a pump section 118 and a gearbox section 120. The pump section 118 extends axially through the housing 102 and is configured to couple to various hydraulic pump components (not shown), such as pistons, gears, and/or vanes. It will be appreciated that the particular hydraulic pump components included in the housing 102 depend on the hydraulic pump type, for example, a centrifugal pump, a positive displacement pump, a reciprocating positive pump, or any other type of pump. The gearbox section 120 extends outside of the housing 102 and has an end 122 configured to couple to a gearbox (not shown).
To minimize friction that may occur when the shaft 104 rotates, a bearing assembly 124 is mounted thereto. The bearing assembly 124 includes an inner race 126, an outer race 128, and balls 130. The inner race 126 contacts the shaft 104 and rotates therewith. The outer race 128 positions the balls 130 against the inner race 126 and is coupled to a portion of the housing 102, such as, for example, to the cover plate 112.
The seal assembly 200 seals the hydraulic fluid within the housing 102 and prevents the hydraulic fluid from leaking between the shaft 104 and the cover plate 112.
With reference now to both
Returning to
The seal case 216 is mounted to the housing 102, for example, the cover plate 112, and surrounds the shaft 104. The seal case 216 includes a cavity 234 formed therein within which the stator 218 is disposed. The stator 218 is configured to sealingly engage with the rotor sealing face 222, and in this regard, includes a sealing face 236. Preferably, a spring 238 is included that has a preload suitable for applying sufficient force against the stator 218 to thereby bias the stator sealing face 236 to sealingly contact the rotor sealing face 222. The stator 218 may be further secured within the seal case 216 by a retaining ring 240 and an O-ring 242.
During operation, the spacer ring 202 and the rotor 214 are engaged with one another via the spacer grooves 210, 212 and rotor flanges 224, 226 and both rotate with the shaft 104 with minimal axial travel along the shaft 104. The spring 238 applies force against the stator 218 so that the stator sealing face 236 and rotor sealing face 222 engage one another to thereby seal the opening 114.
There has now been provided a seal assembly that is effective even when a hydraulic pump stator and a rotor experience axial travel therebetween. In addition, the seal assembly continues to be operational, in the event metal chips are generated inside the pump.
While the invention has been described with reference to a preferred embodiment, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications may be made to adapt to a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this invention, but that the invention will include all embodiments falling within the scope of the appended claims.
This application claims the benefit of U.S. Provisional Application No. 60/656,286, filed Feb. 24, 2005.
Number | Date | Country | |
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60656286 | Feb 2005 | US |