Not Applicable
Not Applicable
1. Field of the Invention
The present invention relates to rotary pump, and more specifically to high speed piston pumps having variable displacement, such as for use in aircraft fuel and hydraulic systems for pumping, metering and control for aircraft systems including engines.
2. Description of the Related Art
Fixed displacement pumps are conventionally employed as fuel pumps for aircraft turbine engines. Such pumps must be capable of providing sufficient fuel pressure and flow to the engine over a wide range of operating speeds from starting to full throttle operation. Therefore, a common practice is for the pump to produce a relatively high output flow rate at all times. The fuel system meters the pump output flow to supply fuel at a rate that is actually required by the engine. The excess flow from the pump bypasses the engine and is recycled to the pump inlet.
However, circulation in the bypass circuit heats the fuel, which may become excessively hot, especially when a relatively low flow fuel flow rate is demanded by the engine. As a result, a heat exchanger typically is provided in the bypass circuit to cool the fuel before returning it to the pump inlet. This adds complexity, weight and expense to the fuel system.
Size and weight are also important characteristics of components used in aircraft. Thus it is desirable to refine existing piston pump technology to reduce the size, reduce the weight, and increase the operating limits for speed, while providing a high degree of pump reliability.
A radial piston pump has a housing with a cavity into which a fluid inlet passage and a fluid outlet passage open. A cylinder ring is located within the cavity and has an aperture within which a cam surface is formed. In a preferred embodiment, the cylinder ring is pivotally supported within the cavity and has a circular aperture with a bearing ring therein that forms an interior cylindrical cam surface, for example.
A cylinder block is mounted for rotation within the aperture of the cylinder ring and has a plurality of radially extending cylinders. Each radially extending cylinder has a port, which selectively communicates with the fluid inlet passage and a fluid outlet passage as the cylinder block rotates. A plurality of cylinders pistons, which are free to slide, are received within the plurality of cylinders and engage the cam surface of the cylinder ring. An actuator is operably coupled to produce movement of the cylinder ring, which alters the spatial relationship between the cylinder ring and the cylinder block to vary the distance that the pistons move within the cylinders.
The magnitude of fluid flow produced by the pump is directly related to the stroke of the pistons, (amount of movement) within the cylinders as the cylinder block rotates. Therefore, varying the position of the cylinder ring in relation to the cylinder block controls the magnitude of fluid flow.
The present invention is being described in the context of a fuel pump for a gas turbine engine for an aircraft, however it should be appreciated that the novel concepts of this invention have application to a wide variety of pumps for other fluids and equipment.
With reference initially to
An inlet port 14 in the housing 12 is connected by an inlet passage 15 with two branches that lead through the second housing segment 13 to two inlet passage openings 20 and 21 into the internal cavity 18. A secondary inlet passage 19 in the first housing segment 11 extends from the outer region of the internal cavity 18 to another inlet passage opening 22 in the central region of the cavity. When the pump 10 is operating, a portion of the fluid introduced into the inlet port 14 flows from opening 20 through the outer region of the internal cavity 18 into the secondary inlet passage 19 and continues to flow to the inlet passage opening 22. An outlet passage 17 extends through the housing 12 from separate openings 23 and 24 in each housing segment 11 and 13, respectively, to an outlet port 16. Note that a portion of the outlet passage 17 extends through the housing 12 behind the internal cavity 18 and is not visible in the cross sectional view of
The two pump sections 28 and 29 are identical, but are shown rotated 180 degrees about the pump shaft with respect to each other. Other angles may be selected depending on application requirements. As a consequence, the openings 21 and 23 of the inlet and outlet passages 15 and 17 for the first pump section 28 are oriented 180 degrees around the pump shaft axis with respect to the openings 22 and 24 of the inlet and outlet passages 19 and 17 for the second pump section 29. That is in the orientation of
The first pump section 28 is shown in detail in
The cylinder ring 30 has a circular aperture 36 through which the drive and pump shafts 25 and 26 extend. An annular bushing 38 is located within the circular aperture 36 and a bearing ring 40 is slideably received within the annular bushing. The inner circumferential surface of the bearing ring 40 has an annular groove that forms a cam surface 42 against which a first plurality of valve pistons 48 travel, as will be described. Although the preferred embodiment of the cylinder ring 30 has a circular aperture 36, that aperture and thus the inner circumferential surface of the bearing ring 40 may have other geometric shapes. It should also be noted that bearing shoes might be placed between the bearing ring 40 and the piston 48.
The first pump section 28 is formed by a portion of the cylinder block 44 and fastened to the pump shaft 26 so as to rotate therewith. The cylinder block 44 has a first set of eight cylinders 46 arranged equal distantly around and extending radially outward from the axis of the pump shaft 26. The interior end of each cylinder has a kidney shaped cylinder port 45 in the cylinder block 44. In different rotational positions of each cylinder 46, its port 45 communicates with the opening 21 of the inlet passage 15 or the opening 23 of the outlet passage 17 shown in
In the maximum flow configuration of the pump, the spring 32 pivots the cylinder ring 30 into the extreme counter-clockwise position as illustrated in
As the cylinder block 44 rotates so that a given cylinder 46 is approaching the bottom dead center point 50, the piston 48 within that cylinder is moving outward thereby expanding the volume of the cylinder chamber. The direction of rotation is such that as the cylinder chamber is expanding, the port 45 for the given cylinder communicates with the inlet passage opening 21 so that fluid is drawn into the cylinder chamber. At the bottom dead center point 50, the cylinder port 45 is adjacent solid wall of the housing and no longer communicates with the inlet passage opening 21. As the cylinder block 44 rotates away from the bottom dead center point 50, the port 45 of the given cylinder 46 is exposed to the outlet passage opening 23. Continued rotation of the cylinder block 44 moves the piston 48 into a region where the gap between the cylinder block 44 and the bearing ring 40 decreases thereby pushing the piston into the given cylinder. This action forces the fluid from the cylinder into the outlet passage 17, pressure resulting from restriction to the fluid flow.
As the given cylinder 48 passes the top dead center point 52, its port 45 is closed off from both the inlet and outlet passage openings 21 and 23. Further rotation of the cylinder block 44 thereafter causes the piston 48 to move out of the given cylinder 46, which expands the cylinder chamber, while the cylinder port 45 communicates with the inlet passage opening 21 thereby repeating the pumping cycle.
By applying different levels of pressure into the control bore 34; the pump actuation piston 33 is operated to pivot the cylinder ring 30 into different positions within the cavity 18. The pivoting of the cylinder ring 30 changes the spatial relationship of the bearing ring 40 to the cylinder block 44, thereby changing the annular gap between those components. Specifically, pivoting the cylinder ring 30 changes the distance of the gap at the bottom dead center point 50 and the top dead center point 52. This varies the amount of piston travel within each cylinder as the pistons revolve around the axis of the pump shaft 26 and thus alters the amount of fluid delivered by the pistons.
As noted previously,
The cylinder block 44 has a second set of eight cylinders 60 arranged parallel to the first set of cylinders 46, which form the second pump section 29 which are visible in
The foregoing description was primarily directed to a preferred embodiment of the invention. Although some attention was given to various alternatives within the scope of the invention, it is anticipated that one skilled in the art will likely realize additional alternatives that are now apparent from disclosure of embodiments of the invention. Accordingly, the scope of the invention should be determined from the following claims and not limited by the above disclosure.