The present invention relates to linkage assemblies that control boost pressure in turbochargers and their use in combination with internal combustion engines.
Turbochargers are generally well known in the art. The basic function of a turbocharger is to increase air flow going into the intake manifold of the engine. Increasing the pressure of the air going into the intake manifold, and hence the piston cylinders, increases the power of the engine. Turbochargers are powered by exhaust gas pressure flowing into a turbine, which in turn rotates a compressor. The compressor is connected to the intake manifold, as the compressor increases in speed, the air pressure going into the intake manifold increases as well. One method used for controlling the flow of exhaust gas into the turbine is the use of a series of vanes circumferentially spaced evenly around the turbine. The turbochargers that use vanes in the way described here are generally known as variable geometry turbochargers. As the vanes change position, the pressure of the exhaust gas flowing into the turbine can be increased or decreased. The vanes are all connected to a single ring, and as the ring rotates, the vanes change position. The ring is typically connected to a shaft; the shaft is fixed about a pivot point for rotation. As the shaft rotates about the pivot point, the ring rotates, changing the position of the vanes. Rotating the shaft is accomplished by a linkage assembly, connected to an actuator.
The torque required to move the shaft may vary with the degree of rotation. The variation is caused by friction within the vanes and by debris that can accumulate on the linkage assembly with normal usage.
A linkage is used to interconnect the shaft of the actuator and the shaft connected to the ring. The linkage also provides a mechanical advantage that will increase the torque provided by the actuator as the linkage moves through its rotation.
Typical linkage designs consist of a four-bar linkage assembly, with various pivot points. A common problem that occurs when using this type of design is the limited ability of the four-bar linkage to closely match the mechanical advantage to the torque required by the vanes through rotation. As previously mentioned, friction within the vanes and debris are the two main causes for the torque to vary with degree of rotation. The debris that builds up on the linkage is from the exhaust gases, which results from normal engine operation. Over time, the debris build up can worsen, having a greater effect on the use of the linkage.
The present invention relates to a linkage assembly for obtaining a mechanical advantage having a first lever having a first end and a second end. The first end of the first lever is connected to an actuator and is rotatable about the first end. There is also a second lever having a moveable first end connected to a device that is being controlled by the linkage assembly. The second lever also has a second end. The second end of the first lever and the second end of the second lever are operably connected together by a mechanical connection. The mechanical connection of the first and second levers are connected in such a way that a variable mechanical advantage is created by varying the effective length of one or more of the levers when the actuator rotates the first lever.
In one embodiment, the mechanical connection for operably connecting the second end of the first lever and second end of the second lever is a pin and slot configuration. The mechanical connection is formed by the second end of the first lever being a pin that is slidable disposed within a slot formed on the second end of the second lever. In order to prevent build up of debris between the slot and the pin another embodiment of the present invention incorporates the use of anticontamination members. Another embodiment of the invention incorporates a guard member on the pin in order to prevent the build up of debris between the pin and slot. In an alternate embodiment, the guard member also has scrapers that scrap debris off the slot as the pin slides along the slot.
Further areas of applicability of the present invention will become apparent from the detailed description provided hereinafter. It should be understood that the detailed description and specific examples, while indicating the preferred embodiment of the invention, are intended for purposes of illustration only and are not intended to limit the scope of the invention.
The present invention will become more fully understood from the detailed description and the accompanying drawings, wherein:
The following description of the preferred embodiment(s) is merely exemplary in nature and is in no way intended to limit the invention, its application, or uses.
The first lever 30 has an elongated slot 40 formed on the first lever 30. The slot 40 extends from a second end 41 of the first lever 30. The second lever 34 has a pin 42 located at a second end 43 of the second lever 34. The pin 42 is slidable disposed in the slot 40 to form a mechanical connection between the first and second levers 30, 34. The torque of the actuator shaft 36 causes the second lever 34 and pin 42 to rotate. The first lever 30 and the control mechanism shaft 32 will follow the movement of the second lever 34 and pin 42. The mechanical advantage of this lever arrangement, at any point through the rotation, is the ratio of the effective lever length of the first lever 30 and the effective lever length of the second lever 34.
The rate of changing the mechanical advantage through the rotation is further controlled by the shape of or contour 44 in the slot 40 of the first lever 30. Adjusting the contour 44 will provide a continuously variable rate through the rotation of the actuator shaft 36. Controlling the mechanical advantage through rotation provides a method of matching the required torque of the control mechanism to the available torque of the actuator 38. For example, a higher torque may be provided at a specific point through the rotation of the control mechanism, by adjusting the contour of the slot.
As the actuator 38 rotates the second lever 34, the pin 42 moves through the slot 40 changing the position of the second lever 34 relative to the second torque arm 30, thereby changing the amount of torque transferred therebetween.
It should be noted that the locations of the pin 42 and slot 40 could be reversed. For example, the slot 40 can be in the second lever 34 and the pin 42 can be located on the first lever 30. It is also within the scope of this invention for the pin 42 and slot 40 assembly to be replaced with some other devices to cause the same interaction between first lever 30 and second lever 34, such as a roller and cam assembly, a rack and pinion combination, or concentric shafts.
The interface of the pin 42 and the surface of the slot 40 can result in friction that will reduce the available torque to the control mechanism. In one embodiment a means of reducing friction is used to maintain the maximum amount of torque available to control the mechanism. The means can be a lubricant or low friction coating such as Teflon or boron nitride to reduce the torque loss. Alternatively a bearing, a bushing or some other type of friction reducing device is used.
The operation of the lever arrangement may also be affected by debris such as dirt and oil. An alternate embodiment of the present invention includes a means for controlling or removing debris build-up. The means for controlling debris build- up is accomplished using a guard, a scraper or some other anti-contamination device.
A “C” clip 54 is inserted into groove 56 in pin 42 to secure guards 48. It is possible to otherwise adhesively bond the guard 48 to the pin 42 such as by way of welding or adhering. An alternate method of retaining the guards 48 would be to integrally form the guard 48 with the pin 42.
The description of the invention is merely exemplary in nature and, thus, variations that do not depart from the gist of the invention are intended to be within the scope of the invention. Such variations are not to be regarded as a departure from the spirit and scope of the invention.
This application claims the benefit of U.S. Provisional Application No. 60/654,924, filed Feb. 22, 2005. The disclosures of the above application(s) is (are) incorporated herein by reference.
Number | Date | Country | |
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60654924 | Feb 2005 | US |