The invention relates generally to camshaft phasers, more specifically to concentric camshaft phasers, and even more specifically to camshaft phasers for diesel engine applications.
It is known to use a concentric camshaft phaser (two cam shafts, one radially inside the other) to control an intake or exhaust valve train for an internal combustion engine. It also is known to use a control gear on the camshaft phaser to drive a second gear or gear driven phaser for the intake or exhaust valve train. For proper timing and operation of the phasers, the radial runout of the control gear (circumferential position of the control gear with respect to the cam shafts) must be precisely controlled. The prior art teaches the use of intermediate components, such as fasteners, to secure the control gear to the camshafts. However, the use of intermediate components introduces tolerance variations associated with the components that add an additional degree of error to the runout of the control gear. The introduced tolerances can result in a less precise circumferential location of the control gear with respect to the camshaft, adversely impacting gear durability, and timing of a system using the phaser. In addition, during operation of the phaser, gear loads are indirectly transferred to the camshafts via the phaser, resulting in unreliable radial transfer of the gear loads. Thus, it is difficult to maintain the necessary gear radial runout for reliable, durable, and repeatable operation of the phasers.
According to aspects illustrated herein, there is provided a concentric cam shaft phaser, including: a first camshaft; a second camshaft located radially inside of the first camshaft; a control gear in contact with the first camshaft and fixedly connected to the first camshaft by a weld, a press fit, or a shrink fit; a rotor non-rotatably connected to the second camshaft; and a stator non-rotatably connected to the control gear.
According to aspects illustrated herein, there is provided a concentric camshaft phaser, including: a first camshaft; a second camshaft located radially inward of the first camshaft; a control gear in contact with a radially outwardly facing surface of the first camshaft and fixedly connected to the first camshaft by a weld, a press fit, or a shrink fit; a rotor non-rotatably connected to the second camshaft; a stator non-rotatably connected to the control gear; and a plurality of chambers at least partially formed by the rotor and the stator and arranged to receive fluid at different pressures to circumferentially displace the rotor with respect to the stator to control a circumferential position of the second camshaft. The control gear is arranged to receive torque to rotate the first and second camshafts and to directly transmit the torque and radial loads to the first camshaft.
According to aspects illustrated herein, there is provided a method of fabricating a camshaft assembly, including: placing a control gear about a first camshaft and in contact with an outer circumferential surface of the first camshaft; positioning the control gear at a specified circumferential position with respect to the outer circumferential surface of the first camshaft; connecting the control gear to the first camshaft by welding, press fitting, or shrink fitting; inserting a second camshaft within the first camshaft; non-rotatably connecting a rotor to the second camshaft; and non-rotatably connecting a stator to the control gear.
The nature and mode of operation of the present invention will now be more fully described in the following detailed description of the invention taken with the accompanying figures, in which:
At the outset, it should be appreciated that like drawing numbers on different drawing views identify identical, or functionally similar, structural elements of the invention. While the present invention is described with respect to what is presently considered to be the preferred aspects, it is to be understood that the invention as claimed is not limited to the disclosed aspect. The present invention is intended to include various modifications and equivalent arrangements within the spirit and scope of the appended claims.
Furthermore, it is understood that this invention is not limited to the particular methodology, materials and modifications described and as such may, of course, vary. It is also understood that the terminology used herein is for the purpose of describing particular aspects only, and is not intended to limit the scope of the present invention, which is limited only by the appended claims.
Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood to one of ordinary skill in the art to which this invention belongs. Although any methods, devices or materials similar or equivalent to those described herein can be used in the practice or testing of the invention, the preferred methods, devices, and materials are now described.
The adverbs “axially,” “radially,” and “circumferentially” are with respect to an orientation parallel to axis 81, radius 82, or circumference 83, respectively. The adverbs “axially,” “radially,” and “circumferentially” also are regarding orientation parallel to respective planes.
In an example embodiment, phaser 100 includes chambers 112 at least partially formed by rotor 108 and stator 110. Chambers 112 are arranged to receive fluid at different pressures to circumferentially displace rotor 108 with respect to stator 110 to control a circumferential position of camshaft 104. In an example embodiment, phaser 100 includes primary drive gear 114 arranged to transmit torque to rotate camshafts 102 and 104.
Rotor 108 is coupled with stator 110 via the fluid, and rotation of stator 110 is transferred to rotor 108 via the fluid coupling. In an example embodiment, at least a portion of stator 110, for example portion 110A, is located radially inward of portion of primary drive gear 114 and is radially aligned with primary drive gear 114. In an example embodiment, at least a portion of stator 110, for example portion 110B is located radially inward of portion of control gear 106, for example portion 106A, and is radially aligned with control gear 106.
In an example embodiment, at least a portion of rotor 108 is located radially inward of at least a portion of stator 110 and radially aligned with stator 110. In an example embodiment, at least a portion rotor 108, for example, portion 108A, is axially aligned with camshafts 102 and 104.
In an example embodiment, a circumferential position of primary drive gear 114 with respect to stator 110 is adjustable and for a particular circumferential position, primary drive gear 114 is fixedly secured to stator 110 by fasteners 116 passing though slots 117 in gear 114. That is, when fasteners 116 are loosened, primary drive gear 114 is rotatable with respect to stator 110 and when fasteners 116 are tightened, the position of primary drive gear 114 with respect to stator 110 is fixed. In an example embodiment (not shown), primary drive gear 114 and stator 110 are formed of a same single piece of material.
In an example embodiment, control gear 106, in particular, radially inwardly facing surface 132, is in direct contact with radially outwardly facing surface 134 of camshaft 102.
The following provides further detail regarding phaser 100. To resolve the problems noted above regarding radial runout of the control gear and to reliably transfer radial gear loads to the camshaft, control gear 106 is directly mounted on outer camshaft 102 by weld, press fit, or shrink fit. Thus, there are no intermediate components involved in the positioning and securing of control gear 106 to camshaft 102 and the tolerance variations and unreliable transfer of radial gear loads associated with indirect transfer of gear loads through the phaser are eliminated. That is, the direct mounting of control gear 106 to outer camshaft 102 enables the radial runout of gear 106 to be better controlled and for gear loads to be transferred directly to outer camshaft 102.
As noted above, stator 110 is positioned within phaser 100 to enable a compact radial and axial packaging space. Rotor 108 is positioned within stator 110 and is fixed to camshaft 104 by means of central bolt 136. Optional primary drive gear/sprocket pulley 114 can be integrated to stator 110 as one piece, or attached by any means known in the art such as bolt, rivet, or weld. Optional primary drive gear/sprocket pulley 114 is driven by crank shaft 138 as known in the art, by means of chain, belt or gear drive 140. In an example embodiment, the circumferential timing position of primary drive gear 114 relative to stator 110 is adjustable via fasteners 116, for example during engine assembly.
As is known in the art, the phase or angle of camshaft 104 can be varied relative to the crankshaft by regulating the oil flow/pressure within chambers 112 formed by rotor vanes 142 and stator 110. In an example embodiment (not shown), primary drive gear 114 is eliminated and control gear 106 is driven by the crankshaft by means of a gear drive system.
The following should be viewed in light of
In an example embodiment, a seventh step non-rotatably connects a primary drive gear to the stator. In an example embodiment, an eighth step forms a plurality of chambers at least partially bounded by the rotor and the stator and arranged to receive fluid at different pressures to circumferentially displace the rotor with respect to the stator to control a circumferential position of the second camshaft. In an example embodiment, at least a first portion of the stator is located radially inward of a portion of the control gear and radially aligned with the control gear, and at least a second portion of the stator is located radially inward of a portion of the primary drive gear and radially aligned with the primary drive gear.
In an example embodiment, at least a first portion of the rotor is located radially inward of a portion of the stator and radially aligned with the stator, and at least a second portion of the rotor is axially aligned with the first and second camshafts. In an example embodiment, a ninth step circumferentially positions the primary drive gear with respect to the stator and a tenth step fixedly secures the primary gear to the stator with at least one fastener, such as fastener 116. In an example embodiment, an eleventh step forms the primary drive gear and the stator of a same single piece of material.
The following describes a present invention method for fabricating a concentric camshaft phaser. Although the method is presented as a sequence of steps for clarity, no order should be inferred from the sequence unless explicitly stated. A first step assembles all the components of the phaser, for example as described above, with the exception of camshafts 102 and 104. A second step assembles camshafts 102 and 104 in the nested configuration described above. A third step connects the nested camshafts to the components assembled in step 1, for example, by shrink fit, press fit, or weld.
The following describes a present invention method for fabricating a concentric camshaft phaser. Although the method is presented as a sequence of steps for clarity, no order should be inferred from the sequence unless explicitly stated. A first step assembles all the components of the phaser, for example as described above, with the exception of gear 106 and camshafts 102 and 104. A second step assembles camshafts 102 and 104 in the nested configuration described above. A third step connects gear 106 to the nested camshafts. A fourth step connects the nested camshafts and gear 106 to the components assembled in step 1, for example, by shrink fit, press fit, or weld.
It will be appreciated that various of the above-disclosed and other features and functions, or alternatives thereof, may be desirably combined into many other different systems or applications. Various presently unforeseen or unanticipated alternatives, modifications, variations, or improvements therein may be subsequently made by those skilled in the art which are also intended to be encompassed by the following claims.
This application claims the benefit under 35 U.S.C. §119(e) of U.S. Provisional Patent Application No. 61/775,904 filed Mar. 11, 2013, which application is incorporated herein in its entirety.
Number | Date | Country | |
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61775904 | Mar 2013 | US |