Apparatus and method for measuring cam phaser locking pin position

Information

  • Patent Grant
  • 6637390
  • Patent Number
    6,637,390
  • Date Filed
    Thursday, May 23, 2002
    22 years ago
  • Date Issued
    Tuesday, October 28, 2003
    21 years ago
Abstract
A vane-type cam phaser wherein a realtime method of measuring the axial position of the phaser's locking pin is provided. A magnet is fixed to the nose portion of the locking pin. A Hall-effect sensor is attached to the stator of the phaser in proximity to the magnet. As the locking pin moves through its range of travel, the magnet moves either toward or away from the sensor resulting in a proportional increase or decrease in sensor output voltage. By reading the voltage output, the axial position of the locking pin can be determined.
Description




TECHNICAL FIELD




The present invention relates to cam phasers for altering the phase relationship between valve motion and piston motion in reciprocating internal combustion engines; more particularly, to cam phasers having a vaned rotor rotatably disposed in an internally-lobed stator wherein the rotor and stator can be mechanically locked together by a locking pin; and most particularly to an apparatus and method for accurately measuring the axial position of the locking pin within its range of travel.




BACKGROUND OF THE INVENTION




Cam phasers are well known in the automotive art as elements of systems for reducing combustion formation of nitrogen oxides (NOX), reducing emission of unburned hydrocarbons, improving fuel economy, and improving engine torque at various speeds. Typically, a cam phaser employs a first element driven in fixed relationship to the crankshaft and a second element adjacent to the first element and mounted to the end of the camshaft in either the engine head or block. A cam phaser is commonly disposed at the camshaft end opposite the engine flywheel. The first element is typically a cylindrical stator mounted inside a crankshaft-driven gear or pulley, the stator having a plurality of radially-disposed inwardly-extending spaced-apart lobes and an axial bore. The second element is a vaned rotor mounted to the end of the camshaft through the stator axial bore and having vanes disposed between the stator lobes to form actuation chambers therebetween such that limited relative rotational motion is possible between the stator and the rotor. Such a phaser is known in the art as a vane-type cam phaser.




The disposition of the rotor in the stator forms a first, or timing-advancing, array of chambers on first sides of the vanes and a second, or timing-retarding, array of chambers on the opposite sides of the vanes. The apparatus is provided with suitable porting so that hydraulic fluid, for example, engine oil under engine oil pump pressure, can be brought to bear controllably on opposite sides of the vanes in the advancing and retarding chambers. Control circuitry and valving, commonly a multiport spool valve, permit the programmable addition and subtraction of oil to the advance and retard chambers to cause a change in rotational phase between the stator and the rotor, in either the rotationally forward or backwards direction, and hence a change in timing between the pistons and the valves.




Under conditions of low engine oil pump pressure, such as during startup, it is desirable to mechanically lock the rotor and stator together in a default mode to prevent unwanted relative angular movement of the rotor/stator when the pump pressure is not high enough to reliably position the rotor relative to the stator. This is typically accomplished by a hydraulically activated locking pin disposed in the rotor and positioned parallel to the rotational axis of the phaser. In the default position, when the rotor and stator are locked together, a locking pin spring biases the cylindrical locking pin outward to engage a pin bore disposed in the stator. When the oil pump pressure reached a pre-determined level, the hydraulic force of the oil causes the locking pin to retract from the pin bore and into the rotor thereby decoupling the rotor from the stator and permitting cam shaft phasing to occur. When the rotor and stator are mechanically locked together in the default mode, the torsional forces applied to the stator by the engine crankshaft are transferred to the rotor/camshaft via lateral loading of the locking pin in the pin bore.




It is desirable for the pin to be retracted from the coupled mode in a predictable manner to assure that the decoupling event occurs precisely when needed. That is, when a predetermined oil pressure is reached after engine start-up. Therefore, during development and testing of the cam phaser, it is desirable to accurately measure the actual axial position of the locking pin relative to oil pump pressure in order, for example, to calibrate the locking pin spring. This measurement is difficult to obtain because the locking pin itself is buried inside the cam phaser and rotates with the cam shaft. Moreover, since space in the area of the cam phaser is limited, there is very little room to mount measuring equipment that could accurately monitor the axial position of the locking pin.




What is needed is in the art is a method of accurately measuring the axial position of the cam phaser locking pin, during “real-time” engine operation, to determine pin position relative to oil pump pressure exerted on the locking pin.




SUMMARY OF THE INVENTION




The present invention is directed to a vane-type camshaft phaser wherein a locking pin assembly, including a locking pin, bushing and spring, is disposed between a rotor and a stator of the phaser to selectively couple the rotor and stator together. The invention allows the axial position of the locking pin to be accurately determined through its entire range of travel by the use of a Hall-effect sensor. A permanent magnet is secured to the nose portion of the locking pin and a sensor is secured to the floor of the mating pin bore. By measuring the voltage output of the Hall-effect sensor as the magnet moves away from the sensor, the axial position of the locking pin can be determined.











BRIEF DESCRIPTION OF THE DRAWINGS




The foregoing and other objects, features, and advantages of the invention, as well as presently preferred embodiments thereof, will become more apparent from a reading of the following description, in connection with the accompanying drawings in which:





FIG. 1

is an exploded isometric view of a vaned cam phaser;





FIG. 2

is an exploded isometric view of a the vaned cam phaser of

FIG. 1

, looking from the back end;





FIG. 3

is an axial view showing the rotor assembled into the stator;





FIG. 4

is a side cross-sectional view of the locking pin mechanism of the present invention; and





FIG. 5

is a plot showing the correlation between the measured output voltage of the sensor and the axial position of the locking pin.











DESCRIPTION OF THE PREFERRED EMBODIMENT




Referring to

FIGS. 1-3

, vane-type cam phaser


10


includes a stator


12


having a plurality of inwardly-extending lobes


14


, and a rotor


16


having a cylindrical hub


18


and a plurality of outwardly-extending vanes


20


. As best shown in

FIG. 3

, when rotor


12


is assembled into stator


16


, a plurality of timing-advancing chambers


15


and timing-retarding chambers


17


are formed between the rotor vanes and the stator lobes. Axially-extending lobe seals


19


and vane seals


21


prevent hydraulic leakage between the chambers. Referring again to

FIG. 1

, back plate


22


, which seals the back side of stator


12


, rotor


16


, and the plurality of chambers


15


,


17


is attached to sprocket


24


for being rotationally driven, as by a timing chain or ribbed belt, from a crankshaft sprocket or gear in known fashion. Bore


23


in back plate


22


typically is receivable of the outer end of an engine camshaft (not shown) of internal combustion engine


25


on which phaser


10


may be thus mounted in known fashion. Opposite back plate


22


is a cover plate


28


for sealing the front side of the phaser hydraulics analogously to back plate


22


. Bolts


34


extend through cover plate


28


and stator


12


and are secured into threaded bores


36


in back plate


22


. The assembled cover plate, stator, and back plate define a unitized housing wherein rotor


16


may rotate through an axial angle sufficient to advance or retard the opening of engine valves through a predetermined angular range, typically about 30°. An actuable locking pin assembly


26


, comprising pin


38


, spring


40


, and bushing


42


, disposed in recess


27


(

FIG. 2

) in a vane of rotor


16


may be extended at certain times in the cam phaser operation, such as during engine start-up, to engage bore


29


in back plate


22


for preventing relative rotation between the rotor and stator. When the oil pump pressure reaches a pre-determined level, the hydraulic force of the oil causes locking pin


38


to retract from its engagement with bore


29


, against the force of spring


40


, and into rotor


12


thereby mechanically decoupling the rotor from the stator and permitting cam shaft phasing to occur. When the oil pump pressure falls below a predetermined level (such as during start-up), spring


40


biases locking pin toward back plate


22


to engage bore


29


. Cam phaser


10


is provided with suitable and separate porting so that engine oil, under engine oil pump pressure, can be brought to bear controllably on either side


30


or side


32


of vanes


20


to rotationally advance or retard the rotor by directing oil into either advancing chambers


15


or retarding chambers


17


(FIG.


3


). Suitable porting is also provided to communicate pressurized engine oil to the locking pin.





FIG. 4

is a cross-section view of rotor


16


, stator


12


and locking pin assembly


26


, with pin


38


in its locking position, and shows the preferred embodiment of the invention. Nose


48


of pin


38


defines bore


52


for receiving permanent magnet


50


. Permanent magnet


50


is secured in place, for example, by an epoxy adhesive or other bonding agent. Hall-effect sensor


54


(such as the ratiometric linear sensor, model number A3515LUA, made by Allegro Microsystems of Worcester, Mass.), is positioned within the magnetic field of magnet


50


and is secured to floor


56


of pin recess


29


also, for example, by an epoxy adhesive or other bonding agent. Passage


58


and channel


60


are provided in stator


12


for receiving sensor wires


62


. Wires


62


terminate at juncture


64


where an electrical connection is made with a slip ring assembly or the like, known in the art, for further connection with outside measuring device


66


.




In use, Hall-effect sensor


54


provides a voltage output proportional to the magnetic field measured from magnet


50


. Sensor


54


has a nominal voltage output of, for example, 2.5 v when the sensor is not subjected to the magnetic field of the magnet. In the cam phaser “locked” position shown in

FIG. 4

, pin


38


is fully engaged in pin bore


29


, and magnet


50


is closest to sensor


54


. Hence, in the pin position shown, the greatest change from the nominal voltage output would be measured by device


66


. As pin


38


retracts from bore


29


in the direction shown by arrow


68


, the magnetic field encompassing sensor


54


becomes less concentrated causing a proportional decrease (or increase depending on the relative polarities of the magnet and sensor) in the sensor's output voltage measured by device


66


. Thus, there is a measurable and predictable change in output voltage as the locking pin moves away from it fully engaged position.





FIG. 5

shows the relationship of measured voltage output of sensor


54


and the axial position of pin


38


, as the locking pin moves away from it fully engaged position. As can be seen, by measuring the output voltage of sensor


54


, the axial position of locking pin


38


within its range of travel can be accurately determined.




In the embodiment shown, magnet


50


is mounted in the lower portion of the locking pin and sensor


54


is mounted on the floor of bore


29


. However, it is understood that the magnet and/or sensor can be mounted anywhere as long as the magnet is in continuous magnetic communication with the sensor.




The foregoing description of the invention, including a preferred embodiment thereof, has been presented for the purpose of illustration and description. It is not intended to be exhaustive nor is it intended to limit the invention to the precise form disclosed. It will be apparent to those skilled in the art that the disclosed embodiments may be modified in light of the above teachings. The embodiments described are chosen to provide an illustration of principles of the invention and its practical application to enable thereby one of ordinary skill in the art to utilize the invention in various embodiments and with various modifications as are suited to the particular use contemplated. Therefore, the foregoing description is to be considered exemplary, rather than limiting, and the true scope of the invention is that described in the following claims.



Claims
  • 1. An apparatus for measuring the axial position of a locking pin of a cam phaser, said cam phaser having a unitized housing including a lobed stator and a vaned rotor disposed within the stator; said apparatus comprising:a) a locking pin assembly disposed in said rotor for selectively coupling said rotor and stator together wherein said locking pin assembly includes said locking pin and a magnet secured to said pin; b) a sensing means secured in a pin bore in said stator for sensing a magnetic field of said magnet and in continuous magnetic communication with said magnet; and c) a means for reading an electrical output of said sensing means through a range of travel of said locking pin.
  • 2. An apparatus in accordance with claim 1, wherein said magnet is secured to a nose portion of said locking pin.
  • 3. An apparatus in accordance with claim 1, wherein said magnet is a permanent magnet.
  • 4. An apparatus in accordance with claim 1, wherein said sensing means is a Hall-effect sensor.
  • 5. An apparatus in accordance with claim 4, wherein said sensor is secured to a floor of said pin bore.
  • 6. An internal combustion engine comprising:a cam phaser having a unitized housing including a lobed stator and a vaned rotor disposed within the stator; a locking pin assembly disposed in said rotor for selectively coupling said rotor and stator together wherein said locking pin assembly includes a locking pin and a magnet secured to said pin; a sensing means disposed in said stator for sensing a magnetic field of said magnet and in continuous magnetic communication with said magnet; and a means for reading an electrical output of said sensing means through a range of travel of said locking pin.
  • 7. An engine in accordance with claim 6, wherein said magnet is secured to a nose portion of said locking pin.
  • 8. An engine in accordance with claim 6, wherein said magnet is a permanent magnet.
  • 9. An engine in accordance with claim 6, wherein said sensing means is a Hall-effect sensor.
  • 10. An engine in accordance with claim 9, wherein said sensor is disposed in a pin bore of said stator.
  • 11. A method of measuring the axial position of a cam phaser locking pin comprising the steps of:attaching a magnet to the locking pin; affixing a sensing means for sensing the magnetic field of said magnet, fixedly positioned with respect to the locking pin, and in continuous magnetic communication with said magnet through a range of travel of said locking pin; and determining the position of the locking pin by measuring a voltage output of the sensing means.
  • 12. A method of measuring in accordance with claim 1, wherein the attaching step includes attaching said magnet to a nose portion of said locking pin.
  • 13. A method of measuring in accordance with claim 11, wherein the affixing step includes affixing said sensing means to a stator of said cam phaser.
US Referenced Citations (4)
Number Name Date Kind
5209202 Maurer et al. May 1993 A
5522352 Adachi et al. Jun 1996 A
5715780 Haller Feb 1998 A
6257186 Heer Jul 2001 B1