Background of the Invention
This invention relates to an automatic compression relief mechanism for internal combustion engines and more particularly to centrifugally responsive apparatus by which, during the compression stroke of an internal combustion engine, compression is partially relieved at engine cranking speeds, but is allowed to build up to full value at running speeds.
Very generally the compression relief mechanism of the present invention is of the type disclosed in U.S. Pat. Nos. 3,314,408, 3,620,203, 3,901,199 and 3,981,289. In each of those prior devices, as in the mechanism of this invention, the valve that controls the flow of gas through a port communicating with the engine combustion chamber is held slightly off its seat during the compression stroke, at cranking speeds of the engine, to allow a certain amount of gas to be displaced through the port, thus relieving the force of compression that opposes cranking rotation of the engine crankshaft. At running speeds, the valve is permitted to remain seated during the compression stroke so that the normal performance of the engine is not impaired.
In the conventional compression release mechanism, the operation of the exhaust valve is controlled by an auxiliary cam member on the camshaft. The auxiliary cam member is arranged to move between an operative, radially extending position, in which the auxiliary cam member effects the desired unseating of the exhaust valve for compression relief, and a retracted inoperative position. The position of the auxiliary cam member is in turn controlled by a centrifugally actuated flyweight that is carried by the camshaft and is mounted for movement relative to the camshaft between defined limits in directions transverse to the camshaft axis. The flyweight is biased to one of its limits of motion and is moved to its other limit of motion by centrifugal force. A connection between the flyweight and the cam member translates the bias produced motion of the flyweight towards its one limit into movement of the cam member towards its extended or operative position, while movement of the flyweight under centrifugal force toward its other limit will retract the cam member to its inoperative position.
The prior compression relief expedients of the general type above described require multiple parts that have relatively complicated shapes or require special tooling and/or modification of the camshaft for installation.
A simplified compression release mechanism is shown in U.S. Pat. No. 3,314,408 in which a generally U-shaped centrifugally actuated latch is pivotally connected to the camshaft. One end of the latch defines an auxiliary cam member, while the opposite end of the latch is provided with a flyweight. The cam member is biased by a spring to the operative valve unseating position, and at running speeds the latch is pivoted to move the cam member to the inoperative position. The device of U.S. Pat. No. 3,314,408 is characterized by the fact that the valve load, when the cam member is in its operative position, is born solely by the pivot pin, thus requiring specially tempered or hardened metals for the pin to prevent failure.
Summary of the Invention
The invention is directed to an improved centrifugally responsive compression release mechanism for an internal combustion engine. The mechanism includes a yoke having a pair of legs that straddle the cam shaft and are pivoted to the camshaft by a pivot pin. The saddle portion of the yoke, which connects the legs, includes an auxiliary cam member, while the legs are provided with counterweights that serve, under non-rotational conditions, to bias the yoke to a position in which the auxiliary cam member is in a valve unseating condition so that the auxiliary cam member will unseat the valve during the compression stroke at engine cranking speeds.
As the rotation speed of the camshaft increases, the centrifugal force acting through the center of mass overcomes the gravitational force and the yoke pivots in the opposite direction resulting in movement of the auxiliary cam member to an inoperative position so that the valve will remain seated during the compression stroke.
In accordance with yet another aspect of the invention, the auxiliary cam member is provided with a load bearing surface that engages the cam shaft, when the cam member is in the operative, valve unseating position, and thus distributes the valve load through the camshaft rather than through the pivot pin.
The present invention thus provides a dependable compression release mechanism that utilizes gravitational and centrifugal forces, and eliminates the need for multiple parts, as required with compression release mechanisms as used in the past.
The present invention also provides a simple, one-piece inexpensive compression release mechanism that can be readily installed without special tooling and without appreciable camshaft modification.
Description of the Drawings
The drawings illustrate the best mode presently contemplated of carrying out the invention.
In the drawings:
FIG. 1 is a side elevation of a valve of an internal combustion engine and actuating mechanism therefor that embodies the principles of this invention, the parts being shown in the positions they occupy during the compression stroke at engine cranking speeds;
FIG. 2 is a view generally similar to FIG. 1, but showing the parts in the position they occupy at normal engine running speeds;
FIG. 3 is a sectional view taken along line 3--3 of FIG. 2.
FIG. 4 is a perspective view of the compression relief yoke of the present invention; and
FIG. 5 is a side view of the compression relief yoke.
Description of the Illustrated Embodiment
As shown in FIGS. 1 and 2, a valve 1, which can be either an exhaust valve or an intake valve, controls flow of gas between a port 2 and the combustion chamber of the engine. The combustion chamber is not specifically illustrated but will be understood to be denoted by the area to the left of the valve in FIGS. 1 and 2.
The valve 1 is of the usual poppet type, having a head 3 that moves to and from engagement with a circumferential seat 4, the valve being closed when the head is engaged with its seat. The valve has an axially movable structure 5 that provides for its actuation between its closed position and an open position. Movable structure 5 comprises a stem 6 that is integral with the head 3 and extends therefrom, and a coaxial tappet 7 that is separated from the stem. The valve stem 6 is confined for axial motion in a valve guide 8 in the engine body, while the tappet 7 is similarly mounted in a coaxial tappet guide 9 in the engine body.
The valve 1 is actuated for its opening and closing motion by an actuating mechanism comprising a valve spring 10 and a cam 11. The valve spring 10 as is conventional, surrounds the valve stem and reacts between the surface of the valve guide and a spring retainer 12 at the end of valve stem 6, to bias the valve towards its closed position. The cam 11, which is on camshaft 13 that rotates in timed relation to the engine cycle, cooperates with follower 14 on tapper 7 to move the valve to its open position against the biasing force of the valve spring and to control the spring return of the valve towards engagement with its seat.
The camshaft is rotated by means of a cam gear 15, which, as is conventional, meshes with a timing gear (not shown) on the engine crankshaft.
According to the present invention, compression is released in the combustion chamber during the compression stroke at engine cranking speeds by a compression release member 16.
As shown in FIG. 4, the member 16 is yoke-shaped, having a pair of legs 17 that straddle camshaft 13 and are pivotally connected to the camshaft by means of pin 18. The legs 17 are connected together by a curved saddle or neck 19, and saddle 19 carries an outwardly curved projection 20 that constitutes an auxiliary cam member.
At the ends of legs 17 are counterweights 21 that extend along a line substantially parallel to the axis of rotation of camshaft 13. Counterweights 21 are received in holes 22 located in cam gear 15. The counterweights 21 serve to bias the yoke member 16 by gravity to the position shown in FIG. 1, in which the auxiliary cam member 20 is in the operative valve unseating position. Engagement of the notched edges 23 of legs 17 with the edges of gear 15 bordering holes 22 serves as a stop to limit the movement of the yoke member under gravitational force. In this condition, during cranking of the engine, the auxiliary cam member 20 will engage the follower 14 during the compression stroke to release compression in the combustion chamber.
Thus at low crankshaft speeds, auxiliary cam member 20 assumes its FIG. 1 position where it engages cam follower 14 to unseat valve 1 to release the compression. In this operable position the load and shock are transferred to camshaft 13 via load bearing surface 24 located at the base of the cam member 20.
As the crankshaft speed increases and reaches running speed, centrifugal force acting through the center of mass will pivot the yoke member 16 to the position shown in FIG. 2, causing the auxiliary cam member 20 to be displaced, generally in an axial direction, to the inoperative position where it will not interfere with the movement of follower 14. Engagement of projection 25 on yoke member 16 with gear 15 serves to limit the pivotal movement of the yoke member under centrifugal action.
When rotation of crankshaft 13 is slowed or stopped, the gravitational force will one again become dominant and yoke member 16 will pivot to its operable FIG. 1 position.
While the drawings show the compression release member 16 being biased to its operative position by gravity, it is contemplated that in certain installations, the compression release member may be biased to its operative position by a spring or other resilient element.
Various modes of carrying out the invention are contemplated as being within the scope of the following claims particularly pointing out and distinctly claiming the subject matter which is regarded as the invention.