Engine-rotation detecting system

Abstract: A first thrust limiting member and a second thrust limiting member are provided on a cam shaft rotatably carried between a lower cam shaft holder and an upper cam shaft holder which are fixed to an upper surface of a cylinder head 1, so that the first and second thrust limiting members and abut against the cam shaft holders 9 5 and 10 5 . The second thrust limiting member has a plurality of detected projections provided around of an outer periphery thereof, so that the detected projections are detected by a TDC sensor 37 mounted to a head cover of the engine. Thus, the rotated position (phase), the angle of rotation and the number of rotations of an rotary shaft of an engine such as a cam shaft 6e and a crankshaft can be detected with good accuracy in a structure including a decreased number of parts, and the axial dimension of the rotary shaft of the engine can be reduced.

Description: BACKGROUND OF THE INVENTION 1. FIELD OF THE INVENTION The present invention relates to an engine-rotation detecting system including a detected portion provided on a rotary shaft of an engine, and a sensor for detecting the position of the detected portion. 2. DESCRIPTION OF THE RELATED ART A detecting system for detecting a crank angle of an engine is conventionally known from Japanese Utility Model Application Laid-open No.62-26566, which includes a detected portion projectingly provided on an outer periphery of a rotatable plate mounted on a crankshaft, and a sensor disposed in the vicinity of the rotatable plate for detecting the position of the detected portion. In general, the rotatable plate for detecting the rotation is conventionally provided separately from a thrust limiting plate for limiting the axial movement of the rotary shaft of the engine, resulting in an increased number of parts due to the rotatable plate. In addition, the position of the rotatable plate is spaced apart from the position of the thrust limiting plate and for this reason, there is a possibility that the position of the rotatable plate may be varied by an influence of the thermal expansion of the rotary shaft or the like, resulting in a reduced detection accuracy of the sensor. SUMMARY OF THE INVENTION Accordingly, it is an object of the present invention to detect the rotated position (phase), the angle of rotation and the number of rotations of the rotary shaft of the engine such as a cam shaft and a crankshaft in a structure including a decreased number of parts, and to reduce the axial dimension of the rotary shaft of the engine. To achieve the above object, according to a first aspect and feature of the present invention, there is provided an engine-rotation detecting system comprising a detected portion provided on a rotary shaft of an engine, and a sensor for detecting the position of the detected portion, wherein the detected portion is provided on a thrust limiting member mounted on the rotary shaft for limiting the axial movement of the rotary shaft. With the above arrangement, the detected portion to be detected by the sensor is provided on the thrust limiting member mounted on the rotary shaft for limiting the axial movement of the rotary shaft. Therefore, a special member for provision of the detected portion is not required, leading to a decreased number of parts. Additionally, the axial dimension of the engine can be reduced and moreover, the position of the detected portion can be prevented from being axially displaced to enhance the detection accuracy. EP698 728, which is considered to represent the closest prior art, shows an engine-rotation detecting system comprising a detected portion provided on a cam shaft supported between an upper cam shaft holder and a lower cam shaft holder mounted on a cylinder head of an engine, and a sensor for detecting a position of said detected portion, wherein said detected portion is provided on a thrust limiting member mounted on said cam shaft, said thrust limiting member being adapted to limit an axial movement of said cam shaft and being further adapted to suppress an axial displacement of said detected portion. The above and other objects, features and advantages of the invention will become apparent from the following description of the preferred embodiments taken in conjunction with the accompanying drawings. BRIEF DESCRIPTION OF THE DRAWINGS Figs.1 to 9 illustrate a presently preferred embodiment of the present invention, wherein Fig.1 is a plan view illustrating a serial 4-cylinder engine in a state in which a head cover has been removed; Fig.2 is an enlarged view of an essential portion shown in Fig.1; Fig.3 is a sectional view taken along a line 3-3 in Fig.2; Fig.4 is a sectional view taken along a line 4-4 in Fig.2; Fig.5 is a sectional view taken along a line 5-5 in Fig.2; Fig.6 is a view (a top view of a lower cam shaft holder) taken along a line 6-6 in Fig.5; Fig.7 is a view (a bottom view of the lower cam shaft holder) taken along a line 7-7 in Fig.5; Fig.8 is a view taken in a direction of an arrow 8 in Fig.5; and Fig.9 is a sectional view taken along a line 9-9 in Fig.5. DETAILED DESCIPTION OF THE PREFERRED EMBODIMENT The present invention will now be described by way of a particular embodiment with reference to Figs.1 to 9. Fig.1 is a plan view illustrating an in-line type 4-cylinder engine E in a state in which a head cover has been removed. In a state mounted to a vehicle body, the direction of an arrow FR is front (on an intake side), and the direction of an arrow RR is rear (on an exhaust side). A head cover coupling surface 1 1 is formed around an upper surface of a cylinder head 1 to which a lower surface of the head cover is coupled. A timing chain 3 for transmitting the rotation of a crankshaft (not shown) to a valve operating device is accommodated in a timing chain chamber 2 which is defined on one side (a right side of a vehicle) of the engine to vertically extend through the head cover coupling surface 1 1 . A chain sprocket 5 is carried on an intermediate shaft 4 which is mounted in the cylinder head 1 to protrude into the timing chain chamber 2, and an upper end of the timing chain 3 is meshed with the chain sprocket 5. An intake cam shaft 6i and an exhaust cam shaft 6e are carried in parallel to each other in the cylinder head 1, and follower helical gears 7i and 7e provided at right ends of the intake and exhaust cam shafts 6i and 6e are meshed with a driving helical gear 8 carried on the intermediate shaft 4. Thus, the rotation of the crankshaft is transmitted through the timing chain 3, the chain sprocket 5, the intermediate shaft 4, the driving helical gear 8 and the follower helical gears 7i and 7e to the intake and exhaust cam shafts 6i and 6e to drive the intake and exhaust cam shafts 6i and 6e at a number of revolutions one half of that of the crankshaft. At this time, a smooth transmission of power from the crankshaft to the intake and exhaust cam shafts 6i and 6e is achieved by meshing of the driving helical gear 8 with the follower helical gears 7i and 7e, but an axial large thrust load is applied to both of the intake and exhaust cam shafts 6i and 6e. Five, #1, #2, #3, #4 and #5, lower cam shaft holders 9 1 , 9 2 , 9 3 , 9 4 and 9 5 are juxtaposed in sequence from the right side to the left side of the vehicle body on an upper surface of the cylinder head 1. The intake and exhaust cam shafts 6i and 6e are rotatably carried between the lower cam shaft holders 9 1 , 9 2 , 9 3 , 9 4 and 9 5 commonly fastened to the cylinder head 1 and an upper cam shaft holder assembly 10 by threadedly inserting a total of 20 bolts 11 passed through an assembly 10 of upper cam shaft holders integrally formed and the five lower cam shafts 9 1 , 9 2 , 9 3 , 9 4 and 9 5 into the upper surface of the cylinder head 1. The upper cam shaft holder assembly 10 includes five upper cam shaft holders 10 1 , 10 2 , 10 3 , 10 4 and 10 5 coupled to upper surfaces of the five lower cam shaft holders 9 1 , 9 2 , 9 3 , 9 4 and 9 5 , and four connecting portions 10 6 which integrally couple the five upper cam shaft holders 10 1 , 10 2 , 10 3 , 10 4 and 10 5 to one another. Provided on an upper surface of each of the connecting portion 10 6 are a spark plug guide 10 7 for mounting and removing a spark plug (not shown), reinforcing ribs 10 8 , 10 8 formed so as to intersect each other in an X-shape, and a plurality of oil return bores 10 10 for returning an oil accumulated on the upper surface of the connecting portion 10 6 downwards. A reinforcing rib 10 9 is provided on the upper surface of each of the upper cam shaft holders 10 1 , 10 2 , 10 3 , 10 4 and 10 5 to extend in a direction perpendicular to axes of the intake and exhaust cam shafts 6i and 6e. As can be seen from Figs.2 to 4, an intake port 15i and an exhaust port 15e are provided in the cylinder head 1 in correspondence to each of cylinders . Valve bores 16i, 16i; 16e, 16e are connected to the intake and exhaust ports 15i and 15e and opened and closed by a pair of intake valves 17i, 17i and a pair of exhaust valves 17e, 17e, respectively. The intake valves 17i, 17i and the exhaust valves 17e, 17e are biased in closing directions by valve springs 18i, 18i; 18e, 18e, respectively. An intake rocker shaft 19i and an exhaust rocker shaft 19e are supported on the five lower cam shaft holders 9 1 , 9 2 , 9 3 , 9 4 and 9 5 . A pair of intake rocker arms 20i, 20i are pivotally supported at one ends thereof on the intake rocker shaft 19i, with the other ends of the intake rocker arms 20i, 20i abutting against stem ends of the intake valves 17i, 17i. A pair of exhaust rocker arms 20e, 20e are pivotally supported at one ends thereof on the exhaust rocker shaft 19e, with the other ends of the exhaust rocker arms 20e, 20e abutting against stem ends of the exhaust valves 17e, 17e. Rollers 21i, 21i are provided at intermediate portions of the lower-speed intake rocker arms 20i, 20i and abut against lower-speed cams 22i, 22i provided on the intake cam shaft 6i. Rollers 21e, 21e are provided at intermediate portions of the lower-speed exhaust rocker arms 20e, 20e and abut against lower-speed cams 22e, 22e provided on the exhaust cam shaft 6e. An exhaust-side valve operating mechanism including the exhaust rocker shaft 19e is shown in Fig.4. As can be seen from Fig.4, a high-speed exhaust rocker arm 23e is pivotally supported on the exhaust rocker shaft 19e, so that it is sandwiched between the pair of lower-speed exhaust rocker arms 20e, 20e. The high-speed exhaust rocker arm 23e abuts against a high-speed cam 24e provided on the exhaust cam shaft 6e. The high-speed exhaust rocker arm 23e and the lower-speed exhaust rocker arms 20e, 20e are capable of being connected to and disconnected from each other by a variable valve timing/lifting mechanism 25. The structure of the variable valve timing/lifting mechanism 25 is know and is not described herein in detail. The structure of an intake-side valve operating mechanism is substantially the same as that of the above-described exhaust-side valve operating mechanism. Thus, during operation of the engine E at a high speed, the high-speed rocker arms 23i and 23e are coupled to the low-speed rocker arms 20i, 20i; 20e, 20e by the variable valve timing/lifting mechanism 25, and the intake valves 17i, 17i and the exhaust valves 17e, 17e are driven by profiles of the high-speed cams 24i and 24e. During operation of the engine E at a low speed, the high-speed rocker arms 23i and 23e are disengaged from the low-speed rocker arms 20i, 20i;20e, 20e by the variable valve timing/lifting mechanism 25, and the intake valves 17i, 17i and the exhaust valves 17e, 17e are driven by profiles of the low-speed cams 22i, 22i; 22e, 22e. As shown in Figs. 2, 4 and 5, first thrust limiting members 31i and 31e and second thrust limiting members 32i and 32e are mounted at left axial ends of the intake and exhaust cam shafts 6i and 6e. Each of the first thrust limiting members 31i and 31e is a disk-like member and integrally formed on each of the intake and exhaust cam shafts 6i and 6e. On the other hand, each of the second thrust limiting members 32i and 32e is a substantially disk-like member having three detected projections 33i, 33e spaced at distances of 90° from each other on an outer periphery thereof, respectively, and is fitted into a stepped portion 6 1 , 6 1 (see Figs.4 and 5) at an axial end of each of the intake and exhaust cam shafts 6i and 6e and fixed by a bolt 35, 35 in a state in which it has been positioned in a rotating direction by a positioning pin 34, 34. Fixed to the head cover 36 coupled to the upper surface of the cylinder head 1 by bolts 38, 38 are a TDC (a top dead center of a piston)sensor 37i for detecting the three detected projections 33i of the second thrust limiting member 32i on the side of the intake cam shaft 6i, and a TDC sensor 37e for detecting the three detected projections 33e of the second thrust limiting member 32e on the side of the exhaust cam shaft 6e. The TDC sensors 37i and 37e are disposed in radiate directions with respect to the cam shafts 6i and 6e, respectively, and in planes of rotation of the second thrust limiting members 32i and 32e in order to shorten the axial dimension of the engine E. As can be seen from Fig. 5, a bonnet 39 covering an upper portion of the engine E is inclined downwards toward the forward direction, so that the front side (intake side) is lower and the rear side (exhaust side) is higher. The interference of the TDC sensors 37i and 37e with the bonnet 39 can be avoided while suppressing the gap between the head cover 36 and the bonnet 39 to the minimum by supporting the TDC sensor 37i on the side of the intake cam shaft 6i substantially horizontally on the front surface of the head cover 36 and supporting the TDC sensor 37e on the side of the exhaust cam shaft 6e substantially vertically on the upper surface of a rear portion of the head cover 36. Thus, the passage of each of the three detected projections 33i, 33e of the second thrust limiting members 32i and 32e can be detected by the TDC sensors 37i and 37e, and TDC of the four cylinders can be detected based on a timing of the detection of such passage. The structure of the #5 lower cam shaft holder 9 5 disposed between the first thrust limiting members 31i and 31e and the second thrust limiting members 32i and 32e will be described below mainly with reference to Figs.6 to 9. Three upper cam shaft holder coupling surfaces 42 are formed on an upper surface of the #5 lower cam shaft holder 9 5 and separated from one another by a pair of semi-circular cam shaft support portions 41, 41 which support the cam shafts 6i and 6e, and two cylinder head coupling surfaces 43, 43 are formed on a lower surface of the #5 lower cam shaft holder 9 5 and separated from each other at a central point of such lower surface. Four bolt bores 44 are provided in the upper cam shaft holder coupling surfaces 42 and the cylinder head coupling surfaces 43 to extend through these surfaces 42 and 43, and the bolts 11 are passed through the bolt bores 44. Two rocker shaft-supporting boss portions 45i and 45e are projectingly provided on a right side (i.e. , a side on the side of the #4 lower rocker shaft holder 9 4 ) of the #5 lower cam shaft holder 9 5 , and the intake-side rocker arm 19i and the exhaust-side rocker arm 19e are supported in fitted states on the rocker shaft supporting boss portions 45i and 45e. A pair of protrusions 43 1 , 43 1 connected to the cylinder head coupling surfaces 43, 43 are formed by extension of the pair of rocker shaft supporting boss portions 45i and 45e to the cylinder head coupling surfaces 43, 43. A pair of protrusions 43 2 , 43 2 connected to the cylinder head coupling surfaces 43, 43 are integrally formed at a lower portion of a left side (i.e., a side on the opposite side from the #4 lower rocker shaft holder 9 4 ) of the #5 lower cam shaft holder 9 5 . First thrust load supporting surfaces 46, 46 are formed on the right side of the #5 lower cam shaft holder 9 5 to surround the cam shaft supporting portions 41, 41, and the first thrust limiting members 31i and 31e are in sliding contact with the first thrust load supporting surfaces 46, 46. Second thrust load supporting surfaces 47, 47 are formed on the left side of the #5 lower cam shaft holder 9 5 to surround the cam shaft supporting portions 41, 41, and the second thrust limiting members 32i and 32e are in sliding contact with the second thrust load supporting surfaces 47, 47. The #5 upper cam shaft holder 10 5 similarly has first and second thrust load supporting surfaces 48,48; 49,49 as shown in Figs. 3 and 5. As can be seen from Fig.3, reinforcing ribs 9 6 , 9 6 intersecting each other in an X-shape are formed on the right side of the #5 lower cam shaft holder 9 5 to connect the pair of cam shaft supporting portions 41, 41 and the pair of rocker shaft supporting boss portions 45i and 45e to each other. Reinforcing ribs 9 7 , 9 7 mirror-symmetrical with the reinforcing ribs 9 6 , 9 6 are also formed on the left side of the #5 lower cam shaft holder 9 5 (see Fig.5). Thus, by fastening the reinforcing ribs 9 6 , 9 6 , 9 7 , 9 7 at points having a higher rigidity in the vicinity of their ends with the bolts 11, a large fastening force can be applied to the bolts 11 to further enhance the rigidity of the #5 upper and lower cam shaft holders 10 5 and 9 5 . Moreover, the rigidity of the thrust load supporting surfaces 46, 46; 47, 47; 48, 48; 49, 49 and the rocker shaft supporting boss portions 45i and 45e can be also enhanced. When the intake and exhaust cam shafts 6i and 6e have received a thrust load due to the meshing of the driving helical gear 8 with the follower helical gears 7i and 7e, the thrust load is supported to limit the axial movements of the cam shafts 6i and 6e by the abutment of the first thrust limiting members 31i and 31e against the first thrust load supporting surfaces 46, 46; 48, 48 (see Fig.3) formed on the right sides of the #5 lower cam shaft holder 9 5 and the #5 upper cam shaft holder 10 5 , or by the abutment of the second thrust limiting members 32i and 32e against the second thrust load supporting surfaces 47, 47; 49, 49 (see Fig.5) formed on the left sides of the #5 lower cam shaft holder 9 5 and the #5 upper cam shaft holder 10 5 . In this case, since the detected projections 33i and 33e adapted to be detected by the TDC sensors 37i and 37e are formed on the outer peripheries of the second thrust limiting members 32i and 32e, the conventional need for provision of a special rotatable plate having a detected projection is eliminated, leading to a reduction in number of parts. Moreover, since the detected projections 33i and 33e are provided on the second thrust limiting members 32i and 32e which limit the axial movements of the cam shafts 6i and 6e, the stable rotation of the detected projections 33i and 33e can be ensured, and the variation in axial position of the detected projections 33i and 33e caused due to an influence of the thermal expansion of the cam shafts 6i and 6e can be suppressed to the minimum to prevent a reduction in detecting accuracy of the TDC sensors 37i and 37e and to enhance the degree of freedom of the layout of the TDC sensors 37i and 37e. Further, since the thrust load supporting surfaces 46, 46, 47, 47 are formed adjacent the cam shaft supporting portions 41, 41 of the #5 lower cam shaft holder 9 5 , the variation in rotation of the detected projections 33i and 33e can be further effectively prevented to enhance the detecting accuracy of the TDC sensors 37i and 37e. When a thrust load from the cam shafts 6i and 6e has been applied to the #5 lower and upper cam shaft holders 9 5 and 10 5 , the axial movement of the #5 lower cam shaft holder 9 5 can be prevented to further reliably support the cam shafts 6i and 6e to enhance the detecting accuracy of the TDC sensors 37i and 37e by the fact that the protrusions 43 1 , 43 1 ; 43 2 , 43 2 projecting axially of the cam shafts 6i and 6e are formed on the cylinder head coupling surface 43 of the #5 lower cam shaft holder 9 5 . Moreover, since the protrusions 43 1 , 43 1 are connected to the rocker shaft supporting boss portions 45i and 45e, the support rigidity of the rocker shaft 19i and 19e is also enhanced. Further, since the #1 to #5 upper cam shaft holders 10 1 to 10 5 are integrally coupled to one another by the connecting portions 10 6 , the thrust load applied to the upper cam shaft holder 10 5 can be dispersed to the #1 to #4 lower cam holders 9 1 to 9 4 through the #1 to #4 upper cam holders 10 1 to 10 4 to further effectively prevent the axial movement of the #5 upper cam shaft holder 10 5 and the #5 lower cam shaft holder 9 5 . Yet further, since the detected projections 33i and 33e are provided on those thrust limiting members 32i and 32e of the first and second thrust limiting members 31i, 31e, 32i and 32e sandwiching the #5 lower and upper cam shaft holders 9 5 and 10 5 , which are located at the axial ends of the cam shafts 6i and 6e and above which there is not the connecting portion 10 6 of the upper cam shaft holder assembly 10, the detected projections 33i and 33e cannot interfere with the connecting portions 10 6 , even if the height of the connecting portion 10 6 from the upper surface of the #5 lower cam shaft holder 9 5 is decreased to reduce the vertical dimension of the engine E. Thus, the size of the second thrust limiting members 32i and 32e having the detected projections 33i and 33e can be increased without increasing the size of the engine E to enhance the detecting accuracy. Although the presently preferred embodiment of the present invention has been described in detail, it will be understood that the present invention is not limited to the above-described embodiment, and that various modifications may be made thereto without departing from the spirit and scope of the invention defined in the claims appended hereinbelow. For example, the engine rotation detecting system according to the present invention is not limited to the use for the detection of the rotated position of the phase of the cam shafts 6i and 6e described above, but is also applicable to the detection of the rotated position, the rotational angle and the number of rotations of the rotary shaft (the crankshaft or the like) of the engine other than the cam shafts 6i and 6e. Although the detected projections 33i, 32e are provided on the thrust limiting members 32i, 32e formed separate from the cam shafts 6i and 6e in the embodiment, they may be provided on thrust limiting members formed integral with the cam shaft 6i and 6e. A first thrust limiting member and a second thrust limiting member are provided on a cam shaft rotatably carried between a lower cam shaft holder and an upper cam shaft holder which are fixed to an upper surface of a cylinder head 1, so that the first and second thrust limiting members and abut against the cam shaft holders 9 5 and 10 5 . The second thrust limiting member has a plurality of detected projections provided around of an outer periphery thereof, so that the detected projections are detected by a TDC sensor 37 mounted to a head cover of the engine. Thus, the rotated position (phase), the angle of rotation and the number of rotations of an rotary shaft of an engine such as a cam shaft 6e and a crankshaft can be detected with good accuracy in a structure including a decreased number of parts, and the axial dimension of the rotary shaft of the engine can be reduced.

Claims: An engine-rotation detecting system comprising a detected portion (33i,33e) provided on a cam shaft (6i,6e) supported between an upper cam shaft holder (10 5 ) and a lower cam shaft holder (9 5 ) mounted on a cylinder head (1) of an engine (E), and a sensor (37i,37e) for detecting a position of said detected portion (33i,33e), wherein said detected portion (33i,33e) is provided on a thrust limiting member (32i,32e) mounted on said cam shaft (6i,6e), said thrust limiting member being adapted to limit an axial movement of said cam shaft (6i,6e) and being further adapted to suppress an axial displacement of said detected portion (33i,33e), said lower cam shaft holder (9 6 ) being formed with an abutment portion (46,47) against which said thrust limiting member (32i,32e) abuts, and said lower cam shaft holder (9 6 ) having a cylinder head coupling surface (43) which is formed with a protrusion (43 1 ,43 2 ) projecting from said abutment portion (46, 47) in a direction axially of said cam shaft (6i,6e). An engine-rotation detecting system according to claim 1, wherein said cam shaft (6i,6e) is supported between a plurality of upper cam shaft holders (10 1 ,10 2 ,10 3 ,10 4 ,10 5 ) and a plurality of lower cam shaft holders (9 1 ,9 2 ,9 3 ,9 4 ,9 5 ) mounted on a cylinder head (1), said upper cam shaft holders(10 1 ,10 2 ,10 3 ,10 4 ,10 5 ) being connected to one another by connecting portions (10 6 ) extending in an axial direction of said cam shaft (6i,6e), said engine (E) including a second thrust limiting member (32i,32e) on said cam shaft (6i,6e) and the two thrust limiting members (31 i,31 e,32i,32e) are disposed on opposite sides of an end one (9 5 ) of said lower cam shaft holders (9 1 ,9 2 ,9 3 ,9 4 ,9 5 ) relative to said axial direction, said detected portion (33i,33e) being provided on the outer periphery of an outermost one (32i,32e) of said two thrust limiting members (31 i,31 e,32i,32e). An engine-rotation detecting system according to claim 2, wherein said outermost one (32i,32e) of said two thrust limiting members (31i,31e,32i,32e) is located adjacent to said end one (9 5 ) of said lower cam shaft holders (9 1 ,9 2 ,9 3 ,9 4 ,9 5 ). An engine-rotation detecting system according to claim 1, wherein said upper (10 5 ) and said lower cam shaft holders (9 5 ) together form a cam shaft holder (9 5 ,10 5 ), said engine (E) including a second thrust limiting member (32i,32e) on said cam shaft (6i,6e), and the two thrust limiting members (31i,31 e,32i,32e) are disposed on opposite sides of the cam shaft holder (9 5 ,10 5 ), which is provided near an end of said cam shaft (6i,6e) in its axial direction, said detected portion being provided on one of said two thrust limiting members (31 i,31 e,32i,32e) which is located adjacent said end of the cam shaft (6i,6e), and said sensor (37i,37e) being mounted at a location opposed to said detected portion (33i,33e). An engine-rotation detecting system according to one of claims 2 to 4, wherein one (31 i,31 e) of said two thrust limiting members (31 i,31 e, 32i,32e) which is located axially inward of said end of the cam shaft (6i,6e) is formed integrally with said cam shaft (6i,6e), and the other of said thrust limiting members (32i,32e) is formed separately from said cam shaft (6i,6e). An engine-rotation detecting system according to one of claims 2 to 5, wherein an opposite end of said cam shaft (6i,6e) has a driving mechanism (7i,7e) for said cam shaft (6i,6e) connected thereto. An engine-rotation detecting system according to one of the preceeding claims, wherein said thrust limiting member (32i,32e) having said detected portion (33i,33e) provided thereon is non-rotatably fixed to the axial end of the cam shaft (6i,6e) by a bolt (35) and a positioning pin (34). An engine-rotation detecting system according to one of the preceeding claims, wherein said protrusion (43 1 ,43 2 ) comprises a rocker shaft supporting boss portion (45i,45e) of the lower cam shaft holder (9 5 ) extended downwards to said cylinder head coupling surface (43). An engine rotation detecting system according to one of the preceeding claims 2 to 8, wherein each said connecting portion (10 6 ) has a plug guide (10 7 ) formed at its central portion for attaching and detaching a spark plug. An engine-rotation detecting system according to claim 9, further including ribs (10 8 ) formed to extend radially from said plug guides (10 7 ) toward cam holder fastening portions of said upper cam shaft holders (10 1 ,10 2 ,10 3 ,10 4 ,10 5 ). An engine-rotation detecting system according to one of the preceeding claims, wherein said sensor (37i,37e) is mounted to a head cover (36) of the engine (E). An engine-rotation detecting system according to claim 1, wherein said sensor (37i,37e) is provided for each of two cam shafts (6i,6e) of said engine (E) and said detected portion (33i,33e) is provided on each of the thrust limiting members (32i,32e), said thrust limiting members being adapted to limit the axial movement of said two cam shafts (6i,6e) and being further adapted to suppress an axial displacement of said detected portions (33i,33e), and wherein each of said two cam shafts (6i,6e) has a cam shaft-driving mechanism (7i,7e) provided axially at one end thereof, and said detected portion (33i,33e) provided at the other end thereof. An engine-rotation detecting system according to any one of the preceding claims, wherein said detected portion (33i,33e) projects in a radial direction from an outer periphery of the thrust limiting member (32i,32e).

Inventors: FUJII NORIAKI, KOSUGE MAMORU, SATO TOSHIYUKI, FUJII, NORIAKI, KOSUGE, MAMORU, SATO, TOSHIYUKI
Applicants: HONDA MOTOR CO LTD, HONDA GIKEN KOGYO KABUSHIKI KAISHA
Application year: 1997
Main classification: F02P7
IPC codes: F02D35, F01L1, F02P7