Abstract:
A four-cycle engine including a magnetic detection sensor mounted on a non-magnetic cam shaft pulley which is rotated in operative association with a crank pulley for detecting a plurality of detecting portions formed on the magnetic detection member by coils mounted in the cylinder head. The magnetic detection member is integrally formed with the plurality of detection portions for different uses such that distances from the center of rotation of the cam shaft pulley to the plurality of detection portions are different, and wherein the coils are separately mounted in correspondence to the detection portions. Thus, it is possible not only to take out timing signals for different uses from a single cam shaft pulley, but also to eliminate interference between the discrete coils.

Description:
This is a division of application Ser. No. 08/127,553 filed Sep. 28, 1993, now U.S. Pat. No. 5,438,963. 
    
    
     BACKGROUND OF THE INVENTION 
     1. Field of the Invention 
     The present invention relates to a 4-cycle engine. 
     2. Description of the Prior Art 
     In recent years, a 4-cycle engine with two cylinder axes disposed in a V-shape has been proposed, which includes an electronically controlled type fuel injection system (for example, see Japanese Utility Model Application Laid-open No.127779/90). In this engine, a substantially Y-shaped distributing type intake pipe is disposed inside a V-bank, and a single injector is disposed upstream from an junction of the intake pipe, so as to supply a fuel. 
     In the above prior art engine, no special consideration is taken into account for reducing the size of an intake device upstream from the injector and thus, there is a problem that an engine becomes large due to such intake device. 
     In general, a 4-cycle marine engine is used in an environment where it is liable to be rusted easily than other engine for a vehicle and thus, many parts of aluminum alloy and stainless steel are employed. For example, a cam pulley forming a portion of a valve-operating system is made of aluminum alloy. Therefore, in order to take out a spark timing pulse from the rotation of the cam pulley, a metal piece of a magnetic material is secured to an inner peripheral surface of a rim portion of the cam pulley, and a picking-up coil is disposed so that it is opposed to the metal piece. 
     With the above construction, however, only one magnetic material is attached to one cam pulley. For example, in a 4-cycle engine including an electronically controlled type fuel injection system, it is difficult to take out a timing pulse for injection of a fuel in addition to the above-described spark timing pulse. 
     SUMMARY OF THE INVENTION 
     Accordingly, it is a first object of the present invention to reduce a size of the intake device of the 4-cycle engine. 
     To achieve the above first object, according to the present invention, there is provided a 4-cycle engine comprising a cylinder block having a substantially horizontal cylinder, a cylinder head coupled to the cylinder block, and a combustion chamber formed in the cylinder head, wherein the engine further includes an intake passage formed in the cylinder head to extend from the combustion chamber and opened into an outer wall of the cylinder head, an intake gas introducing means disposed sideways of the cylinder head to communicate with the intake passage, and a throttle body disposed below the intake gas introducing means to communicate with the intake gas introducing means. 
     With the above construction, the intake gas introducing means and the throttle body are mounted in a vertically superposition as viewed in a plane to reduce the amount of projection sideways of the engine, thereby reducing a size of the engine. 
     It is an object of the present invention to properly take out a plurality of types of timing pulses in 4-cycle engine. 
     To achieve the above second object, according to the present invention, there is provided a 4-cycle engine comprising a magnetic detection member mounted on a cam pulley of a non-magnetic material which is rotated in operative association with a crank pulley, for detecting a plurality of detection portions formed on the detection magnetic member by coils mounted in a cylinder head, wherein the magnetic detection member is integrally formed with the plurality of detection portions for different uses in such a manner that distances from the center of rotation of the cam pulley to the plurality of detection portions are different, and wherein the coils are separately mounted in correspondence to the detection portions. 
     With the above construction, it is possible not only to take out timing signals for different uses from the single cam pulley, but also to eliminate an influence between the discrete coils to prevent a mis-detection. 
    
    
     The above and other objects, features and advantages of the invention will become apparent from the following description of preferred embodiments, taken in conjunction with the accompanying drawings. 
     BRIEF DESCRIPTION OF THE DRAWINGS 
     FIGS. 1 to 12 illustrate a first embodiment of the present invention, wherein 
     FIG. 1 is a side view of the entire outboard motor; 
     FIG. 2 is a sectional view taken along a line 2--2 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. 3; 
     FIG. 5 is a sectional view taken along a line 5--5 in FIG. 4; 
     FIG. 6 is a sectional view taken along a line 6--6 in FIG. 4; 
     FIG. 7 is a sectional view of a right cam pulley; 
     FIG. 8 is a view taken along a line 8--8 in FIG. 7; 
     FIG. 9 is a sectional view of a left cam pulley; 
     FIG. 10 is a view taken in a direction indicated by an arrow 10 in FIG. 9; 
     FIG. 11 is a block diagram of a control system; and 
     FIG. 12 is an enlarged view of an essential portion shown in FIG. 4, illustrating an intake port; and 
     FIGS. 13 and 14 illustrate a second embodiment of the present invention, wherein 
     FIG. 13 is a sectional view of a right cam pulley; and 
     FIG. 14 is a view taken along a line 14--14 in FIG. 13. 
    
    
     DESCRIPTION OF THE PREFERRED EMBODIMENTS 
     A first embodiment of the present invention will now be described in connection with FIGS. 1 to 12. 
     Referring to FIGS. 1 to 4, an outboard motor O includes a mounting member 3 coupled to an upper portion of an extension case 1 through a plurality of bolts 2. A V-type 4-cylinder and 4-cycle engine E is supported on an upper surface of the mounting member 3 through a plurality of bolts 4. An undercase 5 with its upper surface opened is coupled to the mounting member 3 through a plurality of bolts 6, and an engine cover 7 is detachably mounted on an upper portion of the undercase 5. The engine cover 7 is coupled to an upper edge of the undercase 5 through a sealing member 8 provided at a lower edge of the engine cover 7 and is fixed by a pair of front and rear clips 9 and 10. The engine E is accommodated within an engine room 11 defined inside the engine cover 7 in such a manner tha a crankshaft 12 is disposed in a vertical attitude and a pair of banks 13 L  and 13 R  are spreaded rearward. 
     A driving shaft 14 is connected in series to a lower end of the crankshaft 12 of the engine E, and extends downwardly within the extension case 1. A lower end of the driving shaft 14 is connected to a propeller shaft 18 having a propeller 17 at a rear end thereof, through a bevel gear mechanism 16 provided within a gear case 15. A shifting member 19 is connected at its lower end to a front portion of the bevel gear mechanism 16 for changing-over the direction of rotation of the propeller shaft 18. 
     A swivel shaft 22 is fixed between an upper mount 20 provided in the mounting member 3 and a lower mount 21 provided in the extension case 1. A swivel case 23 for rotatably supporting the swivel shaft 22 is vertically swingably supported through a tilt shaft 25 on a stern bracket 24 mounted at a rear end of a hull S. 
     The engine E includes a cylinder block 26 which forms a V-shape as viewed in a plane, a crankcase 27 which cooperates with the cylinder block 26 to define a crank chamber, a pair of cylinder heads 28, 28 coupled to a pair of deck surfaces of the cylinder block 26, and head covers 29, 29 coupled to the cylinder heads 28, 28. The left and right head covers 29, 29 are disposed in proximity to an inner surface of the engine cover 7 and thus, an interior of the engine room 11 is divided into a front space 30 located at a front portion of the engine E and a rear space 31 located at a rear portion of the engine E. Accommodated in the front space 30 are, in addition to a control device 32 for an electronically controlled type fuel injection system and the like and a control device 33 for an spark plug, engine auxiliaries such as a starter motor 93 having a pinion 92 meshed with a gear 911 formed around an outer periphery of a flywheel 91 provided at an upper end of the crankshaft 12, an oil filter 94, and an oil pump 95 provided at a lower end of the crankshaft 12. A fuel supply system and an intake system are accommodated in the rear space 31. 
     Referring also to FIGS. 5 and 6, each of the banks 13 L  and 13 R  of the engine E includes two upper and lower cylinders 34 having a horizontal axis. Four pistons 35 each slidably received in corresponding one of the cylinders 34 are connected to the crankshaft 12 through connecting rods 36. Four combustion chambers 37 are defined in correspondence to tops of the cylinders 34, respectively. Each of the four combustion chambers 37 is provided with two intake valves 39, 39 connected to a bifurcated intake ports 38 defined in the cylinder heads 28, 28, respectively; a single exhaust valve 41 connected to an exhaust port 40 a  defined in the cylinder head 28, 28 and to an exhaust port 40 b  defined in the cylinder block 28; and a single plug 42. 
     Air is drawn into each of the intake ports 38 through an intake silencer 43, an elbow 60, a throttle body 44 and a surge tank 45 which are disposed in the rear space 31 of the engine room 11, and a fuel injected from an injector 46 provided in each of the intake ports 38 is mixed with this air. A pair of exhaust passages 47, 47 formed vertically in the cylinder block 26 are connected to the two exhaust ports 40a and 40b of each of the left and right banks 13 L  and 13 R , and are also connected to a pair of exhaust pipes 49, 49 extending downwardly along opposite sides of an oil pan mounted on a lower surface of the mounting member 3. An exhaust gas discharged from the exhaust pipes 49, 49 is passed through insides of the extension case 1 and the gear case 15 and discharged through a boss of the propeller 17 into water. 
     Water jackets 50 a , 50 b , 50 c , through which cooling water is circulated, are defined in the cylinder heads 28, 28 and the cylinder block 26 which have the exhaust ports 40 a , 40 b  and the exhaust passages 47, 47 defined therein, respectively. More specifically, the water jacket 50 a  is defined in correspondence to the exhaust port 40 a  in the cylinder head 28; the water jacket 50b is defined in correspondence to the exhaust port 40 b  in the cylinder block 26, and the water jacket 50 c  is defined in correspondence to the exhaust passage 47 in the cylinder block 26, and the cooling water flows from the water jacket 50 c  via the water jacket 50 b  into the water jacket 50 a . 
     Temperature sensors 51, 51 for detecting the temperature of walls of the cylinder heads 28, 28 are mounted to the water jacket 50 a  covering outer sides of the exhaust ports 40 a  corresponding to the upper cylinders 34, 34 in each of the banks 13 L  and 13 R , respectively. Anode metals 52, 52 are mounted to the water jackets 50 c , 50 c  in the cylinder block 26, respectively, so that the anode metals are positively corroded to prevent the corrosion of a body of the engine E. 
     Because the temperature sensors 51, 51 are mounted in the cylinder heads 28, 28, they can be disposed without dependence upon the size and shape of the cylinder block 26. Also, because the temperature sensors 51, 51 are mounted on the outer surfaces of the cylinder head 28, 28, i.e., on the outer surface of the left and right banks 13 L  and 13 R , the pair of temperature sensors 51, 51 can be disposed so that they do not interfere with each other. Moreover, since the temperature sensors 51, 51 are disposed at locations near the combustion chambers 37, 37, it is possible to improve the accuracy of detection. 
     The temperature sensors 51, 51 detect the temperature of the engine in an analogue manner, but an output therefrom is mathematically processed in the above-described control device 32. If the temperature rises and exceeds a predetermined value, a signal indicative of an overheat of the engine is outputted. This eliminates the need for an overheat switch which has been conventionally required, thereby enabling a reduction in number of parts. 
     The cylinder head 28 of the right bank 13 R  is provided with an oil separating chamber 53 into which a blow-by gas leaked out of the combustion chambers 37 into the crank chamber is introduced. The blow-by gas resulting from the separation of an oil in the oil separating chamber is introduced through a breather passage 54 into the intake silencer 43. 
     A crank pulley 55 is mounted at an upper end of the crankshaft 12 projecting from an upper surface of the cylinder block 26, and cam pulleys 57 L  and 57 R  are mounted on a pair of cam shafts 56, 56 projecting on upper surfaces of the pair of cylinder heads 28, 28. The crank pulley 55 and cam pulleys 57 L  and 57 R  are interconnected through an endless belt 59 tensioned by a tension pulley 58. 
     The structure of the fuel supply system in the engine E will be described below. 
     A main tank of a large capacity carried in the hull is connected to a connector 62 in a front portion of the engine room 11 through a fuel hose (not shown), and is connected therefrom to a subsidiary tank 68 through a fuel piping P 1 , a filter 63, a fuel piping P 2 , a feed pump 64 driven by the left cam shaft 56 and a fuel piping P 3 . A fuel supplied from the main tank into the subsidiary tank 68 by the feed pump 64 is fed from an injection pump 70 accommodated in the subsidiary tank 68 through a fuel piping P 4 , a filter 83 and a fuel piping P 5  into a fuel passage 84 provided in the right bank 13R. And a portion of such fuel is supplied to the two injectors 46, 46 in the right bank 13R. The remainder of the fuel is supplied through a fuel piping P 6  into a fuel passage 85 provided in the left bank 13 L  and into the two injectors 46, 46 in the left bank 13 L . A surplus fuel is returned through a regulator 88 and a fuel piping P 7  to the subsidiary tank 68. 
     The structure of the intake system in the engine E will be described below. 
     The intake system is accommodated in the rear space 31 of the engine room 11, and is composed of the intake silencer 43, the elbow 60, the throttle body 44, the surge tank 45 and the intake ports 38. The intake silencer 43 is disposed at a left and lower portion of the rear space 31 of the engine room 11 and fixed to the head cover 28 in the left bank 13 L  by means such as bolting. The intake silencer 43 has a plurality of air inlets 43 1  in its rear surface. The elbow 60 connected to a right surface of the intake silencer 43 is curved through 90° to have a horizontal inlet-side axis and a vertical outlet-side axis, and the throttle body 44 is connected to an upper end of the elbow 60. A throttle valve 44 1  is accommodated within the throttle body 44 and is driven for opening and closing through Bowden wire. An air flow meter 65 and a downstream portion of the throttle value 44 1  are connected to each other through a tube 66. The intake silencer 43, the elbow 60 and the throttle body 44 are accommodated in a rear portion of the engine room 11 which projects rearwardly from a rear end of the extension case 1, so that the rear space 31 of the engine room 11 is effectively utilized. 
     A surge tank 45 having a vertically extending axis is connected at its lower end to an upper end of the throttle body 44, and is provided at an upper portion thereof with an intake gas temperature sensor 67. The surge tank 45 has a pair of left and right flanges 45 1 , 45 1  fixed to a rear face of the cylinder block 26 by a plurality of bolts 86. The fuel passages 84 and 85 and the two injectors 46 are fixed to each of the flanges 45 1  by a plurality of bolts 87. The surge tank 45 and the throttle body connected to the lower portion of the surge tank 45 are accommodated in a space defined between the left and right banks 13 L  and 13 R  of the engine E and thus, a waste space between both the banks 13 L  and 13 R  is effectively utilized. 
     The subsidiary tank 68 and the intake silencer 43 are disposed outside the space defined between the left and right banks 13 L  and 13 R  of the engine E. More specifically, the subsidiary tank 68 fixed to the throttle body 44 by bolting or the like is disposed on the right side of a longitudinally center line of the engine E, while the intake silencer 43 is disposed on the left side of such center line. Thus, the subsidiary tank 68 and the intake silencer 43 can be disposed with a good balance in the rear space 31 of the engine room 11. Moreover, the large components such as the intake silencer 43, the subsidiary tank 68 and the like are integrally formed with the engine E and therefore, it is possible to easily assemble the engine E to the outboard motor O. 
     A pair of upper and lower openings 45 2 , 45 2  formed in a right surface of the surge tank 45 are connected to the intake ports 38, 38 extending to the pair of upper and lower combustion chambers 37, 37 defined in the cylinder head 28 of the right bank 13 R , respectively. And a pair of upper and lower openings 45 2 , 45 2  formed in a left surface of the surge tank 45 are connected to the intake ports 38, 38 extending to the pair of upper and lower combustion chambers 37, 37 defined in the cylinder head 28 of the left bank 13 R , respectively. 
     As can be seen from FIG. 12, each intake port 38 is branched into an upper port portion 38 1  and a lower port portion 38 2  which are connected to two intake openings 69 1  and 60 2  in each combustion chamber 37. A junction 38 3  between the upper and lower port portions 38 1  and 38 2  is displaced upwardly by a distance α from a straight line L extending horizontally through a central portion of a line connecting centers of the pair of intake openings 69 1  and 69 2 . And a nozzle 46 1  of the injector 46 is disposed on a line L&#39; extending horizontally through the junction 38 3 . 
     Air drawn through the air inlet 43 1  in the intake silencer 43 flows from the intake silencer 43 through the elbow 60 into the throttle body 44, and passes through the throttle valve 44 1  accommodated in the throttle body 44 into the surge tank 45. The air in the surge tank 45 is distributed through the four openings 45 2  into the four intake ports 38, where the air is mixed with the fuel injected from the injectors 46, and then, the mixed gas is drawn into the combustion chamber 37 through the two intake valves 39, 39 provided in each of the cylinders 34. 
     Because the intake port 38 is branched into the upper and lower port portions 38 1  and 38 2 , if the flow rate of the air-fuel mixture within the intake port 38 is reduced during a low speed operation of the engine, the fuel component tends to stay on a bottom wall of the intake port 38, i.e., a bottom wall of the lower port portion 38 2 . If the throttle valve 44 1  is opened from this condition, it causes a problem that the flow rate of the air-fuel mixture passing through the intake port 38 is rapidly increased and hence, the staying fuel component is drawn quickly into the lower intake opening 69 2  connected to the lower port portion 38 2 , resulting in an over-rich. 
     However, since the junction 38 3  between the upper and lower port portions 38 1  and 38 2  is displaced upwardly by the distance α as shown in FIG. 12, the bottom wall of the lower port portion 38 2  is steeply inclined downwardly toward the lower intake openings 69 2 . This ensures that the fuel component cannot stay on the bottom wall of the lower port portion 38 2 , thereby overcoming the above-described problem arisen when the throttle valve 44 1  is opened. Moreover, since the nozzle 46 1  of the injector 46 is disposed at the same level as the junction 38 3  of the intake port 38, the fuel can be distributed equally into the upper and lower port portions 38 1  and 38 2 . 
     The structure of a timing pulse detecting device will now be described in detail. 
     As can be seen from FIG. 2, a driving force of the crank pulley 55 mounted on the crankshaft 12 is transmitted through the endless belt 59 to the cam pulley 57 R  mounted on the cam shaft 56 in the right bank 13 R  and the cam pulley 57 L  mounted on the cam shaft 56 in the left bank 13 L . A magnetic detection member 71 made of metal plate obtained as a result of a rust-preventing treatment is secured to a lower surface of the right cam pulley 57 R , and a single cylinder-discriminating coil 72 and two spark-triggering coil 73 and 74 are supported on the upper surface of the cylinder head 28, so that these elements 72 to 74 are opposed to the magnetic detection member 71. A magnetic detection member 75 made of metal plate obtained as a result of a rust-preventing treatment is secured to an upper surface of the left cam pulley 57 L , and a single top dead center discriminating coil 76 is supported on the upper surface of the cylinder head 28, so that it is opposed to the magnetic detection member 75. 
     FIGS. 7 and 8 illustrate the right cam pulley 57 R , which is made of aluminum which is a non-magnetic material. The right cam pulley 57 R  includes a boss portion 57 1  fixed to an upper end of the cam shaft 56, a plate-like portion 57 2  extending radially from the boss portion 57 1 , and a toothed portion 57 3  formed around an outer periphery of the plate-like portion 57 2 . The cam pulley 57 R  is provided with the plate-like portion 57 2  directed downwardly such that the plate-like portion 57 2  is opposed to the cylinder head 28. The magnetic detection member 71 is secured to a lower surface of the plate-like portion 57 2  by a plurality of rivets 78. 
     The magnetic detection member 71 has two detection portion 71 1  and 71 2  formed around an outer periphery thereof in a downwardly bent manner at different phases spaced from each other through 180°, and a single detection portion 71 3  cut and risen downwardly at an inner location than the detection portions 71 1  and 71 2  and at a phase different from one of the detection portion 71 1  through 60°. The two spark-triggering coils 73 and 74 are mounted at different phases spaced apart from each other through 90°, so that they are opposed, from the outside, to the two detection portions 71 1  and 71 2  located at radially outer positions. In addition, the cylinder-discriminating coil 72 is mounted, so that it is opposed, from the below, to single detection portion 71 3  located at a radially inner position. 
     FIGS. 9 and 10 illustrate the left cam pulley 57 L  which is a member having the same shape as the right cam pulley 57 R  and includes a boss portion 57 1 , a plate-like portion 57 2  and a toothed portion 57 3 . However, the left cam pulley 57 L  is mounted, such that the plate-like portion 57 2  thereof is directed upwardly, i.e., the left cam pulley 57 L  is turned inside out from the right cam pulley 57 R . This ensures that the left and right cam pulley 57 L  and 57 R  can be produced as identical parts, thereby reducing the producing cost. The magnetic detection member 75 is secured to an upper surface of the plate-like portion 57 2  by a plurality of rivets 78. 
     The magnetic detection member 75 has four detection portions 75 1  to 75 4  formed around an outer periphery thereof at different phases spaced from one another through 90° in an upwardly bent manner. The top dead center discriminating coil 76 is mounted such that it is opposed to these four detection portions 75 1  to 75 4  from the outside. 
     As shown in FIG. 11, a timing pulse from the top dead center discriminating coil 76 and a timing pulse from the cylinder-discriminating coil 72 are inputted, as input signals, into the control device 32 for the electronically controlled type fuel injection system, so that the timing of the injection of the fuel from the four injectors 46 is controlled in response to these timing pulses. Timing pulses from the two spark-triggering coils 73 and 74 are inputted, as an input signal, into the control device 33 for the spark plugs, so that the timing of spark of the four spark plugs is controlled in response to these timing pulses. 
     The operation of the embodiment of the present invention having the above-described construction will be described below. 
     When the crankshaft 12 is rotated by the operation of the engine E, the pair of cam pulleys 57 L  and 57 R  to which the driving force has been transmitted through the crank pulley 55 and the endless belt 59 are rotated at one half number of revolutions of that of the crankshaft 12. When the magnetic detection member 71 is rotated along with the right cam pulley 57 R , the two detection portions 71 1  and 71 2  formed at the radially outer positions on the magnetic detection member 71 pass through the vicinity of the two spark-triggering coils 73 and 74, thereby to output a timing pulse for the triggering of spark. In addition, if the single detection portion 71 3  formed at the radially inner position on the magnetic detection member 71 passes through the vicinity of the cylinder discriminating coil 72, a timing pulse for the discrimination of cylinder is also outputted. Likewise, if the magnetic detection member 75 is rotated along with the left cam pulley 57 L , the four detection portion 75 1  to 75 4  formed on the magnetic detection member 75 pass through the vicinity of the top dead center discriminating coil 76, thereby to output a timing pulse for discrimination of top dead center. 
     Since the detection portions 71 1  and 71 2  for triggering of spark and the detection portion 71 3  for discrimination of cylinder are integrally formed on the magnetic detection member 71 of the right cam pulley 57 R , since and the spark-triggering coils 73 and 74 and the cylinder-discriminating coil 72 are mounted in correspondence to these detection portions 71 1 , 71 2  and 71 3 , two kinds of timing pulses can be taken from the one cam pulley 57 R . At this time, an influence of the coils 72, 73 and 74 on one another is eliminated to prevent a mis-detection, because the spark-triggering detection portions 71 1  and 71 2  and the cylinder-discriminating portion 71 3  are formed in a radially displaced relation, and the two spark-triggering coils 73 and 74 and the single cylinder-discriminating coil 72 are displaced circumferentially. In addition, it is possible to reliably prevent the mis-detection of the cylinder discriminating coil 72, because the magnetic detection member 71 located above the inner cylinder-discriminating coil 72 is circumferentially continuous, excluding the detection portion 71 3 . 
     As can be seen from FIG. 4, the upper surface of the right bank 13 R  of the V-type multi-cylinder engine E is formed at a slightly lower level than the upper surface of the left bank 13 L , and the cam pulleys 57 L  and 57 R  disposed at the upper portions of the banks 13 L  and 13 R  are at the same level as each other. Therefore, a gap between the upper surface of the right bank 13 R  and the lower surface of the cam pulley 57 R  is larger than a gap between the upper surface of the left bank 13 L  and the lower surface of the cam pulley 57 L . Thereupon, by providing the magnetic detection member 71 on the lower surface of the right cam pulley 57 R  and by providing the detection magnetic member 75 on the upper surface of the left cam pulley 57 L , the gaps can effectively be utilized to suppress the height of the engine E to a low level. 
     FIGS. 13 and 14 illustrate a second embodiment of a magnetic detection member 71 mounted on the lower surface of the right cam pulley 57 R . 
     The magnetic detection member 71 of the second embodiment is divided into two parts, i.e., into an outer magnetic detection member 71 o  and an inner magnetic detection member 71 i , both of which are secured to the lower surface of the cam pulley 57 R  by rivets 78. The outer magnetic detection member 71 o  is formed with two detection portions 71 1  and 71 2 , while the inner magnetic detection member 71 i  is formed with a single detection portion 71 3 . 
     In this second embodiment, since the magnetic detection member 71 is not located above the inner cylinder-discriminating coil 72, excluding the detection portion 71 3 , it is possible to reliably prevent the mis-detection of such inner cylinder-discriminating coil 72.