TW575716B - Engine starting apparatus - Google Patents

Engine starting apparatus Download PDF

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Publication number
TW575716B
TW575716B TW91107591A TW91107591A TW575716B TW 575716 B TW575716 B TW 575716B TW 91107591 A TW91107591 A TW 91107591A TW 91107591 A TW91107591 A TW 91107591A TW 575716 B TW575716 B TW 575716B
Authority
TW
Taiwan
Prior art keywords
engine
crankshaft
torque
starting
maximum
Prior art date
Application number
TW91107591A
Other languages
Chinese (zh)
Inventor
Masayuki Toriyama
Original Assignee
Honda Motor Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Honda Motor Co Ltd filed Critical Honda Motor Co Ltd
Application granted granted Critical
Publication of TW575716B publication Critical patent/TW575716B/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02NSTARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
    • F02N19/00Starting aids for combustion engines, not otherwise provided for
    • F02N19/005Aiding engine start by starting from a predetermined position, e.g. pre-positioning or reverse rotation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02NSTARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
    • F02N11/00Starting of engines by means of electric motors
    • F02N11/08Circuits or control means specially adapted for starting of engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B61/00Adaptations of engines for driving vehicles or for driving propellers; Combinations of engines with gearing
    • F02B61/02Adaptations of engines for driving vehicles or for driving propellers; Combinations of engines with gearing for driving cycles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02NSTARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
    • F02N19/00Starting aids for combustion engines, not otherwise provided for
    • F02N19/005Aiding engine start by starting from a predetermined position, e.g. pre-positioning or reverse rotation
    • F02N2019/007Aiding engine start by starting from a predetermined position, e.g. pre-positioning or reverse rotation using inertial reverse rotation

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)

Description

D/D/W 五、發明說明(1) 曼一萌所屬^之枯街 本發明係關於藉由起動 引擎起動裝置,特別Θ =馬f使曲軸動作而將引擎起動之 之慣性力與起動馬達::f由併用了包含曲軸之回轉系 亦可有良好之引擎& 扭矩,即使低扭矩之起動馬達 習知之心引擎起動之引擎起動裝置。 引擎起動時之曲車由 _ (TDO前之最大值(跨越顯示活塞剛到達壓縮上死點 可得以發生之最大 ),為跨越此TDC,以往則採用 扭矩以上之比較大 矩亦即止轉扭矩為前述最大曲軸 _ 起動馬達。 引擎之起動性是起動 此,起動馬達直、4=:驅=矩愈大愈提昇。因 部分作為慣性質旦+ 之冓^中,起動馬達之回轉 動馬達時,特別:加速:動;以採用驅動扭矩大之大型起 例如,一船/丨 速i動4之驅動性不得不下降。 其最大曲軸‘矩達:m採用之1 〇〇cc以下之4衝程引擎 1.3kgfm之起動。但是,最大發生扭矩為 土丄 ^動馬達直結曲軸時,其慣性皙吾 遠大於最適慣性質量 :!·生貝里為40kgcm, 與驅動性成兩者$ p y kgcm。亦即,引擎之起動性 本發明係,很難兩全其美。 引擎起動裝置复疋兔六 述習知技術之問題,提供一種 之引擎起動為的起動馬達之情形,亦能確保良好 而使引擎之起動性與驅動性可兩全其美。 第5頁 C:\2D-00DE\9]-07\9]10759].ptd ^/5716 五、發明說明(2) 為達成上述目 逆轉至所定之位 置中’具備有使 止後,使起動馬 最大發生扭矩為 需之表大曲轴扭 壓縮行程以外所 依據上述之特 速’可得比較大 矩之合力只要可 身之最大發生扭 壓縮行程。 發明之f 的,本 置,以 曲轴正 達逆轉 使引擎 矩之大 必需之 徵,在 之慣性 達到最 矩比最 以下 引擎起 輛甚至 擎自動 開等之 引擎再 車體 體骨格 置物箱 於車 11 ,下 ,參照圖 動裝置之 具有引擎 停止,之 起動操作 起動。 前部與車 之車體框 (均未圖^ 體前部, 方延伸著 ^明八特徵為:引擎停止後,曲軸 》備下次之引擎起動之引擎起動 轉=及逆轉之起動馬達,及引擎停 之逆轉控制機構,前述起動馬達之 起動時其活塞跨越壓縮行程時所必 約6 0%以下,而且在當活塞於進行 曲軸扭矩以上。 活塞達成壓縮行程為止前可充分加 力’此慣性力與起動馬達之驅動扭 大曲軸扭矩,則即使該起動馬達本 大曲軸扭矩為小時,活塞亦可跨越 式詳細說明本發明。圖1為適用本發明之 速克達型自動二輪車之全體側面圖,該車 自動停止、發動機能,其在車輛停止則引 後’σ若節流閥手柄打開,或者起動開關打 被操作時,則使起動馬達被自動驅動而使 體後部介由低的底板部4相連結,作為車 架概由底管6及主管7所構成。燃油箱以及 以主管7支持,於其上方配置座墊8。 由轉向頭5所軸支持而其上方設有手把 前叉12,其下端軸支持前輪FW。手把^之 C:\2D-C0DE\91-07\91107591.ptd 第6頁 575716 五、發明說明(3) 上部覆蓋著兼用儀錶板之手把覆蓋丨3。主管7之站立部下 端=支榜架15,於此支樓架15介由連桿構件16自由。搖動 而連接支持著。擺動裝置2之懸掛支架18。 於擺動裴置2中,其前部裴載單氣缸5〇cc之4行程引擎 E。此引擎E向後方構成皮帶式無段變速機丨〇,其後部介由 離心離合器所設之減速機構9之上則軸支持著後輪Μ。此 減速機構9之上端與主管7之上部彎曲部《間裳言史有後緩衝 裔3。於擺動裝置2之前部中,配設有從引擎£延 吸 :19 :連接之汽化器17以及同一汽化器17所連結之空氣濾 清态1 4。 圖2為前述擺動裝置2之沿著曲軸2〇1切斷之剖面圖,圖3 ,其部分放大圖,顯示與上述同一之元件編號為同一或同 4之部分。 擺動裝置2是由左右之曲軸箱202L、2〇2R合成一體所構 成之曲軸箱202所覆蓋,曲軸201藉由固定於曲軸箱2〇21?之 車^280、209而自由旋轉地支持著。曲軸2〇ι介由曲軸銷 213連結連桿(未圖示)。 左曲軸箱202L兼用皮帶式無段變速箱,於延伸至左曲 2202L之曲軸201中設有可旋轉之皮帶驅動輪m。皮帶驅 動輪210由固定側皮帶輪半邊21〇L及可動側皮帶輪半邊 21 0R所組成,固定側皮帶輪半邊21儿之左端部介由轂2 η 被固定,於其左側則有可動側皮帶輪半邊2i〇r用栓槽故合 於曲軸201 ’而可接近或離開固定側皮帶輪半邊21儿。兩 個皮帶輪半邊210L,21〇R之間掛上¥型皮帶212。 第7頁 c-\2D-CODE\91-07\91107591.ptd 575716 五、發明說明(4) 可動側皮帶輪半邊21 〇R之右側中、凸輪板215固定於曲 軸201,其外周端所設之滑動件215&自由滑動地繫合於位 於可動側皮帶輪半邊2 1 0R之外周端且於軸方向所形成之凸 輪板滑^動轂部210Ra上。可動側皮帶輪半邊21(^之凸輪板 2 1 5其罪近外周處具有向可動側皮帶輪半邊2〗傾斜之錐 面4斜面與半個可動側皮帶輪2 1 〇 R之間之空處容納乾式 鍾球2 1 6。 曲軸201之旋轉速度增加時,則位於可動側皮帶輪半邊 21 0R與凸輪板215之間且共同旋轉之前述乾式錘球216、因 離心力而向離心方向移動,可動侧皮帶輪半邊21〇R受乾式 錘球216之按壓而向左方移動而接近固定側皮帶輪半邊 210L。其結果,兩皮帶輪半邊21〇L、2i〇r間所夾之v型皮 帶212向離心方向移動,其掛上之徑變大。 於車輛之後部中設有與前述皮帶驅動輪2丨〇相對應之被 動皮=輪(未圖示),v型皮帶212掛上此被動皮帶輪。藉由 二皮τ傳動機構’引擎^;之動力被自動調整並傳至離心離 5器,介由前述減速機構9等驅動後輪RW。 :::軸相2 0 2R内’ g己設起動馬達與AC發電機組合 動機兼發電機(ACG起動機M eACG起動機,於曲轴2〇1 之刖端斜錐部用螺紋2 53固定外轉子6〇。 外轉子60之内周側設之靜子5()用螺栓279 於 虫羽°又有政熱裔282,散熱器282用風扇蓋281覆蓋。 如圖3放大所示,靜子5〇之内周中欲入感測器盒28。此D / D / W V. Description of the invention (1) Man Yimeng's dry street This invention relates to the inertial force and starter motor that start the engine by starting the engine starting device, especially Θ = horse f to make the crankshaft move :: f is an engine starting device which can also have good engine & torque even when using a turning system including crankshaft, even a low torque starting motor. When the engine is started, the crank is from _ (the maximum value before TDO (the maximum that the piston can reach the compression top dead center just after it reaches the maximum). In order to overcome this TDC, in the past, a larger torque than the torque, that is, the stop torque It is the largest crankshaft _ starter motor mentioned above. The startability of the engine is to start this, the starter motor is straight, 4 =: drive = the larger the moment, the more the moment is increased. As part of the inertia mass + + ^, when the starter motor rotates the motor Special: Acceleration: Dynamic; To adopt a large starting torque with large driving torque, for example, the driveability of a boat / speed i moving 4 has to be reduced. Its maximum crankshaft 'moment reaches: 4 strokes below 100cc used by m The engine starts at 1.3kgfm. However, the maximum inertia when the motor is directly connected to the crankshaft, the inertia is far greater than the optimal inertial mass:! · Sangbury is 40kgcm, and the driveability is $ py kgcm. That is, The engine startability of the present invention is difficult to get the best of both worlds. The engine starting device is based on the problems of the conventional technology of the rabbit and provides a kind of starter motor that can start the engine. Starting and driving can be the best of both worlds. Page 5 C: \ 2D-00DE \ 9] -07 \ 9] 10759] .ptd ^ / 5716 5. Description of the invention (2) Reversing to the stated position in order to achieve the above purpose ' It is provided with the maximum torque of the starting horse after the stoppage is required. In addition to the large crankshaft torsion compression stroke based on the above-mentioned special speed 'to obtain a relatively large torque combined force, as long as the maximum torsional compression stroke can be achieved. Invention of f This is a necessary sign that the crankshaft is up to the reverse to make the moment of the engine large, in which the moment of inertia reaches the lowest moment than the lowest engine, and even the engine is automatically opened, and then the body frame is placed in the car body. Refer to the figure of the moving device with the engine stopped and the start operation started. The front and the body frame of the car (both are not shown in the figure, the front part of the body is extended ^ Ming eight features: after the engine stops, the crank The engine starting rotation of the engine starts = and the starting motor of the reverse rotation, and the reverse rotation control mechanism of the engine stop. When the aforementioned starting motor starts, its piston must cross the compression stroke below about 60%, and when the piston is cranking the crankshaft, The piston can be fully applied until the compression stroke is reached. 'This inertial force and the driving torque of the starter motor increase the crankshaft torque. Even if the crankshaft torque of the starter motor is small, the piston can leapfrog the invention in detail. Figure 1 In order to apply the present invention to the entire side view of a speed Keda type two-wheeled vehicle, the vehicle automatically stops, the engine can be triggered when the vehicle stops, 'σ if the throttle handle is opened, or the start switch is operated, the The starter motor is automatically driven so that the rear part of the body is connected via a low floor portion 4, and the frame is composed of a bottom pipe 6 and a main pipe 7. The fuel tank is supported by the main pipe 7, and a seat cushion 8 is arranged above it. It is supported by the shaft of the steering head 5 and a handlebar front fork 12 is provided above it. The lower end shaft supports the front wheel FW. C: \ 2D-C0DE \ 91-07 \ 91107591.ptd Page 6 575716 V. Description of the invention (3) The upper part is covered with the handle of the instrument panel. The lower end of the standing part of the supervisor 7 = the support stand 15, and the support stand 15 is free via the link member 16. Shake while the connection is supported. The suspension bracket 18 of the swinging device 2. In the swing Pei set 2, the front Pei contains a single-cylinder 50cc 4-stroke engine E. This engine E constitutes a belt-type stepless speed changer to the rear, and its rear part supports the rear wheel M through a reduction mechanism 9 provided by a centrifugal clutch. The upper end of the speed reduction mechanism 9 and the upper curved portion of the main pipe 7 "Jian Chang Yan Shi has a back cushion 3". In the front part of the swing device 2, a suction from the engine: 19: a connected carburetor 17 and an air filter state 14 connected to the same carburetor 17 are provided. FIG. 2 is a cross-sectional view of the aforementioned swinging device 2 cut along the crankshaft 201, and FIG. 3 is an enlarged view of a part thereof, showing the same component number as the same or the same as the above. The swinging device 2 is covered by a crankcase 202 composed of left and right crankcases 202L and 202R, and a crankshaft 201 is rotatably supported by a vehicle 280, 209 fixed to the crankcase 2021 ?. The crankshaft 200 is connected to a connecting rod (not shown) via a crankpin 213. The left crankcase 202L also serves as a belt-type stepless gearbox. A crankshaft 201 extending to the left curve 2202L is provided with a rotatable belt drive wheel m. The belt driving wheel 210 is composed of a fixed-side pulley half 21L and a movable-side pulley half 21 0R. The left-side end of the fixed-side pulley half 21 is fixed via the hub 2 η, and on its left side is a movable-side pulley half 2i. The r slot is fitted on the crankshaft 201 'and can approach or leave the fixed side pulley half 21. A ¥ -shaped belt 212 is hung between the two pulley halves 210L and 210R. Page 7 c- \ 2D-CODE \ 91-07 \ 91107591.ptd 575716 V. Description of the invention (4) The right side of the movable side pulley half 21 〇R, the cam plate 215 is fixed to the crankshaft 201, and the outer peripheral end is provided with The slider 215 is freely slidably coupled to a cam plate slider 210Ra formed at the outer peripheral end of the movable side pulley half 2 1 0R and formed in the axial direction. The cam plate 2 1 5 of the movable side pulley 2 1 5 has a tapered surface 4 inclined toward the movable side pulley half 2 near the outer periphery. The space between the inclined surface and the half of the movable side pulley 2 1 0R accommodates a dry clock. Ball 2 1 6. When the rotation speed of the crankshaft 201 increases, the aforementioned dry hammer ball 216, which is located between the movable side pulley half 21 0R and the cam plate 215 and rotates together, moves in the centrifugal direction due to centrifugal force, and the movable side pulley half 21 〇R moved to the left by the dry hammer ball 216 and approached the fixed-side pulley half 210L. As a result, the v-belt 212 sandwiched between the two pulley halves 21oL and 2ior moved toward the centrifugal direction, and it hung The upper diameter becomes larger. A passive leather = wheel (not shown) corresponding to the aforementioned belt drive wheel 2 丨 0 is provided in the rear part of the vehicle, and the v-belt 212 is hung on this passive pulley. It is driven by two leather τ The power of the mechanism 'engine ^; is automatically adjusted and transmitted to the centrifugal separator 5, and the rear wheel RW is driven through the aforementioned reduction mechanism 9. etc. ::: Shaft phase 2 0 2R' g has a starter motor and AC generator combination Motive and generator (from ACG starter M eACG As for the motive, the outer rotor 6 is fixed with the thread 2 53 at the sloping cone of the crankshaft 201. The stator 5 () provided on the inner peripheral side of the outer rotor 60 is bolted at 279 to the worm feather and has a heat of 282, The radiator 282 is covered with a fan cover 281. As shown in the enlarged view in FIG. 3, the sensor box 28 is intended to be inserted into the sensor box 28 in the inner periphery.

575716 五、發明說明(5) 感測器盒28内中,沿著外轉子60之轂60a之外周等間隔設 有轉子角度感測器(磁極感測器)2 9以及脈衝感測器(點火 脈衝器)30。轉子角度感測器29是ACG起動機1之對靜子線 圈進行通電控制使用者,對應著ACG起動機1之U相相、 W相各個一對一個而設置。點火脈衝器3 〇是用作為引擎之 ,火控制,而只設一個。轉子角度感測器29以及點火脈衝 器3 0均可由霍爾I C或磁性電阻(MR )元件所構成。 轉子角度感測器29以及點火脈衝器30之導線連接於基板 3 1,甚至於基板3 1結合配線導線3 2。於外轉子6 〇之轂6 〇 a 之外周中,嵌入對轉子角度感測器29以及點火脈衝器3〇之 各個有磁性作用之2段式賦與磁性之磁性環33。 對應於轉子角度感測器29之磁性環33之一方之磁性帶 中,相對應於靜子50之磁極,於圓周方向以3〇。為間隔形 成交互配列之N極及S極,對應於點火脈衝器3〇之磁性環33 之另一方之磁性帶中,於圓周方向之一處於15。至4〇。之 範圍形成磁性部。 前述ACG起動機i為引擎起動時,作為起動馬達(同步馬 達)之機能,係利用從蓄電池供應之電流來驅動隨之旋轉 曲軸2(Π而發動引擎;引擎起動後有同步發電機之機能、 發電後之電流充電蓄電池,而且供給各電裝部之電流。 回至圖2 ’於曲軸201中’前述ACG起動機j及軸承2〇9之 間固定有鏈輪231,此鏈輪231 +,掛上用以從曲軸2〇1驅 動凸=軸(未圖示)之賴。尚且前述鍵輪231與齒輪m形 成-體’該齒輪232係用為傳達動力給循環潤滑油之系 C: \2D-mDE\91 -07\91107591 .ptd 第9頁 575716 五、發明說明(6) 浦0 圖4為含有ACG起動機1之電裝系統之方塊圖。ECU3含有 ACG起動機1之發電機能所發生之三相交流全波整流之3相 全波整流橋式電路300,及將全波整流橋式電路30 0之輸出 限制為既定之調整電壓(調整動作電壓:例如:1 4 · 5 V)之調 整器1 0 0。 甚而’本實施形態之ECU3’尚具有引擎剛停止後可將曲 轴逆轉至所定之位置,以提昇下次引擎之起動性之回擺控 制部7 0 0 ’及引擎起動時降低曲軸扭矩之起動控制部5 〇 〇,575716 V. Description of the invention (5) In the sensor box 28, a rotor angle sensor (magnetic pole sensor) 2 9 and a pulse sensor (ignition) are provided at equal intervals along the outer periphery of the hub 60a of the outer rotor 60. Pulser) 30. The rotor angle sensor 29 is a user for energizing the stator coil of the ACG starter 1, and is provided corresponding to each of the U-phase and W-phase of the ACG starter 1. The ignition pulsator 3 is used as the engine and fire control, but only one. Both the rotor angle sensor 29 and the ignition pulser 30 may be composed of a Hall IC or a magnetic resistance (MR) element. The wires of the rotor angle sensor 29 and the ignition pulser 30 are connected to the substrate 31, and even the substrate 31 is combined with the wiring conductor 32. In the outer periphery of the hub 6 o a of the outer rotor 60, a two-stage magnetic ring 33 for imparting magnetism to each of the rotor angle sensor 29 and the ignition pulser 30 is embedded. One of the magnetic bands corresponding to one of the magnetic rings 33 of the rotor angle sensor 29 corresponds to the magnetic pole of the stator 50 and is 30 ° in the circumferential direction. The N and S poles which are alternately arranged for the interval form, and among the magnetic strips corresponding to the other side of the magnetic ring 33 of the ignition pulser 30, one of them is at 15 in the circumferential direction. To 40. The range forms a magnetic portion. The aforementioned ACG starter i is the function of a starter motor (synchronous motor) when the engine is started. It uses the current supplied from the battery to drive the crankshaft 2 (Π) to start the engine; after the engine starts, it has the function of a synchronous generator. The electric current after power generation charges the battery and supplies the electric current of each electric part. Returning to FIG. 2 'in the crankshaft 201', a sprocket 231 is fixed between the aforementioned ACG starter j and the bearing 209, and this sprocket 231 +, It is attached to drive the convex = shaft (not shown) from the crankshaft 201. Moreover, the aforementioned key wheel 231 and the gear m form a body. The gear 232 is used to transmit power to the circulating lubricant system C: \ 2D-mDE \ 91 -07 \ 91107591 .ptd Page 9 575716 V. Description of the invention (6) PU 0 Figure 4 is a block diagram of an electrical equipment system containing ACG starter 1. ECU3 contains ACG starter 1. The generated three-phase AC full-wave rectification is a three-phase full-wave rectifier bridge circuit 300, and the output of the full-wave rectifier bridge circuit 300 is limited to a predetermined adjustment voltage (adjusting operating voltage: for example: 1 4 · 5 V) Adjuster 1 0 0. Even 'ECU3 of this embodiment' has Immediately after the engine stops, the crankshaft can be reversed to a predetermined position to improve the startability of the next engine. The turning control unit 7 0 0 ′ and the starting control unit that reduces the crankshaft torque at the start of the engine 5 0 0,

及引擎旋轉數於預定之低旋轉範圍增加發電量之發電控制 部40 0 〇 於^1^3’中連接點火線圈2 1,於點火線圈2 1之二次側連 接^星基22。又,於ECU3,中連接節流感測器23、燃油感 f裔24、閱座開關25、怠速開關26、冷卻水溫感測器27、 月J述轉子角度感測器2 9以及點火脈衝器3 〇,從各部發出之 檢測信號輸入ECU3,。 甚而,於ECU3 、 ϋ τ逆接起動繼電器3 4、起動開關3 5、 2關36,37、待機指示器38、燃油指示器39、速度感 °° 、,以及頭燈42。於頭燈42中設有定時開關43。The engine control unit 400 for increasing the power generation amount in a predetermined low rotation range and the number of engine revolutions connects the ignition coil 21 to ^ 1 ^ 3 ', and connects the star base 22 to the secondary side of the ignition coil 21. In addition, the ECU 3 is connected to an influenza sensor 23, a fuel sensor 24, a seat switch 25, an idle switch 26, a cooling water temperature sensor 27, a rotor angle sensor 29, and an ignition pulser. 3 〇, the detection signal from each unit is input to ECU3. Furthermore, ECU3, ϋ τ are reversely connected to start relay 3 4, start switch 3 5, 2 off 36, 37, standby indicator 38, fuel indicator 39, speed sense °°, and headlight 42. A timing switch 43 is provided in the headlight 42.

庙^ Ϊ各4中介由主保險絲44以及主開關45由蓄電池2 "另^ t尚且蓄電池2,藉由起動繼電器34直接連接ECU 連=,面之電亦路有不介由主開關45、僅只介由主讀 其次’針對上述ECU3, <回擺控制部7〇〇,起動控制名^ Ϊ 4 each through the main fuse 44 and the main switch 45 by the battery 2 " Another ^ t still the battery 2, directly connected to the ECU through the start relay 34 =, the surface of the electricity also has no way through the main switch 45, Only through the main reading, next to the above-mentioned ECU3, < the swing control unit 700, the start control name

575716 五、發明說明(7) 500以及發電控制部4〇〇之構成以及 方塊圖加以說明。 F蒼照圖5之機舶 於回擺控制部700中,階段判別部73 器29之輸出信號將曲軸2〇1 據轉子角度感刺 _段,以點火脈衝器3。發生…之 為基準階段_。),來判別说之檢測時機作 階段通過時間檢測部74依據前述階段^別 新的階段至判別出次一階段之時間县 通過時間心。逆轉控制部75依據前;階: = 另=以及濛前述階段通過時間檢測部74所檢測之通= 時間△ t η而發生逆轉驅動指令。 負載比設定部72依據前述階段判別部73之判別姓 態控制供給全波整流橋式電路3〇〇之各功率fet之閑電壓之 負載比。.驅動器80將前述設定之負載比之驅動脈 全波整流橋式電路30 0之各功率FET。 … 其=,對上述回擺控制部700之動作,參照圖6之流 以及圖7之動作說明圖加以說明。 α 圖7(a)為顯示曲軸201逆轉所要之曲軸扭矩(逆轉負 與曲轴角度之關係,曲軸扭矩是剛至壓縮上死點前(逆 時)急速上昇。同圖(b)為顯示曲軸角度與階段之關係, 圖(C)為顯不逆轉時曲轴之角速度之變化。 於步驟S61檢測引擎停止時,於步驟S62、S63中、階 判別部73中參照已經判別得知之目前之階段。此處,目^ 階段為階段#0〜#11中之任一個、則進行步驟S64,若為^575716 V. Description of Invention (7) 500 and the structure and block diagram of the power generation control unit 400 are described. In the swing control unit 700, the output signal of the stage discriminating unit 73 and 29 will stab the crankshaft 201 according to the rotor angle, and the ignition pulser 3 will be ignited. Happened ... is the baseline phase_. ) To determine the detection timing. The phase passing time detection unit 74 determines the time from the new phase to the time when the next phase is determined based on the previous phase. The reversing control unit 75 generates a reversing drive command based on the previous stage: = another = and the pass detected by the time detecting unit 74 at the aforementioned stage = time Δ t η. The duty ratio setting unit 72 controls the duty ratio of the idle voltage of each power fet supplied to the full-wave rectifier bridge circuit 300 based on the discriminated name of the aforementioned stage discrimination unit 73. The driver 80 drives each of the power FETs of the full-wave rectifier bridge circuit 300 with the previously set load ratio. ... It is explained that the operation of the swing-back control unit 700 will be described with reference to the flow of Fig. 6 and the operation explanatory diagram of Fig. 7. α Figure 7 (a) shows the crankshaft torque required for the reverse rotation of crankshaft 201 (the relationship between the negative reversal and the crankshaft angle. The crankshaft torque rises sharply just before the compression top dead center (reverse time). The same figure (b) shows the crankshaft angle. The relationship with the stage, the graph (C) shows the change in the angular velocity of the crankshaft when the reversal is not shown. When the engine is stopped at step S61, the current stage that has been identified and learned is referred to in steps S62, S63, and the stage discrimination unit 73. This If the stage is any of stages # 0 to # 11, step S64 is performed. If it is ^

C:\2D-CODE\91-07\91107591.ptd 第11頁 575716 五、發明說明(8) 段#12〜#32中之任一個,則進行步驟邮,以外(亦即 段#33〜#35中之任一個)則進行步驟⑽。步驟s64、⑽是 於負載比設定部72中設定驅動脈衝之負載 S65則設定為80%。 哪 如此負載比之動態控制如後所詳述,將逆轉時曲軸2〇ι 之角速度在曲軸扭矩將増大之壓縮上死點相當角之前( 轉時)使其充分降低,同時進行角度控制使得在此以外之 角度之快速逆轉驅動成為可能。 ::驟67中,驅動器80依照前述設定之負載比來控制全 波正机橋式電路3〇〇之各功率FET而開始逆轉通電。於+ ^ ^ ^ ^ ^ ^ ^ Δΐη ^ ^ ^ ^ 時間檢測部74檢測。 於步驟S69中,逆轉控制部75判別曲軸2〇1是通過階 亦即上死點附近。若無通過階段㈣,則於步驟S7i 剛通過之前述階段#n之通過時間Atn與更前之通過階、 #(n_l )之通過時間△tnq之比[八比/八饨」]與基準值又 Rref (本實施形態為4/3)相比較。前述通過時間比[△“/ △tn_1]若無比基準值Rref提高,則返回前述步驟S62】鏟 驅動’與此類似之上述各處理反覆進行。 於此,引擎停止位置亦即逆轉開始位置如圖7(〇曲線A 所不、比起前回以及次回之壓縮上死點之中間位置 次,=壓縮上死點,換言之,從通過排氣上死點(正轉時) 至壓縮上死點之過程時,ACG起動機1雖然以7〇%之負載比 逆轉驅動,但曲軸仍可通過階段#〇 (排氣上死點)。因此,C: \ 2D-CODE \ 91-07 \ 91107591.ptd Page 11 575716 V. Description of the invention (8) Any one of paragraphs # 12 ~ # 32, then proceed to step mail (other than paragraphs # 33 ~ # 35), then proceed to step ⑽. In step s64, ⑽ sets the load S65 of the driving pulse in the load ratio setting section 72 to 80%. The dynamic control of such a load ratio is described in detail below. The angular velocity of the crankshaft at 200 rpm during reverse rotation is reduced sufficiently before the crankshaft torque compresses the upper dead center to a considerable angle (when turning). At the same time, the angular control is performed so that Fast reversal drive from other angles becomes possible. :: In step 67, the driver 80 controls each power FET of the full-wave positive bridge circuit 300 according to the previously set load ratio, and starts to be turned on. At + ^ ^ ^ ^ ^ ^ ^ Δΐη ^ ^ ^ ^ ^ The time detection unit 74 detects. In step S69, the reversal control unit 75 determines that the crankshaft 201 has passed the stage, that is, near the top dead center. If there is no passing stage ㈣, then the ratio of the passing time Atn of the aforementioned stage #n to the preceding passing stage, and the passing time △ tnq of # (n_l) [8 ratio / eight 饨 '] and the reference value just passed in step S7i. Rref (4/3 in this embodiment) is compared. If the aforementioned passing time ratio [△ "/ △ tn_1] is increased incomparably with the reference value Rref, the process returns to the foregoing step S62] The shovel drive is similar to the above-mentioned processes repeatedly. Here, the engine stop position, that is, the reverse start position is as shown in the figure. 7 (〇 curve A does not compare with the middle position of the compression top dead point of the previous and second times, = compression top dead point, in other words, the process from passing through the exhaust top dead point (when forward rotation) to the compression top dead point At this time, although the ACG starter 1 is driven in reverse with a load ratio of 70%, the crankshaft can still pass through the phase # 0 (exhaust top dead center). Therefore,

第12頁 575716 五、發明說明(9) ----- 於步驟S69中測知而進行步驟S7〇 階段# 3 2 〇扛am w 千υ i疋否到達 ;,由於別赫曲軸201已到達階段#32時,則於步驟S72 中由於别述圯轉通電已停止,其後,曲軸因 步逆旋轉而後停止。 〖貝性力進 另一方面,逆轉開始位置如圖7(c)曲線B所示 回以及次f之壓縮上死點t中間&置更靠近“之壓縮上 死點’換言之’從通過壓縮上死點(正轉時)至排氣上死點 之,程時,ACG起動機之負載比逆轉驅動,其逆轉 負荷如圖7(a)所示,剛至階段#〇之前(逆轉時)為上昇時, 曲軸201之角速度急速下降。而且,於步驟S71中,判別前 述通過時間比[Δΐ:η/Λι:η-1]為基準值之4/3以上時,於步 驟S72中,停止前述逆轉通電,曲軸之逆轉與停止 致同時停止。 如此,本實施形態之回擺控制中,於引擎停止後之逆轉 驅動時,監視著曲軸是否通過上死點相當角,以及曲軸之 角速度是否下降,曲軸逆轉時通過上死點時之後馬上停止 逆轉通電,且在曲軸之角速度由於逆轉負荷之增大而降低 之情況亦是停止逆轉通電。因此,不論逆轉開始位置、曲 軸可於前回之壓縮上死點之前(逆轉時)返回壓縮反力低之 位置。 、甚而、本實施形態之回擺控制中、依據檢測之轉子角度 感測器2 9以檢測曲軸2 0 1之角速度、其中其為基於可檢測 ACG起動機之轉子角度(亦即階段)之轉子角度感測器之輸 出,而可達成上述之檢測,故不需另行設置專門檢測曲軸Page 12 575716 V. Description of the invention (9) ----- Step S7 is performed in step S69 as measured in step S69. # 3 2 〇 Carry am w 千 υ i 疋 arrived; because the Bech crankshaft 201 has arrived At the stage # 32, in step S72, the energization has been stopped due to the other-mentioned rotation, and thereafter, the crankshaft is stopped due to reverse rotation. 〖Beijing force advancement On the other hand, the start position of the reversal is shown in Figure 7 (c), curve B, and the middle of the compression top dead point t of time f is set closer to the compression top dead point 'in other words, from the compression through From the top dead center (for forward rotation) to the exhaust top dead center, during the process, the load ratio of the ACG starter is reversely driven. The reverse load is shown in Figure 7 (a), just before stage # 〇 (when reversed) When it is rising, the angular velocity of the crankshaft 201 decreases rapidly. In step S71, when it is determined that the passing time ratio [Δΐ: η / Λι: η-1] is 4/3 or more of the reference value, the process stops in step S72. In the aforementioned reverse rotation, the crankshaft reverses and stops at the same time. Thus, in the swing control of this embodiment, during the reverse drive after the engine is stopped, it is monitored whether the crankshaft passes through a top dead center equivalent angle and whether the angular speed of the crankshaft decreases When the crankshaft reverses, the reverse energization is stopped immediately after passing through the top dead center, and when the angular speed of the crankshaft is reduced due to the increase of the reverse load, the reverse energization is also stopped. Therefore, regardless of the start position of the reverse, the crankshaft can be compressed in the previous return Before the top dead point (when reversing), return to the position where the compression reaction force is low. Even in the swing-back control of this embodiment, based on the detected rotor angle sensor 29 to detect the angular velocity of the crankshaft 201, which is Based on the output of the rotor angle sensor that can detect the rotor angle (ie stage) of the ACG starter, the above-mentioned detection can be achieved, so there is no need to set up a special detection crankshaft

C:\2D-CODE\91-07\91107591.ptd 第13頁 575716C: \ 2D-CODE \ 91-07 \ 91107591.ptd Page 13 575716

575716 五、發明說明(11) 於步驟S58中洩壓線圈63成為0FF,於步驟S59中ACG刼 1為OFF。 &動機575716 V. Description of the invention (11) In step S58, the pressure relief coil 63 becomes 0FF, and in step S59, ACG 刼 1 is OFF. & Motivation

如此’本實施形態中引擎起動時強制打開排氣閥, 制於壓縮行程中之氣缸内壓上昇,且壓低最大曲軸扭矩PIn this way, in this embodiment, the exhaust valve is forcibly opened when the engine is started, the internal pressure of the cylinder controlled in the compression stroke is increased, and the maximum crankshaft torque P is reduced.

Tmax ’所以即使是採用最大發生扭矩較小之小型起動 亦可確保良好之起動性。 成、 △回至圖5,發電控制部4 〇 〇通常在控制發電量(電壓)之 月匕之外而且相對於前述ACG起動機1之各相之靜子線、 具有從蓄電池2做延遲角通電,來增加發電量(以么 「ACG通電控制」之機能。 %為 此處,所謂延遲角通電是指基於以前述轉子角度感 29所檢測出前述磁性環33之磁性 檢,: 號,延遲相當分之預定之雷£ ^ /1,] ^ y Q 預疋之電乳角而通電於靜子線圈而古。 客Γ 3敬S Ϊ回轉扼圍為防止由於前述調節器1 0 0動作而 因入敕Ϊ之急速變化而造成引擎回轉不安定化之原 ^ Ϊ : Ϊ器橋式電路3°°之輸出電壓(蓄電池電叫 制糸调整益電壓以下之預定電壓範圍内。 )拴 於發電控制部4 〇 〇中,引聲ρ雜泰 少rr输哭5 * 117轉數判別部48例如依據點 人脈衝态30之檢測信號檢測出弓丨擎 丨够 在預定之發電控制範圍内則將 J數’此引挲回轉數Tmax ’Therefore, it is possible to ensure good startability even with a small start with a small maximum torque. As shown in FIG. 5, the power generation control unit 400 normally has a delay angle from the battery 2 to the static sub-lines of each phase of the ACG starter 1 in addition to the moon dagger that controls the power generation amount (voltage). In order to increase the power generation (the function of the "ACG energization control".% Is here, the so-called delayed angle energization refers to the magnetic detection of the magnetic ring 33 based on the aforementioned rotor angle sense 29, the delay is equivalent. Pre-determined thunder £ ^ / 1,] ^ y Q The electric current angle of the electric circuit is energized in the stator coil. Guest 3 3 S S Ϊ Swiveling encirclement is to prevent the entry of The rapid change caused by the rapid change of the engine causes the engine to turn unstable. ^ Ϊ: The output voltage of the bridge circuit 3 °° (the battery voltage is within the predetermined voltage range below the adjusted voltage.) Tethered to the power generation control unit In 4 〇〇, the phonation ρ miscellaneous rr 5 cry 117 rotation number discriminating unit 48, for example, based on the detection signal of the point pulse state 30 detection bow 丨 engine 丨 enough to within the predetermined power generation control range, the number of J 'This cited rotation number

St甬;後Ϊ驅動器80從延遲角量設定部49讀:預 先6又疋之通电延遲角量而使之延遲角 預 從負載比設定部4 7供給驅動器§ 〇。 、 比則 驅動為8 0藉由轉子角度感測器 ° 所k測出之磁極檢測兮孔St .; Hoop driver 80 is read from the delay angle amount setting section 49: the delay angle is turned on in advance by 6 and the delay angle is preliminarily supplied to the driver from the load ratio setting section 47. § 〇. The ratio is driven to 80. The magnetic pole detected by the rotor angle sensor ° is detected.

\\312\2d-code\91-07\91107591 $ 15頁 __\\ 312 \ 2d-code \ 91-07 \ 91107591 $ 15 pages __

575716 五、發明說明(12) 唬,亦即對應外轉子6 0之磁極所形成之磁 帶,當其每次由感測器2 9檢測出時 ^ % 部分使之延ϋ 攸八么唬之上幵將相當通電延遲角量 吏之乙遲角,向全波整流橋式電 PWM控制信號。 纷之各FET輸出 蓄電池電壓判別部46將蓄電池電 圍之控制電壓最大值VMax以及批制予厂,、規疋冤&控制靶 π播甘^ Γ 控制電壓最小值^匕比較, ^ ^朴二、、Ό ,增減於負載比設定部所設定47之通電負 載,使畜電池電壓納於前述控制範圍Θ。亦即,蓄電 士, ^vb達到控制電壓最大值VMax則將通電負載僅減少預 ^仞!值例如1 %),又當蓄電池電壓Vb下降至控制電壓 最小值VMim則將通電負載僅增加同一之微小值。 圖10為顯示上述發電控制部4〇〇之動作流程圖,由前述 起動控制部500所成之引擎起動控制終了後才起動發電控 制部。 於步驟S4 1中,判斷引擎回轉數是否存在於發電控制範 圍毛電控制範圍例如設定於1 〇 〇 〇 r p m以上3 5 0 0 r p m以下。 引擎回轉數若存在於發電控制範圍,則進行步驟S42,判 ,顯不引擎回轉數存在於發電控制範圍之判別信號旗 是,被設定( = 1)。若信號旗匕⑶無被設定,則進行步驟S43 :又疋仏號旗FACG。於步驟S44中,通電延遲角量acgagl設定 為預定值ACGAGL。預定值ACGAGL可事先適當地設定,但於 本實施例中例如設定為電氣角6 Q。。575716 V. Description of the invention (12) Bluff, that is, the tape formed by the magnetic pole of the outer rotor 60, each time it is detected by the sensor 2 9 ^% makes it longer than the above幵 The second delay angle, which is equivalent to the energization delay angle, is applied to the full-wave rectifier bridge electric PWM control signal. Each of the FET output battery voltage discriminating units 46 assigns the maximum control voltage VMax of the battery voltage to the factory, regulates the & control target, and controls the minimum value of the control voltage. ^ Comparison of the minimum control voltage, ^ ^ Second, Ό, increase or decrease the current-carrying load set by the load ratio setting unit to 47, so that the animal battery voltage is within the aforementioned control range Θ. That is, if the power storage person, ^ vb reaches the maximum control voltage VMax, the energized load will be reduced by only ^ 仞! (For example, 1%), and when the battery voltage Vb drops to the minimum control voltage VMim, the energized load will only increase by the same small value. Fig. 10 is a flowchart showing the operation of the power generation control unit 400, and the power generation control unit is started after the engine start control by the start control unit 500 is completed. In step S41, it is determined whether or not the number of engine revolutions is within the power generation control range. The gross power control range is set to, for example, 1 000 r p m or more and 3 50 0 r p m or less. If the number of engine revolutions is in the power generation control range, step S42 is performed to determine that the flag indicating that the number of engine revolutions is in the power generation control range is yes (= 1). If the signal flag is not set, step S43 is performed: the flag FACG is again set. In step S44, the energization delay amount acgagl is set to a predetermined value ACGAGL. The predetermined value ACGAGL can be appropriately set in advance, but in this embodiment, it is set to, for example, an electrical angle of 6 Q. .

繼續於步驟45中,於通電負載acduty設定初期值ACDUTY C:\2D-C0DE\91-07\91107591.ptd 第16頁 575716 五、發明說明(13) 别述初期值A C D U T Y亦可事先適當地設定,但於本實施形 悲中例如设定為4 0 %。若步驟s 4 3〜S 4 5結束後則進行步驟 S47。若前述步驟S4中結果為是則跳過步驟S43〜S45進行 步驟S47。又,引擎回轉數不存在於前述發電控制範圍 時’則於步驟S 4 6信號旗facg重設(=〇 )後,進行步驟s 4 7。 於步驟S47中,判別信號旗Facg是否設定。若信號旗^^設 定,則於步驟S48判斷蓄電池電壓vb是否在控制電壓量最 大值VMax以上。控制電壓最大值\^ax設定比調節電壓更低 之值,例如13· 5Volt。若蓄電池電壓Vb不是在控制電壓最 大值VMax以上時,進行步驟S49判斷蓄電池電壓Vb是否在 控制電壓最小·值VMin以下。控制電壓最小值VMin例如設定 為 13· OVolt。 於步驟S49蓄電池電壓Vb若不在控制電壓最小值VMin以 下時,判斷Vb是否落在設定為比調節器之調節電壓更低的 值之ACG通電電壓範圍内,則進行步驟50、依據上述通電 延遲角量acgagl及通電負載acduty進行ACG通電控制。 於步驟S48判斷蓄電池電壓Vb在控制電壓最大值VMax以 上時’進行步驟S 5 1 ’將通電負載a c d u t y僅減少微小值 D D U T Y。微小值D D U T Y例如為1 %。又於步驟s 4 9判斷蓄電池 電壓V b在控制電壓最小值V M i η以下時,進行步驟s 5 2,將 通電負載acduty僅增加微小值DDUTY。步驟S51、S52處理 後進行步驟S50。 尚且,通電負載acduty增加時或減少時之前述微小值 DDUTY亦可不必相同’視控制電壓最大值VMax或者控制電Continue to step 45. Set the initial value ACDUTY C: \ 2D-C0DE \ 91-07 \ 91107591.ptd in the power-on load acduty. Page 16 575716 5. Description of the invention (13) The initial value ACDUTY can be set appropriately beforehand. However, in this embodiment, it is set to 40%, for example. After steps s 4 3 to S 4 5 are completed, step S47 is performed. If the result in step S4 is YES, skip steps S43 to S45 and proceed to step S47. When the number of engine revolutions does not exist in the aforementioned power generation control range ', after the signal flag facg is reset (= 0) in step S 4 6, step s 4 7 is performed. In step S47, it is determined whether the signal flag Fagg is set. If the signal flag ^^ is set, it is judged at step S48 whether the battery voltage vb is greater than the maximum control voltage amount VMax. The maximum control voltage \ ^ ax is set to a lower value than the adjustment voltage, such as 13.5Volt. If the battery voltage Vb is not greater than the maximum control voltage value VMax, step S49 is performed to determine whether the battery voltage Vb is less than the minimum control voltage value VMin. The minimum control voltage VMin is set to, for example, 13 · OVolt. In step S49, if the battery voltage Vb is not below the minimum control voltage VMin, it is determined whether Vb falls within the ACG energization voltage range set to a value lower than the regulator's adjustment voltage, then step 50 is performed according to the above-mentioned energization delay angle. ACG is controlled by measuring the amount of acgagl and the load acduty. When it is judged at step S48 that the battery voltage Vb is greater than the maximum control voltage VMax ', step S5 1' is performed to reduce the energized load a c d u t y by only a small value D D U T Y. The minute value D D U T Y is, for example, 1%. When it is determined in step s 4 9 that the battery voltage V b is below the minimum control voltage V M i η, step s 5 2 is performed to increase the energized load acduty by only a small value DDUTY. Steps S51 and S52 are followed by step S50. Moreover, the aforementioned small value DDUTY when the energizing load acduty increases or decreases may not necessarily be the same, depending on the maximum control voltage VMax or the control voltage

C:\2D-C0DE\91-07\91107591.ptd 第17頁 575716 五、發明說明(14) 壓最小值VM i η與現在值之差,而呈比例地改變微小值 DDUTY亦可。 另一方面,於步驟S47若信號旗facg無設定,即可知不在 發電控制範圍,則進行步驟S53停止ACG通電控制。 圖11為顯示A C G通電控制時靜子線圈之各相所流通之電 流(相電流)與轉子角度感測器2 9之輸出之時序圖。無進行 延遲角通電控制、於通常之狀況,響應轉子角度感測器29 之檢測輸出之正負(NS)之變化,電流供給靜子線圈之^、 V、W各相。另一方面,進行延遲角通電控制之情況時,從 轉子角度感測器2 9之檢測輸出之正負(N S)之變化,電流僅 延遲預定之延遲角量d( = 60° )供給靜子線圈之u、V、W各 相。 圖11中,由於負載截斷之通電角T為180。,藉由從負載 比設定部4 7向驅動器8 0供給之通電負載,可於1 8 〇。以内 決定。 圖12為引擎回轉數Ne亦即ACG起動機1之回轉數作為參數 而設定之通電負載之圖表。檢測引擎回轉數、並響應引擎 回轉數而決定通電負載。 如此,依據本實施形態之發電控制,於低回轉範圍並無 須啟動通常之電壓調節器,可謀求穩定地增大發電量。因 此’芯速運轉時等,可減少引擎負荷之變動,而極力減小 引擎回轉之變動,可使怠速運轉穩定化。 其次,於本實施形態中,前述ACG起動機1之規範,特別 是其規格所關係到之最大發生扭矩加以說明。C: \ 2D-C0DE \ 91-07 \ 91107591.ptd page 17 575716 V. Description of the invention (14) The difference between the minimum value VM i η and the current value, and the small value DDUTY may be changed proportionally. On the other hand, if the signal flag facg is not set in step S47, that is, it is known that the signal flag is not in the power generation control range, then step S53 is performed to stop the ACG power-on control. Fig. 11 is a timing chart showing the current (phase current) flowing through each phase of the stator coil and the output of the rotor angle sensor 29 during the AC C G energization control. No delay angle energization control is performed. In normal conditions, in response to changes in the positive and negative (NS) of the detection output of the rotor angle sensor 29, current is supplied to the phases of the stator coil, V, and W. On the other hand, when the delay angle energization control is performed, the current is delayed by a predetermined delay angle amount d (= 60 °) from the change of the positive and negative (NS) detection output of the rotor angle sensor 29. u, V, W phases. In FIG. 11, the conduction angle T due to load interruption is 180. By applying the energized load supplied from the load ratio setting unit 47 to the driver 80, the load can be reduced to 180. Within decision. Fig. 12 is a graph of the energized load set with the number of revolutions of the engine Ne, that is, the number of revolutions of the ACG starter 1 as a parameter. The number of engine revolutions is detected, and the energized load is determined in response to the number of engine revolutions. In this way, according to the power generation control of this embodiment, it is not necessary to activate a normal voltage regulator in a low rotation range, and it is possible to stably increase the power generation amount. Therefore, the variation in engine load can be reduced during "core speed operation", and the variation in engine rotation can be minimized to stabilize the idle operation. Next, in the present embodiment, the specifications of the ACG starter 1 described above, particularly the maximum generated torque related to the specifications, will be described.

C:\2D-C0DE\91-07\91107591.ptd 第18頁 575716 五、發明說明(15) ,之前顯示其==::塞=^ 生”述最大曲轴扭矩Tmax以上之扭矩於。曲_ι中必須產 疋引擎之起動性與驅動性二 態所示,於ACG起動機1直“ ^如本 似起動機!由於曲軸如之慣性 之構造中, 矩較大之大型起動气# \ 乍用,铋用驅動扭 ^ , k 1動馬達時,其加速性能會降低。 之位詈2 y本實施形態所示,引擎停止後曲軸逆轉至所定 之位置之引擎起動裝置神处轉至所疋 行程所需之助走時間加*, J = 達壓縮 往可更提昇,因而包含曲軸如之走回轉數比以 性力。 、u轉糸亦侍比較大之慣 圖13為顯示引擎回轉數Ne(實C: \ 2D-C0DE \ 91-07 \ 91107591.ptd Page 18 575716 V. Description of the Invention (15), which previously showed that == :: plug = ^ generates the torque above the maximum crankshaft torque Tmax. Qu_ The starting and driving characteristics of the engine must be shown in the two states, as shown in the ACG starter 1 "^ This is like a starter!" Due to the inertia structure of the crankshaft, the large starting gas with large moment # \ At first use, when the bismuth is used to drive the motor, its acceleration performance will decrease. Position 詈 2 y As shown in this embodiment, after the engine is stopped, the crankshaft reverses to a predetermined position, and the engine starting device needs to go to the desired stroke to increase the travel time plus *, J = compression can be further increased, so it includes The number of revolutions of the crankshaft is proportional to sexual force. , U turn 糸 also serve the relatively large habit. Figure 13 shows the engine rotation number Ne (actual

Tdrv(實線),包含曲轴之回轉系之 本身之駆動扭矩 及前述驅動扭矩Tdrv與慣性扭矩e Tlnej鏈線)以 線)之時間變化圖。 e之δ成扭矩Tadd(點 矩Τ:η! ί t : I ’如圖1 3所示’顯示於時間tmax時曲軸扭 > H / 仏❿,為使活塞跨越壓縮上死點,至 夕而要1· 3kgfm以上之驅動扭矩。因此, 芏 1需要最大發生扭矩為!. 3kgcm以上之大型已‘達之ACG起動機 ’本實施形態中引擎停止後便先將曲軸逆轉 之< 置,如圖13所示,下次之引擎起動時在達到壓縮行: C:\2D-00DE\91-07\9110759l.ptd 第19頁 575716 五、發明說明(16) '—— 之4引擎回轉數便可達到7 〇 〇至9 〇 〇 rpm。因此,如圖丨4所 示,包含曲軸201之回轉系之慣性扭矩Tine變大,因而八⑶ 起動棧1即使僅此發生驅動扭矩τ d r v,且其遠低於最大曲 軸扭矩Tmax,但其慣性扭矩Tine與驅動扭矩TdrV2合成扭 矩Tadd可超過前述最大曲軸扭矩Tmax(本實施形態為 1· 3kgfm)。亦即,ACG起動機1可成為小型輕量化。 但是,ACG起動機1中,在活塞更進行至壓縮行程以外 其所需要產生必須之曲軸扭矩1(31^,依據發明者等之 貫驗結果,其數值確認為相當於活塞跨越壓縮行程時所必 要之最大曲軸扭矩Tmax之大略20%。因此,本實施形態 中,ACG起動機1之最大發生扭矩希望至少為最大曲軸扭矩 Tmax之大略20%以上。 甚而,如本實施形態所示,若ACG起動機!與曲軸2〇1為 直結構造時,相對於引擎其ACG起動機i作為慣性質量之作 用。此慣性質量之值從加速時之驅動性等觀點來看,如本 貝施形悲所示’在最大曲軸扭矩為13kgfm左右之引擎, 經驗上認為慣性質量以28〜33kgfm為適當值。 圖1 5為顯示ACG起動機1之慣性質量與最大發生扭矩之關 係圖。慣性質量為28〜33kgcm之規格之ACG起動機}其最大 發生扭矩為〇· 5〜0· 8kgfm。此相當於最大曲軸扭矩以⑽之 大約4 0〜6 0 %,而慣性質量在此以上之a c G起動機1其引擎 之起動性雖然良好,但加速時其驅動性則降低。 從以上觀點,本實施形態中ACG起動機1係採用其最大發 生扭矩為最大曲轴扭矩Tmax之2〇至6〇%之小型起動馬達。Tdrv (solid line), which includes the time chart of the crankshaft's rotating torque itself and the aforementioned driving torque Tdrv and inertia torque e Tlnej chain line). The torque δ of e (point moment T: η! ί t: I 'as shown in Figure 1 3' is displayed at the time tmax crankshaft torque > H / 仏 ❿, in order to make the piston across the compression top dead center, to the evening A driving torque of 1 · 3kgfm or more is required. Therefore, 芏 1 needs to have a maximum torque of!. 3kgcm or more of a large ACG starter that has been reached. In this embodiment, after the engine is stopped, the crankshaft is reversed. As shown in Figure 13, when the next engine starts, it will reach the compressed line: C: \ 2D-00DE \ 91-07 \ 9110759l.ptd Page 19 575716 V. Description of the invention (16) '—— 4 engine revolutions It can reach 7000 to 900 rpm. Therefore, as shown in Figure 丨 4, the inertia torque Tine of the turning system including the crankshaft 201 becomes larger. Therefore, even if only the driving torque τ drv occurs in the starting stack 1, and It is far lower than the maximum crankshaft torque Tmax, but the combined torque Tadd of inertia torque Tine and driving torque TdrV2 can exceed the aforementioned maximum crankshaft torque Tmax (1.3 kgfm in this embodiment). That is, the ACG starter 1 can be reduced in size and weight. However, in the ACG starter 1, the piston is further advanced beyond the compression stroke. It is necessary to generate the necessary crankshaft torque 1 (31 ^), which is confirmed to be approximately 20% of the maximum crankshaft torque Tmax necessary when the piston spans the compression stroke according to the results of the inventors and others. Therefore, in this embodiment, It is desirable that the maximum torque of the ACG starter 1 is at least approximately 20% of the maximum crankshaft torque Tmax. Furthermore, as shown in this embodiment, if the ACG starter! Is made of a straight structure with the crankshaft 201, its ACG is relative to the engine. The starter i functions as an inertial mass. From the viewpoint of the driveability during acceleration, the value of the inertial mass, as shown by the Bebesch shape, 'the engine with a maximum crankshaft torque of about 13 kgfm, empirically believes that the inertial mass is 28 ~ 33kgfm is an appropriate value. Figure 15 shows the relationship between the inertia mass of ACG starter 1 and the maximum generated torque. ACG starter with specifications of 28 ~ 33kgcm inertia mass} its maximum generated torque is 0.5 · 0 · 8kgfm. This is equivalent to about 40 ~ 60% of the maximum crankshaft torque, and the ac G starter 1 with inertia mass above this has good engine startability, but its drive when accelerating Is reduced. From the above viewpoint, the present embodiment 1 ACG starter generator system using the maximum torque Tmax as the maximum torque of the crankshaft to 6〇 2〇% of small starter motor.

C:\2D-00DE\91-07\91107591.ptd 第20頁 575716 五、發明說明(17) 換吕之,A C G起動施 起動機1所直結之ώ之最大發生扭矩的選擇, 而做選擇。 軸20〗之慣性質量在其最適 發明之效果 依據本發明,為& & 速,可得比較大之;!;;到;縮行程之前’其 動扭矩之合力可達 ,、要此’丨貝性力與起 之最大發生扭矩比大曲軸扭矩,則即使起 M m kr ^ ^ m 取大曲軸扭矩為小之情形, 越Μ細灯私。因并 蚀π卢π站π 士 起動馬達比以往者可以小 使付在不致彳貝害起無卜 ^ ^ 欠動性下又可提昇驅動性之情 現之爭。 乃是依照該 範圍之上限 已被充分加 動馬達之驅 動馬達本身 活塞亦可跨 型化,因而 形成為可實 元件編號之說曰卩 1 起動機兼發電機(ACG 2 擺動裝 置 2, 蓄電池 3 後緩衝 器 3, ECU 4 底板部 5 轉向頭 6 底管 7 主管 8 座墊 9 減速機構 10 皮帶式 無段變速機C: \ 2D-00DE \ 91-07 \ 91107591.ptd Page 20 575716 V. Description of the invention (17) In other words, A C G starts the selection of the maximum torque generated directly by the starter 1 and makes the selection. The effect of the inertia mass of the shaft 20 in its most suitable invention is according to the present invention, which is & & speed, which can be relatively large;! ;; to; before the reduction stroke 'the resultant force of its dynamic torque is reachable, so to this'丨 Bearing force and the maximum occurrence torque ratio is larger than the crankshaft torque, even if the maximum crankshaft torque from M m kr ^ ^ m is taken as a small case, the more thin the light. Because of the parallel eclipse, the starting motor can be smaller than the previous one, so that it can be used to improve the driving performance without causing undue damage. According to the upper limit of the range, the drive motor itself has been fully driven. The piston itself can also be straddled, so it is formed as a real component number. 1 Starter and generator (ACG 2 swing device 2, battery 3 Rear bumper 3, ECU 4 Base plate part 5 Steering head 6 Bottom pipe 7 Main pipe 8 Seat cushion 9 Reduction mechanism 10 Belt-type stepless speed changer

C:\2D-G0DE\91-07\91107591.ptd 第21頁 575716C: \ 2D-G0DE \ 91-07 \ 91107591.ptd Page 21 575716

五、發明說明(18) 11 手把 12 前叉 13 手把覆蓋 14 空氣濾清器 15 支撐架 16 連桿構件 17 汽化器 18 懸掛支架 19 吸氣管 21 V型皮帶,點火線圈 22 火星塞 23 節流感測器 24 燃油感測器 25 閥座開關 26 怠速開關 27 冷卻水溫感測器 28 感測器盒 29 轉子角度感測器(磁極感測器) 30 點火脈衝器 31 基板 32 配線導線 33 磁性環 34 起動繼電器 35 起動開關 C:\2D-CODE\91-07\91107591.ptd 第22頁 575716V. Description of the invention (18) 11 Handlebar 12 Front fork 13 Handlebar cover 14 Air filter 15 Support frame 16 Connecting rod member 17 Carburetor 18 Suspension bracket 19 Suction pipe 21 V-belt, Ignition coil 22 Mars plug 23 Section Flu sensor 24 Fuel sensor 25 Valve seat switch 26 Idle speed switch 27 Cooling water temperature sensor 28 Sensor box 29 Rotor angle sensor (magnetic pole sensor) 30 Ignition pulsator 31 Substrate 32 Wiring lead 33 Magnetic Ring 34 Start relay 35 Start switch C: \ 2D-CODE \ 91-07 \ 91107591.ptd Page 22 575716

36 停 止 開 關 37 停 止 開 關 38 待 機 指 示 器 39 油 指 示 器 40 速 度 感 測 器 42 頭 燈 43 定 時 開 關 44 主 保 險 絲 45 主 開 關 46 蓄 電 池 電 壓 判 別 部 47 負 載 比 設 定 部 48 引 擎 回 轉 數 判 別 部 49 延 遲 角 量 設 定 部 50 靜 子 51 洩 壓 驅 動 部 52 引 擎 回 轉 數 判 別 部 60 外 轉 子 6 0a 外 轉 子 之 轂 63 洩 壓 線 圈 72 負 載 比 設 定 部 73 階 段 判 別 部 74 階 段 通 過 時 間 檢 測部 75 逆 轉 控 制 部 80 馬區 動 器 第23頁 C:\2D-CODE\91-07\91107591.ptd 575716 五、發明說明 (20) 100 調整器 201 曲軸 202 曲軸箱 20 2L 左曲軸箱 2 0 2R 右曲軸箱 208 轴承 209 軸承 210 皮帶驅動輪 210L 半個固定側皮帶輪 210R 半個可動側皮帶輪 210Ra 凸輪板滑動轂部 211 轂 212 V型皮帶 213 曲軸銷 215 凸輪板 215a 滑動件 216 乾式錘球 231 鏈輪 232 齒輪 246 螺栓 253 螺絲 279 螺栓 280 風扇 281 風扇蓋36 Stop switch 37 Stop switch 38 Standby indicator 39 Oil indicator 40 Speed sensor 42 Headlight 43 Timing switch 44 Main fuse 45 Main switch 46 Battery voltage determination section 47 Load ratio setting section 48 Engine rotation number determination section 49 Delay angle Volume setting section 50 Static child 51 Decompression drive section 52 Engine revolution number discriminating section 60 Outer rotor 6 0a Outer rotor hub 63 Decompression coil 72 Load ratio setting section 73 Phase discriminating section 74 Phase transit time detecting section 75 Reverse control section 80 Horse Zone actuator page 23 C: \ 2D-CODE \ 91-07 \ 91107591.ptd 575716 V. Description of the invention (20) 100 Adjuster 201 crankshaft 202 crankcase 20 2L left crankcase 2 0 2R right crankcase 208 bearing 209 Bearing 210 Belt drive wheel 210L Half fixed side pulley 210R Half movable side pulley 210Ra Cam plate sliding hub 211 Hub 212 V-belt 213 Crank pin 215 Cam plate 215a sliding Pieces 216 dry hammer ball 231 sprocket 232 gear 246 bolt 253 screw 279 bolt 280 fan 281 fan cover

11111111

C:\2D-00DE\91-07\91107591.ptd 第24頁 575716 五、發明說明 (21) 282 散熱器 300 全波整流橋式電路 400 發電控制部 500 起動控制部 700 回擺控制部 E 引擎 FW 前輪 RW 後輪C: \ 2D-00DE \ 91-07 \ 91107591.ptd Page 24 575716 V. Description of the invention (21) 282 Radiator 300 Full-wave rectifier bridge circuit 400 Power generation control unit 500 Start control unit 700 Swing control unit E Engine FW front wheel RW rear wheel

C:\2D-CODE\91-07\91107591.ptd 第25頁C: \ 2D-CODE \ 91-07 \ 91107591.ptd Page 25

3/J/lO 圖式簡單說明 動 輪車之全體側面 圖1為適用本發明之速克達型 圖。 圖2為沿著圖〗之擺動裝置之曲 圖3為圖2之部分放大圖。 之4面圖。 圖4為起動機兼發電機之控制 圖5為顯示圖4ECU之主要部分I塊圖。 圖6為回擺控制之流程圖。 方塊圖。 圖7(a)〜(c)為顯示曲軸角度盘 度之關係圖。 轴扭矩、階段、角速 圖8為引擎起動控制之曲軸扭矩變化。 圖9為洩壓驅動部之動作流程圖。 圖10為ACG發電控制處理之流程圖。 圖11為顯不ACG通雷控告丨昧籍贈 , 徑制可靜子線圈之相電流與轉子角 度感測裔之輸出之時序圖。 圖12為以引擎回轉數為參數之通電負載之圖表。 圖13為顯示引擎回轉數Ne以及曲軸扭矩Tcnk之時間變化 圖。 /圖14為顯不起動馬達之驅動扭矩Tdrv、包含曲軸之回轉 系之慣性扭矩Tine以及驅動扭矩Mrv與慣性扭矩Tine之合 成扭矩Tadd之時間變化圖。 圖1 5為顯示ACG起動機i之慣性質量與最大發生扭矩之關 係圖。3 / J / lO Brief description of the whole side view of the moving wheel Figure 1 is a diagram of a speed keda to which the present invention is applied. FIG. 2 is a curve of the swinging device along the figure. FIG. 3 is an enlarged view of a part of FIG. 2. Figure of 4 faces. Fig. 4 is a starter-generator control. Fig. 5 is a block diagram showing the main part I of the ECU of Fig. 4. Fig. 6 is a flowchart of swing-back control. Block diagram. Figures 7 (a) to (c) are diagrams showing the relationship between the crank angle and the degree of rotation. Shaft Torque, Phase, Angular Speed Figure 8 shows the change in crankshaft torque for engine start control. FIG. 9 is an operation flowchart of the pressure relief driving unit. FIG. 10 is a flowchart of ACG power generation control processing. Fig. 11 is a timing chart showing the ACG thunder control accusation, the phase current of the stator coil and the output of the rotor angle sensor. Figure 12 is a graph of the energized load with the number of engine revolutions as a parameter. Fig. 13 is a graph showing changes over time of the number of revolutions Ne of the engine and the torque Tcnk of the crankshaft. / FIG. 14 is a graph showing the time variation of the driving torque Tdrv of the starter motor, the inertia torque Tine of the slewing system including the crankshaft, and the combined torque Tadd of the driving torque Mrv and the inertia torque Tine. Fig. 15 is a graph showing the relationship between the inertial mass of the ACG starter i and the maximum generated torque.

第26頁 C:\2D-CODE\91-O7\91107591.ptdPage 26 C: \ 2D-CODE \ 91-O7 \ 91107591.ptd

Claims (1)

575716 六、申請專利範圍 轉至所 中,具 後,使 大發生 之最大 程以外 2 ·如 動馬達 直結之 3 ·如 動馬達 上。 4 ·如 其更具 定之基 力減低 種引擎起 定之位置 備有使曲 起動馬達 扭矩為引 曲軸扭矩 所必要之 申請專利 之最大發 曲軸之慣 申請專利 之最大發 申請專利 備有一機 準回轉數 5 ·如申請專利 活塞即將 至900rpm 申請專利 成壓縮行 其中在 7 0 0 rpm 6 ·如 即將達 90 0rpm 動裝置,其特徵為:引擎停止 ,以備下一次之曼曲轴逆 軸正轉以及逆轉之起動擎起動裝置 3之逆轉控制機構,前述起 :f 擎起動時為了使活塞跨越壓"之最 之大約60%以下,而夷私所必要 曲軸扭矩以上。 為活基進至壓縮行 ^圍第1項之引擎起動裝置,其 生扭矩之溪遲古;* 、甲月』边起 性質量成為盆最^ Ϊ依據使該起動馬達所 範圍適轮圍之上限而選擇。 轭圍苐1項之引擎起详 生扭矩為前述衷置/、中珂述起 边最大曲軸扭矩之大約20%以 ΞΐΓ/3項中任一項之引擎起動求置 以下之期間’將壓縮行程中之氣 範圍第1至3項中乜—K t 到達壓縮行程之前J、之引擎起動裝置, 。 仃%之則’弓丨擎回轉數為從 項之引擎起 私之别,引擎回轉“㈣舌基575716 VI. The scope of the patent application is transferred to the institute, and after it is made, the maximum occurrence of the major accident is beyond the limit. 2 · If the motor is directly connected to the 3 · If the motor is on. 4 · If it has a more fixed base force, the starting position of the engine is equipped with the crankshaft torque required for cranking the crankshaft torque. The largest crankshaft customary patent application. The largest patent application with a machine. · If the patent application piston is about to 900rpm, the patent application will be compressed. Among them, it is at 700 rpm 6 · If it is about to reach 900 rpm, the device is characterized by: the engine is stopped for the next MAN crankshaft reverse rotation and reverse rotation Starting the reversing control mechanism of the engine starting device 3, as described above: f In order to make the piston span pressure less than about 60% at the start of the engine, the crankshaft torque required is higher than that required. For the starting of the engine to the compression line ^, the engine starting device of item 1 has a torque-generating stream, Chi Gu; *, Jiayue "The edge quality has become the highest in the basin. Ϊ The basis for making the range of the starting motor suitable for the wheel. The upper limit is selected. The engine starting torque of item 1 of the yoke is approximately 20% of the maximum crankshaft torque mentioned above. The compression stroke will be set within the period below the start of the engine of any of the items ΞΐΓ / 3. Zhongqi range 1 to 3 Zhong 乜 —K t The engine starting device of J, before reaching the compression stroke.仃 % 之 则 ’bow 丨 engine rotation number is from the engine of the item to the private, the engine rotation"
TW91107591A 2001-05-09 2002-04-15 Engine starting apparatus TW575716B (en)

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CN1193166C (en) 2005-03-16
ES2208071B1 (en) 2005-06-16
ITTO20020349A0 (en) 2002-04-22
ES2208071A1 (en) 2004-06-01
JP2002332938A (en) 2002-11-22
JP4039604B2 (en) 2008-01-30
CN1384281A (en) 2002-12-11

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