JPS6140463A - Self-trigger type ignition device - Google Patents

Self-trigger type ignition device

Info

Publication number
JPS6140463A
JPS6140463A JP16082484A JP16082484A JPS6140463A JP S6140463 A JPS6140463 A JP S6140463A JP 16082484 A JP16082484 A JP 16082484A JP 16082484 A JP16082484 A JP 16082484A JP S6140463 A JPS6140463 A JP S6140463A
Authority
JP
Japan
Prior art keywords
magnetic pole
magnetic
magnet
ignition
yoke
Prior art date
Legal status (The legal status 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 status listed.)
Pending
Application number
JP16082484A
Other languages
Japanese (ja)
Inventor
Akio Nomichi
野路 明男
Mitsuru Nakamura
満 中村
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Honda Motor Co Ltd
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
Priority to JP16082484A priority Critical patent/JPS6140463A/en
Publication of JPS6140463A publication Critical patent/JPS6140463A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02PIGNITION, OTHER THAN COMPRESSION IGNITION, FOR INTERNAL-COMBUSTION ENGINES; TESTING OF IGNITION TIMING IN COMPRESSION-IGNITION ENGINES
    • F02P11/00Safety means for electric spark ignition, not otherwise provided for
    • F02P11/02Preventing damage to engines or engine-driven gearing

Abstract

PURPOSE:To prevent an engine from keeping up its reverse rotation in time of starting, by installing a magnet and a pair of magnetic poles at the rotor side, while installing the magnet and a pair of yokes at the fixed side, and setting each magnetic range of these magnetic poles to the specified size. CONSTITUTION:A magnet 4 and a pair of magnetic poles 3 are installed at the rotor side. A pair of yokes 7 having a leg each are installed at the fixed side. A coil 8 is rolled on each yoke. A magnetic range is formed into structure to which the next expression comes into existence thetaP1>thetaY1, thetaP2<=thetaY1, and in time of regular rotation, the side of a magnetic pole 3a wide in a magnetic range is constituted to be set to the inlet side of a leg part 7a of the yoke 7 while the side of a magnetic pole 3b narrow in the magnetic range to the outlet side of a leg part 7b, respectively. Thus, continuation of reverse rotation in time of engine starting is preventable.

Description

【発明の詳細な説明】 (技術分野) 本発明はエンジンの自己トリガ式点火装置に関し、特に
エンジン始動時の逆転を防止するようにした点火装置に
関する。
DETAILED DESCRIPTION OF THE INVENTION (Technical Field) The present invention relates to a self-trigger type ignition device for an engine, and more particularly to an ignition device designed to prevent reverse rotation when starting the engine.

(従来技術) 自己トリガ式の点火装置は従来の点火装置に比して信号
発電コイルを特別に必要としないこと、及び点火コイル
の1次側で発電機の電機子巻線を共用化することが出来
るためにその構造が簡単且つコンパクトである等の理由
から小型汎用のエンジン特に2サイクルエンジンの点火
装置として使用されている。
(Prior art) Compared to conventional ignition devices, a self-trigger type ignition device does not require a special signal generation coil, and the armature winding of the generator is shared on the primary side of the ignition coil. Because of its simple and compact structure, it is used as an ignition device for small general-purpose engines, especially two-stroke engines.

自己トリガ弐点火装置はエンジンの正転時には第5図(
a)に示すような波形の電圧Vaが出力され、負の電圧
−Vaが略ピーク点に達する点Pにおいて点火されるよ
うになされている。ところが、始動時の蹴り返し所謂ケ
ッチン等によりエンジンが逆転した場合には第5図(b
)に示すように前記電圧Vaと反対の波形の電圧vbと
なり、最初の負の電圧−vbの略ピーク点に達する端Q
で点火が行われ、この結果、エンジンの逆回転が継続さ
れることがある。
The self-trigger ignition system is activated when the engine is running normally as shown in Figure 5 (
A voltage Va having a waveform as shown in a) is output, and ignition is made at a point P where the negative voltage -Va reaches approximately the peak point. However, if the engine reverses due to kickback during startup, etc., the situation shown in Fig. 5 (b)
), the voltage vb has a waveform opposite to the voltage Va, and the end Q reaches approximately the peak point of the first negative voltage -vb.
ignition occurs, and as a result, the engine may continue to rotate in reverse.

このような始動時のエンジンの逆回転を防止するように
した点火装置として、ロータ側にマグネットと一対のポ
ールとを備え、固定側に、一対の脚部を有するU字状の
鉄芯と、その一方の脚部に挿着された点火コイルとを備
えて成るエンジンのトランジスタ点火装置の、他方の脚
部側の磁路中の磁気抵抗を大きくし、逆転時において点
火コイルの1次コイルに流れる電流を小さくし、点火不
能とするようにした点火装置が提案されている(実開昭
58−114458)。
An ignition device that prevents reverse rotation of the engine during startup is equipped with a magnet and a pair of poles on the rotor side, a U-shaped iron core with a pair of legs on the fixed side, The magnetic resistance in the magnetic path on the other leg side of an engine transistor ignition device comprising an ignition coil inserted into one leg of the engine is increased, and the primary coil of the ignition coil is An ignition device has been proposed in which the flowing current is reduced and ignition is disabled (Utility Model Application Laid-Open No. 58-114458).

しかしながら、上記点火装置は前記U字状の鉄芯の脚部
の磁気抵抗の調整が困難であり、組付性が悪い等の問題
がある。
However, the above-described ignition device has problems such as difficulty in adjusting the magnetic resistance of the legs of the U-shaped iron core and poor assemblability.

(発明の目的) 本発明は上述の点に鑑みてなされたもので、エンジンの
逆回転時に発生される電圧信号のうち、点火に寄与する
側の負の電圧を小さくして点火を不能とし、点火に寄与
しない側の負の電圧を大きくしてエネルギ放電を積極的
に行わせるようにし、逆転時の点火を継続させないよう
にすることを目的とする。
(Object of the Invention) The present invention has been made in view of the above points, and includes reducing the negative voltage on the side that contributes to ignition among the voltage signals generated when the engine rotates in reverse to disable ignition. The purpose is to increase the negative voltage on the side that does not contribute to ignition to actively discharge energy and prevent ignition from continuing during reverse rotation.

(発明の概要) 上記目的を達成するために本発明においては、ロータ側
に半径方向の磁界を発生するマグネットと、前記ロータ
の回転方向に対して前記マグネットの両側に配設された
一対の磁極とを備え、固定側に前記マグネット及び各磁
極と対向可能な一対の脚部を有するヨークと、該ヨーク
に巻回された点火コイルとを備えたエンジンの自己トリ
カ点火装置において、前記ロータの正転時に前記マグネ
ットに対して回転方向前方に位置する前記磁極の回転方
向に沿う磁極幅を回転方向後方に位置する前記磁極の回
転方向に沿う磁極幅よりも広くし、前記ロータの逆転時
に点火に寄与しないタイミングで点火信号のエネルギ放
電を行わせて点火を継続させないようにしたエンジンの
自己トリガ弐点火装置を提供するものである。
(Summary of the Invention) In order to achieve the above object, the present invention includes a magnet that generates a radial magnetic field on the rotor side, and a pair of magnetic poles arranged on both sides of the magnet with respect to the rotational direction of the rotor. A self-trigger ignition system for an engine, comprising: a yoke having a pair of legs on a fixed side that can face the magnet and each magnetic pole; and an ignition coil wound around the yoke. The width of the magnetic pole along the direction of rotation of the magnetic pole located forward in the direction of rotation with respect to the magnet is made wider than the width of the magnetic pole along the direction of rotation of the magnetic pole located at the rear of the direction of rotation, so that when the rotor reverses rotation, the width of the magnetic pole is greater than the width of the magnetic pole along the direction of rotation of the magnet. To provide a self-trigger ignition device for an engine that discharges the energy of an ignition signal at a timing that does not contribute to the continuation of ignition.

(発明の実施例) 以下本発明の一実施例を添附図面に基づいて詳述する。(Example of the invention) An embodiment of the present invention will be described in detail below with reference to the accompanying drawings.

第1図は本発明を適用した自己トリガ弐点火装置を示し
、エンジンのクランク軸1の一端に固着されたフライホ
イール2は例えばアルミニウム等の非磁性部材で形成さ
れ、その周面2aの所定箇所には周方向に沿う所定長さ
の円弧状の切欠2bが同心的に形成され、この切欠2b
には鉄等の磁性部材で形成された略U字状のヨーク3が
嵌装されている。ヨーク3の脚部3a、3bの中間には
マグネット4が配設され、一端面4aは当該ヨーク3の
対向面3cに圧着して固定されている。このマグネット
4は端面4a、4bが夫々磁極をなし、フライホイール
2の半径方向の磁界を発生する。従ちて、例えばマグネ
ット4の端面4bがN極、4bがS極である場合には、
ヨーク3の脚部3a、3bは共にS極となる。そこで、
以下脚部3a、3bを磁極と称する。これらのヨーク3
の各磁極3a、3bの周面及びマグネット4の周面4b
はフライホイール′2の周面2aと同一面をなしている
。また、フライホイール2はロータと兼用して使用され
る。
FIG. 1 shows a self-trigger ignition device to which the present invention is applied, in which a flywheel 2 fixed to one end of a crankshaft 1 of an engine is formed of a non-magnetic material such as aluminum, and a predetermined location on its circumferential surface 2a is shown. An arcuate notch 2b of a predetermined length along the circumferential direction is concentrically formed in the notch 2b.
A substantially U-shaped yoke 3 made of a magnetic material such as iron is fitted in the yoke 3 . A magnet 4 is disposed between the legs 3a and 3b of the yoke 3, and one end surface 4a is crimped and fixed to the opposing surface 3c of the yoke 3. This magnet 4 has end faces 4a and 4b each forming a magnetic pole, and generates a magnetic field in the radial direction of the flywheel 2. Therefore, for example, when the end surface 4b of the magnet 4 is the N pole and the end face 4b is the S pole,
The legs 3a and 3b of the yoke 3 both serve as south poles. Therefore,
The legs 3a and 3b are hereinafter referred to as magnetic poles. these yokes 3
The circumferential surface of each magnetic pole 3a, 3b and the circumferential surface 4b of the magnet 4
is flush with the circumferential surface 2a of the flywheel '2. Further, the flywheel 2 is also used as a rotor.

ヨーク3の磁極3a、3bの周方向の幅θP 1 rθ
P2は異なり、フライホイール2の矢印Cで示す正回転
方向に対してマグネット4の前方に位置する磁極3aの
幅θP1は当該マグネット4の後方に位置する磁極3b
の幅θP2よりも広く (θP1〉θP2)設定され、
これらの各磁極3a、3bとマグネット4との間には所
定幅θN1.θN2(=θN1)の空隙5,5′が設け
られている。
Circumferential width θP 1 rθ of magnetic poles 3a and 3b of yoke 3
P2 is different, and the width θP1 of the magnetic pole 3a located in front of the magnet 4 is different from the width θP1 of the magnetic pole 3b located in the rear of the magnet 4 with respect to the forward rotation direction shown by the arrow C of the flywheel 2.
is set wider than the width θP2 (θP1>θP2),
There is a predetermined width θN1 between each of these magnetic poles 3a, 3b and the magnet 4. Gaps 5 and 5' of θN2 (=θN1) are provided.

尚、これらの各空隙5,5“に非磁性部材を介装しても
よく、また空隙のままでもよい。
Incidentally, a nonmagnetic member may be interposed in each of these gaps 5, 5'', or the gaps may remain as they are.

イグニッションコイル6のヨーク7は略コ字状をなし、
両端面7a、7bはフライホイール2の周面2aと所定
の間隔で離隔対向して配設され、当該フライホイール2
の回転時にヨーク3の各磁極3a、3b及びマグネット
4と対向可能に配置されている。このヨーク7の中央部
7cにはコイル8が巻回されている。このヨーク7の各
脚部7a。
The yoke 7 of the ignition coil 6 has a substantially U-shape,
Both end surfaces 7a and 7b are arranged to face and be spaced apart from the circumferential surface 2a of the flywheel 2 at a predetermined interval.
The magnetic poles 3a and 3b of the yoke 3 and the magnet 4 are arranged so as to be able to face each other when the yoke 3 rotates. A coil 8 is wound around the central portion 7c of the yoke 7. Each leg 7a of this yoke 7.

7bのフライホイール2の回転方向に沿う幅θYllθ
Y2及びこれら両脚部7a、?b間の間隔θY。
Width θYllθ along the rotational direction of the flywheel 2 of 7b
Y2 and both legs 7a, ? The interval θY between b.

マグネット4の磁極4bの周方向の幅θM1及びヨーク
3の各磁極3a、3bの幅θpi、  θP2゜空隙5
,5“の幅θNl、  θN2は以下のように設定する
Circumferential width θM1 of magnetic pole 4b of magnet 4 and width θpi, θP2 of each magnetic pole 3a, 3b of yoke 3 Air gap 5
, 5" widths θNl and θN2 are set as follows.

即ち、 0758M           ・・・(1)θN+
 =θN2≦θYl =θY2・・・(2)上式(1)
、  (2)の条件において次式、−θP1〉θY1 
(=θY2)   ・・・(3)θP2≦θyt  (
=θY2)   ・・・(4)が成立′する構造に形成
する。
That is, 0758M...(1) θN+
=θN2≦θYl =θY2...(2) Above formula (1)
, Under the condition of (2), the following formula, -θP1>θY1
(=θY2) ... (3) θP2≦θyt (
=θY2)...A structure is formed in which (4) holds true.

しかも、前述したようにフライホイール2が矢印Cで示
す正回転時に磁極幅の広い磁極3a側をヨーク7の脚部
7aの入り側、磁極幅の狭い磁極3b側を脚部7bの抜
は側に構成する。
Moreover, as described above, when the flywheel 2 rotates in the forward direction shown by arrow C, the magnetic pole 3a side with the wide magnetic pole width is the entry side of the leg 7a of the yoke 7, and the magnetic pole 3b side with the narrow magnetic pole width is the exit side of the leg 7b. Configure.

このように構成することにより、フライホイール2の正
転時(矢印C方向)にはコイル7に第3図(a)に示す
ような波形の電圧Vaが発生され、磁極3aによる入り
側の正の電圧+Valが磁極3bによる抜は側の正の電
圧+Va3に比して大きくなる。また、フライホイール
2の逆転時にはコイル7に発生される電圧vbは上述と
は反対に第3図(f)に示すように変化し、磁極3aに
よる抜は側の負の電圧−Vb3が磁極3bによる入り側
の負の電圧−Vb、よりも大きくなる。
With this configuration, when the flywheel 2 rotates normally (in the direction of arrow C), a voltage Va having a waveform as shown in FIG. The voltage +Val becomes larger than the positive voltage +Va3 on the extraction side by the magnetic pole 3b. Further, when the flywheel 2 is reversed, the voltage vb generated in the coil 7 changes as shown in FIG. It becomes larger than the negative voltage -Vb on the input side.

ところで、2サイクルエンジンの逆回転可能な点火時期
ゾーンは一般的に第3図(’e )に斜線で示すように
BTDC130° (逆転方向)からATDC30”(
逆転方向)程度である。これに対して本発明の点火装置
では正転点火時期を第3図(d)に示すようにBTDC
20”とした場合、逆転の点火時期が第3図(e)、(
f)に示すようにATDC70° (逆転方向)前後と
なり、前記逆転可能点火時期ゾーンから大幅に外れる。
By the way, the ignition timing zone in which reverse rotation is possible for a two-stroke engine generally ranges from BTDC 130° (reverse direction) to ATDC 30" (as shown by diagonal lines in Fig. 3 ('e)).
(reverse direction). On the other hand, in the ignition system of the present invention, the forward rotation ignition timing is set to BTDC as shown in FIG. 3(d).
20", the reverse ignition timing is as shown in Figure 3(e), (
As shown in f), ATDC is around 70° (reverse direction), which is significantly outside the reversible ignition timing zone.

第2図は本発明の点火装置の回路構成を示し、イグニッ
ションコイル6のコイル8の1次コイル8aの各端は線
20.21に接続され、線20には点火ユニット10の
トランジスタTrt+Trzの各エミッタが接続され、
トランジスタ7r2のベースは線20.21間に直列接
続された分圧回路の抵抗R2,R3の接続点に接続され
る。トランジスタTrlのコレクタは線21に、トラン
ジスタTr2のコレクタは抵抗R1を介して線21に接
続され、トランジスタTr、のベースはトランジスタ’
l’r2のコレクタに接続される。コイル8の2次コイ
ル8bの一端は点火プラグ11の一端に接続され、該2
次コイル8b及び点火プラグ11の各他端は夫々線21
に接続され、該線21は接地される。
FIG. 2 shows the circuit configuration of the ignition device of the present invention, in which each end of the primary coil 8a of the coil 8 of the ignition coil 6 is connected to a line 20, 21, and each end of the primary coil 8a of the coil 8 of the ignition coil 6 is connected to a line 20, and each of the transistors Trt+Trz of the ignition unit 10 is connected to the line 20. emitter is connected,
The base of transistor 7r2 is connected to the connection point of resistors R2 and R3 of a voltage divider circuit connected in series between lines 20 and 21. The collector of the transistor Trl is connected to the line 21, the collector of the transistor Tr2 is connected to the line 21 via the resistor R1, and the base of the transistor Tr is connected to the line 21.
Connected to the collector of l'r2. One end of the secondary coil 8b of the coil 8 is connected to one end of the spark plug 11, and the second
The other ends of the secondary coil 8b and the spark plug 11 are connected to wires 21, respectively.
, and the line 21 is grounded.

次に作動を説明する。Next, the operation will be explained.

フライホイール2が正回転時において、コイル8の1次
コイル8aに電圧Vaが発生される際、先ずトランジス
タTr1のエミッタ側が正電位となる電圧+Va1 (
第3図(a))が発生された場合には、トランジスタ”
、+ Tr2は共にオフ状態となり点火ユニット10は
作動しない。次いでトランジスタTr、のコレクタ側が
正電位となる電圧−Va2となると、トランジスタTr
lがオンとなり、このトランジスタTrlを通してコイ
ル8の1次コイル8aに1次電流1a(第3図(b) 
)が流れる。トランジスタTr、のコレクタ・エミッタ
電位が徐々に上昇し、抵抗R2+R3で分圧されるトラ
ンジスタTr2のベース電圧がトリガ電圧に達すると、
トランジスタTr2がオンし、トランジスタTr1がオ
フとなり、コイル8の1次コイル8aの前記1次電流I
aが遮断(第3図(b))され、この結果、当該コイル
8の2次コイル8bに高電圧パルスVp(第3図(C)
)が誘導されて点火プラグ11にスパークを発生させる
。このときの点火時期ゾーンは第3図(d)に示すよう
にBTDC20°である。
When the flywheel 2 rotates forward, when the voltage Va is generated in the primary coil 8a of the coil 8, the voltage +Va1 (
If the situation shown in Fig. 3(a) occurs, the transistor "
, +Tr2 are both turned off, and the ignition unit 10 does not operate. Next, when the voltage -Va2 at which the collector side of the transistor Tr becomes a positive potential, the transistor Tr
Trl is turned on, and a primary current 1a (Fig. 3(b)
) flows. When the collector-emitter potential of the transistor Tr gradually rises and the base voltage of the transistor Tr2 divided by the resistors R2+R3 reaches the trigger voltage,
The transistor Tr2 is turned on, the transistor Tr1 is turned off, and the primary current I of the primary coil 8a of the coil 8 is
a is interrupted (FIG. 3(b)), and as a result, a high voltage pulse Vp (FIG. 3(C)) is applied to the secondary coil 8b of the coil 8.
) is induced to cause the spark plug 11 to generate a spark. The ignition timing zone at this time is BTDC 20° as shown in FIG. 3(d).

トランジスタTr1のエミッタ側が正電位となる電圧+
Va3  (第3図(a))となると、前述と同様に点
火ユニット10は不作動となる。
Voltage + at which the emitter side of transistor Tr1 has a positive potential
When Va3 (FIG. 3(a)) is reached, the ignition unit 10 becomes inoperative as described above.

さて、エンジン始動時にフライホイール2が逆回転して
コイル8の1次コイル8aに第3図(f)に示す電圧v
bが発生される際、トランジスタTr1のコレクタ側が
正電位となる電圧−V b tが発生されると、トラン
ジスタTr1がオンとなり、コイル8の1次コイル8a
に1次電流1b(第3図(g))が流れる。しかしなが
らこのときの電圧−vb、は低いためにトランジスタT
r2がオン。
Now, when the engine starts, the flywheel 2 rotates in reverse and the voltage V shown in FIG. 3(f) is applied to the primary coil 8a of the coil 8.
When voltage -V b t is generated such that the collector side of the transistor Tr1 has a positive potential, the transistor Tr1 is turned on and the primary coil 8a of the coil 8 is turned on.
A primary current 1b (FIG. 3(g)) flows through. However, since the voltage -vb at this time is low, the transistor T
r2 is on.

し得す、即ち、1次電流Ibが遮断する電圧レベルまで
達せず、2次コイル8bに高電圧が発生しない。次にト
ランジスタTrlのコレクタ側が正電位となる電圧−v
b3 (第3図(f))が発生されると、先ずトランジ
スタTr、がオンとなり1次コイル8aに1次電流Ib
が流れる。このとときの電圧=■b3はトランジスタT
r2をオンさせるに充分な電圧でなり、トランジスタT
r2がオンとなると、トランジスタTr、がオフとなり
、1次電流rbが遮断(第3図(g))され、2次コイ
ル8bに高電圧パルスVp’(第3図(h))が誘起さ
れ、点火ブラシ゛11にスパークを発生させる。このと
きの点火位置は第1図に示す磁極3aの抜は側の波形位
置であり、第2図(e)に示すようにATDC70°附
近となり逆転可能点火時期ゾーンから充分離れた位置で
あるため、逆転の可能性はない。
In other words, the voltage level at which the primary current Ib is cut off is not reached, and no high voltage is generated in the secondary coil 8b. Next, the voltage −v at which the collector side of the transistor Trl becomes a positive potential
When b3 (FIG. 3(f)) is generated, first the transistor Tr is turned on and the primary current Ib flows through the primary coil 8a.
flows. Voltage at this time = ■ b3 is the transistor T
The voltage is sufficient to turn on r2, and the transistor T
When r2 is turned on, the transistor Tr is turned off, the primary current rb is cut off (Fig. 3 (g)), and a high voltage pulse Vp' (Fig. 3 (h)) is induced in the secondary coil 8b. , causing the ignition brush 11 to generate a spark. The ignition position at this time is the waveform position on the side where the magnetic pole 3a is removed as shown in Fig. 1, and as shown in Fig. 2 (e), it is close to ATDC 70° and is sufficiently far from the reversible ignition timing zone. , there is no possibility of reversal.

第4図は本梵明の他の実施例を示し、フライホイール2
′を鉄等の強磁性部材で形成し、マグネット装着用切欠
2b’及び各磁極2c“、 2d“を一体に形成したも
のである。この場合、各磁極2c“。
FIG. 4 shows another embodiment of the present Bonmei, in which the flywheel 2
' is made of a ferromagnetic material such as iron, and the magnet mounting notch 2b' and the magnetic poles 2c'' and 2d'' are integrally formed. In this case, each magnetic pole 2c".

2d”を形成するために、各磁極2c“、 2d“の外
周面の半径rを段差をなす外周面2a“の半径r“より
も太き((r>r“)設定する。
2d'', the radius r of the outer circumferential surface of each magnetic pole 2c'', 2d'' is set to be larger ((r>r'') than the radius r'' of the outer circumferential surface 2a'' forming the step.

(発明の効果) 以上説明したように本発明によれば、ロータの正転時に
マグネットに対して回転方向前方に位置する磁極の回転
方向に沿う磁極幅を回転方向後方に位置する磁極の回転
方向に沿う磁極幅よりも広くし、ロータの逆転時に逆転
不可能な点火時期ゾーンで点火コイルのエネルギ放電を
積極的に行わせ、点火可能時期ゾーンでは点火を行わせ
ないようにしたので、エンジン始動時の逆回転の回転持
続を防止することができる。また磁極幅を変えるだけで
よく構成も簡単であり、fI!i1整箇所もなく組付性
の向上を図ることができる等の利点がある。
(Effects of the Invention) As explained above, according to the present invention, when the rotor rotates forward, the magnetic pole width along the rotational direction of the magnetic pole located in the front of the magnet in the rotational direction is changed in the rotational direction of the magnetic pole located in the rear of the rotational direction. When the rotor reverses, the ignition coil's energy is actively discharged in the ignition timing zone where it cannot be reversed, and ignition is not performed in the ignition timing zone where it is possible to start the engine. It is possible to prevent the clock from continuing to rotate in the opposite direction. In addition, the configuration is simple, just by changing the magnetic pole width, and fI! There are advantages such as there is no adjustment point and the ease of assembly can be improved.

【図面の簡単な説明】[Brief explanation of drawings]

第1図は本発明に係るエンジンの自己トリガ弐点火装置
の一実施例を示す構成図、第2図は点火回路の一例を示
す回路図、第3図は第2図に示す回路図のロータの正転
時及び逆転時の各部信号の波形を示すグラフ、第4図は
本発明の他の実施例を示す構成図、第5図は従来の自己
トリガ弐点火装置の電圧波形を示すグラフである。 1・・・クランク軸、2.2′・・・フライホイール、
3・・・ヨーク、4・・・マグネット、6・・・イグニ
ッションコイル、7・・・ヨーク、8・・・コイル、1
o・・・点火ユニット、11・・・点火プラグ。 出願人  本田技研工業株式会社 代理人  弁理士 渡 部 敏 音 間 長門侃二 第1図 5o    ′;1L127
FIG. 1 is a block diagram showing one embodiment of the self-trigger ignition device for an engine according to the present invention, FIG. 2 is a circuit diagram showing an example of an ignition circuit, and FIG. 3 is a rotor diagram of the circuit diagram shown in FIG. 2. FIG. 4 is a diagram showing the configuration of another embodiment of the present invention, and FIG. 5 is a graph showing voltage waveforms of a conventional self-trigger ignition device. be. 1... Crankshaft, 2.2'... Flywheel,
3...Yoke, 4...Magnet, 6...Ignition coil, 7...Yoke, 8...Coil, 1
o...Ignition unit, 11...Spark plug. Applicant Honda Motor Co., Ltd. Agent Patent Attorney Toshi Watanabe Otoma Kanji Nagato Figure 1 5o'; 1L127

Claims (1)

【特許請求の範囲】[Claims] 1、ロータ側に半径方向の磁界を発生するマグネットと
、前記ロータの回転方向に対して前記マグネットの両側
に配設された一対の磁極とを備え、固定側に前記マグネ
ット及び各磁極と対向可能な一対の脚部を有するヨーク
と、該ヨークに巻回された点火コイルとを備えたエンジ
ンの自己トリガ式点火装置において、前記ロータの正転
時に前記マグネットに対して回転方向前方に位置する前
記磁極の回転方向に沿う磁極幅を回転方向後方に位置す
る前記磁極の回転方向に沿う磁極幅よりも広くしたこと
を特徴とするエンジンの自己トリガ式点火装置。
1. A magnet that generates a radial magnetic field on the rotor side, and a pair of magnetic poles arranged on both sides of the magnet with respect to the rotational direction of the rotor, and the fixed side can face the magnet and each magnetic pole. In the self-trigger type ignition device for an engine, the engine includes a yoke having a pair of legs, and an ignition coil wound around the yoke. A self-trigger type ignition device for an engine, characterized in that a magnetic pole width along the rotational direction of the magnetic pole is wider than a magnetic pole width along the rotational direction of the magnetic pole located at the rear in the rotational direction.
JP16082484A 1984-07-31 1984-07-31 Self-trigger type ignition device Pending JPS6140463A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP16082484A JPS6140463A (en) 1984-07-31 1984-07-31 Self-trigger type ignition device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP16082484A JPS6140463A (en) 1984-07-31 1984-07-31 Self-trigger type ignition device

Publications (1)

Publication Number Publication Date
JPS6140463A true JPS6140463A (en) 1986-02-26

Family

ID=15723200

Family Applications (1)

Application Number Title Priority Date Filing Date
JP16082484A Pending JPS6140463A (en) 1984-07-31 1984-07-31 Self-trigger type ignition device

Country Status (1)

Country Link
JP (1) JPS6140463A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1989001570A1 (en) * 1987-08-13 1989-02-23 Komatsu Zenoah Co. Reversibly rotating engine
ES2111438A2 (en) * 1993-05-24 1998-03-01 Honda Motor Co Ltd Reverse preventer for internal combustion engine
US5962939A (en) * 1997-01-22 1999-10-05 Honda Giken Kogyo Kabushiki Kaisha Outer-rotor type engine-operated generator
JP2019218920A (en) * 2018-06-21 2019-12-26 東洋電装株式会社 Ignition device

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5341682U (en) * 1976-09-14 1978-04-11
JPS5569756A (en) * 1978-11-01 1980-05-26 Outboard Marine Corp Capacitorrdischarged ignition system

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5341682U (en) * 1976-09-14 1978-04-11
JPS5569756A (en) * 1978-11-01 1980-05-26 Outboard Marine Corp Capacitorrdischarged ignition system

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1989001570A1 (en) * 1987-08-13 1989-02-23 Komatsu Zenoah Co. Reversibly rotating engine
US5161489A (en) * 1987-08-13 1992-11-10 Komatsu Zenoah Company Reversible engine
ES2111438A2 (en) * 1993-05-24 1998-03-01 Honda Motor Co Ltd Reverse preventer for internal combustion engine
US5962939A (en) * 1997-01-22 1999-10-05 Honda Giken Kogyo Kabushiki Kaisha Outer-rotor type engine-operated generator
JP2019218920A (en) * 2018-06-21 2019-12-26 東洋電装株式会社 Ignition device
CN110630423A (en) * 2018-06-21 2019-12-31 东洋电装株式会社 Ignition device
CN110630423B (en) * 2018-06-21 2022-04-29 东洋电装株式会社 Ignition device

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