JPH0423108B2 - - Google Patents

Info

Publication number
JPH0423108B2
JPH0423108B2 JP58163134A JP16313483A JPH0423108B2 JP H0423108 B2 JPH0423108 B2 JP H0423108B2 JP 58163134 A JP58163134 A JP 58163134A JP 16313483 A JP16313483 A JP 16313483A JP H0423108 B2 JPH0423108 B2 JP H0423108B2
Authority
JP
Japan
Prior art keywords
weight
center
shaft
rod
straight line
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.)
Expired - Lifetime
Application number
JP58163134A
Other languages
Japanese (ja)
Other versions
JPS6056171A (en
Inventor
Seiichi Seya
Masao Oomori
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.)
Hitachi Ltd
Original Assignee
Hitachi 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 Hitachi Ltd filed Critical Hitachi Ltd
Priority to JP16313483A priority Critical patent/JPS6056171A/en
Publication of JPS6056171A publication Critical patent/JPS6056171A/en
Publication of JPH0423108B2 publication Critical patent/JPH0423108B2/ja
Granted 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
    • F02P5/00Advancing or retarding ignition; Control therefor
    • F02P5/04Advancing or retarding ignition; Control therefor automatically, as a function of the working conditions of the engine or vehicle or of the atmospheric conditions
    • F02P5/05Advancing or retarding ignition; Control therefor automatically, as a function of the working conditions of the engine or vehicle or of the atmospheric conditions using mechanical means
    • F02P5/06Advancing or retarding ignition; Control therefor automatically, as a function of the working conditions of the engine or vehicle or of the atmospheric conditions using mechanical means dependent on engine speed

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • High-Pressure Fuel Injection Pump Control (AREA)

Description

【発明の詳細な説明】 〔発明の利用分野〕 本発明は、自動車用配電器のガバナ進角装置に
関するものである。
DETAILED DESCRIPTION OF THE INVENTION [Field of Application of the Invention] The present invention relates to a governor advance device for a power distribution device for an automobile.

〔発明の背景〕[Background of the invention]

第1図は実公昭42−12898号公報に見られるよ
うな一般に知られている従来のガバナ進角装置の
平面図を示し、1はシヤフトであり、シヤフト1
にはウエイト取付台6が嵌着固定され、ウエイト
取付台6にはシヤフト1を中心にウエイト支軸
2,3及びばね掛け4,5が固定されている。
7,8はウエイトでそれぞれ一端側をウエイト支
軸2,3に回動自在に支持され、他端側には第
1、第2ロツド9,10がそれぞれ植立されてい
る。第1、第2ロツド9,10は回転磁極(図示
せず)を伴なつたロータシヤフト11と一体に固
定されているタイミングレバー12にそれぞれ形
成された矩形状の第1、第2長溝穴13,14に
それぞれ嵌入されている。第1、第2長溝穴1
3,14はその長手方向が半径方向となる位置に
開口されている。第2図は横軸にエンジン回転数
をとり縦軸に点火進角をとつて示した進角特性説
明図である。15は第2図の進角特性の実線の曲
線Dの進角度零の始点Aより作用する第1スプリ
ング、16は中間のB点より第1スプリング15
と共同して作用する第2スプリングであり、それ
ぞればね掛け4,5に一端を固定され他端を第
1、第2ウエイト7,8に固定されている。尚、
矢印Hは回転方向(進角)である。
FIG. 1 shows a plan view of a generally known conventional governor advance device as seen in Japanese Utility Model Publication No. 42-12898, in which 1 is a shaft;
A weight mount 6 is fitted and fixed to the weight mount 6, and weight support shafts 2, 3 and spring hooks 4, 5 are fixed to the weight mount 6 around the shaft 1.
Weights 7 and 8 are rotatably supported at one end by weight support shafts 2 and 3, and first and second rods 9 and 10 are installed at the other end, respectively. The first and second rods 9 and 10 are rectangular first and second slotted holes 13 respectively formed in a timing lever 12 which is integrally fixed to a rotor shaft 11 with rotating magnetic poles (not shown). , 14, respectively. First and second long slot holes 1
3 and 14 are opened at positions where the longitudinal direction thereof is the radial direction. FIG. 2 is an explanatory diagram of the advance angle characteristic, with the horizontal axis representing the engine speed and the vertical axis representing the ignition advance angle. 15 is the first spring that acts from the start point A of the advance angle of zero on the solid line curve D of the advance angle characteristic in FIG. 2, and 16 is the first spring 15 that acts from the intermediate point B.
This is a second spring that acts in cooperation with the spring hooks 4 and 5, and has one end fixed to the spring hooks 4 and 5, and the other end fixed to the first and second weights 7 and 8, respectively. still,
Arrow H indicates the rotation direction (advanced angle).

上記の構造において、エンジンの低速回転時の
角加速度が上死点の手前でマイナスになつたと
き、ロータシヤフト11は、慣性により第1、第
2長溝穴13,14を介し第1、第2ロツド9,
10に第1長溝穴13の矩形状の長手方向の内壁
(第2ロツド10側は図示せず)より90度方向の
第1ウエイト7の回転により第1ロツド9が押圧
される方向に力Fを作用させ第1、第2ウエイト
7,8はモーメントF.lで開かれることになる。
このため、第2図の進角特性の二点鎖線Eに示す
ように過進角現象が発生しノツキングゾーンにか
かる不具合を起こす場合がある。また、従来もガ
バナの過進角に対して実公昭42−12898のように
一部考慮が払われているが、低速時に対しては不
十分であつた。
In the above structure, when the angular acceleration of the engine during low-speed rotation becomes negative before the top dead center, the rotor shaft 11 moves to the first and second slots via the first and second slotted holes 13 and 14 due to inertia. Rod 9,
10, a force F is applied in the direction in which the first rod 9 is pressed by the rotation of the first weight 7 in the 90 degree direction from the rectangular longitudinal inner wall of the first slotted hole 13 (the second rod 10 side is not shown). , the first and second weights 7 and 8 are opened by a moment Fl.
For this reason, an over-advanced angle phenomenon may occur, as shown by the two-dot chain line E of the advance angle characteristic in FIG. 2, and a problem related to the knocking zone may occur. In addition, some consideration has been given to the overadvance angle of the governor in the past, as in Publication of Utility Model Publication No. 12898/1973, but this was insufficient for low speeds.

特開昭53−90537号公報には、回転方向にタイ
ミングレバー長穴をあける角度Eだけ傾けた装置
の例が記載されているが、エンジン低速時のトル
ク変動に伴う過進角については考慮されていなか
つた。また、実公昭46−8259号公報にも、タイミ
ングレバー長穴を回転方向にある角度だけ傾けた
装置の例が記載されているが、エンジン低速時の
トルク変動に伴う過進角の抑制については考慮さ
れていなかつた。
Japanese Patent Laid-Open No. 53-90537 describes an example of a device in which the timing lever is tilted by an angle E in which an elongated hole is drilled in the rotation direction, but overadvance due to torque fluctuations at low engine speeds is not taken into consideration. I wasn't there. In addition, Japanese Utility Model Publication No. 46-8259 also describes an example of a device in which the elongated hole of the timing lever is tilted by a certain angle in the direction of rotation. It wasn't taken into account.

〔発明の目的〕[Purpose of the invention]

本発明に上記の状態に鑑みなされたものであ
り、エンジンの低速時に発生し易いトルク変動に
よる過進角を防止できるガバナ進角装置を提供す
ることを目的としたものである。
The present invention has been developed in view of the above-mentioned situation, and it is an object of the present invention to provide a governor advance device that can prevent overadvance due to torque fluctuations that tend to occur when the engine runs at low speeds.

〔発明の概要〕[Summary of the invention]

本発明は、往復動エンジンで駆動されるシヤフ
トに固定されたウエイト取付台上の上記シヤフト
軸心周囲に植立された2本のウエイト支軸と、該
ウエイト支軸にそれぞれ一端側を回動自在に支持
され他端側にそれぞれ第1、第2ロツドが植立さ
れた第1ウエイト及び第2ウエイトと、該第1ウ
エイトに一端が連結され他端が上記ウエイト取付
台に連結され回転数−点火進角曲線の進角零の始
点から前記両連結点間に引張力を作用するように
形成された第1スプリングと、上記第2ウエイト
に一端が連結され他端が上記ウエイト取付台に連
結され上記第1スプリングに共同して前記両連結
点間に引張力を作用するように形成された第2ス
プリング上記シヤフトに遊嵌されたロータシヤフ
トに固定され長手方向をほぼ半径方向として開口
された第1長溝穴及び第2長溝穴を有し該第1長
溝穴、第2長溝穴にそれぞれ上記第1、第2ロツ
ドを該第1長溝穴、第2長溝穴の長手方向壁面に
摺動可能に遊嵌させたタイミングレバーとを設け
たガバナ進角装置において、前記第1ウエイトを
軸支するウエイト支軸は、エンジン停止状態近傍
での前記第1ロツドの中心を通り前記第1長溝穴
の長手方向壁面のうちのシヤフト回転方向後側の
壁面に垂直な直線に平行で前記第1ロツドのシヤ
フト側外周面に接する直線の延長線上に配置され
ていることと、前記第1ロツドが遊嵌されている
上記第1長溝穴内の位置はエンジン停止状態での
該第1ロツドと上記第1長溝穴の長手方向壁面の
うちのシヤフト回転方向前側の壁面の間にギヤツ
プgが形成される位置であることと、上記第2ス
プリングは、回転数−点火進角曲線の中間の点か
ら前記両連結点間に引張力を作用するように形成
されたものであることと、上記シヤフトの中心か
ら上記第1、第2ウエイトの重心までの半径がそ
れぞれ最大飛開状態で等しく形成されていること
と、上記シヤフトの中心と上記第1ウエイトを軸
支するウエイト支軸の中心とを結ぶ直線が該ウエ
イト支軸の中心と第1ロツドの中心とを結ぶ直線
となす角raと、上記シヤフトの中心と上記第2ウ
エイトを軸支するウエイト支軸の中心とを結ぶ直
線が該ウエイト支軸の中心と第2ロツドの中心と
を結ぶ直線とをなす角rbとの関係がra<rbである
ことと、前記第1長溝穴の長手方向壁面の外周側
端部と内周側端部を結ぶ直線は、前記シヤフトの
中心と第1ロツドの中心を結ぶ直線に平行かつ前
記内周側端部を通る直線に対し外周側端部が回転
方向前方に離れる方向に傾斜し、第2長溝穴の長
手方向壁面の外周側端部と内周側端部を結ぶ直線
は、前記シヤフトの中心と第1ロツドの中心を結
ぶ直線に平行かつ前記内周側端部を通る直線に対
し外周側端部が回転方向後方に離れる方向に傾斜
していることとを特徴とする。
The present invention includes two weight spindles installed around the axis of the shaft on a weight mounting base fixed to a shaft driven by a reciprocating engine, and a weight spindle that rotates at one end of each of the weight spindles. A first weight and a second weight that are freely supported and have first and second rods respectively planted on the other end side, one end of which is connected to the first weight and the other end of which is connected to the weight mounting base, and the rotation speed is adjusted. - a first spring formed to apply a tensile force between the two connection points from the start point of zero advance of the ignition advance curve; one end connected to the second weight and the other end connected to the weight mount; A second spring is connected to the first spring and is formed to apply a tensile force between the two connection points; the second spring is fixed to the rotor shaft loosely fitted to the shaft, and is opened with the longitudinal direction being substantially the radial direction; The first and second rods are slid onto the longitudinal wall surfaces of the first and second slotted holes, respectively. In the governor advance device, which is provided with a timing lever that can be loosely fitted, a weight support shaft that pivotally supports the first weight passes through the center of the first rod when the engine is in a stopped state, and is connected to the first slotted hole. The first rod is parallel to a straight line perpendicular to the rear wall in the shaft rotation direction of the longitudinal wall surface and is in contact with the shaft-side outer peripheral surface of the first rod, and the first rod is free. The position in the first slotted hole where the rod is fitted is a position where a gap g is formed between the first rod and the front wall in the direction of shaft rotation among the longitudinal wall surfaces of the first slotted hole when the engine is stopped. and the second spring is formed so as to apply a tensile force between the two connection points from a point in the middle of the rotation speed-ignition advance angle curve; The radii to the centers of gravity of the first and second weights are the same in the maximum flying state, and the straight line connecting the center of the shaft and the center of the weight support shaft that supports the first weight is The angle ra formed by the straight line connecting the center of the weight support shaft and the center of the first rod and the straight line connecting the center of the shaft and the center of the weight support shaft that pivotally supports the second weight is the weight support shaft. The relationship between the angle r b formed by the straight line connecting the center of the rod and the center of the second rod is r a < r b , and the outer peripheral end of the longitudinal wall surface of the first slot and the inner peripheral side The straight line connecting the ends is parallel to the straight line connecting the center of the shaft and the center of the first rod, and is inclined in a direction in which the outer end is separated forward in the rotational direction with respect to the straight line passing through the inner end. A straight line connecting the outer peripheral end and the inner peripheral end of the longitudinal wall surface of the two long slots is parallel to the straight line connecting the center of the shaft and the center of the first rod, and with respect to a straight line passing through the inner peripheral end. It is characterized in that the outer peripheral side end portion is inclined in a direction away from the rear in the rotational direction.

〔発明の実施例〕[Embodiments of the invention]

以下本発明のガバナ進角装置を実施例を用い従
来と同部品は同符号で示し同部分の構造の説明は
省略し第3図により説明する。第3図は平面図を
示す。タイミングレバー12の矩形の第1長溝穴
13は、その長手方向をタイミングレバー12の
ほぼ半径方向として形成され、該長手方向壁面の
外周側端部と内周側端部を結ぶ直線は、前記シヤ
フト1の中心と第1ロツド9の中心を結ぶ直線に
平行かつ前記内周側端部を通る直線に対し、外周
側端部が回転方向前方に離れる方向に角度αだけ
傾いている。
Hereinafter, the governor advance device of the present invention will be explained with reference to FIG. 3 using an embodiment, in which the same parts as those in the conventional art are denoted by the same reference numerals, and the explanation of the structure of the same parts will be omitted. FIG. 3 shows a plan view. The rectangular first long slot 13 of the timing lever 12 is formed with its longitudinal direction being substantially the radial direction of the timing lever 12, and a straight line connecting the outer circumferential end and the inner circumferential end of the longitudinal wall surface is defined by the shaft. With respect to a straight line parallel to the straight line connecting the center of the rod 1 and the center of the first rod 9 and passing through the inner end, the outer end is inclined by an angle α in a direction away from the front in the rotational direction.

一方、タイミングレバー12の矩形の第2長溝
穴14は、その長手方向をタイミングレバー12
のほぼ半径方向として形成され、該長手方向壁面
の外周側端部と内周側端部を結ぶ直線は、前記シ
ヤフト1の中心と第2ロツド10の中心を結ぶ直
線に平行かつ前記内周側端部を通る直線に対し、
外周側端部が回転方向後方に離れる方向に角度β
だけ傾いていて、前記第1長溝穴13とは非対象
になつている。
On the other hand, the rectangular second long slot 14 of the timing lever 12 has its longitudinal direction aligned with the timing lever 12.
The straight line connecting the outer peripheral end and the inner peripheral end of the longitudinal wall surface is parallel to the straight line connecting the center of the shaft 1 and the center of the second rod 10, and For a straight line passing through the end,
Angle β in the direction in which the outer peripheral end moves away from the rear in the rotational direction.
, and is asymmetrical to the first slotted hole 13 .

またエンジン停止時において、直径dなる第1
ロツド9の第1長溝穴13内における遊嵌位置
は、該第1ロツド9が接する第1長溝穴13の回
転方向後方の長手方向壁面(点P)に垂直な直線
に平行でかつ第1ロツド9のシヤフト1側外周面
に接する直線の延長線がウエイト支軸2に交叉
し、該延長線とウエイト支軸2の中心を通つて該
延長線に垂直な直線の交点と、該垂直な直線のウ
エイト支軸2の外周面上の点との距離がΔLとな
る位置である。またエンジン停止時において、第
1ロツド9の第1長溝穴13内における遊嵌位置
は、上記条件に加え、該第1ロツド9の外周面と
長方形の第1長溝穴13の内周側内壁(幅方向壁
面のうち、シヤフト1に近い側)の間にギヤツプ
Gが、第1ロツド9の外周面と前記第1長溝穴1
3の回転方向前方の長手方向壁面の間にギヤツプ
gがそれぞれ形成され、回転方向後方の長手方向
壁面には点Pで接する位置となつている。
Also, when the engine is stopped, the first
The loosely fitted position of the rod 9 in the first slotted hole 13 is parallel to a straight line perpendicular to the rear longitudinal wall surface (point P) in the rotational direction of the first slotted hole 13 with which the first rod 9 is in contact. 9, an extension of a straight line touching the outer peripheral surface of the shaft 1 side intersects the weight support shaft 2, and the intersection of the extension line and a straight line passing through the center of the weight support shaft 2 and perpendicular to the extension line, and the perpendicular straight line. This is the position where the distance from the point on the outer peripheral surface of the weight support shaft 2 is ΔL. In addition to the above conditions, when the engine is stopped, the loosely fitted position of the first rod 9 in the first slotted hole 13 is determined by the outer circumferential surface of the first rod 9 and the inner wall of the rectangular first slotted hole 13 ( A gap G is provided between the outer circumferential surface of the first rod 9 and the first slotted hole 1 (the side closer to the shaft 1 among the widthwise wall surfaces).
A gap g is formed between the front longitudinal wall surfaces of No. 3 in the rotational direction, and is in contact with the rear longitudinal wall surface in the rotational direction at a point P.

上記の構造においてその作用を説明すると、比
較的大きな慣性モーメントを有するロータシヤフ
ト(図示しない配電子を含む)11が、角加速度
が上死点の手前でマイナスになる加速度を受けた
とき、タイミングレバー12の第1長溝穴13よ
り第1ロツド9を介して作用する力Faはウエイ
ト支軸2の中心より腕の長さaのところに作用す
る。一方第2長溝穴14側はFbの力で腕の長さ
bの位置に作用する。そして、Fa・aのモーメ
ントは第1図のF・lのモーメントより少ないこ
とは明らかである。即ち、エンジン低速時(第1
ロツド9がエンジン停止時の位置近傍にあると
き)にタイミングレバー12から第1ロツド9を
介して第1ウエイト7に作用する力Faの中心線
が、ウエイト支軸2の表面から0.5d−ΔLしか離
れておらず(0.5d<ΔLのときは、力Faの中心線
はウエイト支軸2の表面より内側になる)、該力
Faは第1ウエイト7をウエイト支軸2の周囲に
回転させるようにすると同時に、該第1ウエイト
7をウエイト支軸2に押しつけて該第1ウエイト
7とウエイト支軸2の間の摩擦力を高める。従つ
てタイミングレバー12から第1ロツド9を介し
て第1ウエイト7に作用する力Faによる第1ウ
エイト7の回転(飛開)が抑制され、エンジン低
速回転時の角加速度が上死点の手前てマイナスに
なるときの角加速度変化による過進角が阻止され
る。
To explain its operation in the above structure, when the rotor shaft (including the not-shown distribution arm) 11, which has a relatively large moment of inertia, receives an acceleration whose angular acceleration becomes negative before the top dead center, the timing lever The force Fa acting through the first rod 9 from the first long slot 13 of 12 acts at a distance a of the arm from the center of the weight support shaft 2. On the other hand, on the second long slot 14 side, the force Fb acts at a position at arm length b. It is clear that the moment of Fa·a is smaller than the moment of F·l in FIG. That is, at low engine speed (first
When the rod 9 is near the position when the engine is stopped, the center line of the force Fa acting on the first weight 7 from the timing lever 12 via the first rod 9 is 0.5d-ΔL from the surface of the weight support shaft 2. (When 0.5d<ΔL, the center line of force Fa is inside the surface of weight support shaft 2), and the force
Fa causes the first weight 7 to rotate around the weight support shaft 2, and at the same time presses the first weight 7 against the weight support shaft 2 to reduce the frictional force between the first weight 7 and the weight support shaft 2. enhance Therefore, the rotation (jump) of the first weight 7 due to the force Fa acting on the first weight 7 from the timing lever 12 via the first rod 9 is suppressed, and the angular acceleration when the engine rotates at low speed is reduced to just before top dead center. Over-advancing due to changes in angular acceleration when the value becomes negative is prevented.

また、エンジン低速回転時のピストン上死点手
前で、角加速度が負になり、タイミングレバー
(及びロータシヤフト)が慣性で回転して該タイ
ミングレバーによつて第1ロツドが押されても、
該第1ロツドと第1長溝穴の回転方向側長手方向
壁面の間にギヤツプgがあるので、タイミングレ
バーによつて押された該第1ロツドが前記第1長
溝穴の回転方向側長手方向壁面に接触してタイミ
ングレバーが回動してさらにロータシヤフト11
が回動するのが避けられる。
Furthermore, even if the angular acceleration becomes negative before the top dead center of the piston when the engine is rotating at low speed, the timing lever (and rotor shaft) rotates due to inertia, and the first rod is pushed by the timing lever.
Since there is a gap g between the first rod and the longitudinal wall surface on the rotational direction side of the first slotted hole, the first rod pushed by the timing lever touches the longitudinal wall surface on the rotational direction side of the first slotted hole. The timing lever rotates upon contact with the rotor shaft 11.
rotation can be avoided.

従来のガバナ進角装置では、静止状態では、タ
イミングレバーの二つの長溝穴のシヤフト側の壁
面にそれぞれのロツドが接触するような構成にな
つているが、実際には、ガバナ進角装置の各部品
の寸法ばらつきにより、第1ロツド9が第1長溝
穴で接触したり、あるいは第2ロツド10が第2
長溝穴で接触したりして静止状態におけ第1ロツ
ドの位置が不安定であり、過進角の要因となつて
いた。前記ギヤツプGを設けたことにより、静止
状態では、第1スプリング15によつて第1ウエ
イトが引き付けられると、タイミングレバー12
が時計周り方向に回転し、常に、第1ロツド9よ
りもさきに第2ロツド10が長溝穴の壁面に当接
し、タイミングレバー12の位置が安定的に定ま
る。
In a conventional governor advance device, when the lever is at rest, each rod is in contact with the shaft-side wall of the two long slot holes in the timing lever, but in reality, each rod in the governor advance device Due to dimensional variations in the parts, the first rod 9 may come into contact with the first long slot, or the second rod 10 may come into contact with the second slot.
The position of the first rod was unstable in a stationary state due to contact in the long slot, which caused overadvance. By providing the gap G, in a stationary state, when the first weight is attracted by the first spring 15, the timing lever 12
rotates clockwise, and the second rod 10 always comes into contact with the wall of the slotted hole before the first rod 9, so that the position of the timing lever 12 is stably determined.

そして、第3図において、第1、第2長溝穴1
3,14を非対称に図示したが、βをαに対し向
きと角度を同一にしてもよいことは勿論である。
しかし、第1長溝穴13、第2長溝穴14ともα
の値にすると横軸にエンジン回転数をとり縦軸に
点火進角をとつて示した第4図の破線で示す如く
特性のわん曲が大きくなる。また、曲線Dの戻り
のときのおくれを生じるヒステリシスが増加する
欠点を生じる。従つて、一般には、α≠βがよく
回転変動、即ち、上記の角加速度が上死点の手前
でマイナスになつたときに対する過進角抑止作用
は第1長溝穴13側で決まるため、特に差は生じ
ない。また、エンジンのトルク変動が少ない場合
は、第1、第2ウエイト7,8はタイミングレバ
ー12の第1、第2長溝穴13,14が非対称で
も遠心力fが働き飛開は従来レベルで行われる。
そして、力Faの作用する腕の長さaはウエイト
支軸2の半径より小であれば更によく、第2長溝
穴14側では第2ロツド10は回転方向内壁側の
Q点で接するるようになつている。
In FIG. 3, the first and second slotted holes 1
3 and 14 are shown asymmetrically, it goes without saying that β may have the same direction and angle as α.
However, both the first long slot 13 and the second long slot 14 are α
When the value is set to , the curvature of the characteristic increases as shown by the broken line in FIG. 4, where the horizontal axis represents the engine speed and the vertical axis represents the ignition advance angle. Further, there is a drawback that hysteresis, which causes a delay when the curve D returns, increases. Therefore, in general, when α≠β often fluctuates in rotation, that is, when the above-mentioned angular acceleration becomes negative before the top dead center, the overadvance angle suppression effect is determined on the first slotted hole 13 side. There is no difference. In addition, if the engine torque fluctuation is small, the first and second weights 7 and 8 will be able to fly at the conventional level due to the centrifugal force f even if the first and second slotted holes 13 and 14 of the timing lever 12 are asymmetrical. be exposed.
It is better if the length a of the arm on which the force Fa acts is smaller than the radius of the weight support shaft 2, so that on the second long slot 14 side, the second rod 10 contacts at point Q on the inner wall side in the rotational direction. It's getting old.

このように、本実施例のガバナ進角装置は、第
1長溝穴をその長手方向壁が回転方向側に傾斜角
αになるように形成され、第1ロツド9及びウエ
イト支軸2はエンジン停止状態での第1ロツド9
が接する第1長溝穴13の回転方向後方の長手方
向壁面(点P)に垂直な直線に平行でかつ第1ロ
ツド9のシヤフト1側外周面に接する直線の延長
線がウエイト支軸2に交叉するように配置され、
かつ、前記第1ロツドはエンジン停止状態での該
第1ロツドと上記第1長溝穴の長手方向壁面のう
ちのシヤフト回転方向前側の壁面の間にギヤツプ
gが形成される位置に遊嵌されているので、エン
ジンの低速時に発生しやすいトルク変動による過
進角現象を防止できる。
As described above, the governor advance device of this embodiment is formed such that the longitudinal wall of the first slotted hole is inclined at an angle α toward the rotational direction, and the first rod 9 and the weight support shaft 2 are connected to each other when the engine is stopped. 1st rod 9 in state
An extension line of a straight line that is parallel to a straight line perpendicular to the rear longitudinal wall surface (point P) of the first long slot 13 in the rotational direction and that is in contact with the outer circumferential surface of the first rod 9 on the shaft 1 side intersects the weight support shaft 2. arranged so that
The first rod is loosely fitted in a position where a gap g is formed between the first rod and the front wall in the direction of shaft rotation among the longitudinal wall surfaces of the first slotted hole when the engine is stopped. This prevents over-advancement caused by torque fluctuations that tend to occur at low engine speeds.

第5図は他の実施例を示し、本実施例は第4図
の点線を実線に近接させることと、両ウエイトが
それぞれ最大に飛開したときのアンバランスを避
けることを目的としたものである。このため、シ
ヤフト1の中心から第1、第2ウエイトの各重心
までの最大に開いたときの半径が同一に形成さ
れ、第2長溝穴14は第1長溝穴13の円周方向
の傾き方向と逆に反回転方向に傾けられ、更に、
シヤフト1の中心及び第1ウエイト7のウエイト
支軸2の中心を結ぶ直線並びにウエイト支軸2の
中心と第1ロツドの9の中心を結ぶ直線のなす角
γaと、シヤフト1の中心及びウエイト支軸3の中
心を結ぶ直線並びにウエイト支軸3の中心及び第
2ロツド10の中心を結ぶ直線のかす角γbとの関
係を、γa<γbに形成されている。そして、第2長
溝穴14は第1長溝穴13の円周方向の傾斜方向
に対し逆方向に傾けられているのでγbが大きく形
成され、また、第2ウエイト8の回転角に対しタ
イミングレバー12の回転角が大きくなるように
なつている。このタイミングレバー12の回転角
の大きいことにより第4図の点線を実線に近接さ
せるようになつている。尚、第2ロツド10によ
るタイミングレバーの操作はB点からであり、A
〜B点間は第1スプリング15によつて両ウエイ
ト分の張力に対応させ実線方向へ作用させるよう
になつている。本実施例も第4図の点線を実線に
近接させると共に最大飛開時のウエイトのアンバ
ランスを阻止できる他上記実施例と同様の作用効
果を有するものである。
Figure 5 shows another embodiment, and this embodiment aims to bring the dotted line in Figure 4 close to the solid line and to avoid imbalance when both weights jump to their maximum. be. Therefore, the maximum radius from the center of the shaft 1 to the center of gravity of the first and second weights is the same, and the second long slot 14 is formed in the direction of inclination of the first long slot 13 in the circumferential direction. On the contrary, it is tilted in the counter-rotation direction, and further,
The angle γ a formed by the straight line connecting the center of the shaft 1 and the center of the weight support shaft 2 of the first weight 7 and the straight line connecting the center of the weight support shaft 2 and the center of 9 of the first rod, the center of the shaft 1, and the weight The relationship between the straight line connecting the centers of the support shaft 3 and the straight line connecting the centers of the weight support shaft 3 and the center of the second rod 10 with the helix angle γ b is set to satisfy γ ab . Since the second long slot 14 is inclined in the opposite direction to the circumferential direction of the first long slot 13, γ b is formed large, and the timing lever The rotation angle of 12 is increased. The large rotation angle of the timing lever 12 causes the dotted line in FIG. 4 to approach the solid line. Note that the timing lever operation by the second rod 10 is from point B, and from point A.
.about.B, the first spring 15 corresponds to the tension of both weights and acts in the direction of the solid line. This embodiment also brings the dotted line in FIG. 4 closer to the solid line, and has the same effects as the above-mentioned embodiments, in addition to being able to prevent the weight from being unbalanced at the time of maximum jump.

〔発明の効果〕〔Effect of the invention〕

以上記述したごとく本発明のガバナ進角装置に
よれば、エンジンの低速時に発生しやすいトルク
変動にともなう、タイミングレバーの慣性から生
ずる第1ウエイトの飛開の抑制が可能となり、エ
ンジンの低速時のトルク変動にともなう過進角が
防止される。
As described above, according to the governor advance device of the present invention, it is possible to suppress the jump of the first weight caused by the inertia of the timing lever due to torque fluctuations that tend to occur when the engine is running at low speed. Overadvanced angle due to torque fluctuations is prevented.

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

第1図は従来のガバナ進角装置の平面図、第2
図は第1図の装置の進角特性説明図、第3図は本
発明のガバナ進角装置の実施例の平面図、第4図
は第3図の進角特性説明図、第5図は本発明のガ
バナ進角装置の他の実施例の平面図である。 1……シヤフト、2,3……ウエイト支軸、6
……ウエイト取付台、7……第1ウエイト、8…
…第2ウエイト、9……第1ロツド、10……第
2ロツド、11……ロータシヤフト、12……タ
イミングレバー、13……第1長溝穴、14……
第2長溝穴、15……第1スプリング、16……
第2スプリング、G,g……ギヤツプ、γa,γb
…角、α……傾斜角、D……進角曲線、A……始
点、B……点。
Figure 1 is a plan view of a conventional governor advance device;
3 is a plan view of an embodiment of the governor advance device of the present invention, FIG. 4 is an explanatory diagram of the advance angle characteristic of the device shown in FIG. 3, and FIG. FIG. 7 is a plan view of another embodiment of the governor advance device of the present invention. 1...Shaft, 2, 3...Weight spindle, 6
...Weight mounting base, 7...First weight, 8...
...Second weight, 9...First rod, 10...Second rod, 11...Rotor shaft, 12...Timing lever, 13...First slotted hole, 14...
Second long slot, 15... First spring, 16...
Second spring, G, g...Gap, γ a , γ b ...
...Angle, α...Inclination angle, D...Advance angle curve, A...Start point, B...Point.

Claims (1)

【特許請求の範囲】 1 往復動エンジンで駆動されるシヤフトに固定
されたウエイト取付台上の上記シヤフト軸心周囲
に植立された2本のウエイト支軸と、該ウエイト
支軸にそれぞれ一端側を回動自在に支持され他端
側にそれぞれ第1、第2ロツドが植立された第1
ウエイト及び第2ウエイトと、該第1ウエイトに
一端が連結され他端が上記ウエイト取付台に連結
され回転数−点火進角曲線の進角零の始点から前
記両連結点間に引張力を作用するように形成され
た第1スプリングと、上記第2ウエイトに一端が
連結され他端が上記ウエイト取付台に連結され上
記第1スプリングに共同して前記両連結点間に引
張力を作用するように形成された第2スプリング
上記シヤフトに遊嵌されたロータシヤフトに固定
され長手方向をほぼ半径方向として開口された第
1長溝穴及び第2長溝穴を有し該第1長溝穴、第
2長溝穴にそれぞれ上記第1、第2ロツドを該第
1長溝穴、第2長溝穴の長手方向壁面に摺動可能
に遊嵌させたタイミングレバーとを設けたガバナ
進角装置において、 前記第1ウエイトを軸支するウエイト支軸
は、エンジン停止状態近傍での前記第1ロツド
の中心を通り前記第1長溝穴の長手方向壁面の
うちのシヤフト回転方向後側の壁面に垂直な直
線に平行で前記第1ロツドのシヤフト側外周面
に接する直線の延長線上に配置されていること
と、 前記第1ロツドが遊嵌されている上記第1長
溝穴内の位置はエンジン停止状態での該第1ロ
ツドと上記第1長溝穴の長手方向壁面のうちの
シヤフト回転方向前側の壁面の間にギヤツプg
が形成される位置であることと、 上記第2スプリングは、回転数−点火進角曲
線の中間の点から前記両連結点間に引張力を作
用するように形成されたものであることと、 上記シヤフトの中心から上記第1、第2ウエ
イトの重心までの半径がそれぞれ最大飛開状態
で等しく形成されていることと、 上記シヤフトの中心と上記第1ウエイトを軸
支するウエイト支軸の中心とを結ぶ直線が該ウ
エイト支軸の中心と第1ロツドの中心とを結ぶ
直線となす角raと、上記シヤフトの中心と上記
第2ウエイトを軸支するウエイト支軸の中心と
を結ぶ直線が該ウエイト支軸の中心と第2ロツ
ドの中心とを結ぶ直線となす角rbとの関係がra
<rbであることと、 前記第1長溝穴の長手方向壁面の外周側端部
と内周側端部を結ぶ直線は、前記シヤフトの中
心と第1ロツドの中心を結ぶ直線に平行かつ前
記内周側端部を通る直線に対し外周側端部が回
転方向前方に離れる方向に傾斜し、第2長溝穴
の長手方向壁面の外周側端部と内周側端部を結
ぶ直線は、前記シヤフトの中心と第1ロツドの
中心を結ぶ直線に平行かつ前記内周側端部を通
る直線に対し外周側端部が回転方向後方に離れ
る方向に傾斜していることと、 を特徴とするガバナ進角装置。
[Scope of Claims] 1. Two weight spindles installed around the shaft axis on a weight mounting base fixed to a shaft driven by a reciprocating engine, and one end side of each of the weight spindles. The first rod is rotatably supported, and the first and second rods are respectively planted on the other end side.
A weight and a second weight, one end of which is connected to the first weight and the other end of which is connected to the weight mounting base, and a tensile force is applied between the two connection points from the starting point of zero advance of the rotation speed-ignition advance curve. a first spring having one end connected to the second weight and the other end connected to the weight mount so as to work together with the first spring to apply a tensile force between the two connection points. The second spring is fixed to the rotor shaft that is loosely fitted to the shaft, and has a first elongated slot hole and a second elongated slot hole that are opened with the longitudinal direction being substantially radial. In the governor advance device, a timing lever is provided in which the first and second rods are slidably and loosely fitted into the longitudinal wall surfaces of the first and second slotted holes, respectively, and the first weight. The weight support shaft is parallel to a straight line that passes through the center of the first rod near the engine stop state and is perpendicular to the rear wall in the shaft rotational direction of the longitudinal wall of the first slot. The first rod is disposed on an extension of a straight line that is in contact with the shaft-side outer peripheral surface of the first rod, and the position in the first slot into which the first rod is loosely fitted is the same as that of the first rod when the engine is stopped. A gap g is formed between the longitudinal wall surfaces of the first long slot on the front side in the direction of shaft rotation.
The second spring is formed so as to apply a tensile force between the two connection points from an intermediate point of the rotation speed-ignition advance angle curve; The radius from the center of the shaft to the center of gravity of the first and second weights is the same in the maximum flying state, and the center of the shaft and the center of the weight support shaft that supports the first weight The angle r a made by the straight line connecting the weight support shaft with the straight line connecting the center of the weight support shaft and the center of the first rod, and the straight line connecting the center of the shaft and the center of the weight support shaft that pivotally supports the second weight. The relationship between the angle r b formed by the straight line connecting the center of the weight support shaft and the center of the second rod is r a
<r b , and the straight line connecting the outer peripheral end and the inner peripheral end of the longitudinal wall surface of the first slotted hole is parallel to the straight line connecting the center of the shaft and the center of the first rod, and The outer circumference end is inclined in a direction away from the front in the rotational direction with respect to the straight line passing through the inner circumference side end, and the straight line connecting the outer circumference side end and the inner circumference side end of the longitudinal wall surface of the second long slot is A governor characterized in that an outer peripheral end is inclined in a direction away from the rear in the rotational direction with respect to a straight line that is parallel to a straight line connecting the center of the shaft and the center of the first rod and passes through the inner peripheral end. Advance angle device.
JP16313483A 1983-09-07 1983-09-07 Governor timing control device Granted JPS6056171A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP16313483A JPS6056171A (en) 1983-09-07 1983-09-07 Governor timing control device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP16313483A JPS6056171A (en) 1983-09-07 1983-09-07 Governor timing control device

Publications (2)

Publication Number Publication Date
JPS6056171A JPS6056171A (en) 1985-04-01
JPH0423108B2 true JPH0423108B2 (en) 1992-04-21

Family

ID=15767838

Family Applications (1)

Application Number Title Priority Date Filing Date
JP16313483A Granted JPS6056171A (en) 1983-09-07 1983-09-07 Governor timing control device

Country Status (1)

Country Link
JP (1) JPS6056171A (en)

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6055714B2 (en) * 1977-01-21 1985-12-06 株式会社日立製作所 Ignition timing adjustment device

Also Published As

Publication number Publication date
JPS6056171A (en) 1985-04-01

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