JPH044252Y2 - - Google Patents

Info

Publication number
JPH044252Y2
JPH044252Y2 JP20119384U JP20119384U JPH044252Y2 JP H044252 Y2 JPH044252 Y2 JP H044252Y2 JP 20119384 U JP20119384 U JP 20119384U JP 20119384 U JP20119384 U JP 20119384U JP H044252 Y2 JPH044252 Y2 JP H044252Y2
Authority
JP
Japan
Prior art keywords
holder
governor
rotation center
output arm
pivot pin
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
Application number
JP20119384U
Other languages
Japanese (ja)
Other versions
JPS61115213U (en
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 filed Critical
Priority to JP20119384U priority Critical patent/JPH044252Y2/ja
Publication of JPS61115213U publication Critical patent/JPS61115213U/ja
Application granted granted Critical
Publication of JPH044252Y2 publication Critical patent/JPH044252Y2/ja
Expired legal-status Critical Current

Links

Landscapes

  • High-Pressure Fuel Injection Pump Control (AREA)

Description

【考案の詳細な説明】[Detailed explanation of the idea]

〈産業上の利用分野〉 本考案は、エンジンの遠心式ガバナのフライウ
エイト装置に関し、出力腕を長くするとともに、
出力腕に枢支したローラに摺動抵抗が負荷される
ことを防止して、ガバナの応答感度を高くできる
ものを提供する。 そして、本考案の前提となる技術の利用分野を
さらに詳述すれば、例えば、第1図若しくは第7
図に示すように、ウエイトホルダ1の回転中心B
から偏位する位置に支点軸3を介してフライウエ
イト2を揺動自在に枢支し、フライウエイト2の
出力腕6をホルダ回転中心B側に延出し、出力腕
6に枢支ピン18を介して回転輪7をホルダ回転
中心Bから横に離れた位置で回転自在に枢支して
構成したものに関する。 〈従来技術〉 従来のウエイト装置においては、第7図に示す
ように、回転輪7としてローラを使用し、支点軸
3と枢支ピン18との間の腕長さKをホルダ回転
中心Bと支点軸3との間の偏心距離Hに略等しく
形成していた。
<Industrial Application Field> The present invention relates to a flyweight device for a centrifugal engine governor, and the output arm is lengthened.
To provide a governor capable of increasing response sensitivity by preventing sliding resistance from being applied to a roller pivotally supported on an output arm. Further details of the field of application of the technology on which the present invention is based include, for example, Figure 1 or Figure 7.
As shown in the figure, the rotation center B of the weight holder 1
A flyweight 2 is swingably supported via a fulcrum shaft 3 at a position deviating from the center, an output arm 6 of the flyweight 2 is extended toward the holder rotation center B, and a pivot pin 18 is attached to the output arm 6. The rotary ring 7 is rotatably supported at a position laterally apart from the holder rotation center B through the holder rotation center B. <Prior Art> In the conventional weight device, as shown in FIG. 7, a roller is used as the rotating wheel 7, and the arm length K between the fulcrum shaft 3 and the pivot pin 18 is set to the holder rotation center B. It was formed to be approximately equal to the eccentric distance H between it and the fulcrum shaft 3.

【従来技術の問題点】[Problems with conventional technology]

しかしながら、この従来装置においては、ロー
ラ7はウエイトホルダ1の回転中心Bの回りに回
転運動を行なつているので、回転中心Bから離れ
る方向に遠心力R0を受けて出力腕6の内壁に押
し付けられる。 このため、ローラ7は摺動抵抗力を受けてガバ
ナスリーブ5の押圧が円滑に行なえず、ガバナの
応答感度を低下させてしまうという欠点があつ
た。
However, in this conventional device, since the roller 7 performs rotational movement around the rotation center B of the weight holder 1, it receives centrifugal force R 0 in a direction away from the rotation center B and is applied to the inner wall of the output arm 6. Being pushed. For this reason, the roller 7 is subjected to a sliding resistance force and cannot press the governor sleeve 5 smoothly, resulting in a disadvantage that the response sensitivity of the governor is reduced.

【先行技術】[Prior art]

一方、当該出願人は本考案に先だつて、第6図
及び第4図に示すように、ガバナスリーブ5を介
するガバナレバー24の入力部揺動寸法を長くし
てガバナ精度を高めるために、上記腕長さKを偏
心距離Hより長く設定するものを考えた。 〈考案が解決しようとする問題点〉 しかしながら、この先行考案では、ガバナ軸を
中心として回転するローラはガバナスリーブ5に
よつて、その回転軌跡に接する方向の押し出し力
F0を受けるので、この押し出し力F0のうち、枢
支ピン18方向の分力、即ち、スラスト分力E
が、ローラ7を出力腕6の内壁に押し付けようと
する摺動抵抗力となつて顕現する。 このため、やはり、ローラ7は円滑にガバナス
リーブ5を押圧できず、ガバナの精度は実質的に
大きくできないという問題を生ずる。 〈問題点を解決するための手段〉 本考案は、上記問題点を解消するもので、出力
腕を長くするとともに、回転輪に遠心力やガバナ
スリーブからのスラスト力が加わつても、回転輪
の回転を円滑に維持して、ガバナの応答感度を高
くできることを目的として提案されたもので、こ
の目的を達するための構成を実施例に対応する第
1図乃至第5図を用いて、以下に説明する。 即ち、支点軸3と枢支ピン18との間の腕長さ
Kをホルダ回転中心Bと支点軸3との間の偏心距
離Hよりも長く設定し、ホルダ回転中心Bを通り
支点軸3と平行な仮想直線Lよりもウエイトホル
ダ1の回転方向Mの下手側に枢支ピン18を偏位
させ、回転輪7としてラジアル軸受50を用いて
そのインナレース51を枢支ピン18に外嵌し、
インナレース51のホルダ回転中心Bから遠い側
の外端面53を出力腕6に受止めさせるととも
に、そのアウタレース52の外端面54を出力腕
6に対して隙間55を空けて離間せしめて構成し
たものである。 〈作用〉 そこで、上記構成によつてもたらされる本考案
の作用を述べると、回転輪としてラジアル軸受5
0を用いて、そのアウタレース52の外端面54
を出力腕6に対して離間させるので、このラジア
ル軸受50のアウタレース52にガバナスリーブ
5からの押し出し力F0のうちのスラスト分力F1
或いは遠心力が加わつて(即ち、ガバナスリーブ
5に接当するラジアル軸受の実質的な箇所はアウ
タレース52なので、このアウタレース52が外
力を受けることになる)、当該ガバナスリーブ5
がウエイトホルダ1の回転中心Bの方向に押し付
けられようとしても、出力腕6との間の隙間55
の中でスラスト移動が行なわれる。 このため、アウタレース52の外端面54が出
力腕6の内壁56に押し付けられることはなくな
る。 しかも、摺動分力Fで回転中心Bの方向に押し
付けられるアウターレース52に対してインナレ
ース51はボール60の転動を介して回転するの
で、アウターレース52の回転に支障はなく、ラ
ジアル軸受50はガバナスリーブ5をガバナ軸8
に沿つて円滑に水平移動することが出来る。 〈考案の効果〉 従つて、本考案によれば、出力腕を長くしてガ
バナレバーの入力部の揺動寸法を長くできるとと
もに、ラジアル軸受を介してガバナフオースを精
確、宜つ、スムーズにガバナスリーブに伝えるこ
とができるので、ガバナの応答感度をより大きく
向上することができる。 〈実施例〉 以下、本考案の実施例を図面に基いて説明す
る。 第1図はウエイト装置の出力腕周辺の要部縦断
正面図、第2図は機械式ガバナの揺動式ウエイト
装置の分解斜視図、第3図はデイーゼルエンジン
における同ウエイト装置周辺の縦断側面図、第4
図は同エンジンの縦断正面図、第5図はウエイト
装置の正面図であつて、デイーゼルエンジンEの
横側壁に燃料噴射ポンプ室20を形成し、燃料噴
射ポンプ21を当該ポンプ室20に収容し、ポン
プ室20の前後に亘つて軸架した噴射カム軸22
に噴射ポンプ21を連動する。 また、ポンプ室20の下方にガバナ軸8を配置
し、上記噴射カム軸22と平行に軸架したうえで
ウエイト装置10を取付け、当該ウエイト装置1
0に燃料噴射ポンプ21の燃料調整ラツク23を
ガバナレバー24を介して連動する。 即ち、ウエイト装置10は、第2図に示すよう
に、ガバナ軸8に円筒函状のホルダペース11、
略直方体状のウエイトホルダ1及びガバナスリー
ブ5を順次嵌挿し、ウエイトホルダ1に2個のフ
ライウエイト2を支点軸3を介して遠心方向に揺
動自在に枢支する。 当該ウエイトホルダ1は、いわば円盤状体の左
右両側壁13,12を平滑に切り欠いた形状を呈
し、その中央部に前後方向に亘つてガバナ軸嵌挿
孔14を、左・右両側壁13,12に亘つて一対
の支軸嵌挿孔15を(即ち、支軸嵌挿孔15はガ
バナ軸嵌挿孔14に対して上下方向に離れた直交
状に位置する)各々明け、この状態でホルダベー
ス11に固定してガバナ軸8に嵌挿されるととも
に、その前方にガバナスリーブ5を摺動自在に配
置する。 前記各フライウエイト2は、半円筒体16の両
端部の背後に垂直方向に出力腕6を延設し、両出
力腕6の上方に枢支孔17を明け、一方の出力腕
6の下方に枢支ピン18を支持し、枢支ピン18
の内端に回転輪7を回動自在に枢支する。 そして、力両力腕6の枢支孔17をウエイトホ
ルダ1の支軸嵌挿孔15に合わせ、支点軸3を両
孔15,17に嵌挿することで、2個のフライウ
エイト2をウエイトホルダ1の上・下に揺動自在
に各々枢支する。 上記出力腕6は、支点軸3と枢支ピン18との
間の腕長さKをホルダ回転中心Bと支点軸3との
間の偏心距離Hよりも長く設定し、ホルダ回転中
心Bを通り支点軸3と平行な仮想直線Lよりもウ
エイトホルダ1の回転方向Mの下手側に枢支ピン
18を偏位させて構成し、もつて、フライウエイ
ト2の揺動変位に対し出力腕6の押し出し変位を
大きくとり、ガバナスリーブ5の摺動変位を大き
く確保して、下記ガバナレバー24の入力部の揺
動寸法を大きく設定する。 また、上記回転輪7は、ラジアル軸受、より具
体的にはラジアル玉軸受50を使用し、そのイン
ナレース51を枢支ピン18に外嵌し、当該イン
ナレース51を枢支ピン18に外嵌し、当該イン
ナレース51のホルダ回転中心Bから遠い側の外
端面53をカラー57を介して出力腕6の内壁5
6に受止めさせる。 そして、上記カラー57の介装により、軸受5
0のアウタレース52の外端面54を出力腕6の
内壁56に対して隙間55を空けて離間せしめ、
アウタレース52がガバナスリーブ50から押し
出し力を受けても、スラスト移動をこの隙間55
の中で行なうように設定する。 一方、前記ガバナ軸8に嵌挿したガバナスリー
ブ5の前方に、二股状のガバナレバー24を配置
し、当該二股の基部25をポンプ室20に水平に
軸支した支持軸26に揺動自在に枢支し、二股の
先端部27に支持したローラ28をガバナスリー
ブ5の前鍔部29に接当可能に構成する。 斯くしてなるガバナ装置においては、エンジン
回転数が上昇すると、ガバナ軸8の回転速度も上
昇し、ウエイト2は遠心方向の推力を受けて支点
軸3を支点としてウエイトホルダ1の上・下端の
方向に開いてゆく。 そして、ウエイト2はその支持腕6をガバナ軸
8の前方に向かつて揺動せしめ、ラジアル軸受5
0はガバナスリーブ5の後鍔部30を前方向に押
圧摺動させる。 前方に摺動したガバナスリーブ5は、その前鍔
部29でガバナレバー24の二股先端部27を前
方に押し、支持軸26を中心に揺動したガバナレ
バー24はガバナスプリングの張力に抗して燃料
噴射ポンプ21の燃料調整ラツク23を燃料減量
側に移動せしめて、エンジン回転数を所定回転数
に減速するのである。 また、エンジン回転数が下降すると、ガバナス
プリングの張力でガバナレバー24は燃料調整ラ
ツク23を燃料増量側に移動せしめて、エンジン
回転数を所定回転数まで増速するのである。 以上のように、本考案は、エンジン回転数を一
定域に調整するガバナ装置において、ガバナ装置
を構成する要素の一つであるウエイト部分の回転
輪をラジアル軸受にしたうえで所定位置に取付け
たものなので、ラジアル受取は前述のようなラジ
アル玉軸受に限らず、例えば、複列球面コロ軸受
等にしても良い。 また、回転輪に特徴を持たせたものなので、ウ
エイトの形状やウエイトの支持軸への枢支態様も
問わないことは言うまでもない。
On the other hand, prior to the present invention, the applicant had developed a system for increasing the precision of the governor by increasing the swinging dimension of the input portion of the governor lever 24 via the governor sleeve 5, as shown in FIGS. 6 and 4. We considered setting the length K to be longer than the eccentric distance H. <Problem to be solved by the invention> However, in this prior invention, the roller rotating around the governor shaft is subjected to an extrusion force in a direction tangent to its rotational trajectory by the governor sleeve 5.
Since F 0 is received, out of this extrusion force F 0 , the component force in the direction of the pivot pin 18, that is, the thrust component force E
This manifests itself as a sliding resistance force that tries to press the roller 7 against the inner wall of the output arm 6. For this reason, the roller 7 cannot press the governor sleeve 5 smoothly, resulting in the problem that the accuracy of the governor cannot be substantially increased. <Means for solving the problems> The present invention solves the above problems by increasing the length of the output arm, and even when centrifugal force or thrust force from the governor sleeve is applied to the rotating wheels, the rotating wheels are not affected. This was proposed for the purpose of maintaining smooth rotation and increasing the response sensitivity of the governor.The configuration for achieving this purpose is described below using FIGS. 1 to 5 corresponding to the embodiment. explain. That is, the arm length K between the fulcrum shaft 3 and the pivot pin 18 is set longer than the eccentric distance H between the holder rotation center B and the fulcrum shaft 3, and the arm length K between the fulcrum shaft 3 and the pivot pin 18 is set to be longer than the eccentric distance H between the holder rotation center B and the fulcrum shaft 3. The pivot pin 18 is deviated to the lower side in the rotation direction M of the weight holder 1 than the parallel imaginary straight line L, and the inner race 51 is externally fitted onto the pivot pin 18 using a radial bearing 50 as the rotating ring 7. ,
The outer end surface 53 of the inner race 51 on the side far from the holder rotation center B is received by the output arm 6, and the outer end surface 54 of the outer race 52 is spaced apart from the output arm 6 with a gap 55. It is. <Function> Therefore, to describe the function of the present invention brought about by the above configuration, the radial bearing 5 is used as a rotating ring.
0, the outer end surface 54 of the outer race 52
is separated from the output arm 6, so that the thrust component F1 of the pushing force F0 from the governor sleeve 5 is applied to the outer race 52 of the radial bearing 50.
Alternatively, when centrifugal force is applied (that is, since the substantial portion of the radial bearing that contacts the governor sleeve 5 is the outer race 52, this outer race 52 receives external force), the governor sleeve 5
Even if the weight holder 1 is pressed in the direction of the rotation center B, the gap 55 between the weight holder 1 and the output arm 6
Thrust movement takes place inside. Therefore, the outer end surface 54 of the outer race 52 is no longer pressed against the inner wall 56 of the output arm 6. Moreover, since the inner race 51 rotates through the rolling motion of the balls 60 with respect to the outer race 52 which is pressed in the direction of the rotation center B by the sliding component F, the rotation of the outer race 52 is not hindered, and the radial bearing 50 connects the governor sleeve 5 to the governor shaft 8
It is possible to move horizontally smoothly along the <Effect of the invention> Therefore, according to the invention, the output arm can be lengthened to lengthen the swinging dimension of the input part of the governor lever, and the governor force can be accurately and smoothly transferred to the governor sleeve via the radial bearing. Therefore, the response sensitivity of the governor can be greatly improved. <Example> Hereinafter, an example of the present invention will be described based on the drawings. Fig. 1 is a longitudinal sectional front view of the main parts around the output arm of the weight device, Fig. 2 is an exploded perspective view of the oscillating weight device of the mechanical governor, and Fig. 3 is a longitudinal sectional side view of the vicinity of the same weight device in a diesel engine. , 4th
The figure is a longitudinal front view of the same engine, and FIG. , an injection cam shaft 22 extending from the front and back of the pump chamber 20;
The injection pump 21 is interlocked. Further, a governor shaft 8 is disposed below the pump chamber 20, and the weight device 10 is mounted after the governor shaft 8 is mounted parallel to the injection cam shaft 22.
0, the fuel adjustment rack 23 of the fuel injection pump 21 is interlocked via the governor lever 24. That is, as shown in FIG.
A substantially rectangular parallelepiped weight holder 1 and a governor sleeve 5 are fitted in sequence, and two fly weights 2 are pivoted to the weight holder 1 via a fulcrum shaft 3 so as to be swingable in the centrifugal direction. The weight holder 1 has a shape in which left and right side walls 13 and 12 of a disc-shaped body are smoothly cut out, and a governor shaft insertion hole 14 is provided in the center thereof in the front and back direction, and a governor shaft insertion hole 14 is formed in the center part of the left and right side walls 13 and 12. , 12 (that is, the support shaft insertion hole 15 is located perpendicularly apart from the governor shaft insertion hole 14 in the vertical direction), and in this state. It is fixed to the holder base 11 and fitted onto the governor shaft 8, and a governor sleeve 5 is slidably disposed in front of the governor shaft 8. Each of the flyweights 2 has an output arm 6 extending vertically behind both ends of a semi-cylindrical body 16, a pivot hole 17 formed above both output arms 6, and a pivot hole 17 formed below one output arm 6. supports the pivot pin 18;
A rotary ring 7 is rotatably supported at the inner end of the rotary ring 7. Then, by aligning the pivot hole 17 of the power and power arm 6 with the support shaft insertion hole 15 of the weight holder 1, and inserting the support shaft 3 into both holes 15 and 17, the two fly weights 2 can be used as weights. They are pivotably supported above and below the holder 1, respectively. The output arm 6 passes through the holder rotation center B by setting the arm length K between the fulcrum shaft 3 and the pivot pin 18 to be longer than the eccentric distance H between the holder rotation center B and the fulcrum shaft 3. The pivot pin 18 is configured to be deviated to the lower side in the rotational direction M of the weight holder 1 than the imaginary straight line L parallel to the fulcrum shaft 3, so that the output arm 6 is The pushing displacement is large, the sliding displacement of the governor sleeve 5 is large, and the swinging dimension of the input part of the governor lever 24 is set large. Further, the rotating ring 7 uses a radial bearing, more specifically a radial ball bearing 50, and an inner race 51 thereof is fitted onto the pivot pin 18, and the inner race 51 is fitted onto the pivot pin 18. Then, the outer end surface 53 of the inner race 51 on the side far from the holder rotation center B is connected to the inner wall 5 of the output arm 6 via the collar 57.
Let 6 accept it. By interposing the collar 57, the bearing 5
The outer end surface 54 of the outer race 52 of No. 0 is separated from the inner wall 56 of the output arm 6 with a gap 55,
Even if the outer race 52 receives an extrusion force from the governor sleeve 50, the thrust movement is limited to this gap 55.
Set it so that it is done inside. On the other hand, a bifurcated governor lever 24 is disposed in front of the governor sleeve 5 fitted into the governor shaft 8, and the bifurcated base 25 is pivotably pivoted on a support shaft 26 which is horizontally supported in the pump chamber 20. A roller 28 supported by a bifurcated tip 27 is configured to be able to come into contact with a front flange 29 of the governor sleeve 5. In the governor device constructed in this way, when the engine speed increases, the rotation speed of the governor shaft 8 also increases, and the weight 2 receives centrifugal thrust and rotates the upper and lower ends of the weight holder 1 about the fulcrum shaft 3. It opens in the direction. Then, the weight 2 swings its support arm 6 toward the front of the governor shaft 8, and the radial bearing 5
0 presses and slides the rear flange portion 30 of the governor sleeve 5 in the forward direction. The governor sleeve 5 that has slid forward pushes the bifurcated tip 27 of the governor lever 24 forward with its front flange 29, and the governor lever 24 that has swung around the support shaft 26 injects fuel against the tension of the governor spring. The fuel adjustment rack 23 of the pump 21 is moved to the fuel reduction side to reduce the engine speed to a predetermined speed. Furthermore, when the engine speed decreases, the tension of the governor spring causes the governor lever 24 to move the fuel adjustment rack 23 toward the fuel increase side, thereby increasing the engine speed to a predetermined speed. As described above, the present invention is a governor device that adjusts the engine speed within a certain range, in which the rotating ring of the weight part, which is one of the elements that make up the governor device, is made into a radial bearing and is mounted at a predetermined position. Therefore, the radial receiver is not limited to the radial ball bearing as described above, but may also be, for example, a double row spherical roller bearing. Furthermore, since the rotary wheel is unique, it goes without saying that the shape of the weight and the manner in which the weight is pivoted to the support shaft do not matter.

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

第1図乃至第5図は本考案の実施例を示すもの
で、第1図はウエイト装置の出力腕周辺の要部縦
断正面図、第2図は機械式ガバナの揺動式ウエイ
ト装置の分解斜視図、第3図はデイーゼルエンジ
ンにおける同ウエイト装置周辺の縦断側面図、第
4図は同エンジンの縦断正面図、第5図はウエイ
ト装置の正面図、第6図は先行技術のウエイト装
置を示す概略正面図、第7図は従来例を示す第6
図相当図である。 1……ウエイトホルダ、2……フライウエイ
ト、3……支点軸、6……出力腕、7……回転
輪、18……枢支ピン、50……ラジアル軸受、
51……インナレース、52……アウタレース、
53……51の外端面、54……52の外端面、
55……54と6の隙間、B……ホルダ回転中
心、H……Bと3との距離、K……3と18との
間の腕長さ、L……Bを通り3と平行な仮想直
線、M……1の回転方向。
Figures 1 to 5 show an embodiment of the present invention. Figure 1 is a longitudinal sectional front view of the main parts around the output arm of the weight device, and Figure 2 is an exploded view of the swinging weight device of the mechanical governor. 3 is a vertical sectional side view of the vicinity of the weight device in a diesel engine, FIG. 4 is a vertical sectional front view of the same engine, FIG. 5 is a front view of the weight device, and FIG. 6 is a front view of the weight device of the prior art. FIG. 7 is a schematic front view showing a conventional example.
It is a figure equivalent figure. 1... Weight holder, 2... Fly weight, 3... Fulcrum shaft, 6... Output arm, 7... Rotating ring, 18... Pivot pin, 50... Radial bearing,
51... Inner lace, 52... Outer lace,
53... Outer end surface of 51, 54... Outer end surface of 52,
55... Gap between 54 and 6, B... Center of holder rotation, H... Distance between B and 3, K... Arm length between 3 and 18, L... Passing through B and parallel to 3 The rotation direction of the virtual straight line, M...1.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] ウエイトホルダ1の回転中心Bから偏位する位
置に支点軸3を介してフライウエイト2を揺動自
在に枢支し、フライウエイト2の出力腕6をホル
ダ回転中心B側に延出し、出力腕6に枢支ピン1
8を介して回転輪7をホルダ回転中心Bから横に
離れた位置で回転自在に枢支して構成したエンジ
ンの遠心式ガバナのフライウエイト装置におい
て、支点軸3と枢支ピン18との間の腕長さKを
ホルダ回転中心Bと支点軸3との間の偏心距離H
よりも長く設定し、ホルダ回転中心Bを通り支点
軸3と平行な仮想直線Lよりもウエイトホルダ1
の回転方向Mの下手側に枢支ピン18を偏位さ
せ、回転輪7としてラジアル軸受50を用いてそ
のインナレース51を枢支ピン18に外嵌し、イ
ンナレース51のホルダ回転中心Bから遠い側の
外端面53を出力腕6に受止めさせるとともに、
そのアウタレース52の外端面54を出力腕6に
対して隙間55を空けて離間せしめて構成した事
を特徴とするエンジンの遠心式ガバナのフライウ
エイト装置。
A flyweight 2 is swingably supported via a fulcrum shaft 3 at a position offset from the rotation center B of the weight holder 1, and the output arm 6 of the flyweight 2 is extended toward the holder rotation center B, and the output arm 6 to pivot pin 1
In a flyweight device for a centrifugal engine governor, which is constructed by rotatably supporting a rotary wheel 7 at a position laterally away from the holder rotation center B via a holder shaft 8, between the fulcrum shaft 3 and the pivot pin 18. The arm length K is the eccentric distance H between the holder rotation center B and the fulcrum shaft 3.
The weight holder 1 is set longer than the imaginary straight line L passing through the holder rotation center B and parallel to the fulcrum shaft 3.
The pivot pin 18 is deviated to the downstream side in the rotation direction M, and the inner race 51 is fitted onto the pivot pin 18 using a radial bearing 50 as the rotating ring 7, and the inner race 51 is moved from the holder rotation center B. The outer end surface 53 on the far side is received by the output arm 6, and
This flyweight device for a centrifugal governor for an engine is characterized in that the outer end surface 54 of the outer race 52 is separated from the output arm 6 with a gap 55.
JP20119384U 1984-12-28 1984-12-28 Expired JPH044252Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP20119384U JPH044252Y2 (en) 1984-12-28 1984-12-28

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP20119384U JPH044252Y2 (en) 1984-12-28 1984-12-28

Publications (2)

Publication Number Publication Date
JPS61115213U JPS61115213U (en) 1986-07-21
JPH044252Y2 true JPH044252Y2 (en) 1992-02-07

Family

ID=30762749

Family Applications (1)

Application Number Title Priority Date Filing Date
JP20119384U Expired JPH044252Y2 (en) 1984-12-28 1984-12-28

Country Status (1)

Country Link
JP (1) JPH044252Y2 (en)

Also Published As

Publication number Publication date
JPS61115213U (en) 1986-07-21

Similar Documents

Publication Publication Date Title
JPH044252Y2 (en)
JPH044251Y2 (en)
JPH044249Y2 (en)
JPS6230085Y2 (en)
JPH044248Y2 (en)
JP2884309B2 (en) Governor force transmission device for centrifugal governor of engine
JPS6011316Y2 (en) Variable cam mechanism in piston drive
JPS59192834A (en) Governor apparatus for engine
JPS5912869B2 (en) I can&#39;t wait for the next day&#39;s trip
JPS6230084Y2 (en)
JPH0234441Y2 (en)
JPS5842588Y2 (en) How do you get started?
JPH0229241Y2 (en)
JPH0426676Y2 (en)
JPH0310350Y2 (en)
JPH0732925Y2 (en) Throttle valve drive for internal combustion engine
JPS5922571Y2 (en) Traveling transmission device for mobile agricultural machinery
JP2577205Y2 (en) Rack drive link bearing device
JP3305195B2 (en) Centrifugal governor for diesel engine
JPH03130466U (en)
JPS597556Y2 (en) Governor device of internal combustion engine
JPH065045B2 (en) Fuel control device for the diesel engine
JPH0546789Y2 (en)
JPH0223582U (en)
JP2884310B2 (en) Governor force transmission device for centrifugal governor of engine