JPS6242152B2 - - Google Patents
Info
- Publication number
- JPS6242152B2 JPS6242152B2 JP17465583A JP17465583A JPS6242152B2 JP S6242152 B2 JPS6242152 B2 JP S6242152B2 JP 17465583 A JP17465583 A JP 17465583A JP 17465583 A JP17465583 A JP 17465583A JP S6242152 B2 JPS6242152 B2 JP S6242152B2
- Authority
- JP
- Japan
- Prior art keywords
- weight
- advance
- drive shaft
- drive
- angle
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02P—IGNITION, OTHER THAN COMPRESSION IGNITION, FOR INTERNAL-COMBUSTION ENGINES; TESTING OF IGNITION TIMING IN COMPRESSION-IGNITION ENGINES
- F02P5/00—Advancing or retarding ignition; Control therefor
- F02P5/04—Advancing or retarding ignition; Control therefor automatically, as a function of the working conditions of the engine or vehicle or of the atmospheric conditions
- F02P5/05—Advancing 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
- F02P5/06—Advancing 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)
- Ignition Installations For Internal Combustion Engines (AREA)
- One-Way And Automatic Clutches, And Combinations Of Different Clutches (AREA)
Description
【発明の詳細な説明】
〔発明の分野〕
この発明は例えば内燃機関の点火用配電機器に
用いて点火時期を制御する遠心進角装置、特にそ
の進角特性の安定化を図り得る装置に関するもの
である。[Detailed Description of the Invention] [Field of the Invention] The present invention relates to a centrifugal advance device for controlling ignition timing, which is used, for example, in an ignition power distribution device of an internal combustion engine, and in particular to a device capable of stabilizing the advance characteristics thereof. It is.
第1図、第2図は従来の遠心進角装置を内燃機
関の点火用配電器の例で示したものである。図に
おいて、1は駆動軸、2はこの駆動軸1に固定さ
れている台板、3はこの台板2に植立されたピ
ン、4はこのピン3に遊嵌されているウエイト、
5はこのウエイト4に植立された進角ピン、6は
進角プレートで、長穴6aを備えており、この長
穴6aを上記進角ピン5に係合させている。7は
上記駆動軸1に遊嵌している進角スリーブで上記
進角プレート6とは一体固着されている。8はス
プリングで、上記台板2と上記ウエイト4とのそ
れぞれに設けられたスプリング掛け部の間に張架
されている。
FIGS. 1 and 2 show a conventional centrifugal advance device as an example of an ignition power distribution device for an internal combustion engine. In the figure, 1 is a drive shaft, 2 is a base plate fixed to this drive shaft 1, 3 is a pin planted on this base plate 2, 4 is a weight loosely fitted to this pin 3,
Reference numeral 5 denotes an advance angle pin mounted on this weight 4, and 6 an advance angle plate, which is provided with an elongated hole 6a, and this elongated hole 6a is engaged with the advance angle pin 5. An advance angle sleeve 7 is loosely fitted onto the drive shaft 1 and is integrally fixed to the advance angle plate 6. A spring 8 is stretched between spring hooks provided on each of the base plate 2 and the weight 4.
従来の遠心進角装置は上記のように構成されて
おり、駆動軸1の回転とともに装置全体が回転す
るとウエイト4は遠心力によつて、ピン3を軸と
した飛開モーメントを受け、スプリング8の張力
によるモーメントと釣合う位置まで飛開するの
で、このウエイト4と一体で動く進角ピン5が長
穴6aとの係合部を通じて進角プレート6および
これと一体の進角スリーブ7を駆動軸1に対して
進角させる。このように原理的には回転速度の函
数で生じる遠心力とスプリングの張力特性との釣
合い関係から、相対的角度変位を作り出している
もので第3図に符号aで示したような進角特性が
得られる。 The conventional centrifugal advance device is constructed as described above, and when the entire device rotates with the rotation of the drive shaft 1, the weight 4 receives a flying moment about the pin 3 due to centrifugal force, and the spring 8 The advance angle pin 5, which moves integrally with the weight 4, drives the advance angle plate 6 and the advance angle sleeve 7 integral therewith through the engagement portion with the elongated hole 6a. Advance the angle relative to axis 1. In principle, a relative angular displacement is created from the balance between the centrifugal force generated as a function of the rotational speed and the tension characteristics of the spring, and the advance angle characteristic is shown by the symbol a in Figure 3. is obtained.
しかしながら従来の遠心進角装置は遠心力対応
言いかえれば、駆動軸の角速度対応での機構原理
を主に成り立たせたものであり、駆動軸の角加速
度対応がなされておらず、用途によつては非常に
不安定な進角特性が現われていた。すなわち、第
3図中に符号bで示すような進角の異常跳ね上り
とか、同図中に符号cで示すような進角ふらつき
とかが生じて、機関のノツキング発生や排気ガス
濃度の変化などの支障をもたらすという基本的な
欠点があつた。 However, conventional centrifugal advance devices are mainly based on mechanical principles that respond to centrifugal force, in other words, to respond to the angular velocity of the drive shaft, and do not correspond to the angular acceleration of the drive shaft, and may vary depending on the application. showed very unstable lead angle characteristics. In other words, abnormal jumps in the advance angle as shown by the symbol b in Figure 3, or fluctuations in the advance angle as indicated by the symbol c in the same figure, occur, resulting in engine knocking, changes in exhaust gas concentration, etc. The basic drawback was that it caused problems.
この発明は上記のような従来のものの欠点を除
去するためになされたもので、駆動軸の角加速度
対応での機構原理をとり入れ、ウエイト支持部材
を駆動軸に遊嵌させるとともに、ウエイト支持部
材とウエイトとウエイトの遠心力に抗する弾性部
材とをサブアツセンブリ化したユニツトとして構
成して組み立てが容易で、安定な進角特性が得ら
れるような遠心進角装置を得るものである。
This invention was made in order to eliminate the drawbacks of the conventional ones as described above, and it incorporates a mechanism principle that corresponds to the angular acceleration of the drive shaft, allows the weight support member to fit loosely on the drive shaft, and also allows the weight support member to fit loosely into the drive shaft. To obtain a centrifugal advance device which is easy to assemble and provides stable advance characteristics by constructing a weight and an elastic member that resists the centrifugal force of the weight as a subassembly unit.
第4図、第5図はこの発明の遠心進角装置を内
燃機関の点火用配電器の例で示したものである。
図において、9は駆動軸1にその軸心と直角な面
をなすよう固定されている駆動プレート、9aは
上記駆動プレート9に設けられている駆動用長溝
10は進角スリーブ7にその軸心と直角な面をな
すよう固定されている進角プレート、10aはこ
の進角プレート10に設けられ、上記駆動用長溝
9aの形状をもとに、この装置の進角特性と相関
して定まるところの形状を有する進角用長溝であ
る。11はウエイト支持部材で、支持ピン11
a、弾性部材係合部11bおよび中央穴11cを
有している。この中央穴11cの部位で上記ウエ
イト支持部材11は上記駆動軸1に遊嵌されてい
る。12はウエイトで、被支持穴12aおよび弾
性部材係合部12bを有している。上記被支持穴
12aの部位で上記ウエイト12は上記支持ピン
11aに遊嵌されている。13は上記ウエイト1
2に植立固着されたロツドで、このロツド13は
上記ウエイト12を貫通して、その一方の面に上
記駆動用長溝9aに挿入係合させる駆動用柱状突
起13aと、他の一方の面に上記進角用長溝10
aに挿入係合させる進角用柱状突起13bとをそ
れぞれ形成している。14は弾性部材で、この例
では引張スプリングが用いてあり、上記弾性部材
係合部11bと上記弾性部材係合部12bとの間
に張架されている。
FIGS. 4 and 5 show the centrifugal advance device of the present invention as an example of an ignition power distribution device for an internal combustion engine.
In the figure, reference numeral 9 denotes a drive plate fixed to the drive shaft 1 so as to form a plane perpendicular to the axial center of the drive shaft 1, and 9a denotes a drive long groove 10 provided in the drive plate 9 whose axis is centered on the advance sleeve 7. The advance angle plate 10a is fixed to form a plane perpendicular to the advance angle plate 10, and is determined based on the shape of the driving long groove 9a and in correlation with the advance angle characteristics of this device. This is a long groove for advance angle having the shape of . 11 is a weight support member, and a support pin 11
a, an elastic member engaging portion 11b, and a central hole 11c. The weight support member 11 is loosely fitted onto the drive shaft 1 at the center hole 11c. A weight 12 has a supported hole 12a and an elastic member engaging portion 12b. The weight 12 is loosely fitted to the support pin 11a at the supported hole 12a. 13 is the weight 1 above
This rod 13 passes through the weight 12 and has a driving columnar protrusion 13a on one side that is inserted into and engaged with the long driving groove 9a, and on the other side. The above long groove for advance angle 10
A columnar protrusion 13b for advancing angle is formed to be inserted into and engaged with a. Reference numeral 14 denotes an elastic member, which is a tension spring in this example, and is stretched between the elastic member engaging portion 11b and the elastic member engaging portion 12b.
そして、ウエイト支持部材11とウエイト12
と弾性部材14は第6図に示すようにサブアツセ
ンブリ化して飛開ユニツト15として構成され、
駆動軸1、駆動プレート9の駆動側構成部材およ
び進角プレート10、進角スリーブ7の進角スリ
ーブ側構成部材とは独立している。 Then, the weight support member 11 and the weight 12
and the elastic member 14 are formed into a subassembly to form a jump unit 15 as shown in FIG.
The drive shaft 1 and the drive side components of the drive plate 9 and the advance angle plate 10 and the advance sleeve side components of the advance angle sleeve 7 are independent.
上記ように構成されたこの発明の実施例では、
駆動軸1からウエイト12への回転力伝達機構に
大きな特徴がある。すなわち従来装置では、第1
図による説明で明白なように、ウエイト4は駆動
軸1からの回動力をピン3から受けると共に、遠
心力によつて飛開する軸もまたピン3であつた。
しかるに第4図による説明から理解できるよう
に、この発明の実施例では、ウエイト2は駆動軸
1からの回転力を駆動用注状突起13aで受ける
が、遠心力によつて飛開する軸は支持ピン11a
である。ところでこの発明の実施例においても上
述した従来装置と同様に駆動軸1の角度速対応で
の機構原理、すなわちウエイト12の遠心力によ
つてのみ作用するときは、第3図に破線aで示し
た進角特性が得られる。これは第1図におけるピ
ン3と進角ピン5とが、第4図における支持ピン
11aとロツド13とにそれぞれ対応して機構的
には同一であると云えるためである。 In the embodiment of the present invention configured as described above,
A major feature is the mechanism for transmitting rotational force from the drive shaft 1 to the weight 12. In other words, in the conventional device, the first
As is clear from the explanation with the figures, the weight 4 receives the rotational force from the drive shaft 1 from the pin 3, and the pin 3 is also the shaft that is blown open by centrifugal force.
However, as can be understood from the explanation with reference to FIG. 4, in the embodiment of the present invention, the weight 2 receives the rotational force from the drive shaft 1 with the drive funnel 13a. Support pin 11a
It is. By the way, in the embodiment of the present invention, as in the conventional device described above, the mechanical principle corresponding to the angular velocity of the drive shaft 1, that is, when it acts only by the centrifugal force of the weight 12, is shown by the broken line a in FIG. It is possible to obtain advanced angle characteristics. This is because pin 3 and advance pin 5 in FIG. 1 correspond to support pin 11a and rod 13 in FIG. 4, respectively, and can be said to be mechanically the same.
次に駆動軸1が角加速度を受けたときの作用に
関する機構原理を定性的に説明する。一般に内燃
機関の点火用配電器における角加速度による進角
異常は、駆動軸1からの駆動伝達経路として、ウ
エイト12より後段につながる機素すなわち進角
プレート10、進角スリーブ7および図示してい
ない配電ローターなどの慣性モーメントに応じて
発生する慣性トルクの影響が主体を示める。第7
図、第8図はいずれも駆動軸1に負の角加速度が
生じたときの、進角装置を構成する機素に慣性に
よつて生じる力の関係を説明したものである。第
7図に示す従来装置では、進角ピン5にウエイト
4より後段につながる機素の慣性によつて発生す
る力F1が作用し、ピン3には駆動軸1側からの
反力R1が作用している。ウエイト4に対しては
上記の力F1が飛開軸であるピン3の上記反力R
1の作用点から上記の力F1の作用線への垂線の
脚dとの相乗積に比例して飛開トルクを与える。
上記反力R1には、ウエイト4の飛開に対する作
用成分はほとんどなく、すなくともウエイト4の
飛開を抑制する作用は認められない。第8図に示
すこの発明による実施例では、進角用柱状突起1
3bにウエイト12より後段につながる機素の慣
性によつて発生する力F2が作用し、駆動軸1側
からの反力R2が駆動用柱状突起13aに作用す
る。すなわち、ロツド13を進角用長溝10aと
駆動用長溝9aとで、くさびを形成して締め寄せ
るかたちをとつており、ウエイト12に対する力
F2による飛開トルクは、反力R2の作用点との
関係で上述した従来装置の場合に比しはるかに小
さい。なおかつ反力R2により駆動用長溝9aと
駆動用柱状突起13aとの間に生じる摩擦力によ
つて、上述した従来装置には備わつていない新た
な飛開抑制トルクが発生する。この新たな飛開抑
制トルクの一つの大きな特徴は、これが角加速度
対応時のみに発生する摩擦力によるものであるこ
とで、従つて角速度に対応して定まる進角特性の
質を悪化するヒステリシスの増大は生じない。本
発明装置が以上に説明した新たな特徴を有し得る
機構原理上の顕著な理由は、ウエイト支持部材1
1が、駆動軸1に隆嵌されているところにあり、
このためにいかなる場合においても支持ピン11
aには駆動軸1側からの作用力は生じ得ないとい
う点にある。なお、上記した本発明の実施例にお
けるウエイト支持部材11が有する支持ピン11
aと、ウエイト12が有する被支持穴12aとの
軸、穴嵌合関係を相互に入れ替えて構成しても、
本発明の効果は保たれる。 Next, the mechanism principle regarding the action when the drive shaft 1 receives angular acceleration will be qualitatively explained. Generally, an abnormality in the advance angle due to angular acceleration in the ignition power distributor of an internal combustion engine is caused by elements connected to the drive transmission path from the drive shaft 1 after the weight 12, that is, the advance angle plate 10, the advance angle sleeve 7, and the elements (not shown). It can be seen that the main influence is the inertial torque generated according to the moment of inertia of the power distribution rotor, etc. 7th
8 and 8 both illustrate the relationship between the forces generated by inertia in the elements constituting the advance angle device when negative angular acceleration occurs on the drive shaft 1. In the conventional device shown in FIG. 7, a force F1 generated by the inertia of an element connected to a stage subsequent to the weight 4 acts on the advance pin 5, and a reaction force R1 from the drive shaft 1 side acts on the pin 3. are doing. For the weight 4, the above force F1 is the reaction force R of the pin 3, which is the jump axis.
The flying torque is applied in proportion to the multiplicative product of the perpendicular line from the point of action of F1 to the line of action of the force F1 with the leg d.
The reaction force R1 has almost no effect on the flying of the weight 4, and at least has no effect on suppressing the flying of the weight 4. In the embodiment according to the invention shown in FIG.
A force F2 generated by the inertia of an element connected to a stage subsequent to the weight 12 acts on the drive shaft 3b, and a reaction force R2 from the drive shaft 1 side acts on the drive columnar projection 13a. In other words, the advance angle long groove 10a and the drive long groove 9a form a wedge in the rod 13, and the jump torque caused by the force F2 on the weight 12 is caused by the point of action of the reaction force R2. This is much smaller than in the case of the conventional device mentioned above in relation to this. Furthermore, due to the frictional force generated between the driving long groove 9a and the driving columnar protrusion 13a due to the reaction force R2, a new fly-opening suppressing torque that is not provided in the above-mentioned conventional device is generated. One of the major features of this new jump suppression torque is that it is due to the friction force that occurs only when responding to angular acceleration, and therefore it prevents hysteresis that deteriorates the quality of the advance angle characteristic that is determined in response to angular velocity. No increase occurs. The reason why the device of the present invention can have the above-described new features is that the weight support member 1
1 is located where it is fitted into the drive shaft 1,
For this purpose, in any case the support pin 11
The point is that no acting force from the drive shaft 1 side can be generated at a. Note that the support pin 11 included in the weight support member 11 in the embodiment of the present invention described above
Even if the shaft and hole fitting relationship between a and the supported hole 12a of the weight 12 are interchanged,
The effects of the present invention are maintained.
また、上記飛開ウエイトユニツト15について
考えるならば、第4図、第5図および第8図にお
いては、特定の方向に限定して説明したが、もし
駆動用柱状突起13aと進角用柱状突起13bと
を同一形状にしておくならば、飛開ウエイトユニ
ツト15は丸ごと裏返して、進角用柱状突起13
bを駆動用長溝9aに係合させ、駆動用柱状突起
13aを進角用長溝10aに係合させても、この
装置の所定の進角特性を得ることは支障なく達成
できる。すなわち、飛開ウエイトユニツト15は
時計方向、反時計方向の両回転用として同一に機
能させ得る。 Furthermore, considering the jump weight unit 15, although the explanation was limited to a specific direction in FIGS. 4, 5, and 8, if the drive columnar projection 13a and the advance angle columnar projection 13a 13b, the jump weight unit 15 should be completely turned over and the advance angle columnar protrusion 13
Even if the drive columnar protrusion 13a is engaged with the long drive groove 9a and the drive columnar projection 13a is engaged with the advance long groove 10a, the predetermined advance angle characteristics of this device can be achieved without any problem. That is, the jump weight unit 15 can function equally for both clockwise and counterclockwise rotation.
さらに、第4図、第8図に表わしている駆動用
長溝9aを、回転軸に対して放射状の形状にする
ならば、駆動軸1、駆動プレート9は回転方向に
限定されることなく、時計方向、反時計方向の両
回転用に共通化でき、全く同一に機能させ得る。 Furthermore, if the driving long groove 9a shown in FIGS. 4 and 8 is formed into a radial shape with respect to the rotating shaft, the driving shaft 1 and the driving plate 9 can be rotated without being limited to the rotating direction. It can be used commonly for both direction and counterclockwise rotation, and can function in exactly the same way.
以上の通りこの発明によれば、駆動伝達経路の
途中にあり、かつ重要な機素であるウエイトへの
力の作用点を変えて、機構原理的に新たで、かつ
優れた特徴を示す摩擦力を生じせしめるよう構成
できるので、駆動軸の角加速度に対する進角の不
安定さを解消し、かつ、製造上で組立性の容易化
や部品の共通化が望めるすぐれた遠心進角装置が
得られる効果がある。
As described above, according to this invention, by changing the point of application of force to the weight, which is an important element located in the middle of the drive transmission path, the friction force exhibits new and excellent features in terms of mechanical principle. Since it can be constructed so as to cause the angular acceleration of the drive shaft, an excellent centrifugal advance device can be obtained that eliminates the instability of the advance angle with respect to the angular acceleration of the drive shaft, and also allows for easier assembly and common parts during manufacturing. effective.
第1図は従来装置の概要を示す平面図、第2図
は第1図装置の側断面図、第3図は進角特性を示
す特性図、第4図はこの発明装置の一実施例の概
要を示す平面図、第5図は第4図装置の側断面
図、第6図は本発明の一実施例である飛開ウエイ
トユニツトを示す平面図、第7図は第1図、第2
図に示す従来装置の動作を説明するための図、第
8図は第4図、第5図に示す本発明装置の動作を
説明するための図である。
図中、1は駆動軸、7は進角スリーブ、9は駆
動プレート、9aは駆動用長溝、10は進角プレ
ート、10aは進角用長溝、11はウエイト支持
部材、11a,11b,11cはそれぞれ支持ピ
ン、弾性部材係合部、中央穴、12はウエイト、
12a,12bはそれぞれ被支持穴、弾性部材係
合部、13はロツド、13a,13bはそれぞれ
駆動用柱状突起、進角用柱状突起、14は弾性部
材、15は飛開ウエイトユニツトである。なお、
図中同一符号は同一または相当部分を示す。
Fig. 1 is a plan view showing an outline of the conventional device, Fig. 2 is a side sectional view of the device shown in Fig. 1, Fig. 3 is a characteristic diagram showing advance angle characteristics, and Fig. 4 is an embodiment of the device of the present invention. 5 is a side sectional view of the device shown in FIG. 4, FIG. 6 is a plan view showing a jumping weight unit which is an embodiment of the present invention, and FIG. 7 is a side sectional view of the device shown in FIG.
FIG. 8 is a diagram for explaining the operation of the conventional apparatus shown in the figure, and FIG. 8 is a diagram for explaining the operation of the apparatus of the present invention shown in FIGS. 4 and 5. In the figure, 1 is a drive shaft, 7 is an advance angle sleeve, 9 is a drive plate, 9a is a long groove for driving, 10 is an advance angle plate, 10a is a long groove for advance angle, 11 is a weight support member, 11a, 11b, 11c are respectively a support pin, an elastic member engaging part, a center hole, 12 a weight,
12a and 12b are supported holes and elastic member engaging portions, 13 is a rod, 13a and 13b are a driving columnar projection and an advancing columnar projection, respectively, 14 is an elastic member, and 15 is a flying weight unit. In addition,
The same reference numerals in the figures indicate the same or corresponding parts.
Claims (1)
させ、弾性部材の弾性力に抗して上記ウエイトを
飛開せしめ、進角スリーブを上記駆動軸に対して
相対的に進角させる装置において、上記駆動軸に
遊嵌されているウエイト支持部材を設け、このウ
エイト支持部材に上記ウエイトを飛開自在に支持
する手段と、上記弾性部材の係合手段とを持たせ
て、上記ウエイト支持部材と上記ウエイトと上記
弾性部材とが、駆動側構成部材および進角スリー
ブ側構成部材からは独立したサブアツセンブリさ
れたユニツトとして構成したことを特徴とする遠
心進角装置用飛開ウエイトユニツト。 2 駆動軸に遊嵌し、この駆動軸側の構成部材で
ある駆動プレートの駆動用長溝に係合する駆動用
柱状突起と、進角スリーブ側の構成部材である進
角プレートの進角用長溝に係合する進角用柱状突
起とを備えていることを特徴とする特許請求の範
囲第1項記載の遠心進角装置用飛開ウエイトユニ
ツト。 3 駆動用柱状突起と進角用柱状突起とが同一の
形状寸法に形成されていて、これら両柱状突起の
それぞれと係合する駆動用長溝と進角用長溝との
対を入れ替えても同一に機能するようになされて
いることを特徴とする特許請求の範囲第2項記載
の遠心進角装置用飛開ウエイトユニツト。[Claims] 1 A centrifugal force is applied to the weight by the rotation of the drive shaft, the weight is made to fly against the elastic force of the elastic member, and the advance sleeve is advanced relative to the drive shaft. In the squaring device, a weight support member is provided that is loosely fitted to the drive shaft, and the weight support member has means for supporting the weight in a freely swingable manner and means for engaging the elastic member, A jumper for a centrifugal angle advance device, characterized in that the weight support member, the weight, and the elastic member are configured as a sub-assembled unit independent of the drive side component and the advance sleeve side component. weight unit. 2. A driving columnar projection that loosely fits onto the drive shaft and engages with a long driving groove of the drive plate, which is a component on the drive shaft side, and a long advance groove on the advance plate, which is a component on the advance sleeve side. 2. The fly-out weight unit for a centrifugal angle advance device according to claim 1, further comprising a columnar protrusion for advancing angle that engages with. 3. The drive columnar projection and the advance angle columnar projection are formed to have the same shape and dimensions, and even if the pairs of the drive long groove and the advance angle long groove that engage with each of these columnar projections are replaced, they will remain the same. The flying weight unit for a centrifugal advance device according to claim 2, wherein the flying weight unit is adapted to function.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP17465583A JPS6065278A (en) | 1983-09-20 | 1983-09-20 | Spring-out weight unit for centrifugal advance apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP17465583A JPS6065278A (en) | 1983-09-20 | 1983-09-20 | Spring-out weight unit for centrifugal advance apparatus |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS6065278A JPS6065278A (en) | 1985-04-15 |
| JPS6242152B2 true JPS6242152B2 (en) | 1987-09-07 |
Family
ID=15982381
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP17465583A Granted JPS6065278A (en) | 1983-09-20 | 1983-09-20 | Spring-out weight unit for centrifugal advance apparatus |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6065278A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS63129247U (en) * | 1987-02-09 | 1988-08-24 |
-
1983
- 1983-09-20 JP JP17465583A patent/JPS6065278A/en active Granted
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS63129247U (en) * | 1987-02-09 | 1988-08-24 |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS6065278A (en) | 1985-04-15 |
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