JPH0228290Y2 - - Google Patents
Info
- Publication number
- JPH0228290Y2 JPH0228290Y2 JP18289384U JP18289384U JPH0228290Y2 JP H0228290 Y2 JPH0228290 Y2 JP H0228290Y2 JP 18289384 U JP18289384 U JP 18289384U JP 18289384 U JP18289384 U JP 18289384U JP H0228290 Y2 JPH0228290 Y2 JP H0228290Y2
- Authority
- JP
- Japan
- Prior art keywords
- inner shaft
- propeller
- gear
- large gear
- side large
- 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
- 238000005452 bending Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 238000007689 inspection Methods 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
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- Gear Transmission (AREA)
Description
【考案の詳細な説明】
〔産業上の利用分野〕
本考案は、船舶の推進装置として使用される二
重反転プロペラ装置に関する。[Detailed Description of the Invention] [Industrial Application Field] The present invention relates to a counter-rotating propeller device used as a propulsion device for ships.
従来の舶用二重反転プロペラ装置としては第3
図に示すようなものがあり、主機10により回転
駆動される内軸3が主機10内のスラスト軸受9
に支持されてそなえられ、その後端には後側プロ
ペラ1が装着されるとともに、この内軸3に重合
する管状の外軸4がスラスト軸受8に支持されて
そなえられ、その後端には前側プロペラ2が後側
プロペラ1の前側に位置するように装着されてい
る。
The third conventional marine contra-rotating propeller system
There is a model as shown in the figure, in which the inner shaft 3 that is rotationally driven by the main engine 10 is mounted on a thrust bearing 9 inside the main engine 10.
A rear propeller 1 is attached to the rear end, a tubular outer shaft 4 overlapping the inner shaft 3 is supported by a thrust bearing 8, and a front propeller is attached to the rear end. 2 is mounted so as to be located in front of the rear propeller 1.
そして、後側プロペラ1および前側プロペラ2
を互いに逆転させるため、入力側大歯車6cが、
内軸3と同方向へ回転するように、同内軸3に同
軸的に弾性継手7を介して装着される一方、出力
側大歯車5bが外軸4の前端部に同軸的に装着さ
れており、これらの入力側大歯車6cと出力側大
歯車5bとの間に、両大歯車6cおよび5bを互
いに逆転させる連動歯車機構Mが設けられてい
る。 Then, the rear propeller 1 and the front propeller 2
In order to reverse each other, the input side large gear 6c is
The output side large gear 5b is coaxially mounted on the front end of the outer shaft 4, while the output side large gear 5b is coaxially mounted on the inner shaft 3 via an elastic joint 7 so as to rotate in the same direction as the inner shaft 3. An interlocking gear mechanism M is provided between the input side large gear 6c and the output side large gear 5b to rotate both the large gears 6c and 5b in the reverse direction.
この連動歯車機構Mは、第3〜5図に示すよう
に、出力側大歯車5bに噛み合う出力側小歯車5
aと、同出力側小歯車5aにたわみ軸14を介し
て接続された入力側小歯車6aと、同入力側小歯
車6aと入力側大歯車6cとの間に介装されたア
イドル歯車6bとから構成される。 As shown in FIGS. 3 to 5, this interlocking gear mechanism M includes an output side small gear 5 that meshes with an output side large gear 5b.
a, an input side small gear 6a connected to the output side small gear 5a via a deflection shaft 14, and an idle gear 6b interposed between the input side small gear 6a and the input side large gear 6c. It consists of
なお、第3図において小歯車5a,6a、アイ
ドル歯車6b、大歯車5b,6cの軸受は図示を
省略されている。 In addition, in FIG. 3, the bearings of the small gears 5a, 6a, the idle gear 6b, and the large gears 5b, 6c are omitted from illustration.
このような舶用二重反転プロペラ装置では、後
側プロペラ1は内軸3により主機10に直結され
て回転駆動される一方、前側プロペラ2は次のよ
うにして回転駆動される。 In such a marine counter-rotating propeller device, the rear propeller 1 is directly connected to the main engine 10 through the inner shaft 3 and is rotationally driven, while the front propeller 2 is rotationally driven as follows.
すなわち、主機10に直結する内軸3の中間部
から弾性継手7により変動分について平滑化され
たトルクが入力側大歯車6cに伝えられ、第5図
に示すように、入力側小歯車6aにはアイドル歯
車6bにより入力側大歯車6cと同方向の回転が
与えられる。そして、たわみ軸14を介し入力側
小歯車6aの回転が出力側小歯車5aへ伝えら
れ、第4図に示すように、この小歯車5aと噛み
合う出力側大歯車5bには入力側大歯車6cと逆
方向の回転が伝えられる。 That is, the torque whose variation has been smoothed by the elastic joint 7 is transmitted from the intermediate portion of the inner shaft 3 directly connected to the main engine 10 to the input side large gear 6c, and as shown in FIG. 5, is transmitted to the input side small gear 6a. is rotated in the same direction as the input side large gear 6c by the idle gear 6b. The rotation of the input side small gear 6a is transmitted to the output side small gear 5a via the deflection shaft 14, and as shown in FIG. Rotation in the opposite direction is transmitted.
これにより、前側プロペラ2は後側プロペラ1
と逆方向に回転駆動される。なお、このとき上述
した歯車のギア比は適当に設定され、前側プロペ
ラ2と後側プロペラ1とはほぼ同じ回転速度で互
いに逆転するようになつている。 As a result, the front propeller 2 becomes the rear propeller 1.
It is rotated in the opposite direction. At this time, the gear ratio of the above-mentioned gears is set appropriately, so that the front propeller 2 and the rear propeller 1 rotate in opposite directions at approximately the same rotational speed.
したがつて、上述のように構成される二重反転
プロペラ装置をそなえた船舶では、プロペラ1,
2の後方に流出していた回転エネルギが回収され
て、一般の単一プロペラを有する船舶に比較し、
その推進効率を高めることができる。 Therefore, in a ship equipped with a counter-rotating propeller device configured as described above, the propellers 1,
The rotational energy that was flowing out to the rear of the ship is recovered, and compared to a general ship with a single propeller,
The propulsion efficiency can be increased.
しかしながら、上述のような従来の舶用二重反
転プロペラ装置では、内軸3は、主機10内のス
ラスト軸受9により支持されているだけであるの
で、同スラスト軸受9よりも後側においてたわみ
を生じ、同内軸3が外軸4と接触して不具合を生
じるという問題点がある。
However, in the conventional marine counter-rotating propeller device as described above, the inner shaft 3 is only supported by the thrust bearing 9 in the main engine 10, so that the inner shaft 3 is deflected at the rear side of the thrust bearing 9. However, there is a problem in that the inner shaft 3 comes into contact with the outer shaft 4, causing problems.
また、内軸3は、上述のようなたわみにより、
大きな曲げ応力を加えられた状態で回転するの
で、この内軸3に繰り返し応力が作用し、内軸3
の使用寿命が短くなるという問題点もある。 Moreover, due to the above-mentioned deflection, the inner shaft 3
Since it rotates under a large bending stress, repeated stress acts on the inner shaft 3, causing the inner shaft 3 to
Another problem is that the service life of the device is shortened.
本考案は、これらの問題点の解消をはかろうと
するもので、内軸のたわみの発生を防止できるよ
うにして、内軸に作用する曲げ応力の軽減をはか
つた、舶用二重反転プロペラ装置を提供すること
を目的とする。 The present invention attempts to solve these problems, and is a counter-rotating marine propeller that prevents the occurrence of deflection of the inner shaft and reduces the bending stress acting on the inner shaft. The purpose is to provide equipment.
このため、本考案の舶用二重反転プロペラ装置
は、主機により回転駆動される内軸と、同内軸の
後端に装着された後側プロペラとをそなえるとと
もに、上記内軸に重合する管状の外軸と、同外軸
の後端に装着されて上記後側プロペラの前側に配
設された前側プロペラとをそなえ、上記内軸と同
方向へ回転しうるように同内軸に同軸的に装着さ
れた入力側大歯車と、上記外軸の前端部に同軸的
に装着された出力側大歯車との間に両大歯車を互
いに逆転させる連動歯車機構が設けられて、上記
内軸を支持する軸受が、上記の入力側大歯車と出
力側大歯車との間に配設され、同軸受が分解可能
の2つ割れ構造に構成されていることを特徴とし
ている。
Therefore, the contra-rotating marine propeller device of the present invention has an inner shaft that is rotationally driven by the main engine, a rear propeller that is attached to the rear end of the inner shaft, and a tubular propeller that overlaps the inner shaft. It has an outer shaft and a front propeller attached to the rear end of the outer shaft and disposed in front of the rear propeller, and is coaxially connected to the inner shaft so that it can rotate in the same direction as the inner shaft. An interlocking gear mechanism is provided between the mounted input-side large gear and the output-side large gear coaxially mounted on the front end of the outer shaft to support the inner shaft. A bearing is disposed between the input-side large gear and the output-side large gear, and is characterized in that the bearing is structured in two pieces that can be disassembled.
上述の本考案の舶用二重反転プロペラ装置で
は、内軸が入力側大歯車と出力側大歯車との間に
おいて支持されるので、内軸におけるたわみの発
生が防止される。
In the marine counter-rotating propeller device of the present invention described above, since the inner shaft is supported between the input side large gear and the output side large gear, generation of deflection in the inner shaft is prevented.
以下、図面により本考案の一実施例としての舶
用二重反転プロペラ装置について説明すると、第
1図はその要部を模式的に示す縦断面図、第2図
はその軸受を示す分解斜視図である。
Below, a contra-rotating marine propeller device as an embodiment of the present invention will be explained with reference to the drawings. Fig. 1 is a vertical sectional view schematically showing the main parts thereof, and Fig. 2 is an exploded perspective view showing its bearings. be.
第1図に示すように、主機10(第3図参照)
により回転駆動される内軸3が主機10内のスラ
スト軸受9(第3図参照)に支持されてそなえら
れ、その後端には後側プロペラ1(第3図参照)
が装着されるとともに、この内軸3に重合する管
状の外軸4がスラスト軸受8に支持されてそなえ
られ、その後端には前側プロペラ2(第3図参
照)が後側プロペラ1の前側に位置するように装
着されている。 As shown in Fig. 1, the main engine 10 (see Fig. 3)
An inner shaft 3 that is rotatably driven by the main engine 10 is supported by a thrust bearing 9 (see Fig. 3), and a rear propeller 1 (see Fig. 3) is provided at the rear end.
is installed, and a tubular outer shaft 4 that overlaps the inner shaft 3 is supported by a thrust bearing 8, and a front propeller 2 (see Fig. 3) is attached to the front end of the rear propeller 1 at the rear end. It is attached to the position.
そして、後側プロペラ1および前側プロペラ2
を互いに逆転させるため、入力側大歯車6cが、
内軸3と同方向へ回転するように、同内軸3に同
軸的に弾性継手7を介して装着される一方、出力
側大歯車5bが外軸4の前端部に同軸的に装着さ
れており、これらの入力側大歯車6cと出力側大
歯車5bとの間に、両大歯車6cおよび5bを互
いに逆転させる連動歯車機構Mが設けられてい
る。 Then, the rear propeller 1 and the front propeller 2
In order to reverse each other, the input side large gear 6c is
The output side large gear 5b is coaxially mounted on the front end of the outer shaft 4, while the output side large gear 5b is coaxially mounted on the inner shaft 3 via an elastic joint 7 so as to rotate in the same direction as the inner shaft 3. An interlocking gear mechanism M is provided between the input side large gear 6c and the output side large gear 5b to rotate both the large gears 6c and 5b in the reverse direction.
この連動歯車機構Mは、出力側大歯車5bに噛
み合う出力側小歯車5aと、同出力側小歯車5a
にたわみ軸14を介して接続された入力側小歯車
6aと、同入力側小歯車6aと入力側大歯車6c
との間に介装されたアイドル歯車6b(第3,5
図参照)とから構成される。 This interlocking gear mechanism M includes an output side small gear 5a that meshes with an output side large gear 5b, and an output side small gear 5a that meshes with the output side large gear 5b.
The input side small gear 6a is connected to the input side small gear 6a via the deflection shaft 14, and the input side small gear 6a and the input side large gear 6c
Idle gear 6b (3rd, 5th
(see figure).
一方、上記の入力側大歯車6cと出力側大歯車
5bとの間には、内軸3を支持する内軸軸受11
が配設され、この内軸軸受11は、第2図に示す
ように、上部部材11aおよび下部部材11bか
ら成る分解可能の2つ割れ構造に構成されてい
る。 On the other hand, an inner shaft bearing 11 supporting the inner shaft 3 is provided between the input side large gear 6c and the output side large gear 5b.
As shown in FIG. 2, the inner shaft bearing 11 has a removable two-part structure consisting of an upper member 11a and a lower member 11b.
また、本実施例では、第2図に示すように、内
軸軸受11の前後に、入力側大歯車6cの突出部
および外軸4の突出部をそれぞれ支持する軸受1
2が内軸軸受11と一体になつて配設されてお
り、この軸受12も上部部材12aおよび下部部
材12bから成る分解可能の2つ割れ構造に構成
されている。 In addition, in this embodiment, as shown in FIG.
2 is disposed integrally with the inner shaft bearing 11, and this bearing 12 is also constructed in a removable two-piece structure consisting of an upper member 12a and a lower member 12b.
さらに、第1図に示すように、入力側大歯車6
cの前側部や出力側大歯車5b後側の外軸4を2
つ割れ構造の軸受12により支持してもよいし、
小歯車5a,6a、アイドル歯車6bを2つ割れ
構造の軸受13により支持してもよい。 Furthermore, as shown in FIG.
c and the outer shaft 4 on the rear side of the output side large gear 5b.
It may be supported by a bearing 12 with a split structure, or
The small gears 5a, 6a and the idle gear 6b may be supported by a bearing 13 having a two-piece structure.
本考案の舶用二重反転プロペラ装置は上述のご
とく構成されているので、従来のものと同様、後
側プロペラ1は内軸3により主機10に直結され
て回転駆動される一方、前側プロペラ2は次のよ
うにして回転駆動される。 Since the contra-rotating marine propeller device of the present invention is constructed as described above, the rear propeller 1 is directly connected to the main engine 10 by the inner shaft 3 and is rotationally driven, while the front propeller 2 is It is rotated as follows.
すなわち、主機10に直結する内軸3の中間部
から弾性継手7により変動分について平滑化され
たトルクが入力側大歯車6cに伝えられ、第5図
に示すように、入力側小歯車6aにはアイドル歯
車6bにより入力側大歯車6cと同方向の回転が
与えられる。そして、たわみ軸14を介し入力側
小歯車6aの回転が出力側小歯車5aへ伝えら
れ、第4図に示すように、この小歯車5aと噛み
合う出力側大歯車5bには入力側大歯車6cと逆
方向の回転が伝えられる。 That is, the torque whose variation has been smoothed by the elastic joint 7 is transmitted from the intermediate portion of the inner shaft 3 directly connected to the main engine 10 to the input side large gear 6c, and as shown in FIG. is rotated in the same direction as the input side large gear 6c by the idle gear 6b. The rotation of the input side small gear 6a is transmitted to the output side small gear 5a via the deflection shaft 14, and as shown in FIG. Rotation in the opposite direction is transmitted.
これにより、前側プロペラ2は後側プロペラ1
と逆方向に回転駆動される。なお、このとき上述
した歯車のギア比は適当に設定され、前側プロペ
ラ2と後側プロペラ1とはほぼ同じ回転速度で互
いに逆転するようになつている。 As a result, the front propeller 2 becomes the rear propeller 1.
It is rotated in the opposite direction. At this time, the gear ratio of the above-mentioned gears is set appropriately, so that the front propeller 2 and the rear propeller 1 rotate in opposite directions at approximately the same rotational speed.
したがつて、本考案の二重反転プロペラ装置を
そなえた船舶でも、従来のものと同様、プロペラ
1,2の後方に流出していた回転エネルギが回収
されて、一般の単一プロペラを有する船舶に比較
し、その推進効率を高めることができる。 Therefore, even in a ship equipped with the counter-rotating propeller device of the present invention, the rotational energy that was flowing out behind the propellers 1 and 2 can be recovered, as in the conventional case, and it can be used in a ship equipped with a general single propeller. The propulsion efficiency can be increased compared to the previous model.
一方、内軸3は、入力側大歯車6cと出力側大
歯車5bとの間において、内軸軸受11により支
持されるので、内軸3におけるたわみの発生が防
止され、この内軸3に作用していた大きな曲げ応
力が解消されて、内軸3の使用寿命が延びるとと
もに、従来、内軸3と外軸4とが接触することに
よつて生じていた不具合も解消される。 On the other hand, since the inner shaft 3 is supported by the inner shaft bearing 11 between the input side large gear 6c and the output side large gear 5b, the occurrence of deflection in the inner shaft 3 is prevented, and the inner shaft 3 is The large bending stress caused by the inner shaft 3 is eliminated, the service life of the inner shaft 3 is extended, and the problems conventionally caused by contact between the inner shaft 3 and the outer shaft 4 are also eliminated.
また、内軸軸受11あるいは軸受12,13は
2つ割れ構造に形成されているので、その上部部
材11aあるいは12a等を取り外すことによ
り、その内部の点検やメンテナンスを容易に行な
えるのである。 Further, since the inner shaft bearing 11 or the bearings 12 and 13 are formed in a two-piece structure, inspection and maintenance of the inside thereof can be easily performed by removing the upper member 11a or 12a, etc.
なお、内軸軸受11の二重反転プロペラ装置内
への組込は、同内軸軸受11の下部部材11bの
みを据付けた状態で内軸3を挿入した後、その上
部部材11aを取り付けることによつて行なわれ
る。 The inner shaft bearing 11 can be assembled into the counter-rotating propeller device by inserting the inner shaft 3 with only the lower member 11b of the inner shaft bearing 11 installed, and then attaching its upper member 11a. It is done by twisting.
以上詳述したように、本考案の舶用二重反転プ
ロペラ装置によれば、主機により回転駆動される
内軸と、同内軸の後端に装着された後側プロペラ
とをそなえるとともに、上記内軸に重合する管状
の外軸と、同外軸の後端に装着されて上記後側プ
ロペラの前側に配設された前側プロペラとをそな
え、上記内軸と同方向へ回転しうるように同内軸
に同軸的に装着された入力側大歯車と、上記外軸
の前端部に同軸的に装着された出力側大歯車との
間に両大歯車を互いに逆転させる連動歯車機構が
設けられて、上記内軸を支持する軸受が、上記の
入力側大歯車と出力側大歯車との間に配設され、
同軸受が分解可能の2つ割れ構造になつていると
いう極めて簡素な構成で、内軸におけるたわみの
発生が防止されるようになり、これにより、同内
軸と外軸とが接触することによつて生じていた不
具合が解消されるとともに、回転に伴つて発生し
ていた繰り返し応力による内軸の疲労が軽減され
るので、内軸の寿命を延ばすことができるのであ
る。
As described in detail above, the marine contra-rotating propeller device of the present invention includes an inner shaft rotationally driven by the main engine, a rear propeller attached to the rear end of the inner shaft, and It has a tubular outer shaft that overlaps with the shaft, and a front propeller that is attached to the rear end of the outer shaft and disposed in front of the rear propeller, and is rotatable in the same direction as the inner shaft. An interlocking gear mechanism is provided between an input-side large gear coaxially mounted on the inner shaft and an output-side large gear coaxially mounted on the front end of the outer shaft, which rotates both the large gears in reverse rotation. , a bearing supporting the inner shaft is disposed between the input side large gear and the output side large gear,
The bearing has an extremely simple structure in which the bearing is split into two parts that can be disassembled, which prevents the inner shaft from deflecting, which prevents the inner and outer shafts from coming into contact with each other. This eliminates the problems caused by this, and reduces the fatigue of the inner shaft due to repeated stress that occurs with rotation, thereby extending the life of the inner shaft.
また、軸受が2つ割れ構造であるため、その上
部部材を取り外すことにより、その内部の点検や
メンテナンスを容易に行なえる利点もある。 Further, since the bearing has a two-piece structure, there is an advantage that inspection and maintenance of the inside can be easily performed by removing the upper member.
第1,2図は本考案の一実施例としての舶用二
重反転プロペラ装置を示すもので、第1図はその
要部を模式的に示す縦断面図、第2図はその軸受
を示す分解斜視図であり、第3〜5図は従来の舶
用二重反転プロペラ装置を示すもので、第3図は
その縦断面図、第4図はその出力側大歯車および
出力側小歯車の作用を説明するための模式図、第
5図はその入力側大歯車、入力側小歯車およびア
イドル歯車の作用を説明するための模式図であ
る。
1……後側プロペラ、2……前側プロペラ、3
……内軸、4……外軸、5a……出力側小歯車、
5b……出力側大歯車、6a……入力側小歯車、
6b……アイドル歯車、6c……入力側大歯車、
7……弾性継手、8,9……スラスト軸受、10
……主機、11……内軸軸受、11a……上部部
材、11b……下部部材、12……軸受、12a
……上部部材、12b……下部部材、13……軸
受、14……たわみ軸、M……連動歯車機構。
Figures 1 and 2 show a counter-rotating marine propeller device as an embodiment of the present invention. Figure 1 is a vertical cross-sectional view schematically showing its main parts, and Figure 2 is an exploded view showing its bearings. FIG. 3 is a perspective view, and FIGS. 3 to 5 show a conventional marine counter-rotating propeller device, FIG. 3 is a longitudinal sectional view thereof, and FIG. FIG. 5 is a schematic diagram for explaining the functions of the input side large gear, input side pinion gear, and idle gear. 1... Rear propeller, 2... Front propeller, 3
...Inner shaft, 4...Outer shaft, 5a...Output side small gear,
5b... Output side large gear, 6a... Input side small gear,
6b...Idle gear, 6c...Input side large gear,
7...Elastic joint, 8, 9...Thrust bearing, 10
... Main engine, 11 ... Inner shaft bearing, 11a ... Upper member, 11b ... Lower member, 12 ... Bearing, 12a
...Upper member, 12b...Lower member, 13...Bearing, 14...Deflection shaft, M...Interlocking gear mechanism.
Claims (1)
端に装着された後側プロペラとをそなえるととも
に、上記内軸に重合する管状の外軸と、同外軸の
後端に装着されて上記後側プロペラの前側に配設
された前側プロペラとをそなえ、上記内軸と同方
向へ回転しうるように同内軸に同軸的に装着され
た入力側大歯車と、上記外軸の前端部に同軸的に
装着された出力側大歯車との間に両大歯車を互い
に逆転させる連動歯車機構が設けられて、上記内
軸を支持する軸受が、上記の入力側大歯車と出力
側大歯車との間に配設され、同軸受が分解可能の
2つ割れ構造に構成されていることを特徴とす
る、舶用二重反転プロペラ装置。 It has an inner shaft that is rotationally driven by the main engine, a rear propeller attached to the rear end of the inner shaft, a tubular outer shaft that overlaps the inner shaft, and a rear propeller attached to the rear end of the outer shaft. a front propeller disposed in front of the rear propeller; an input large gear coaxially attached to the inner shaft so as to rotate in the same direction as the inner shaft; and a front end of the outer shaft. An interlocking gear mechanism is provided between the input side large gear and the output side large gear coaxially mounted on the input side large gear, and an interlocking gear mechanism that rotates both large gears in reverse rotation with respect to each other. A counter-rotating propeller device for marine use, characterized in that the contra-rotating propeller device is disposed between a gear and a coaxial bearing and is configured in a two-piece structure that can be disassembled.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP18289384U JPH0228290Y2 (en) | 1984-11-30 | 1984-11-30 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP18289384U JPH0228290Y2 (en) | 1984-11-30 | 1984-11-30 |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS6197649U JPS6197649U (en) | 1986-06-23 |
JPH0228290Y2 true JPH0228290Y2 (en) | 1990-07-30 |
Family
ID=30740425
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP18289384U Expired JPH0228290Y2 (en) | 1984-11-30 | 1984-11-30 |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH0228290Y2 (en) |
-
1984
- 1984-11-30 JP JP18289384U patent/JPH0228290Y2/ja not_active Expired
Also Published As
Publication number | Publication date |
---|---|
JPS6197649U (en) | 1986-06-23 |
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