JPH0529999Y2 - - Google Patents
Info
- Publication number
- JPH0529999Y2 JPH0529999Y2 JP3991585U JP3991585U JPH0529999Y2 JP H0529999 Y2 JPH0529999 Y2 JP H0529999Y2 JP 3991585 U JP3991585 U JP 3991585U JP 3991585 U JP3991585 U JP 3991585U JP H0529999 Y2 JPH0529999 Y2 JP H0529999Y2
- Authority
- JP
- Japan
- Prior art keywords
- shaft
- bearing
- thrust
- propeller
- thrust bearing
- 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
Links
- 230000008878 coupling Effects 0.000 description 4
- 238000010168 coupling process Methods 0.000 description 4
- 238000005859 coupling reaction Methods 0.000 description 4
- 230000002093 peripheral effect Effects 0.000 description 4
- 238000009434 installation Methods 0.000 description 3
- 238000012423 maintenance Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 238000012856 packing Methods 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
Landscapes
- Sliding-Contact Bearings (AREA)
Description
【考案の詳細な説明】
(産業上の利用分野)
本考案は、内、外軸によつて駆動される船舶用
二重反転プロペラ装置のスラスト軸受に関するも
のである。[Detailed Description of the Invention] (Industrial Application Field) The present invention relates to a thrust bearing for a counter-rotating marine propeller device driven by inner and outer shafts.
(従来の技術)
前記船舶用二重反転プロペラ装置の従来例を実
願昭58−110127号によつて説明すると、低速デイ
ーゼル主機9の出力軸に直結状に連結された内軸
3によつて船尾側プロペラ1が回転され、内軸3
に設けた弾性継手5と遊星歯車式の反転装置6を
介して外軸4を逆回転させ、同外軸4によつて船
首側プロペラ2が逆回転される構造になつてお
り、前記遊星歯車式反転装置6は、太陽歯車6a
と、大、小遊星歯車6b,6cと、リングリヤ6
d等によつて構成されているとともに、低速デイ
ーゼル主機9内のスラスト軸受8aと内、外軸間
に設けられたスラスト軸受8bによつて前記内、
外軸3,4がスラスト軸受で支持され、船尾側プ
ロペラ1により発生するスラストは、スラスト軸
受8aで受けられるとともに、船首側プロペラ2
で発生するスラストは、スラスト軸受8bにより
内軸4に伝えられ前記スラスト軸受8aで受けら
れて、前記反転装置6即ちそのリングギヤ6dを
保護した構成になつている。(Prior Art) A conventional example of the contra-rotating propeller device for ships is described in Utility Model Application No. 110127/1985. The stern propeller 1 is rotated, and the inner shaft 3
The structure is such that the outer shaft 4 is reversely rotated through an elastic joint 5 and a planetary gear-type reversing device 6 provided in The type reversing device 6 is a sun gear 6a.
, large and small planetary gears 6b, 6c, and ring rear 6
d, etc., and the above-mentioned inner,
The outer shafts 3 and 4 are supported by thrust bearings, and the thrust generated by the stern propeller 1 is received by the thrust bearing 8a, and the thrust generated by the stern propeller 2 is received by the thrust bearing 8a.
The thrust generated in the above is transmitted to the inner shaft 4 by the thrust bearing 8b and received by the thrust bearing 8a, thereby protecting the reversing device 6, that is, its ring gear 6d.
また、特願昭57−206065号によつて他の従来例
を説明すると、船尾側プロペラ1駆動用の内軸
3、船首側プロペラ2駆動用の外軸4と、中速デ
イーゼル主機9′の出力軸9aとの間に、出力軸
9aで回転される歯車7a、該歯車7aで駆動さ
れる油圧ポンプ7b、該油圧ポンプ7bで作動さ
れる油圧モータ7c、出力軸9aで駆動される太
陽歯車7d、太陽歯車7d上に噛合・配設され前
記油圧モータ7cに連設されるとともに前記内軸
3に出力する複数の遊星歯車7e、遊星歯車7e
に噛合され外軸4に出力するリングギヤ7f等か
らなり、減速、逆回転機能を有する遊星歯車式二
重反転装置7を設けた構造になつている。 Another conventional example is explained in Japanese Patent Application No. 57-206065, which includes an inner shaft 3 for driving the stern propeller 1, an outer shaft 4 for driving the bow propeller 2, and a medium-speed diesel main engine 9'. A gear 7a rotated by the output shaft 9a, a hydraulic pump 7b driven by the gear 7a, a hydraulic motor 7c operated by the hydraulic pump 7b, and a sun gear driven by the output shaft 9a. 7d, a plurality of planetary gears 7e, which are meshed and disposed on the sun gear 7d, are connected to the hydraulic motor 7c, and output to the inner shaft 3;
The ring gear 7f meshes with the outer shaft 4 and outputs the output to the outer shaft 4, and the structure includes a planetary gear type counter-rotating device 7 having deceleration and reverse rotation functions.
(従来技術の問題点)
第5図に示した従来例は、低速デイーゼル主機
9を駆動源とする場合の船舶用二重反転プロペラ
装置であつて、船尾側プロペラ1で発生するスラ
ストは、内軸3を経て主機内のスラスト軸受8a
で受けられ、船首側プロペラ2で発生するスラス
トは、外軸4、スラスト軸受8bを経て内軸3に
伝えられスラスト軸受8aで受けられて、遊星歯
車式反転装置6に前記スラストが影響を及ぼさな
い構造になつているが、内軸3と外軸4間にスラ
スト軸受8bを組込むことは技術的に極めて難し
く、該スラスト軸受8bの組付精度にバラツキが
生じ勝ちであつて信頼性に問題があり、また、前
記スラスト軸受8bの介装により内、外軸3,4
の組込、配設が難しくなるなどの問題点がある。(Problems with the Prior Art) The conventional example shown in FIG. Thrust bearing 8a inside the main engine via shaft 3
The thrust generated by the bow propeller 2 is transmitted to the inner shaft 3 via the outer shaft 4 and the thrust bearing 8b, and is received by the thrust bearing 8a, so that the thrust does not affect the planetary gear type reversing device 6. However, it is technically extremely difficult to assemble the thrust bearing 8b between the inner shaft 3 and the outer shaft 4, and the assembly accuracy of the thrust bearing 8b is likely to vary, resulting in reliability problems. Also, by interposing the thrust bearing 8b, the inner and outer shafts 3, 4
There are problems such as making it difficult to incorporate and arrange.
また、第6図に示した従来例は、中速デイーゼ
ル主機9′を駆動源とする場合の船舶用二重反転
プロペラ装置であつて、この場合は減速とともに
逆回転をすることが必要となり、図示のように複
雑な機構の遊星歯車式二重反転装置7が使用され
ているため、前記二重反転装置7側に、船尾側プ
ロペラ1、船首側プロペラ2で発生するスラスト
が影響しないように特に留意する必要があるが、
図示のようにその対策が施されてなく技術的課題
になつている。 Furthermore, the conventional example shown in FIG. 6 is a contra-rotating propeller device for a ship when the medium-speed diesel main engine 9' is used as the drive source, and in this case, it is necessary to reverse rotation while decelerating. As shown in the figure, since a planetary gear type counter-rotating device 7 with a complicated mechanism is used, it is necessary to prevent the thrust generated by the stern propeller 1 and the bow propeller 2 from affecting the counter-rotating device 7 side. Particular attention should be paid to
As shown in the figure, no countermeasures have been taken and this has become a technical issue.
(考案の目的、問題点の解決手段)
本案は、従来の船舶用二重反転プロペラ装置に
おける前記のような問題点に対処するための考案
であつて、反転装置とプロペラ間の内軸外周面に
固設された鍔と、該鍔に対応させて外軸に介装し
連結された軸受用外軸と、該軸受用外軸の内周側
に取付けられ前記鍔の両側面に対設された着脱さ
れる1対のスラストパツド付軸受金具とを具備し
た構成に特徴を有し、反転装置とプロペラ間の内
軸外周面に設けた鍔に対応させて、外軸に軸受用
外軸を介装し連結するとともに、前記軸受用外側
の内周側に1対のスラストパツド付軸受金具を着
脱可能に取付けることにより、反転装置とプロペ
ラ間における内、外軸間にストラスト軸受を組込
むことができ、反転装置へのスラストの影響を解
消するとともに、該スラスト軸受の介装組込み配
置、保守管理を容易にして、組付精度を高めスラ
スト軸受性能、信頼性を著しく向上させるととも
に、内、外軸の組込み配置を容易にして前記のよ
うな問題点を解消した船舶用二重反転プロペラ装
置のスラスト軸受を提供するにある。(Purpose of the invention, means for solving problems) This invention is an invention to deal with the above-mentioned problems in the conventional contra-rotating propeller device for ships, and it is a flange fixed to the flange; an outer bearing shaft interposed and connected to the outer shaft in correspondence with the flange; It is characterized by a structure that includes a pair of bearing fittings with thrust pads that can be attached and detached, and the outer shaft for bearings is attached to the outer shaft in correspondence with the flange provided on the outer circumferential surface of the inner shaft between the reversing device and the propeller. At the same time, a thrust bearing can be installed between the inner and outer shafts between the reversing device and the propeller by removably attaching a pair of bearing fittings with thrust pads to the inner peripheral side of the outer side of the bearing. In addition to eliminating the influence of thrust on the reversing device, it also facilitates the installation and maintenance of the thrust bearing, increases assembly accuracy, and significantly improves thrust bearing performance and reliability. It is an object of the present invention to provide a thrust bearing for a counter-rotating propeller device for a ship, which can be easily assembled and arranged and eliminates the above-mentioned problems.
(考案の実施例)
第1図ないし第4図に本考案の一実施例を示し
ており、第1図において11は船尾側プロペラ、
12は船首側プロペラ、13は船尾側プロペラ1
1が直結されている主内軸、14は船首側プロペ
ラ12が直結されている主外軸であつて、前記主
内軸13に第1中間内軸13aと第2中間内軸1
3bを軸継手20によつて着脱可能に連結して内
軸13,13a,13bに構成し、前記主外軸1
4に二つ割れの中空外軸14aと14bをスラス
ト軸受30の介装により軸継手ボルト等で着脱可
能に連結して内軸14,14a,14bに構成さ
れている。(Embodiment of the invention) An embodiment of the invention is shown in Figs. 1 to 4. In Fig. 1, 11 is a stern propeller;
12 is the bow propeller, 13 is the stern propeller 1
1 is a main inner shaft to which is directly connected, and 14 is a main outer shaft to which the bow propeller 12 is directly connected, and the main inner shaft 13 has a first intermediate inner shaft 13a and a second intermediate inner shaft 1.
3b are removably connected by a shaft coupling 20 to form the inner shafts 13, 13a, 13b, and the main outer shaft 1
The inner shafts 14, 14a, 14b are constructed by removably connecting hollow outer shafts 14a and 14b, which are split into two halves, with a thrust bearing 30 interposed therebetween, using a shaft coupling bolt or the like.
さらに、前記内軸13,13a,13bの第2
中間内軸13bと前記外軸14,14a,14b
の中空外軸14bは、中速デイーゼル主機19の
出力軸19aに弾性継手15と遊星歯車式二重反
転装置17によつて駆動連結され、該遊星歯車式
二重反転装置17は、第1,2図に示すように弾
性継手15に連結された入力用の太陽歯車17a
と、該太陽歯車17aに噛合され前記第2中間内
軸13bに連結、出力する複数の遊星歯車17
b、および前記遊星歯車17bに噛合され前記中
空外軸14bに連結されたリングギヤ17cから
なり、中速デイーゼル主機19′の動力が弾性継
手15を介して太陽歯車17aに伝達され、遊星
歯車17bを介して内軸13,13a,13bが
矢示方向に減速回転されるとともに、遊星歯車1
7b、リングギヤ17cを介して外軸14,14
a,14bが矢示方向に減速逆回転され、減速と
逆回転機能を有する構成になつている。なお、図
中17dはリングギヤ17cに設けられたスラス
ト軸受である。 Further, the second inner shaft 13, 13a, 13b
Intermediate inner shaft 13b and the outer shafts 14, 14a, 14b
The hollow outer shaft 14b is drivingly connected to the output shaft 19a of the medium-speed diesel main engine 19 by an elastic joint 15 and a planetary gear type counter-rotating device 17. As shown in FIG. 2, an input sun gear 17a connected to an elastic joint 15
and a plurality of planetary gears 17 meshed with the sun gear 17a and connected to and output from the second intermediate inner shaft 13b.
b, and a ring gear 17c meshed with the planetary gear 17b and connected to the hollow outer shaft 14b.The power of the medium-speed diesel main engine 19' is transmitted to the sun gear 17a via the elastic joint 15, and the ring gear 17c meshes with the planetary gear 17b and is connected to the hollow outer shaft 14b. The inner shafts 13, 13a, 13b are rotated at a reduced speed in the direction of the arrow, and the planetary gear 1
7b, and the outer shafts 14, 14 via the ring gear 17c.
a and 14b are decelerated and reversely rotated in the direction of the arrow, and are configured to have deceleration and reverse rotation functions. In addition, 17d in the figure is a thrust bearing provided in the ring gear 17c.
さらにまた、前記スラスト軸受30について詳
述すると、第1,3,4図に示すように前記遊星
歯車式二重反転装置17と船尾、船首側プロペラ
11,12との間の内軸13,13a,13b、
即ちその第1中間内軸13aの外周面に鍔31を
固設し、該鍔31に対応させて前記中空外軸14
aと14bとの間に軸受用外軸32を介装し軸継
手ボルト等の手段で着脱可能に連結するととも
に、前記軸受用外軸32の内周に、リング板状に
形成された二つ割れの軸受金具33,33を複数
のリーマボルト・ナツト35,36で着脱可能に
取付けられ、該軸受金具33,33は、前記鍔3
1の両側面に所定の間隙を設けて対設され、対接
面側にスラストパツド34が付設された構成にな
つている。なお、図中32a,33aはリーマボ
ルト35のリーマボルト穴、32bは中空外軸1
4a,14bとの結合用ボルト用のボルト穴、3
7はパツキンであり、また40aは船体、40b
は機関室の後部隔壁である。 Furthermore, to explain the thrust bearing 30 in detail, as shown in FIGS. ,13b,
That is, a flange 31 is fixed to the outer peripheral surface of the first intermediate inner shaft 13a, and the hollow outer shaft 14 is made to correspond to the flange 31.
A bearing outer shaft 32 is interposed between a and 14b and removably connected by means such as a shaft coupling bolt, and two rings formed in the shape of a ring plate are provided on the inner periphery of the bearing outer shaft 32. The bearing fittings 33, 33 of the cracks are removably attached with a plurality of reamer bolts/nuts 35, 36, and the bearing fittings 33, 33 are attached to the flange 3.
The thrust pads 34 are arranged opposite to each other with a predetermined gap on both sides of the thrust pad 1, and a thrust pad 34 is attached to the opposing surface. In addition, in the figure, 32a and 33a are the reamer bolt holes of the reamer bolt 35, and 32b is the hollow outer shaft 1.
Bolt hole for connecting bolt with 4a, 14b, 3
7 is the packing, 40a is the hull, and 40b
is the rear bulkhead of the engine room.
(作用)
本考案の実施例は、前記のような構成になつて
おり、中速デイーゼル主機19を駆動源にした場
合には、減速とともに相対的に逆回転させて内、
外軸を回転する必要があるため、前記のような構
成よりなる遊星歯車式二重反転装置17を用い
て、内軸13,13a,13bと外軸14,14
a,14bを減速回転させるとともに、相対的に
逆回転する1入力軸に対し2出力軸の機構になつ
ており、減速とともに船尾側プロペラ11と船尾
側プロペラ12を相対的に逆回転駆動できる。
(第6図に示した従来例と同様な機能になつてい
る)
さらに、前記スラスト軸受30は、前記二重反
転装置17と船尾、船首側プロペラ11,12と
の間で内、外軸間に介装・配設されており、船首
側プロペラ12で発生するスラストは、主内軸1
4、中空外軸14aを介しさらに軸受用外軸3
2、軸受金具33、スラストパツド34、鍔31
を介して内軸の第1中間軸受13aに伝わり、船
尾側プロペラ11で発生するスラストとともにさ
らに第2中間内軸13b、出力軸19aを介し
て、中速デイーゼル主機19内に配設されている
スラスト軸受(図示省略)で受けられるため、前
記遊星歯車式二重反転装置17への前記スラスト
の影響は殆んどない。(Function) The embodiment of the present invention has the above-described configuration, and when the medium-speed diesel main engine 19 is used as the drive source, the engine is rotated in a relatively reverse direction as it decelerates.
Since it is necessary to rotate the outer shaft, a planetary gear type counter-rotating device 17 having the above-mentioned configuration is used to rotate the inner shafts 13, 13a, 13b and the outer shafts 14, 14.
A, 14b are rotated at a deceleration rate, and the stern side propeller 11 and the stern side propeller 12 can be driven to rotate in a relatively reverse direction while decelerating.
(It has the same function as the conventional example shown in FIG. 6.) Furthermore, the thrust bearing 30 is provided between the inner and outer shafts between the counter-rotating device 17 and the stern and bow propellers 11 and 12. The thrust generated by the bow propeller 12 is transmitted through the main inner shaft 1.
4. The outer shaft for bearing 3 is further connected via the hollow outer shaft 14a.
2, bearing fittings 33, thrust pad 34, collar 31
The thrust is transmitted to the first intermediate bearing 13a of the inner shaft via the stern propeller 11, and is further disposed in the medium-speed diesel main engine 19 via the second intermediate inner shaft 13b and the output shaft 19a. Since the thrust is received by a thrust bearing (not shown), the thrust has almost no effect on the planetary gear type counter-rotating device 17.
また、前記スラスト軸受30は、第4図に示す
ように内軸13,13a,13bの第1中間内軸
13aにおける鍔31部に軸受用外軸32を嵌装
し、該軸受用外軸32の両側から軸受金具33,
33を挿入し、該軸受金具33,33を軸受用外
軸32の内周側に複数のリーマボルト35、パツ
キン37、ナツト36によつて締付、固定でき
て、鍔31に対する軸受金具33,33の対接配
置を正確に調節でき、前記軸受用外軸32を中空
外軸14a,14b間に介装し軸継手ボルト等で
連結して組込むことができる。また、軸受金具3
3に付設されているスラストパツド34の保守は
二つ割れの中空軸14a,14bを外し、リーマ
ボルト35を抜くことにより容易に行うことがで
きる。 Further, as shown in FIG. 4, the thrust bearing 30 has an outer shaft 32 for a bearing fitted in a flange 31 portion of the first intermediate inner shaft 13a of the inner shafts 13, 13a, 13b. From both sides of the bearing fittings 33,
33, and the bearing fittings 33, 33 can be tightened and fixed to the inner circumferential side of the outer bearing shaft 32 with a plurality of reamer bolts 35, packings 37, and nuts 36, and the bearing fittings 33, 33 can be fixed to the collar 31. The bearing outer shaft 32 can be interposed between the hollow outer shafts 14a and 14b and connected by a shaft coupling bolt or the like and assembled. In addition, bearing fittings 3
Maintenance of the thrust pad 34 attached to 3 can be easily performed by removing the hollow shafts 14a and 14b, which are split into two, and pulling out the reamer bolt 35.
さらにまた、前記スラスト軸受30の分離、結
合とともに内、外軸の組込みが容易になつている
とともに、内軸13,13a,13bは、主内軸
13と第1中間内軸13aおよび第2中間内軸1
3bに分離、結合でき、外軸14,14a,14
bも主外軸14と中空外軸14aおよび14bに
分離、結合でき、内、外軸の組込み配置を容易に
行うことができる。 Furthermore, the separation and connection of the thrust bearing 30 and the assembly of the inner and outer shafts are facilitated. Inner shaft 1
3b, can be separated and combined into outer shafts 14, 14a, 14
b can also be separated and combined into the main outer shaft 14 and the hollow outer shafts 14a and 14b, making it easy to incorporate and arrange the inner and outer shafts.
(考案の効果)
前述のように本考案は、反転装置17とプロペ
ラ11,12間の内軸外周面に固設された鍔31
と、該鍔31に対応させて外軸に介装し連結され
た軸受用外軸32と、該軸受用外軸32の内周側
に取付けられ前記鍔31の両側面に対設された着
脱される1対のスラストパツド34付軸受金具3
3,33とを具備した構成になつているため、反
転装置とプロペラ間における内、外軸間にスラス
ト軸受を組込むことができ、反転装置へのスラス
トの影響が解消されているとともに、前記内、外
軸間へのスラスト軸受の組込み配置、保守管理が
容易であり、組付精度が高められスラスト軸受性
能、信頼性が著しく向上されており、さらに、前
記スラスト軸受の介装連結により内、外軸の組込
み配置を容易にできるなどの効果を有している。
本考案は、外軸に軸受用外軸が一体的に介装、連
結されているため、外軸の動力伝達強度が高めら
れ、軸受用外軸に1対の軸受金具を着脱可能に取
付けているため、鍔に対する軸受金具の取付位置
調整が可能であつて、組付精度が高められてい
る。(Effects of the invention) As mentioned above, the present invention has a flange 31 fixed to the outer peripheral surface of the inner shaft between the reversing device 17 and the propellers 11 and 12.
, an outer bearing shaft 32 interposed and connected to the outer shaft in correspondence with the flange 31, and a removable shaft 32 attached to the inner peripheral side of the outer shaft 32 and opposite to both sides of the flange 31. Bearing fitting 3 with a pair of thrust pads 34
3 and 33, it is possible to incorporate a thrust bearing between the inner and outer shafts between the reversing device and the propeller, eliminating the influence of thrust on the reversing device, and eliminating the influence of thrust on the reversing device. , the installation and maintenance of the thrust bearing between the outer shafts is easy, the assembly accuracy is increased, and the thrust bearing performance and reliability are significantly improved.Furthermore, the interposed connection of the thrust bearing allows the inner This has the advantage of facilitating the installation and arrangement of the outer shaft.
In this invention, the outer shaft for bearings is integrally interposed and connected to the outer shaft, so the power transmission strength of the outer shaft is increased, and a pair of bearing fittings are removably attached to the outer shaft for bearings. Therefore, it is possible to adjust the mounting position of the bearing fitting with respect to the flange, and the assembly accuracy is improved.
第1図は本考案の一実施例を示す全体の縦断面
図、第2図は第1図の−部分の断面図、第3
図は第1図の部分の拡大断面図、第4図はスラ
スト軸受の分解斜視図、第5図は従来例を示す縦
断面図、第6図Aは他の従来例を示す機構図、第
6図Bは第6図Aの−部分の断面図である。
11,12……プロペラ、13,13a,13
b……内軸、14,14a,14b……外軸、1
7……反転装置、30……スラスト軸受、31…
…鍔、32……軸受用外軸、33……軸受金具、
34……スラストパツド。
Fig. 1 is an overall vertical cross-sectional view showing one embodiment of the present invention, Fig. 2 is a cross-sectional view of the - portion of Fig. 1, and Fig. 3 is a cross-sectional view of the - portion of Fig.
The figures are an enlarged sectional view of the part shown in Fig. 1, Fig. 4 is an exploded perspective view of the thrust bearing, Fig. 5 is a vertical sectional view showing a conventional example, Fig. 6A is a mechanism diagram showing another conventional example, FIG. 6B is a sectional view of the - portion of FIG. 6A. 11, 12... Propeller, 13, 13a, 13
b...Inner shaft, 14, 14a, 14b...Outer shaft, 1
7... Reversing device, 30... Thrust bearing, 31...
...Brim, 32...Outer shaft for bearing, 33...Bearing fitting,
34...Thrust pad.
Claims (1)
た鍔と、該鍔に対応させて外軸に介装し連結され
た軸受用外軸と、該軸受用外軸の内周側に取付け
られ前記鍔の両側面に対設された着脱される1対
のスラストパツド付軸受金具とを具備したことを
特徴とする船舶用二重反転プロペラ装置のスラス
ト軸受。 A collar fixed to the outer circumferential surface of the inner shaft between the reversing device and the propeller, an outer bearing shaft interposed and connected to the outer shaft corresponding to the collar, and attached to the inner circumferential side of the outer shaft for the bearing. 1. A thrust bearing for a counter-rotating propeller device for a ship, characterized in that the thrust bearing is provided with a pair of bearing fittings with thrust pads that are attached and detached and are installed oppositely on both sides of the flange.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP3991585U JPH0529999Y2 (en) | 1985-03-22 | 1985-03-22 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP3991585U JPH0529999Y2 (en) | 1985-03-22 | 1985-03-22 |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS61157095U JPS61157095U (en) | 1986-09-29 |
JPH0529999Y2 true JPH0529999Y2 (en) | 1993-07-30 |
Family
ID=30548310
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP3991585U Expired - Lifetime JPH0529999Y2 (en) | 1985-03-22 | 1985-03-22 |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH0529999Y2 (en) |
-
1985
- 1985-03-22 JP JP3991585U patent/JPH0529999Y2/ja not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
JPS61157095U (en) | 1986-09-29 |
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