JPH0535598U - Shaft structure of marine counter-rotating propeller device - Google Patents

Shaft structure of marine counter-rotating propeller device

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Publication number
JPH0535598U
JPH0535598U JP9312891U JP9312891U JPH0535598U JP H0535598 U JPH0535598 U JP H0535598U JP 9312891 U JP9312891 U JP 9312891U JP 9312891 U JP9312891 U JP 9312891U JP H0535598 U JPH0535598 U JP H0535598U
Authority
JP
Japan
Prior art keywords
shaft
output shaft
elastic joint
input shaft
attached
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.)
Granted
Application number
JP9312891U
Other languages
Japanese (ja)
Other versions
JP2591910Y2 (en
Inventor
政利 江田
彰 保志
昇 峠
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries 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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP1991093128U priority Critical patent/JP2591910Y2/en
Publication of JPH0535598U publication Critical patent/JPH0535598U/en
Application granted granted Critical
Publication of JP2591910Y2 publication Critical patent/JP2591910Y2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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  • Support Of The Bearing (AREA)
  • Structure Of Transmissions (AREA)
  • Gear Transmission (AREA)
  • Retarders (AREA)

Abstract

(57)【要約】 (修正有) 【目的】 舶用二重反転プロペラ装置に関し、外軸の軸
受部の改良に関する。 【構成】 機関の出力軸1aに取付けられた組立てフラ
ンジ8とこれに取付けられた弾性継手7と、前端部を弾
性継手7にて接続されるとともに中空状の外軸5と、前
端部を出力軸1aに接続されるとともに後部プロペラを
取付けられた内軸2とをそなえた、舶用二重反転プロペ
ラ装置において、入力軸61を弾性継手7の出力軸71に接
続するとともに入力軸軸受11を設け、弾性継手7の出力
軸を出力軸71の前端部附近に配設することにより、スパ
ンL0を大きく設定することができ、弾性継手7の重量
が出力軸71にかかっても入力軸61が傾斜するのを防止
し、その結果反転歯車装置の信頼性を向上できるように
した。
(57) [Summary] (Corrected) [Purpose] To improve the bearing of the outer shaft of a marine counter-rotating propeller device. [Structure] An assembly flange 8 attached to an output shaft 1a of an engine, an elastic joint 7 attached thereto, a front end portion thereof is connected by an elastic joint 7, and a hollow outer shaft 5 and a front end portion are output. In a marine counter-rotating propeller device that is connected to the shaft 1a and has an inner shaft 2 to which a rear propeller is attached, an input shaft 61 is connected to an output shaft 71 of an elastic joint 7 and an input shaft bearing 11 is provided. By arranging the output shaft of the elastic joint 7 near the front end portion of the output shaft 71, the span L 0 can be set to a large value, and the input shaft 61 can be set even if the weight of the elastic joint 7 is applied to the output shaft 71. The tilting is prevented, and as a result, the reliability of the reversing gear device can be improved.

Description

【考案の詳細な説明】[Detailed description of the device]

【0001】[0001]

【産業上の利用分野】[Industrial applications]

本考案は、舶用二重反転プロペラ装置に関し、特にその外軸の軸受部の改良に 関する。 The present invention relates to a contra-rotating propeller device for a ship, and more particularly to improvement of a bearing portion of its outer shaft.

【0002】[0002]

【従来の技術】[Prior Art]

中空状の外軸の後端部に前部プロペラを取付けられるとともに、上記外軸の内 部にこれと同芯状に配設され後端部に後部プロペラを取付けられた内軸とからな り、上記の内軸と外軸とが互いに反対方向に回転させられるように構成された舶 用二重反転プロペラ装置が、従来から知られている。 It consists of a hollow outer shaft with a front propeller attached to the rear end, and an inner shaft with the rear propeller attached to the inner end of the outer shaft concentrically. A marine counter-rotating propeller device configured to rotate the inner shaft and the outer shaft in mutually opposite directions has been conventionally known.

【0003】 その1例を図2,図3により説明すると、図2において、符号1は主機関を示 しており、主機関1の出力軸1aに内軸2を介して後方プロペラ3が直接駆動さ れるように接続される一方、反転歯車装置6を介して、外軸5とこれに接続され た前方プロペラ4とが主機関1と逆方向に回転するように弾性継手7を介して主 機関の出力軸1aに接続されている。なお弾性継手7は主機関1の変動トルクか ら反転歯車装置6の歯面を保護するために設けられている。An example thereof will be described with reference to FIGS. 2 and 3. In FIG. 2, reference numeral 1 indicates a main engine, and the rear propeller 3 is directly connected to the output shaft 1a of the main engine 1 via the inner shaft 2. While being connected so as to be driven, the outer shaft 5 and the front propeller 4 connected to the outer shaft 5 via the reversing gear device 6 are connected via an elastic joint 7 so as to rotate in the opposite direction to the main engine 1. It is connected to the output shaft 1a of the engine. The elastic joint 7 is provided to protect the tooth surface of the reversing gear device 6 from the fluctuation torque of the main engine 1.

【0004】 内軸2の前端部は、図3に示すようにテーパ状に形成されて組立てフランジ8 と嵌合し、この組立てフランジ8は主機関1の出力軸1a及び弾性継手本体7と 結合される。符号71は弾性継手の出力軸を示しており、反転歯車装置6の入力軸 61と結合される。符号61aは入力軸61に一体形成された太陽歯車を示していて、 太陽歯車61aは遊星歯車63と噛み合う。遊星歯車63はケーシング9に固定された 遊星軸65により支持され、これに内歯歯車64が噛み合っていて、出力軸67が主機 関1と逆方向に回転するように構成されている。As shown in FIG. 3, the front end portion of the inner shaft 2 is formed in a tapered shape and fits with the assembly flange 8. The assembly flange 8 is coupled with the output shaft 1a of the main engine 1 and the elastic joint body 7. To be done. Reference numeral 71 denotes an output shaft of the elastic joint, which is connected to the input shaft 61 of the reversing gear device 6. Reference numeral 61a indicates a sun gear integrally formed with the input shaft 61, and the sun gear 61a meshes with the planetary gear 63. The planetary gear 63 is supported by a planetary shaft 65 fixed to the casing 9, and an internal gear 64 is meshed with the planetary gear 65 so that the output shaft 67 rotates in the direction opposite to the main engine 1.

【0005】 入力軸61を軸支すべく一対の入力軸軸受10a,10bが間隔Lをあけて配設さ れている。符号68は出力軸軸受を示し、また符号66は固定リングを示し、固定リ ングは複数個で遊星軸65を固定し、かつケーシング9に固定されたアーム69とも 結合することにより、遊星歯車63の位置を正しく保持するよう機能している。A pair of input shaft bearings 10 a and 10 b are arranged at a distance L 2 to support the input shaft 61. Reference numeral 68 indicates an output shaft bearing, reference numeral 66 indicates a fixed ring, and a plurality of fixed rings fix the planetary shaft 65 and are also connected to an arm 69 fixed to the casing 9 to form a planetary gear 63. It functions to hold the position of.

【0006】 ここで、弾性継手本体7の重量は組立てフランジ8と弾性継手の出力軸71とに かかる。一方、出力軸71と結合された反転歯車装置の入力軸61には太陽歯車61a が装着されているため、弾性継手本体7の重量により入力軸61が傾斜して太陽歯 車61aの歯当りが悪化しない様、一対の入力軸軸受10a,10bが装備されている 。Here, the weight of the elastic joint body 7 depends on the assembly flange 8 and the output shaft 71 of the elastic joint. On the other hand, since the sun gear 61a is mounted on the input shaft 61 of the reversing gear device coupled to the output shaft 71, the weight of the elastic joint body 7 causes the input shaft 61 to tilt and the tooth contact of the sun gear 61a to be reduced. A pair of input shaft bearings 10a and 10b are installed to prevent deterioration.

【0007】[0007]

【考案が解決しようとする課題】[Problems to be solved by the device]

ところで、上述のような従来の舶用二重反転プロペラ装置の軸構造では、次の ような問題点がある。 (1) 弾性継手の重量はかなり大きい為、入力軸の軸受2個で支持する場合、入力 軸軸受の間隔Lを大きくしないと、入力軸との傾斜角が大きすぎたり、軸受荷 重も大きくなってしまう。 (2) 太陽歯車と遊星歯車との噛み合い精度すなわち入力軸軸受の傾斜角は厳しく 管理する必要がある。この精度が悪いと遊星歯車の損傷の原因となり、最悪の場 合反転歯車装置を使用できなくなり、船舶の航行が不能となる重大事故に至る。 しかし上述の2個の入力軸軸受をケーシングに設計値通りに装着すること及びそ の装着精度の確認が難しく、重大事故のリスクをはらんでいる。 (3) 入力軸に入力軸軸受を2個装備するために、結果的に反転歯車装置の全長L1 が大きくなり軸系装置の全長も長くなってしまう。この場合機関室を大きくし船 倉スペースを縮める等の対策も必要となり船の経済性をそこなう。 又、反転歯車装置自身の重量も増加し、コストも高くなってしまう。By the way, the above-mentioned conventional shaft structure of the marine counter-rotating propeller device has the following problems. (1) Since the weight of the elastic joint is considerably large, when supporting with two bearings of the input shaft, the angle of inclination with the input shaft is too large and the bearing load is also increased unless the distance L 2 between the input shaft bearings is increased. It gets bigger. (2) The meshing accuracy between the sun gear and the planetary gears, that is, the inclination angle of the input shaft bearing must be strictly controlled. If this accuracy is poor, it may cause damage to the planetary gears, and in the worst case, the reversing gear system cannot be used, resulting in a serious accident that renders the ship unable to navigate. However, it is difficult to fit the above-mentioned two input shaft bearings to the casing according to the design values and to check the mounting accuracy, which poses a serious accident risk. (3) Since the input shaft is equipped with two input shaft bearings, as a result, the total length L 1 of the reversing gear device becomes large and the total length of the shaft system device also becomes long. In this case, it is necessary to take measures such as enlarging the engine room and reducing the cargo space, which impairs the economy of the ship. In addition, the weight of the reversing gear device itself increases and the cost also increases.

【0008】 本考案はこのような問題点の解決をはかろうとするもので、反転歯車装置の入 力軸軸受は1個とするとともに弾性継手の重量を支える為に弾性継手の出力軸の 前端部内面に軸受を装備し、これを組立てフランジに支持させて両軸受間の間隔 を大きくしながら反転歯車装置の全長を小さくできるようにした、舶用二重反転 プロペラ装置の軸構造を提供することを目的とする。The present invention is intended to solve such a problem, in which the reversing gear device has only one input shaft bearing and the front end of the output shaft of the elastic joint in order to support the weight of the elastic joint. To provide a shaft structure of a double-reversal propeller device for a ship, in which a bearing is provided on the inner surface of the section, and the assembled flange is supported by the flange to increase the distance between both bearings and reduce the total length of the reversing gear device. With the goal.

【0009】[0009]

【課題を解決するための手段】[Means for Solving the Problems]

上述の目的を達成するため、本考案の舶用二重反転プロペラ装置の軸構造は、 機関の出力軸に取付けられた組立てフランジと同組立てフランジに取付けられた 弾性継手と、前端部を上記弾性継手に反転歯車装置を介して接続されるとともに 後端部に前部プロペラを取付けられた中空状の外軸と、同外軸の内部にこれと同 芯的に配設され前端部を上記機関の出力軸に上記組立てフランジを介して接続さ れるとともに後端部に後部プロペラを取付けられた内軸とをそなえ、上記反転歯 車装置の入力軸が上記弾性継手の出力軸に接続される一方、上記反転歯車装置の 入力軸をその外周部で軸支可能な入力軸軸受が設けられ、上記弾性継手の出力軸 をその内周部で上記組立てフランジに軸支可能な軸受が上記出力軸の前端部附近 に配設されていることを特徴としている。 In order to achieve the above-mentioned object, the shaft structure of the contra-rotating propeller device for a ship according to the present invention comprises an assembly flange attached to an output shaft of an engine, an elastic joint attached to the assembly flange, and a front end portion of the elastic joint. And a hollow outer shaft having a front propeller attached to the rear end and a front end that is concentrically arranged inside the outer shaft and the front end of the engine. The output shaft is connected through the assembly flange and has an inner shaft with a rear propeller attached to the rear end, and the input shaft of the reversing gear device is connected to the output shaft of the elastic joint. An input shaft bearing capable of supporting the input shaft of the reversing gear device at its outer peripheral portion is provided, and a bearing capable of supporting the output shaft of the elastic joint at its inner peripheral portion on the assembly flange is at the front end of the output shaft. Located near the department It is characterized in that.

【0010】[0010]

【作用】[Action]

上述の本考案の舶用二重反転プロペラ装置の軸構造では、反転歯車装置の入力 軸と弾性継手の出力軸とを支える軸受のスパンを大きくとることが出来る為、歯 車装置の入力軸の傾斜を防止する作用が行なわれ、また、弾性継手の出力軸と組 立てフランジとの回転方向および回転数が同一である為、弾性継手の出力軸の内 面に設けられた軸受の性能は十分に確保され、さらにこの軸受は回転軸を支える 摺動部が無いため、焼付き等の事故の心配がない。 In the shaft structure of the above-described marine counter-rotating propeller device according to the present invention, since the span of the bearing supporting the input shaft of the reversing gear device and the output shaft of the elastic joint can be made large, the inclination of the input shaft of the gear device Since the output shaft of the elastic joint and the assembly flange have the same rotation direction and number of rotations, the performance of the bearing installed on the inner surface of the output shaft of the elastic joint is not sufficient. The bearing is secured and there is no sliding part that supports the rotating shaft, so there is no risk of accidents such as seizure.

【0011】[0011]

【実施例】【Example】

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の軸構 造について説明すると、図1は軸受部を示す断面図である。なお図1中図2およ び図3と同じ符号はほぼ同一の部材を示している。 Hereinafter, the shaft structure of a contra-rotating propeller device for a ship according to an embodiment of the present invention will be described with reference to the drawings. FIG. In FIG. 1, the same reference numerals as those in FIGS. 2 and 3 indicate almost the same members.

【0012】 この実施例も、後端部に前部プロペラを取付けられた中空状の外軸5と、外軸 5内にこれと同芯状に配設されるとともに後端部に後部プロペラを取付けられた 外軸2とをそなえ、内軸2と外軸5とが互いに反対方向に回転駆動されるように 構成されている。Also in this embodiment, a hollow outer shaft 5 having a front propeller attached to a rear end thereof, a hollow outer shaft 5 arranged concentrically with the outer shaft 5 and a rear propeller mounted at the rear end thereof. It has an outer shaft 2 attached thereto, and is configured so that the inner shaft 2 and the outer shaft 5 are rotationally driven in opposite directions.

【0013】 すなわち、後方プロペラ(図示せず)を後端部に取付けられた内軸2の前端テ ーパ部が組立てフランジ8のテーパー部に嵌合され、組立てフランジ8に主機関 の出力軸1a及び弾性継手本体7が結合されている。弾性継手の出力軸71は反転 歯車装置6の入力軸61に結合されると共に、前端内面が軸受10を介して組立てフ ランジ8に支持されている。That is, the front end taper portion of the inner shaft 2 having the rear propeller (not shown) attached to the rear end portion is fitted to the taper portion of the assembly flange 8, and the assembly flange 8 is attached to the output shaft of the main engine. 1a and the elastic joint body 7 are joined together. The output shaft 71 of the elastic joint is connected to the input shaft 61 of the reversing gear device 6, and the inner surface of the front end is supported by the assembly flange 8 via the bearing 10.

【0014】 一端をケーシング9に固定された遊星軸65で遊星歯車63が支承され、この遊星 歯車63は入力軸61の後端部に形成された太陽歯車61a及び反転歯車装置6の出力 軸67の前端部に形成された内歯歯車64と噛合し、内歯歯車64は出力軸67を介して 外軸5に連結され、前方プロペラ(図示せず)を主機関の出力軸1aと逆方向に 回転駆動させるように構成されている。A planetary gear 63 is supported by a planetary shaft 65 whose one end is fixed to the casing 9. The planetary gear 63 is formed on the rear end of the input shaft 61, and the sun gear 61 a and the output shaft 67 of the reversing gear device 6 are supported. Meshes with the internal gear 64 formed at the front end of the internal gear 64, and the internal gear 64 is connected to the outer shaft 5 through the output shaft 67, and the front propeller (not shown) is in the opposite direction to the output shaft 1a of the main engine. It is configured to be driven to rotate.

【0015】 遊星軸65の軸端に固定リング66が装着され、この固定リング66はアーム69によ りケーシング9に支承されており、遊星歯車63の位置精度を保持している。符号 11は入力軸軸受を示しており、従来例の入力軸軸受10aおよび10bに相当する。A fixed ring 66 is attached to the shaft end of the planetary shaft 65, and the fixed ring 66 is supported by the casing 9 by an arm 69 to maintain the positional accuracy of the planetary gear 63. Reference numeral 11 indicates an input shaft bearing, which corresponds to the conventional input shaft bearings 10a and 10b.

【0016】 したがって、この実施例の場合、弾性継手の出力軸71と反転歯車装置6の入力 軸61とが、間隔L0のもとに配設された2つの軸受10,11で支持されることにな る。間隔L0は従来例(図3参照)の場合の間隔L2よりはるかに大きいので、出 力軸71と入力軸61とを精度良く支持することが可能となり、その結果太陽歯車61 aと遊星歯車63との噛み合いをスムースに行なわせることが可能となる。Therefore, in the case of this embodiment, the output shaft 71 of the elastic joint and the input shaft 61 of the reversing gear device 6 are supported by the two bearings 10 and 11 arranged at the distance L 0. It will be. Since the distance L 0 is much larger than the distance L 2 in the case of the conventional example (see FIG. 3), it becomes possible to accurately support the output shaft 71 and the input shaft 61, and as a result, the sun gear 61a and the planetary gears can be supported. It is possible to smoothly mesh with the gear 63.

【0017】 又、弾性継手の出力軸7に固定された軸受10が、これを支承する側となる組立 てフランジ8と同方向に同一回転数で回るため、軸受10に摺動部がなく、したが って極めて簡単で信頼性の高い軸受が得られることになる。Further, since the bearing 10 fixed to the output shaft 7 of the elastic joint rotates at the same rotational speed in the same direction as the assembly flange 8 on the side supporting the same, there is no sliding portion in the bearing 10. Therefore, an extremely simple and highly reliable bearing can be obtained.

【0018】 さらに、1個の入力軸軸受11で反転歯車装置5の入力軸61を支持する構成であ るため、反転歯車装置5の全長を、従来例の場合のL'(図3参照)に比べて L1と短くすることが可能となる。Furthermore, since the input shaft 61 of the reversing gear device 5 is supported by one input shaft bearing 11, the total length of the reversing gear device 5 is L ′ 1 in the case of the conventional example (see FIG. 3). It is possible to shorten to L 1 compared to ().

【0019】[0019]

【考案の効果】[Effect of the device]

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の軸構造によれば次 のような効果ないし利点が得られる。 (1) 反転歯車装置の入力軸軸受と弾性継手の出力軸の内面の軸受とのスパンを大 きくとることが出来る為、弾性継手の重量が継手の出力軸にかかっても、反転歯 車装置の入力軸の傾斜すなわち太陽歯車の歯当り悪化を抑えることが出来る。 As described above in detail, the shaft structure of the marine counter-rotating propeller device of the present invention provides the following effects and advantages. (1) Since the span between the input shaft bearing of the reversing gear device and the bearing on the inner surface of the output shaft of the elastic joint can be made large, even if the weight of the elastic joint is applied to the output shaft of the joint, the reversing gear device It is possible to suppress the inclination of the input shaft, that is, the deterioration of the tooth contact of the sun gear.

【0020】 このため、遊星歯車の噛合い不良による事故の確率が大きく減り、反転歯車装 置の信頼性が向上する。 (2) 反転歯車装置の入力軸軸受が1個で済む為、歯車装置の全長を大幅に短縮で き、反転歯車装置の重量軽減、コスト低減に寄与する。 更に、軸装置の全体の短縮化により、主機関の配置が容易となる。Therefore, the probability of an accident due to poor meshing of the planetary gears is greatly reduced, and the reliability of the reversing gear device is improved. (2) Since only one input shaft bearing is required for the reversing gear device, the total length of the gear device can be significantly shortened, which contributes to weight reduction and cost reduction of the reversing gear device. Further, the shortening of the entire shaft device facilitates the arrangement of the main engine.

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

【図1】本考案の一実施例としての舶用二重反転プロペ
ラ装置の軸構造の要部断面図である。
FIG. 1 is a sectional view of an essential part of a shaft structure of a contra-rotating propeller device for a ship according to an embodiment of the present invention.

【図2】従来の舶用二重反転プロペラ装置の軸構造の模
式側面図である。
FIG. 2 is a schematic side view of a shaft structure of a conventional marine counter-rotating propeller device.

【図3】同要部断面図である。FIG. 3 is a sectional view of the same main part.

【符号の説明】[Explanation of symbols]

1a 機関の出力軸 2 内軸 5 外軸 6 反転歯車装置 7 弾性継手 10 軸受 11 入力軸軸受 61 反転歯車装置の入力軸 71 弾性継手の出力軸 1a Output shaft of engine 2 Inner shaft 5 Outer shaft 6 Inversion gear device 7 Elastic joint 10 Bearing 11 Input shaft bearing 61 Input shaft of inversion gear device 71 Output shaft of elastic joint

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 【請求項1】 舶用二重反転プロペラ装置において、機
関の出力軸に取付けられた組立てフランジと、同組立て
フランジに取付けられた弾性継手と、前端部を上記弾性
継手に反転歯車装置を介して接続されるとともに後端部
に前部プロペラを取付けられた中空状の外軸と、同外軸
の内部にこれと同芯的に配設され前端部を上記機関の出
力軸に上記組立てフランジを介して接続されるとともに
後端部に後部プロペラを取付けられた内軸とをそなえ、
上記反転歯車装置の入力軸が上記弾性継手の出力軸に接
続される一方、上記反転歯車装置の入力軸をその外周部
で軸支可能な入力軸軸受が設けられ、上記弾性継手の出
力軸をその内周部で上記組立てフランジに軸支可能な軸
受が上記出力軸の前端部附近に配設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の軸構造。
1. A marine counter-rotating propeller device, wherein an assembly flange attached to an output shaft of an engine, an elastic joint attached to the assembly flange, and a front end portion are connected to the elastic joint via an inversion gear device. A hollow outer shaft having a front propeller attached to its rear end, and a hollow outer shaft concentrically arranged inside the outer shaft, and the front end being connected to the output shaft of the engine through the assembly flange. And an inner shaft with a rear propeller attached to the rear end,
While the input shaft of the reversing gear device is connected to the output shaft of the elastic joint, an input shaft bearing capable of supporting the input shaft of the reversing gear device at its outer peripheral portion is provided, and the output shaft of the elastic joint is A shaft structure of a contra-rotating propeller device for a ship, wherein a bearing capable of being pivotally supported by the assembly flange at an inner peripheral portion thereof is arranged near a front end portion of the output shaft.
JP1991093128U 1991-10-18 1991-10-18 Shaft structure of marine contra-rotating propeller device Expired - Lifetime JP2591910Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1991093128U JP2591910Y2 (en) 1991-10-18 1991-10-18 Shaft structure of marine contra-rotating propeller device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1991093128U JP2591910Y2 (en) 1991-10-18 1991-10-18 Shaft structure of marine contra-rotating propeller device

Publications (2)

Publication Number Publication Date
JPH0535598U true JPH0535598U (en) 1993-05-14
JP2591910Y2 JP2591910Y2 (en) 1999-03-10

Family

ID=14073885

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1991093128U Expired - Lifetime JP2591910Y2 (en) 1991-10-18 1991-10-18 Shaft structure of marine contra-rotating propeller device

Country Status (1)

Country Link
JP (1) JP2591910Y2 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20150097026A (en) * 2014-02-17 2015-08-26 현대중공업 주식회사 Propulsion apparatus for ship
KR20160024021A (en) * 2014-08-22 2016-03-04 현대중공업 주식회사 Propulsion apparatus for ship

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5954399U (en) * 1982-10-04 1984-04-10 川崎重工業株式会社 double rotating propeller
JPS60121191A (en) * 1984-10-16 1985-06-28 Mitsubishi Heavy Ind Ltd Double contrarotating propeller device for ship

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5954399U (en) * 1982-10-04 1984-04-10 川崎重工業株式会社 double rotating propeller
JPS60121191A (en) * 1984-10-16 1985-06-28 Mitsubishi Heavy Ind Ltd Double contrarotating propeller device for ship

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20150097026A (en) * 2014-02-17 2015-08-26 현대중공업 주식회사 Propulsion apparatus for ship
KR20160024021A (en) * 2014-08-22 2016-03-04 현대중공업 주식회사 Propulsion apparatus for ship

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Effective date: 19981209

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