JPH0545598Y2 - - Google Patents
Info
- Publication number
- JPH0545598Y2 JPH0545598Y2 JP16408588U JP16408588U JPH0545598Y2 JP H0545598 Y2 JPH0545598 Y2 JP H0545598Y2 JP 16408588 U JP16408588 U JP 16408588U JP 16408588 U JP16408588 U JP 16408588U JP H0545598 Y2 JPH0545598 Y2 JP H0545598Y2
- Authority
- JP
- Japan
- Prior art keywords
- shaft
- flange
- oil
- attached
- joint
- 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
- 238000005461 lubrication Methods 0.000 claims description 6
- 239000003921 oil Substances 0.000 description 56
- 230000002093 peripheral effect Effects 0.000 description 11
- 239000010687 lubricating oil Substances 0.000 description 6
- 238000010276 construction Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 238000005553 drilling Methods 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000004323 axial length Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
Landscapes
- Sliding-Contact Bearings (AREA)
- Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
- General Details Of Gearings (AREA)
Description
【考案の詳細な説明】
〔産業上の利用分野〕
本考案は舶用二重反転プロペラー軸系の継手潤
滑構造に関する。[Detailed Description of the Invention] [Industrial Application Field] The present invention relates to a joint lubrication structure for a marine counter-rotating propeller shaft system.
舶用二重反転プロペラーの軸系構造としては、
従来、例えば、第2図縦断面図に示すようなもの
が知られている。
The shaft system structure of a marine contra-rotating propeller is as follows:
Conventionally, for example, a device as shown in the longitudinal sectional view of FIG. 2 is known.
すなわち、内軸014及びこれに同軸的に外挿
された中空外軸015で駆動される舶用二重反転
プロペラー軸系装置において、反転歯車016の
入力側と中間短軸022の後端との間に挿入され
板ばね019を介して反転歯車016にトルクを
分岐する弾性継手020と、それと主機関出力軸
021との間に挿入され弾性継手020の軸方向
長さよりも長い中間短軸022とを具えており、
中間短軸022を外すことにより、弾性継手02
0の点検及び解放を容易に行うことができるよう
になつている。 That is, in a marine counter-rotating propeller shaft system device driven by an inner shaft 014 and a hollow outer shaft 015 coaxially extrapolated thereto, the space between the input side of the reversing gear 016 and the rear end of the intermediate short shaft 022 An elastic joint 020 is inserted into the main engine output shaft 021 to branch torque to the reversing gear 016 via a leaf spring 019, and an intermediate short shaft 022 is inserted between the elastic joint 020 and the main engine output shaft 021 and is longer than the axial length of the elastic joint 020. It is equipped with
By removing the intermediate short shaft 022, the elastic joint 02
0 can be easily inspected and released.
この種の構造では、弾性継手020を嵌着する
円筒部付フランジ01は中間内軸017の先端テ
ーパー部に油圧により嵌着され、また円筒部付フ
ランジ01の円周方向に放射状に複数組(同図で
は12組)板ばね019が取付けられた円筒部付フ
ランジ01外周の溝023(第3図参照)には潤
滑油が供給される。 In this type of structure, the cylindrical flange 01 to which the elastic joint 020 is fitted is hydraulically fitted to the tapered end of the intermediate inner shaft 017, and a plurality of sets ( Lubricating oil is supplied to the groove 023 (see FIG. 3) on the outer periphery of the flange 01 with the cylindrical portion to which the leaf springs 019 (12 sets in the figure) are attached.
そこで、第3図部分拡大図に示すように、油圧
により中間内軸017の先端テーパー部に円筒部
付フランジ01を嵌着するため、それの内周面に
らせん状油溝024が凹設され、それに油孔02
5を通じて外部から高圧油026を供給すること
ができるようになつており、また板ばね019に
潤滑油027を供給するために、円筒部付フラン
ジ01の内周面に油溜め028が凹設されるとと
もに、油溜め028と円筒部付フランジ01の前
端との間には給油孔029が、油溜め028と円
筒部付フランジ01外周の溝023との間には油
孔030がそれぞれ穿設されている。 Therefore, as shown in the partially enlarged view of FIG. 3, in order to fit the cylindrical flange 01 to the tapered end of the intermediate inner shaft 017 using hydraulic pressure, a spiral oil groove 024 is formed in the inner circumferential surface of the flange 01. , and oil hole 02
High-pressure oil 026 can be supplied from the outside through 5, and an oil reservoir 028 is recessed in the inner circumferential surface of the cylindrical flange 01 to supply lubricating oil 027 to the leaf spring 019. In addition, an oil supply hole 029 is provided between the oil reservoir 028 and the front end of the flange 01 with the cylindrical portion, and an oil hole 030 is provided between the oil reservoir 028 and the groove 023 on the outer periphery of the flange 01 with the cylindrical portion. ing.
しかしながら、このような継手潤滑構造では、
下記のような欠点がある。 However, in such a joint lubrication structure,
It has the following drawbacks.
(1) 円筒部付フランジ01の内周面に油溜め02
8が凹設されているので、円筒部付フランジ0
1の強度が著しく低下する。また、円筒部付フ
ランジ01を中間内軸017に圧入する際、ら
せん状油溝024に500〜1000Kg/cm2の高圧油
026をかけるが、これが円筒部付フランジ0
1の内周面を伝つて油溜め028に入り、そこ
から更に最高圧が約6Kg/cm2の低圧設計の弾性
継手020に侵入し、それを壊す惧れがある。(1) Oil reservoir 02 on the inner peripheral surface of flange 01 with cylindrical part
Since 8 is recessed, the flange with cylindrical part 0
The strength of No. 1 is significantly reduced. Furthermore, when the flange 01 with a cylindrical part is press-fitted into the intermediate inner shaft 017, high pressure oil 026 of 500 to 1000 kg/cm 2 is applied to the spiral oil groove 024.
1 and enters the oil sump 028, and from there there is a risk of entering the elastic joint 020, which has a low-pressure design with a maximum pressure of about 6 kg/cm 2 , and damaging it.
(2) そこで、第4図に示す構造のように、油溜め
を廃止し、板ばね019のつけ根に複数の軸方
向給油孔031を設ける構造も知られている
が、このような構造では、給油孔031を加工
するのが難しく、また各給油孔031への潤滑
油供給方法が複雑となり信頼性が低下する。(2) Therefore, a structure is known in which the oil reservoir is abolished and a plurality of axial oil supply holes 031 are provided at the base of the leaf spring 019, such as the structure shown in FIG. 4, but in such a structure, It is difficult to process the oil supply holes 031, and the method for supplying lubricating oil to each oil supply hole 031 becomes complicated, reducing reliability.
(3) 第3図,第4図に示す構造とも、円筒部付フ
ランジ01の内周面は中間内軸017と現物摺
合わせする必要があるが、円筒部付フランジ0
1の外周面に板ばね019を取付ける作業は弾
性継手メーカーで行われるので、弾性接手02
0として軸系を組立てる際にそれぞれの加工工
程が互いに干渉する。(3) In both the structures shown in Fig. 3 and Fig. 4, the inner peripheral surface of the flange 01 with a cylindrical part needs to be actually slid together with the intermediate inner shaft 017, but the flange 01 with a cylindrical part
The work of attaching the leaf spring 019 to the outer peripheral surface of the elastic joint 02 is done by the elastic joint manufacturer.
When assembling the shaft system as 0, each machining process interferes with each other.
(4) 板ばね019つけ根は焼入れする必要がある
が、その熱により円筒部付フランジ01の内面
変形が考えられるので、板ばね019取付け後
に円筒部付フランジ01内面の仕上げ加工が必
要となり、従つて軸系組立工期が長くなる。(4) It is necessary to harden the base of the leaf spring 019, but the heat may cause deformation of the inner surface of the flange 01 with the cylindrical part, so it is necessary to finish the inner surface of the flange 01 with the cylindrical part after the leaf spring 019 is installed. Therefore, the assembly period for the shaft system will be longer.
本考案は、このような事情に鑑みて提案された
もので、内周面に油溜めを凹設する必要がなく、
らせん状油溝に高圧油を加えた際にそれが弾性継
手に流入せず、溝への給油孔の穿設が容易でそれ
への潤滑油供給機構が簡単で、加工工程に重複が
ない組立フランジ等を有する強度面,安全性,加
工性,信頼性,工期面等で優れた舶用二重反転プ
ロペラー軸系の継手潤滑構造を提供することを目
的とする。
The present invention was proposed in view of these circumstances, and eliminates the need for recessing an oil reservoir on the inner peripheral surface.
When high-pressure oil is applied to the helical oil groove, it does not flow into the elastic joint, making it easy to drill the oil supply hole in the groove, and the mechanism for supplying lubricating oil to it is simple, and there is no duplication of processing steps. The purpose is to provide a joint lubrication structure for a marine counter-rotating propeller shaft system that has flanges, etc. and is excellent in terms of strength, safety, workability, reliability, construction time, etc.
そのために本考案は内軸及びこれに同軸的に外
挿されかつ反転歯車が付設された中空外軸でそれ
ぞれ後部プロペラー,前部プロペラーが駆動され
る二重反転プロペラー軸と、上記反転歯車の入力
側に付設され円筒部付フランジを介して上記内軸
の前端に外嵌されかつ外周に装着された弾性体を
介して上記反転歯車にトルクを分岐する弾性継手
とを有する舶用二重反転プロペラー軸系構造にお
いて、上記円筒部付フランジの円筒部に外嵌固着
され外周に上記弾性継手が付設された中空継手軸
と、上記中空継手軸の内周面に凹設され上記円筒
部付フランジと協働して形成される環状油溜め
と、上記円筒部付フランジの前端から上記油溜め
に通ずる給油孔,上記油溜めから上記弾性体に通
ずる油孔とを具えたことを特徴とする。
To this end, the present invention includes a counter-rotating propeller shaft in which a rear propeller and a front propeller are driven by an inner shaft and a hollow outer shaft coaxially extrapolated to the inner shaft and equipped with a reversing gear, and an input of the reversing gear. a counter-rotating propeller shaft for marine vessels, the shaft having an elastic joint attached to the side and externally fitted on the front end of the inner shaft via a flange with a cylindrical portion, and branching torque to the reversing gear via an elastic body attached to the outer periphery; In the system structure, a hollow joint shaft is fitted and fixed to the cylindrical part of the flange with a cylindrical part and the elastic joint is attached to the outer periphery, and a hollow joint shaft is recessed in the inner peripheral surface of the hollow joint shaft and cooperates with the flange with the cylindrical part. The present invention is characterized by comprising: an annular oil reservoir formed by the flange with the cylindrical portion; an oil supply hole communicating with the oil reservoir from the front end of the flange with the cylindrical portion; and an oil hole communicating from the oil reservoir with the elastic body.
弾性継手への給油孔が1本で済むので、その穿
設作業が容易になる。また組立フランジの内周面
に油溜めが凹設されていないので、組立フランジ
の強度が増加するとともに高圧油が弾性継手へ流
入する惧れがなくなる。更に組立フランジの内周
面を摺合わせたのちにそれの外周面にボルトを介
して弾性継手の完成品を取付けることができる。
Since only one oil supply hole is required for the elastic joint, the drilling work is facilitated. Furthermore, since no oil reservoir is recessed in the inner peripheral surface of the assembly flange, the strength of the assembly flange is increased and there is no risk of high pressure oil flowing into the elastic joint. Furthermore, after the inner circumferential surfaces of the assembled flanges have been slid together, the completed elastic joint can be attached to the outer circumferential surface of the assembled flanges via bolts.
本考案の一実施例を図面について説明すると、
第2〜4図と同一の符番はそれぞれ同図と同一の
部材を示し、第1図縦断面図において、1は外周
面の前後方向央部に央部フランジ2が突設された
組立フランジ、3は外周に複数の板ばね019が
取付けられ中空継手軸で、それはボルト4を介し
て央部フランジ2に固着される。
An embodiment of the present invention will be explained with reference to the drawings.
The same reference numbers as in Figures 2 to 4 indicate the same members as in the same figure, and in the longitudinal cross-sectional view of Figure 1, 1 is an assembly flange with a central flange 2 protruding from the center of the outer peripheral surface in the front and back direction. , 3 is a hollow joint shaft having a plurality of leaf springs 019 attached to its outer periphery, and is fixed to the central flange 2 via bolts 4.
4aは中空継手軸3の内周面に凹設されるとと
もに組立フランジ1の外周面と協働して形成され
る環状油溜め、5は組立フランジ1の前面から一
部がそれの軸線に沿つて穿設され残部が半径方向
に延びて油溜め4aに通ずるL字型給油孔、6は
油溜め4から各板ばね019のつけ根に等間隔で
導設された複数の油孔、7,8はそれぞれ中空継
手軸3,反転歯車入力軸9に穿設された排油孔、
10,11はそれぞれ中間内軸017,反転歯車
入力軸9の軸受,12はラビリンスである。 4a is an annular oil reservoir recessed in the inner circumferential surface of the hollow joint shaft 3 and formed in cooperation with the outer circumferential surface of the assembly flange 1; 5 is an annular oil reservoir formed along the axis of the assembly flange 1; 6 is a plurality of oil holes led from the oil sump 4 to the base of each leaf spring 019 at equal intervals; 7, 8; are oil drain holes drilled in the hollow joint shaft 3 and the reversing gear input shaft 9, respectively;
10 and 11 are bearings for the intermediate inner shaft 017 and the reversing gear input shaft 9, respectively, and 12 is a labyrinth.
このような構造において、組立フランジ1を中
間内軸017に嵌着するための高圧油026は油
孔025及びらせん状油溝024を通じて注入さ
れる。また潤滑油027はまず給油孔5を通じて
油溜め4aに供給され、そこからそれぞれ油孔6
を通じて各板ばね019のつけ根へ供給され、そ
の油は排油孔7,8を通じて図示せざるタンクへ
回収される。 In such a structure, high pressure oil 026 for fitting the assembly flange 1 onto the intermediate inner shaft 017 is injected through the oil hole 025 and the spiral oil groove 024. Also, the lubricating oil 027 is first supplied to the oil reservoir 4a through the oil supply hole 5, and from there to the oil hole 6, respectively.
The oil is supplied to the base of each leaf spring 019 through the oil drain holes 7 and 8 and collected into a tank (not shown).
このような構造によれば、下記効果が奏せられ
る。 According to such a structure, the following effects can be achieved.
(1) 弾性継手への給油孔が1本で済むので、それ
の穿設作業が極めて容易で経済的になる。(1) Since only one oil supply hole is required for the elastic joint, the drilling work is extremely easy and economical.
(2) 内周面に油溜めが凹設けされていないので、
組立フランジの強度が向上するとともにらせん
状油溝の高圧油が弾性継手に流入する惧れがな
くなり、それの信頼性が向上する。(2) Since the oil reservoir is not recessed on the inner peripheral surface,
The strength of the assembled flange is improved, and there is no risk that high-pressure oil in the spiral oil groove will flow into the elastic joint, improving its reliability.
(3) 組立フランジの内周面を摺合わせたのちに、
弾性継手の完成品を一体でボルトを介して組立
フランジの外周面に取付けることが可能なの
で、加工工程の重複がなく、工期を短縮するこ
とができる。(3) After sliding the inner peripheral surfaces of the assembly flanges together,
Since the finished elastic joint can be attached to the outer circumferential surface of the assembly flange in one piece via bolts, there is no duplication of processing steps and the construction period can be shortened.
要するに本考案によれば、内軸及びこれに同軸
的に外挿されかつ反転歯車が付設された中空外軸
でそれぞれ後部プロペラー,前部プロペラーが駆
動される二重反転プロペラー軸と、上記反転歯車
の入力側に付設され円筒部付フランジを介して上
記内軸の前端に外嵌されかつ外周に装着された弾
性体を介して上記反転歯車にトルクを分岐する弾
性継手とを有する舶用二重反転プロペラー軸系構
造において、上記円筒部付フランジの円筒部に外
嵌固着され外周に上記弾性継手が付設された中空
継手軸と、上記中空継手軸の内周面に凹設され上
記円筒部付フランジと協働して形成される環状油
溜めと、上記円筒部付フランジの前端から上記油
溜めに通ずる給油孔,上記油溜めから上記弾性体
に通ずる油孔とを具えたことにより、内周面に油
溜めを凹設する必要がなく、らせん状油溝に高圧
油を加えた際にそれが弾性継手に流入せず、溝へ
の給油孔の穿設が容易でそれへの潤滑油供給機構
が簡単で、加工工程に重複がない組立フランジ等
を有する強度面,安全性,加工性,信頼性,工期
面等で優れた舶用二重反転プロペラー軸系の継手
潤滑構造を得るから、本考案は産業上極めて有益
なものである。
In short, according to the present invention, there is provided a counter-rotating propeller shaft in which a rear propeller and a front propeller are driven by an inner shaft and a hollow outer shaft that is coaxially extrapolated to the inner shaft and has a reversing gear attached thereto, and a counter-rotating propeller shaft that drives a rear propeller and a front propeller, respectively, and and an elastic joint attached to the input side of the inner shaft and externally fitted on the front end of the inner shaft via a flange with a cylindrical part and branching torque to the reversing gear via an elastic body attached to the outer periphery. In the propeller shaft system structure, the hollow joint shaft is fitted onto the cylindrical part of the flange with a cylindrical part and has the elastic joint attached to the outer periphery, and the flange with the cylindrical part is recessed in the inner peripheral surface of the hollow joint shaft. The inner peripheral surface There is no need to install an oil reservoir in the groove, and when high-pressure oil is applied to the spiral oil groove, it does not flow into the elastic joint, making it easy to drill an oil supply hole in the groove and providing a lubricant supply mechanism to it. This invention provides a joint lubrication structure for a marine counter-rotating propeller shaft system that is easy to assemble, has an assembly flange, etc. that does not overlap machining processes, and is excellent in terms of strength, safety, workability, reliability, construction time, etc. is extremely useful for industry.
第1図は本考案の一実施例を示す縦断面図であ
る。第2図は公知の舶用二重反転プロペラーの軸
系構造を示す縦断面図、第3図は第2図部を示
す部分拡大図、第4図は第3図と異なる公知の継
手潤滑構造を示す同じく部分拡大図である。
1……組立フランジ、2……央部フランジ、3
……中空継手軸、4……ボルト、4a……油溜
め、5……給油孔、6……油孔、7,8……排油
孔、9……反転歯車入力軸、10,11……軸
受、12……ラビリンス、01……円筒部付フラ
ンジ、017……中間内軸、019……板ばね、
024……らせん状油溝、025……油孔、02
6……高圧油、027……潤滑油。
FIG. 1 is a longitudinal sectional view showing an embodiment of the present invention. Fig. 2 is a vertical cross-sectional view showing the shaft system structure of a known contra-rotating marine propeller, Fig. 3 is a partially enlarged view of the part shown in Fig. 2, and Fig. 4 shows a known joint lubrication structure different from Fig. 3. It is also a partially enlarged view shown in FIG. 1... Assembly flange, 2... Central flange, 3
... Hollow joint shaft, 4 ... Bolt, 4a ... Oil reservoir, 5 ... Oil supply hole, 6 ... Oil hole, 7, 8 ... Oil drain hole, 9 ... Reversing gear input shaft, 10, 11 ... ... Bearing, 12 ... Labyrinth, 01 ... Flange with cylindrical part, 017 ... Intermediate inner shaft, 019 ... Leaf spring,
024...Spiral oil groove, 025...Oil hole, 02
6...High pressure oil, 027...Lubricating oil.
Claims (1)
が付設された中空外軸でそれぞれ後部プロペラ
ー,前部プロペラーが駆動される二重反転プロペ
ラー軸と、上記反転歯車の入力側に付設され円筒
部付フランジを介して上記内軸の前端に外嵌され
かつ外周に装着された弾性体を介して上記反転歯
車にトルクを分岐する弾性継手とを有する舶用二
重反転プロペラー軸系構造において、上記円筒部
付フランジの円筒部に外嵌固着され外周に上記弾
性継手が付設された中空継手軸と、上記中空継手
軸の内周面に凹設され上記円筒部付フランジと協
働して形成される環状油溜めと、上記円筒部付フ
ランジの前端から上記油溜めに通ずる給油孔,上
記油溜めから上記弾性体に通ずる油孔とを具えた
ことを特徴とする舶用二重反転プロペラー軸系の
継手潤滑構造。 A counter-rotating propeller shaft that drives a rear propeller and a front propeller, respectively, by an inner shaft and a hollow outer shaft that is coaxially inserted into the inner shaft and has a reversing gear attached thereto, and a cylindrical shaft attached to the input side of the reversing gear. In the marine counter-rotating propeller shaft system structure, the structure includes an elastic joint that is externally fitted onto the front end of the inner shaft via a attached flange and branches torque to the reversing gear via an elastic body attached to the outer periphery. a hollow joint shaft that is externally fitted and fixed to the cylindrical part of the flange with a cylindrical part and has the elastic joint attached to the outer periphery; A counter-rotating propeller shaft system for marine vessels, comprising: an annular oil reservoir; an oil supply hole communicating from the front end of the flange with the cylindrical portion to the oil reservoir; and an oil hole communicating from the oil reservoir to the elastic body. Joint lubrication structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP16408588U JPH0545598Y2 (en) | 1988-12-19 | 1988-12-19 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP16408588U JPH0545598Y2 (en) | 1988-12-19 | 1988-12-19 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH0283195U JPH0283195U (en) | 1990-06-27 |
| JPH0545598Y2 true JPH0545598Y2 (en) | 1993-11-22 |
Family
ID=31449384
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP16408588U Expired - Lifetime JPH0545598Y2 (en) | 1988-12-19 | 1988-12-19 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0545598Y2 (en) |
-
1988
- 1988-12-19 JP JP16408588U patent/JPH0545598Y2/ja not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| JPH0283195U (en) | 1990-06-27 |
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