JPS6024717Y2 - Two-speed switching device for multi-engine propulsion plants - Google Patents

Two-speed switching device for multi-engine propulsion plants

Info

Publication number
JPS6024717Y2
JPS6024717Y2 JP9187278U JP9187278U JPS6024717Y2 JP S6024717 Y2 JPS6024717 Y2 JP S6024717Y2 JP 9187278 U JP9187278 U JP 9187278U JP 9187278 U JP9187278 U JP 9187278U JP S6024717 Y2 JPS6024717 Y2 JP S6024717Y2
Authority
JP
Japan
Prior art keywords
engine
cruise
gear
speed
clutch
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
Application number
JP9187278U
Other languages
Japanese (ja)
Other versions
JPS558086U (en
Inventor
善正 酒井
敏昭 岩本
Original Assignee
川崎重工業株式会社
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 川崎重工業株式会社 filed Critical 川崎重工業株式会社
Priority to JP9187278U priority Critical patent/JPS6024717Y2/en
Publication of JPS558086U publication Critical patent/JPS558086U/ja
Application granted granted Critical
Publication of JPS6024717Y2 publication Critical patent/JPS6024717Y2/en
Expired legal-status Critical Current

Links

Description

【考案の詳細な説明】 本考案は、プロペラ軸を低速域では巡航エンジンで高速
域では巡航エンジンとブーストエンジンで駆動する形式
の多機種機関推進プラントにおける2速切換装置に関す
る。
[Detailed Description of the Invention] The present invention relates to a two-speed switching device in a multi-engine propulsion plant in which the propeller shaft is driven by a cruise engine in a low speed range and by a cruise engine and a boost engine in a high speed range.

対象なる機関方式は、例えば巡航エンジンとして小容量
のガスタービンまたはディーゼルエンジンのいずれか一
つとフ゛−ストエンジンとしての大容量のガスタービン
との組合わせである。
The target engine type is, for example, a combination of either a small-capacity gas turbine or a diesel engine as a cruise engine and a large-capacity gas turbine as a first engine.

この種多機種機関推進プラントの減速装置においては、
一般に巡航エンジンの動力伝達経路は1経路で、その減
速比は巡航エンジンとブーストエンジンの同時駆動とな
る高速比での巡航エンジンの最高回転数がプロペラ軸回
転数で100%になるように設定されており、このため
第1図すおよび第2図すに示す如く、巡航エンジン出力
は主軸回転数の低下と共に略直線的に逓減して低速域上
限でのエンジン出力は最大出力よりかなり低下し、巡航
エンジン出力を低速域で有効に活用できない欠点があっ
た。
In the reduction gear of this kind of multi-model engine propulsion plant,
Generally, a cruise engine has one power transmission path, and its reduction ratio is set so that the maximum rotation speed of the cruise engine at a high speed ratio where the cruise engine and boost engine are driven simultaneously is 100% of the propeller shaft rotation speed. Therefore, as shown in Figures 1 and 2, the cruising engine output decreases approximately linearly as the main shaft rotation speed decreases, and the engine output at the upper limit of the low speed range is considerably lower than the maximum output. The drawback was that the cruise engine output could not be used effectively at low speeds.

そこで、巡航エンジン動力伝達機構を低速側と高速側に
分け、それぞれの動力伝達経路に切換え用としての摩擦
クラッチを配して低速域のエンジン出力を高めるように
したものが一部提案された。
Therefore, some proposals have been made to divide the cruise engine power transmission mechanism into a low-speed side and a high-speed side, and to increase the engine output in the low speed range by placing a friction clutch for switching in each power transmission path.

しかしこのものは第3図に示す如く、巡航エンジン動力
伝達機構は巡航エンジン1の出力軸2からギヤー3.4
.5を経てプロペラ軸6に至る高速側動力伝達経路と、
出力軸2からギヤー7.8、中間軸9、ギヤー4,5を
経てプロペラ軸6に至る低速側動力伝達経路に分け、出
力軸2にはギ・ヤー3を出力軸に連結するための摩擦ク
ラッチ10を、中間軸9にはギヤー8を中間軸に連結す
るための摩擦クラッチ11を備え、2速切換えは、プロ
ペラ軸6の回転数と巡航エンジン1の回転数を入力信号
にとるクラッタ操作用自動・手動回路12の切換信号に
より動作する方向切換弁13を介してポンプ14からの
圧液を摩擦クラッチ10または11に選択的に導くこと
で行っておリ、されに、摩擦クラッチに接続する油路1
5゜16にはそれぞれ摩擦クラッチの嵌から脱への急激
な切換えによるショックをさけるために、アキュムレー
タ17.18、絞り弁19,20.逆止弁21,22を
介装していたから、複雑な油圧制御装置を必要とした。
However, as shown in FIG.
.. 5 to the propeller shaft 6;
It is divided into a low-speed power transmission path from the output shaft 2 to the propeller shaft 6 via the gears 7 and 8, the intermediate shaft 9, and the gears 4 and 5, and the output shaft 2 has friction for connecting the gear 3 to the output shaft. The intermediate shaft 9 is equipped with a friction clutch 11 for connecting the gear 8 to the intermediate shaft, and the second speed switching is a clutter operation that takes the rotation speed of the propeller shaft 6 and the rotation speed of the cruise engine 1 as input signals. This is done by selectively guiding the pressure fluid from the pump 14 to the friction clutch 10 or 11 via the directional switching valve 13 operated by the switching signal of the automatic/manual circuit 12. oil passage 1
At 5° 16, accumulators 17, 18, throttle valves 19, 20, . Since the check valves 21 and 22 were interposed, a complicated hydraulic control device was required.

本考案は、前記の実情に鑑み、巡航エンジンの2速切換
えを1個の被制御クラッチと入出力軸の相対回転数差を
利用して機械的にクラッチ嵌脱をなす1個の自己周期自
動嵌脱クラッチにて行わしめることにより、この種多機
種機関推進プラントの油圧制御装置の簡素化ならびにコ
スト低減を図ったものである。
In view of the above-mentioned circumstances, the present invention has developed a self-periodic automatic system that mechanically engages and disengages the clutch by utilizing the relative rotational speed difference between the controlled clutch and the input and output shafts for switching between two speeds of a cruise engine. By using an engagement/disengagement clutch, it is possible to simplify the hydraulic control system of this type of multi-engine propulsion plant and reduce costs.

以下本考案の実施例を図面について説明すると、第4図
において、25は巡航エンジンたる小容量のガスタービ
ン、26はブーストエンジンたる大容量のガスタービン
、27はプロペラ軸である。
An embodiment of the present invention will be described below with reference to the drawings. In FIG. 4, 25 is a small-capacity gas turbine that is a cruise engine, 26 is a large-capacity gas turbine that is a boost engine, and 27 is a propeller shaft.

巡航エンジン25の出力軸28にはピニオン29が軸着
され、このピニオン29に第1中間軸30に軸着された
ギヤー31と第2中間軸32に軸着されたギヤー33が
噛合せしめられている。
A pinion 29 is attached to the output shaft 28 of the cruise engine 25, and a gear 31 attached to the first intermediate shaft 30 and a gear 33 attached to the second intermediate shaft 32 are meshed with the pinion 29. There is.

第1中間軸30は、プロペラ軸27に軸着された主ギヤ
ー34と噛合するピニオン35およびこのピニオン35
を第1中間軸に着脱するための公知の前記自己周期自動
嵌脱クラッチ36を備え、ギヤー31、クラッチ36、
ピニオン35、主ギヤー34とで低速側動力伝達機構を
構威し、第2中間軸32は、主ギヤー34と噛合するピ
ニオン37およびこのピニオン37を第2中間軸に着脱
するための被制御クラッチ例えば摩擦クラッチ38を備
え、ギヤー33、クラッチ38、ピニオン37、主ギヤ
ー34とで高速側動力伝達機構を構成する。
The first intermediate shaft 30 includes a pinion 35 that meshes with a main gear 34 that is pivotally attached to the propeller shaft 27;
The gear 31, the clutch 36,
The pinion 35 and the main gear 34 form a low-speed power transmission mechanism, and the second intermediate shaft 32 includes a pinion 37 that meshes with the main gear 34 and a controlled clutch for attaching and detaching the pinion 37 to and from the second intermediate shaft. For example, a friction clutch 38 is provided, and the gear 33, clutch 38, pinion 37, and main gear 34 constitute a high-speed side power transmission mechanism.

ブーストエンジン26の出力軸39には自己周期自動嵌
脱クラッチ40とこれにより出力軸39に着脱されるピ
ニオン41を備え、このピニオン41とプロペラ軸27
の主ギヤー34は2個のギヤー42.45および2個の
ピニオン43゜44て連結しである。
The output shaft 39 of the boost engine 26 is equipped with a self-periodic automatic engagement/disengagement clutch 40 and a pinion 41 that is attached to and detached from the output shaft 39. This pinion 41 and the propeller shaft 27
The main gear 34 is composed of two gears 42, 45 and two pinions 43, 44 connected together.

本実施例は前記するような構成であるから、巡航エンジ
ン25の単独運転となる低速域では、摩擦クラッチ38
は脱、自己周期自動嵌脱クラッチ36は嵌の状態にある
Since this embodiment has the above-described configuration, in the low speed range where the cruise engine 25 is operating independently, the friction clutch 38
is disengaged, and the self-cyclic automatic engagement/disengagement clutch 36 is in the engaged state.

即ち、巡航エンジン25の単独運転で摩擦クラッチ38
が脱では、自己周期自動嵌脱クラッチ36の入側となる
ギヤー31は駆動され出側となる主ギヤー34は停止し
ているので入側回転数が出側より大となり、クラッチ3
6は自動的に嵌となる。
That is, when the cruise engine 25 is operating independently, the friction clutch 38
When disengaged, the gear 31 on the input side of the self-periodic automatic engagement/disengagement clutch 36 is driven, and the main gear 34 on the output side is stopped, so the rotation speed on the input side is higher than the output side, and the clutch 3
6 is automatically fitted.

従って、低速域での巡航エンジントルクはギヤー31、
第1中間軸30、クラッチ36、ピニオン35、ギヤー
34を経てプロペラ軸27に伝達される。
Therefore, the cruise engine torque in the low speed range is gear 31,
The signal is transmitted to the propeller shaft 27 via the first intermediate shaft 30, clutch 36, pinion 35, and gear 34.

巡航エンジン25とブーストエンジン26の並列運転と
なる高速域では、摩擦クラッチ38の嵌で主ギヤー34
は駆動され、この主ギヤー34と噛合するピニオン35
はギヤー31より高速となるために、自己周期自動嵌脱
クラッチ36は自動的に脱となる。
At high speeds where the cruise engine 25 and boost engine 26 operate in parallel, the main gear 34 is engaged by the engagement of the friction clutch 38.
is driven and a pinion 35 meshes with this main gear 34.
is faster than the gear 31, so the self-periodic automatic engagement/disengagement clutch 36 is automatically disengaged.

かくて高速域での巡航エンジントルクはギヤー33、第
2中間軸32、摩擦クラッチ38、ピニオン37、主ギ
ヤー34を経てプロペラ軸27に伝達される。
Thus, cruise engine torque in a high speed range is transmitted to the propeller shaft 27 via the gear 33, second intermediate shaft 32, friction clutch 38, pinion 37, and main gear 34.

以上説明した如く本考案によれば、巡航エンジン動力伝
達機構は低速側と高速側に分かれていて低速域の上限お
よび高速域の上限では巡航エンジンは最大回転数で駆動
して最大出力が得られ、第1図aおよび第2図aに示す
如く、巡航エンジン出力を低速域でも最大限に活用でき
る。
As explained above, according to the present invention, the cruise engine power transmission mechanism is divided into a low speed side and a high speed side, and at the upper limit of the low speed range and the upper limit of the high speed range, the cruise engine is driven at the maximum rotation speed and maximum output is obtained. , as shown in FIGS. 1a and 2a, the cruise engine output can be maximized even in the low speed range.

しかも、低速側動力伝達機構に自己周期自動嵌脱クラッ
チが配されていることによって巡航エンジンの2速切換
えが1個の摩擦クラッチの切換操作のみで行えるために
、第3図に示す方向切換弁13以降の2系統の油圧制御
回路のうち1系統を省略でき、油圧制御装置が簡単とな
ってこの種多機種機関推進プラントのコスト低減を図り
得る優れた効果を奏する。
Moreover, because the low-speed power transmission mechanism is equipped with a self-periodic automatic engagement/disengagement clutch, the cruising engine can be switched to two speeds by simply switching one friction clutch. One of the two hydraulic control circuits after No. 13 can be omitted, and the hydraulic control device becomes simple, which has an excellent effect of reducing the cost of this type of multi-engine propulsion plant.

なお、前記の如き図面および記載は本考案の好適な実施
例に過ぎず、固より本考案はこの実施例のみに限定され
るものではない。
It should be noted that the above drawings and descriptions are merely preferred embodiments of the present invention, and the present invention is not limited to these embodiments.

本実施例の構造は本考案の要旨を逸脱しない範囲で種々
の改変を加え得るものであり、例えば第5図に示すよう
に、第4図の主ギヤー34と噛合するピニオン35と4
3、ピニオン37と44を一つにして、この1組のピニ
オンを巡航エンジン25とブーストエンジン26で共用
するようにしてもよい。
The structure of this embodiment can be modified in various ways without departing from the gist of the invention. For example, as shown in FIG.
3. The pinions 37 and 44 may be combined into one set so that the cruise engine 25 and the boost engine 26 share this set of pinions.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図および第2図はそれぞれ多機種機関推進プラント
における巡航エンジンのa2連切換えとb切換えなしの
場合の推進性能特性線図、第3図は従来装置の巡航エン
ジンギヤートレンと油圧回路図、第4図および第5図は
それぞれ本考案の実施例を示す2速切換減速装置のギヤ
ートレン図である。 25・・・・・・巡航エンジン、26・・・・・・ブー
ストエンジン、27・・・・・・プロペラ軸、28.3
9・・・・・・出力軸、29,35,41,43,44
・・・・・ゼニオン、30・・・・・・第1中間軸、3
1,33,42.45・・・・・・ギヤー 32・・・
・・・第2中間軸、34・・旧主ギヤー、36,40・
・間自己周期自動嵌脱クラッチ、38・・・・・・摩擦
クラッチ。
Figures 1 and 2 are propulsion performance characteristic diagrams of a cruise engine in a multi-engine propulsion plant with A dual switching and without B switching, respectively; Figure 3 is a cruise engine gear train and hydraulic circuit diagram of a conventional system; FIG. 4 and FIG. 5 are gear train diagrams of a two-speed switching reduction gear, respectively, showing an embodiment of the present invention. 25... Cruise engine, 26... Boost engine, 27... Propeller shaft, 28.3
9... Output shaft, 29, 35, 41, 43, 44
...Zenion, 30...First intermediate shaft, 3
1,33,42.45...Gear 32...
...Second intermediate shaft, 34...Old main gear, 36,40...
・Self-cycle automatic engagement/disengagement clutch, 38...Friction clutch.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] プロペラ軸を低速域では巡航エンジンで高速域では巡航
エンジンとブーストエンジンで駆動する形式の多機種機
関推進プラントにおいて、巡航エンジン動力伝達機構を
低速と高速の2系統に分けて間隔をおいて配設し、低速
側動力伝達機構の入力側ギヤーと出力側ギヤーとの間に
自己周期自動嵌脱クラッチを設け、高速側動力伝達機構
の入力側ギヤーと出力側ギヤーとの間に被制御クラッチ
を設けたことを特徴とする多機種機関推進プラントの2
速切換装置。
In a multi-engine propulsion plant where the propeller shaft is driven by a cruise engine in the low speed range and a cruise engine and a boost engine in the high speed range, the cruise engine power transmission mechanism is divided into two systems, low speed and high speed, and arranged at intervals. A self-periodic automatic engagement/disengagement clutch is provided between the input gear and the output gear of the low-speed power transmission mechanism, and a controlled clutch is provided between the input gear and the output gear of the high-speed power transmission mechanism. 2 of a multi-engine propulsion plant characterized by
Fast switching device.
JP9187278U 1978-07-03 1978-07-03 Two-speed switching device for multi-engine propulsion plants Expired JPS6024717Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP9187278U JPS6024717Y2 (en) 1978-07-03 1978-07-03 Two-speed switching device for multi-engine propulsion plants

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP9187278U JPS6024717Y2 (en) 1978-07-03 1978-07-03 Two-speed switching device for multi-engine propulsion plants

Publications (2)

Publication Number Publication Date
JPS558086U JPS558086U (en) 1980-01-19
JPS6024717Y2 true JPS6024717Y2 (en) 1985-07-24

Family

ID=29021531

Family Applications (1)

Application Number Title Priority Date Filing Date
JP9187278U Expired JPS6024717Y2 (en) 1978-07-03 1978-07-03 Two-speed switching device for multi-engine propulsion plants

Country Status (1)

Country Link
JP (1) JPS6024717Y2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4323354A (en) * 1979-02-15 1982-04-06 Outboard Marine Corporation Two-speed automatic transmission for a marine propulsion device
WO2003026957A1 (en) * 2001-09-25 2003-04-03 Yanmar Co.,Ltd. Hybrid ship propelling mechanism

Also Published As

Publication number Publication date
JPS558086U (en) 1980-01-19

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