JPH03164534A - Two-shaft type gas turbine for suction pump - Google Patents

Two-shaft type gas turbine for suction pump

Info

Publication number
JPH03164534A
JPH03164534A JP30394989A JP30394989A JPH03164534A JP H03164534 A JPH03164534 A JP H03164534A JP 30394989 A JP30394989 A JP 30394989A JP 30394989 A JP30394989 A JP 30394989A JP H03164534 A JPH03164534 A JP H03164534A
Authority
JP
Japan
Prior art keywords
shaft
reverse rotation
intermediate shaft
turbine
suction pump
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
JP30394989A
Other languages
Japanese (ja)
Other versions
JP2976074B2 (en
Inventor
Yukito Yoneda
米田 幸人
Hiroshi Ogawa
博史 小川
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.)
Yanmar Co Ltd
Original Assignee
Yanmar Diesel Engine Co 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 Yanmar Diesel Engine Co Ltd filed Critical Yanmar Diesel Engine Co Ltd
Priority to JP1303949A priority Critical patent/JP2976074B2/en
Publication of JPH03164534A publication Critical patent/JPH03164534A/en
Application granted granted Critical
Publication of JP2976074B2 publication Critical patent/JP2976074B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

PURPOSE:To prevent the reverse rotation of a high-speed rotated power turbine shaft positively by providing a reverse rotation impeding device, for impeding the reverse rotation of an intermediate shaft, at the intermediate shaft in a reduction gear for transmitting the rotating force of the power turbine shaft of a gas turbine to an output shaft. CONSTITUTION:A two-shaft type gas turbine for a suction pump is provided with an output turbine receiving high-temperature high pressure combustion gas generated at a gas generator, and the rotating power of this output turbine is transmitted to an output shaft 17 after being reduced to the specified rotating speed by a reduction gear 4. The reduction gear 4 is formed being provided with an intermediate shaft 18, plural gears 21, 29, and the like. In this case, a reverse rotation impeding device 30 for impeding the reverse rotation of the intermediate shaft 18 is fitted at the end part of the intermediate shaft 18. This reverse rotation impeding device 30 is formed of an inner wheel 32 fitted at a protruding part 18a provided at the end part of the intermediate shaft 18, an outer wheel 34 fitted, with play in the relatively rotatable state, at the outer periphery of the inner wheel 32 through a pair of ball hearings 33a, 33b, and a one-way clutch 35 interposed between the inner and outer wheels 32, 34.

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明は、出力軸が吸水ポンプの回転軸に直結された2
軸式のガスタービンに関するものである。
DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention provides a two
This relates to a shaft-type gas turbine.

(従来の技術) 商用電源を用いずに吸水ポンプを駆動する場合、原動機
として一般にはディーゼルエンジンが用いられている。
(Prior Art) When driving a water suction pump without using a commercial power source, a diesel engine is generally used as the prime mover.

ところで、吸水管のバルブが故障して閉弁しない事態に
陥ると、吸水ポンプの運転を停止したときに、水が逆流
して原動機が逆転し、軸受等を損傷する。
By the way, if the valve of the water suction pipe malfunctions and does not close, water will flow backwards when the water suction pump is stopped, causing the prime mover to reverse, damaging bearings and the like.

従来−船釣には、原動機の出力軸と吸水ポンプの回転軸
との間の動力伝達機構に、油圧クラッチ等を介装してい
たため、問題は回避されていた。
Conventionally, in boat fishing, the problem has been avoided because a hydraulic clutch or the like has been interposed in the power transmission mechanism between the output shaft of the prime mover and the rotating shaft of the water suction pump.

(発明が解決しようとする課題) ガスタービンはディーゼルエンジンと比較して小型・軽
量で高出力であり、特に2軸式ガスタービンは吸水ポン
プを駆動するのに最適の出力特性を有している。吸水ポ
ンプの原動機としてこのような2軸式ガスタービンを用
いた場合、出力軸が逆転すると、オイルポンプが正常に
作動せずに潤滑油が供給されない状態でパワータービン
軸が高速回転するので、軸受の損傷が激しく、逆転対策
は不可欠である。
(Problem to be solved by the invention) Gas turbines are smaller, lighter, and have higher output than diesel engines, and two-shaft gas turbines in particular have optimal output characteristics for driving water intake pumps. . When such a two-shaft gas turbine is used as the prime mover for a water suction pump, if the output shaft is reversed, the oil pump will not operate properly and the power turbine shaft will rotate at high speed without lubricating oil being supplied. The damage is severe and countermeasures against reversal are essential.

ところが従来のように原動機の出力軸と吸水ポンプの回
転軸との間の動力伝達機構に油圧クラッチを介装した場
合、伝達トルクが大きいことがら油圧クラッチが大型化
し、コストが高価であると共に設置スペースを多く必要
とする。
However, when a hydraulic clutch is installed in the power transmission mechanism between the output shaft of the prime mover and the rotating shaft of the water suction pump as in the past, the hydraulic clutch becomes large due to the large transmission torque, making it expensive and difficult to install. Requires a lot of space.

また油圧クラッチを保守・点検の容品な場所に設置する
余裕のない場合もあり、原動機側に逆転対策を施す要請
が強かった。
Additionally, there are cases where there is no room to install the hydraulic clutch in a location that is convenient for maintenance and inspection, and there has been a strong demand for a countermeasure against reverse rotation on the prime mover side.

(課題を解決するための手段) 上記課題を解決するため、本発明の吸水ポンプ用2軸式
ガスタービンは、吸水ポンプの回転軸に直結された出力
軸と、中間軸と複数の歯車とからなりパワータービン軸
の回動力を前記出力軸に伝達する減速装置とを備えた吸
水ポンプ用2軸式ガスタービンにおいて、前記中間軸の
逆転を阻止する逆転防止装置を設けたものである。
(Means for Solving the Problems) In order to solve the above problems, the two-shaft gas turbine for water suction pumps of the present invention includes an output shaft directly connected to the rotating shaft of the water suction pump, an intermediate shaft, and a plurality of gears. The present invention is a two-shaft gas turbine for a water suction pump that includes a speed reduction device that transmits rotational force of a power turbine shaft to the output shaft, and is provided with a reverse rotation prevention device that prevents the intermediate shaft from reversing.

(作用) 水の逆流により吸水ポンプの回転軸を介して出力軸が逆
転しても、逆転防止装置により中間軸の逆転が阻止され
る。したがって高速回転のパワータービン軸は逆転しな
い。
(Function) Even if the output shaft is reversed through the rotating shaft of the water suction pump due to a backflow of water, the reverse rotation prevention device prevents the intermediate shaft from reversing. Therefore, the high speed rotating power turbine shaft does not reverse rotation.

(実施例) 以下、本発明の一実施例を第1図〜第3図に基づいて説
明する。
(Example) Hereinafter, an example of the present invention will be described based on FIGS. 1 to 3.

第2図は本発明の一実施例における吸水ポンプ用2軸式
ガスタービンの概略縦断正面図で、潤滑油を貯溜するオ
イルパンを兼用した台床1上には、空気を吸入して高温
・高圧の燃焼ガスを発生するガス発生機2と、ガス発生
機2で発生した燃焼ガスから回転動力を取出す出力ター
ビン3と、出力タービン3で取出した回転動力を所定の
回転数に減速する減速装置4とが左側から右側にこの順
に配置されている。ガス発生機2の左側の側面には各種
補機類の軸受や歯車等を収容する補機ギヤボックス5が
取付けられている。
FIG. 2 is a schematic longitudinal sectional front view of a two-shaft gas turbine for a water suction pump according to an embodiment of the present invention. On the platform 1, which also serves as an oil pan for storing lubricating oil, air is sucked and heated. A gas generator 2 that generates high-pressure combustion gas, an output turbine 3 that extracts rotational power from the combustion gas generated by the gas generator 2, and a reduction gear that reduces the rotational power extracted by the output turbine 3 to a predetermined rotation speed. 4 are arranged in this order from left to right. An auxiliary equipment gear box 5 is attached to the left side surface of the gas generator 2, which accommodates bearings, gears, etc. of various auxiliary equipment.

ガス発生機2は、空気を圧縮する遠心圧縮機のロータ部
分を構成するインペラ7や、圧縮された空気と燃料とを
混合して燃焼させることにより高温・高圧の燃焼ガスを
作出する燃焼器8や、燃焼ガスにより回転駆動されてイ
ンペラ7を回転させる高圧タービンロータ9や、高圧タ
ービンロータ9の下流側に位置して高圧タービンロータ
9と同様の動作をする低圧タービンロータ10等を備え
ている。出力タービン3は、低圧タービンロータ10の
下流側に位置して燃焼ガスにより回転駆動されるパワー
タービンロータ12や、パワータービンロータ12を駆
動した後の燃焼ガスすなわち排気ガスを渦を発生させず
に減速させる排気デイフユーザ13や、排気ガスを放出
する排気ダクト14や、パワータービンロータ12と一
体に回転するパワータービン軸15等を備えている。減
速装置4は、パワータービン軸15の回転動力を所定の
回転速度に減速させて出力軸17に伝達するための、中
間軸18や複数の歯車19〜22等を備えている。
The gas generator 2 includes an impeller 7 that constitutes the rotor part of a centrifugal compressor that compresses air, and a combustor 8 that creates high-temperature, high-pressure combustion gas by mixing and combusting compressed air and fuel. , a high-pressure turbine rotor 9 that is rotationally driven by combustion gas to rotate the impeller 7, and a low-pressure turbine rotor 10 that is located downstream of the high-pressure turbine rotor 9 and operates in the same manner as the high-pressure turbine rotor 9. . The output turbine 3 includes a power turbine rotor 12 located downstream of the low-pressure turbine rotor 10 and rotated by combustion gas, and a power turbine rotor 12 that is located downstream of the low-pressure turbine rotor 10 and rotates the combustion gas, that is, the exhaust gas after driving the power turbine rotor 12, without generating a vortex. It includes an exhaust differential user 13 for deceleration, an exhaust duct 14 for releasing exhaust gas, a power turbine shaft 15 that rotates integrally with the power turbine rotor 12, and the like. The speed reduction device 4 includes an intermediate shaft 18, a plurality of gears 19 to 22, and the like for reducing the rotational power of the power turbine shaft 15 to a predetermined rotational speed and transmitting the rotational power to the output shaft 17.

パワータービン軸15は、一端部(第2図では左端部)
を玉軸受24により、また他端部(第2図では右端部)
を1対のころ軸受25g、25bにより、各々軸芯回り
に回動自在に支持されている。中間軸18は1対のころ
軸受26a、26bにより軸芯回りに回動自在に支持さ
れており、出力軸17は1対のころ軸受27a、27b
により軸芯回りに回動自在に支持されている。歯車19
はパワータービン軸15の雌端部外周に嵌合固定されて
、中間軸18の一端部外周に嵌合固定された歯車20に
噛合している。歯車21は中間軸18の雌端部外周に設
けられており、出力軸17の一端に固定された歯車22
に噛合している。中間軸18の他端部には中間軸18の
逆転を阻止する逆転防止装置30が取付けられている。
The power turbine shaft 15 has one end (the left end in FIG. 2).
by the ball bearing 24, and the other end (the right end in Fig. 2)
are supported by a pair of roller bearings 25g and 25b so as to be rotatable about their respective axes. The intermediate shaft 18 is rotatably supported around the axis by a pair of roller bearings 26a, 26b, and the output shaft 17 is supported by a pair of roller bearings 27a, 27b.
It is rotatably supported around its axis. gear 19
is fitted and fixed on the outer periphery of the female end of the power turbine shaft 15 and meshes with a gear 20 that is fitted and fixed on the outer periphery of one end of the intermediate shaft 18 . The gear 21 is provided on the outer periphery of the female end of the intermediate shaft 18, and the gear 22 is fixed to one end of the output shaft 17.
It meshes with the A reverse rotation prevention device 30 is attached to the other end of the intermediate shaft 18 to prevent the intermediate shaft 18 from rotating in reverse.

第1図は本発明の一実施例における吸水ポンプ用2軸式
ガスタービンの要部拡大横断平面図で、逆転防止装置3
0は、中間軸18の他端部に同芯状に一体に突設された
突出部18aの外周にキー嵌合する内輪32と、1対の
玉軸受33a、33bを介して内輪32の外周に相対回
動自在に遊嵌する外輪34と、内輪32と外輪34との
間に介装されたパッケージタイプのワンウェイクラッチ
35とにより構成されている。外輪34は複数のボルト
36によりブラケット37に取付けられており、ブラケ
ット37は複数のボルト38によりギアボックス本体3
9に取付けられている。外輪34には複数のボルト40
aによりカバ一体40bが取付けられている。
FIG. 1 is an enlarged cross-sectional plan view of the essential parts of a two-shaft gas turbine for a water suction pump according to an embodiment of the present invention.
0 is an inner ring 32 that is key-fitted to the outer periphery of a protrusion 18a that is concentrically and integrally protruded from the other end of the intermediate shaft 18, and an outer periphery of the inner ring 32 via a pair of ball bearings 33a and 33b. It is composed of an outer ring 34 that is loosely fitted in a relatively rotatable manner, and a package type one-way clutch 35 that is interposed between the inner ring 32 and the outer ring 34. The outer ring 34 is attached to a bracket 37 with a plurality of bolts 36, and the bracket 37 is attached to the gearbox body 3 with a plurality of bolts 38.
It is attached to 9. A plurality of bolts 40 are attached to the outer ring 34.
A cover unit 40b is attached by a.

第3図は本発明の一実施例における吸水ポンプ用2軸式
ガスタービンを採用した揚水設備の概略構成図で、2軸
式ガスタービン41の出力軸17はトルクメータ42を
介して傘歯車減速機43の入力端の軸44に連結されて
おり、傘歯車減速機43の出力側の軸45は連結軸46
を介して吸水ポンプ47の回転軸48に連結されている
。吸水ポンプ47の吐出側には吐水管49の一端が接続
されており、吐水管4つの他端は例えば処理用の水槽(
図示せず)等に接続されている。吸水ポンプ47は揚水
基の槽内に配置されている。吸水ポンプ47の回転軸4
8は吐水管49の鉛直部を貫通している。なお図示して
いないが、吐水管49の適所には開閉弁が設置されてい
る。
FIG. 3 is a schematic configuration diagram of water pumping equipment that employs a two-shaft gas turbine for a water suction pump according to an embodiment of the present invention. The output side shaft 45 of the bevel gear reducer 43 is connected to a connecting shaft 46.
It is connected to a rotating shaft 48 of a water suction pump 47 via. One end of a water discharge pipe 49 is connected to the discharge side of the water suction pump 47, and the other end of the four water discharge pipes is connected to a water tank for processing, for example.
(not shown) etc. The water suction pump 47 is arranged in the tank of the water pumping base. Rotating shaft 4 of water suction pump 47
8 penetrates the vertical part of the water discharge pipe 49. Although not shown, on-off valves are installed at appropriate locations on the water discharge pipe 49.

次に動作を説明する。2軸式ガスタービン41の運転時
には、パワータービンロータ12と一体に回転するパワ
ータービン軸15の回動力が歯車19.20を介して中
間軸18に伝達され、さらに歯車21.22を介して出
力軸17に伝達され、さらに傘歯車減速機43と連結軸
46とを介して回転軸48に伝達されて吸水ポンプ47
が駆動される。このとき中間軸18は正転方向に回動す
るので、逆転防止装置30は中間軸18の回動を阻止し
ない。
Next, the operation will be explained. During operation of the two-shaft gas turbine 41, the rotational force of the power turbine shaft 15, which rotates together with the power turbine rotor 12, is transmitted to the intermediate shaft 18 via the gear 19.20, and is further transmitted to the output via the gear 21.22. It is transmitted to the shaft 17 and further transmitted to the rotating shaft 48 via the bevel gear reducer 43 and the connecting shaft 46, and the water suction pump 47
is driven. At this time, the intermediate shaft 18 rotates in the forward direction, so the reverse rotation prevention device 30 does not prevent the intermediate shaft 18 from rotating.

吐水管49の開閉弁が故障して閉弁しなくなると、2軸
式ガスタービン41の運転を停止したときに、吐水管4
9内を水が逆流し、吸水ポンプ47の回転軸48に逆転
方向のトルクが加わる。このトルクは連結軸46と傘歯
車減速機43とを介して2軸式ガスタービン41の出力
軸17に伝達され、さらに歯車22と歯車21とを介し
て中間軸18に伝達される。これにより中間軸18が逆
転しようとするが、逆転防止装置30のワンウェイクラ
ッチ35により中間軸18の逆転は強固に阻止される。
If the on-off valve of the water discharge pipe 49 fails and does not close, when the operation of the two-shaft gas turbine 41 is stopped, the water discharge pipe 4
Water flows backward through the pump 9, and torque in the reverse direction is applied to the rotating shaft 48 of the water suction pump 47. This torque is transmitted to the output shaft 17 of the two-shaft gas turbine 41 via the connecting shaft 46 and the bevel gear reducer 43, and further transmitted to the intermediate shaft 18 via the gears 22 and 21. As a result, the intermediate shaft 18 attempts to reverse, but the one-way clutch 35 of the reverse rotation prevention device 30 firmly prevents the intermediate shaft 18 from reversing.

したがってパワータービン軸15は逆回転せず、玉軸受
24やころ軸受25a、25bが損傷することはない。
Therefore, the power turbine shaft 15 does not rotate in the opposite direction, and the ball bearing 24 and roller bearings 25a and 25b are not damaged.

このとき、中間軸18が回転しないので、出力軸17や
吸水ポンプ47の回転軸48も回転しない。
At this time, since the intermediate shaft 18 does not rotate, the output shaft 17 and the rotating shaft 48 of the water suction pump 47 also do not rotate.

なお、1対の軸受28a、28bにより軸芯周りに回動
自在に支持されたアイドラー歯車29は出力軸17の回
転方向を切替えるためのもので、アイドラー歯車2つを
用いずに歯車21と歯車22とが噛合するようにすると
、2軸式ガスタービン41の運転時に出力軸17はパワ
ータービン軸15と同方向に回転する。中間軸18の設
置位置を若干ずらせて、歯車21が歯車22に噛合せず
アイドラー歯車29に噛合するようにすると、中間軸1
8の回動力がアイドラー歯車29を介して出力軸17に
伝達されるので、21d1式ガスタービン41の運転時
に出力軸17はパワータービン軸15と逆方向に回転す
る。
Note that the idler gear 29, which is rotatably supported around the axis by a pair of bearings 28a and 28b, is for switching the rotation direction of the output shaft 17, and the gear 21 and the gear 29 are connected to each other without using two idler gears. 22, the output shaft 17 rotates in the same direction as the power turbine shaft 15 when the two-shaft gas turbine 41 is in operation. If the installation position of the intermediate shaft 18 is slightly shifted so that the gear 21 does not mesh with the gear 22 but meshes with the idler gear 29, the intermediate shaft 1
8 is transmitted to the output shaft 17 via the idler gear 29, the output shaft 17 rotates in the opposite direction to the power turbine shaft 15 when the 21d1 type gas turbine 41 is operating.

このように、逆転防止装置3oにより中間軸18の逆転
を阻止するように構成したので、経済的にパワータービ
ン軸15の逆転を防止でき、出力軸17と吸水ポンプ4
7の回転軸48とを支障なく直結できる。すなわち逆転
防lF:、装置3oによりパワータービン軸15の逆転
を直接阻止しようとすると、パワータービン軸15は高
速回転であるので逆転防止装置30の玉軸受33a、3
3bもそれに耐え得る特殊なものを用いる必要があり、
コストが高価になる。しがちパワータービン軸15の周
囲には逆転防止装置3oを設置するスペースがない。ま
た逆転防止装置3oにより出力軸17の逆転を阻止しよ
うとすると、出力軸17は低速でトルクが大きいので逆
転防止装置3oが大型化してコストが高価になる。
As described above, since the reverse rotation prevention device 3o is configured to prevent the intermediate shaft 18 from reversing, it is possible to economically prevent the power turbine shaft 15 from reversing, and the output shaft 17 and the water suction pump 4 can be prevented from reversing.
7 can be directly connected to the rotating shaft 48 without any problem. In other words, reverse rotation prevention lF: If an attempt is made to directly prevent the reverse rotation of the power turbine shaft 15 using the device 3o, the ball bearings 33a, 3 of the reverse rotation prevention device 30 will
3b also needs to be made of a special material that can withstand it.
The cost becomes high. There is no space around the power turbine shaft 15 to install the reverse rotation prevention device 3o. Further, if the reverse rotation prevention device 3o is used to prevent the output shaft 17 from reversing, the output shaft 17 has a low speed and a large torque, so the reverse rotation prevention device 3o becomes large and expensive.

(別の実施例) 上記実施例においては、逆転防止装置3oとしてワンウ
ェイクラッチ35を利用したが、本発明はこのような構
成に限定されるものではなく、逆転防止装置30として
例えばバンド式のブレーキを利用してもよい。
(Another Embodiment) In the above embodiment, the one-way clutch 35 was used as the reversal prevention device 3o, but the present invention is not limited to such a configuration. You may also use

(発明の効果) 以上説明したように本発明によれば、逆転防止装置によ
り中間軸の逆転を阻止するように構成したので、経済的
にパワータービン軸の逆転を防止でき、出力軸と吸水ポ
ンプの回転軸とを支障なく直結できる。すなわち逆転防
止装置によりパワータービン軸の逆転を直接阻止しよう
とすると、バワータービン軸は高速回転であるので逆転
防止装置の軸受等もそれに耐え得る特殊なものを用いる
必要があり、コストが高価になる。しかもパワータービ
ン軸の周囲には逆転防止装置を設置するスペースがない
。また逆転防止装置により出力軸の逆転を阻止しようと
すると、出力軸は低速でトルクが大きいので逆転防止装
置が大型化してコストが高価になる。本発明はこれらの
問題を一挙に解決したものである。
(Effects of the Invention) As explained above, according to the present invention, since the reverse rotation prevention device is configured to prevent the intermediate shaft from reversing, it is possible to economically prevent the power turbine shaft from reversing. It can be directly connected to the rotating shaft of the In other words, if an attempt is made to directly prevent the power turbine shaft from reversing using a reverse rotation prevention device, the power turbine shaft rotates at high speed, so special bearings and the like for the reverse rotation prevention device must be used to withstand the high speed rotation, resulting in high costs. . Moreover, there is no space around the power turbine shaft to install a reverse rotation prevention device. Further, if an attempt is made to prevent the output shaft from reversing with a reverse rotation prevention device, the output shaft has a low speed and a large torque, so the reverse rotation prevention device becomes large and expensive. The present invention solves these problems all at once.

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

第1図は本発明の一実施例における吸水ポンプ用2軸式
ガスタービンの要部拡大横断平面図、第2図は同吸水ポ
ンプ用2軸式ガスタービンの概略縦断正面図、第3図は
同吸水ポンプ用2軸式ガスタービンを採用した揚水設備
の概略構成図である。
FIG. 1 is an enlarged cross-sectional plan view of essential parts of a two-shaft gas turbine for a water suction pump according to an embodiment of the present invention, FIG. 2 is a schematic longitudinal sectional front view of the two-shaft gas turbine for a water suction pump, and FIG. It is a schematic block diagram of the water pumping equipment which adopted the two-shaft gas turbine for the water suction pump.

Claims (1)

【特許請求の範囲】[Claims] 1、吸水ポンプの回転軸に直結された出力軸と、中間軸
と複数の歯車とからなりパワータービン軸の回動力を前
記出力軸に伝達する減速装置とを備えた吸水ポンプ用2
軸式ガスタービンにおいて、前記中間軸の逆転を阻止す
る逆転防止装置を設けたことを特徴とする吸水ポンプ用
2軸式ガスタービン。
1. For a water suction pump, which is equipped with an output shaft directly connected to the rotating shaft of the water suction pump, and a reduction gear that includes an intermediate shaft and a plurality of gears and transmits the rotational force of the power turbine shaft to the output shaft.
A two-shaft gas turbine for a water suction pump, characterized in that the shaft-type gas turbine is provided with a reverse rotation prevention device that prevents the intermediate shaft from reversing.
JP1303949A 1989-11-22 1989-11-22 Two-shaft gas turbine for suction pump Expired - Fee Related JP2976074B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1303949A JP2976074B2 (en) 1989-11-22 1989-11-22 Two-shaft gas turbine for suction pump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1303949A JP2976074B2 (en) 1989-11-22 1989-11-22 Two-shaft gas turbine for suction pump

Publications (2)

Publication Number Publication Date
JPH03164534A true JPH03164534A (en) 1991-07-16
JP2976074B2 JP2976074B2 (en) 1999-11-10

Family

ID=17927233

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1303949A Expired - Fee Related JP2976074B2 (en) 1989-11-22 1989-11-22 Two-shaft gas turbine for suction pump

Country Status (1)

Country Link
JP (1) JP2976074B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008057541A (en) * 2006-08-29 2008-03-13 Snecma Device for driving rotor of turbine engine auxiliary

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008057541A (en) * 2006-08-29 2008-03-13 Snecma Device for driving rotor of turbine engine auxiliary

Also Published As

Publication number Publication date
JP2976074B2 (en) 1999-11-10

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