JPS58566B2 - turbine starting device - Google Patents
turbine starting deviceInfo
- Publication number
- JPS58566B2 JPS58566B2 JP6121778A JP6121778A JPS58566B2 JP S58566 B2 JPS58566 B2 JP S58566B2 JP 6121778 A JP6121778 A JP 6121778A JP 6121778 A JP6121778 A JP 6121778A JP S58566 B2 JPS58566 B2 JP S58566B2
- Authority
- JP
- Japan
- Prior art keywords
- turbine
- annular groove
- shaft
- pin
- starting device
- 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
Links
Landscapes
- Control Of Turbines (AREA)
Description
【発明の詳細な説明】
この発明は動力式のターニング装置の補助として設けら
れる手動式のタービン始動装置の改良に関する。DETAILED DESCRIPTION OF THE INVENTION This invention relates to an improvement in a manual turbine starter provided as an auxiliary to a powered turning device.
タービン始動装置は始めてのタービン起動時。The turbine starter is used when starting the turbine for the first time.
または軸受の潤滑油の温度が低い時に1手動によりター
ビンの軸を回転して起動を助ける装置である。Alternatively, it is a device that helps start the turbine by manually rotating the turbine shaft when the temperature of the lubricating oil in the bearing is low.
第1図および第2図に従来のタービン始動装置を示すに
、タービンの軸1の軸継手フランジ部2と、他のタービ
ンまたは回転機の軸3の軸継手フランジ部4とが1円板
5を介してボルト6およびナツト7で締結されている。1 and 2 show a conventional turbine starting device, in which a shaft coupling flange portion 2 of a shaft 1 of a turbine and a shaft coupling flange portion 4 of a shaft 3 of another turbine or rotating machine are connected to a circular plate 5. It is fastened with a bolt 6 and a nut 7 via.
円板5の外周には。軸1と平行な側面8を持つ多数の歯
9が形成されている。On the outer periphery of the disk 5. A number of teeth 9 are formed with side surfaces 8 parallel to the axis 1.
また円板5の外周に配設された翼10は油圧によるター
ニング装置のものである。Further, the blades 10 disposed on the outer periphery of the disc 5 are of a hydraulic turning device.
軸受台カバー15に固定された支持台11に、軸1に平
行にかつ回転可能に、支持軸12が取付けられている。A support shaft 12 is rotatably attached to a support base 11 fixed to a bearing base cover 15 in parallel to the shaft 1.
支持軸12のはゾ中夫に、支持軸12に直角に穴13が
設けられている。A hole 13 is provided in the center of the support shaft 12 at right angles to the support shaft 12.
穴13に駆動レバー14が差し込まれている。A drive lever 14 is inserted into the hole 13.
このレバー14を手動により支持軸12を支点として、
先端部が第2図の一点鎖線の位置から二点鎖線の位置に
移動するように揺動させ、レバー14の先端部で歯9を
押し上げてタービン回転させる。This lever 14 is manually operated using the support shaft 12 as a fulcrum.
The tip is swung so that it moves from the position indicated by the one-dot chain line in FIG. 2 to the position indicated by the two-dot chain line in FIG. 2, and the tip of the lever 14 pushes up the teeth 9 to rotate the turbine.
上記従来のタービン始動装置の場合、歯の加工をホブ盤
などの歯切り機械で能率的に行なうために ロータと別
の円板5が必要とされ、そのための材料費、加工費およ
び組立費が必要であり全体として高価になるという欠点
がある。In the case of the above-mentioned conventional turbine starter, a disc 5 separate from the rotor is required in order to efficiently machine the teeth with a gear cutting machine such as a hobbing machine, which requires material, processing, and assembly costs. The disadvantage is that it is necessary and overall expensive.
この発明は上記のような欠点を除去して安価なタービン
始動装置を提供することを目的とする。The object of the present invention is to eliminate the above-mentioned drawbacks and provide an inexpensive turbine starter.
この発明によれば上記の目的はタービンの軸継手フラン
ジ部の外周面に環状溝を設け、該環状溝の側壁を貫通し
て環状溝の中に複数個のピンを円周方向に分布して設け
、軸継手フランジ部の外周側に前記ピンに対向する位置
に、軸継手フランジ部の接線方向に揺動して前記ピンと
適宜係脱する駆動レバーを設けて成るタービン始動装置
によって達せられる。According to the present invention, the above object is achieved by providing an annular groove on the outer circumferential surface of a shaft coupling flange portion of a turbine, and penetrating the side wall of the annular groove and distributing a plurality of pins in the annular groove in the circumferential direction. This is achieved by a turbine starter, which is provided with a drive lever provided on the outer circumferential side of the shaft joint flange at a position opposite to the pin and swings in a tangential direction of the shaft joint flange to appropriately engage and disengage from the pin.
以下この発明の実施例を第3図および第4図にもとづい
て説明する。Embodiments of the present invention will be described below with reference to FIGS. 3 and 4.
図において、第1図および第2図と同符合のものは、同
じ構造と機能とを持つものである。In the figures, the same reference numerals as in FIGS. 1 and 2 have the same structure and function.
軸1の軸継手フランジ部22の外周に環状溝23が設け
られている。An annular groove 23 is provided on the outer periphery of the shaft coupling flange portion 22 of the shaft 1 .
環状溝23の中には、その側壁25を貫通して多数のピ
ン24が配設されている。A number of pins 24 are disposed inside the annular groove 23 and passing through a side wall 25 thereof.
第1図および第2図で述べたものと同様な駆動レバー1
4の先端でピン24を押し上げて、タービンを回転させ
る。Drive lever 1 similar to that described in FIGS. 1 and 2
Push up the pin 24 with the tip of the pin 24 to rotate the turbine.
上記のように構成されたこの発明によるタービン始動装
置の場合、駆動レバーと係合する部分がたソ環状溝23
とピン24とだけでフランジ部外周面に直に形成されて
いるので、その動作および組立は簡単かつ安価になる。In the turbine starter according to the present invention configured as described above, the portion that engages with the drive lever has the annular groove 23.
Since only the and pins 24 are formed directly on the outer circumferential surface of the flange portion, its operation and assembly are simple and inexpensive.
すなわち環状溝は旋、またピンを配設する穴はボール盤
で容易に加工でき、ピン自体は安価な鋼棒で済み、更に
従来のような特別な円板が不要になる。That is, the annular groove can be easily machined using a circular groove, and the hole in which the pin is to be placed can be easily machined using a drill press, the pin itself can be made of an inexpensive steel rod, and there is no need for a special disc as in the past.
第1図は従来のタービン始動装置の部分的縦断面図、第
2図は第1図の■−■矢視の部分的横断面図、第3図は
この発明によるタービン始動装置の一実施例を示す部分
的縦断面図、第4図は第3図の■−■矢視の部分的横断
面図である。
1・・・・・・軸、12・・・・・・支持軸、14・・
・・・・レバー、22・・・・・・軸継手フランジ部、
23・・・・・・環状溝。
24・・・・・・ピン、25・・・・・・環状溝の側壁
。FIG. 1 is a partial vertical cross-sectional view of a conventional turbine starting device, FIG. 2 is a partial cross-sectional view taken along the ■-■ arrow in FIG. 1, and FIG. 3 is an embodiment of the turbine starting device according to the present invention. FIG. 4 is a partial cross-sectional view taken along the line ■-■ in FIG. 3. 1... shaft, 12... support shaft, 14...
... Lever, 22 ... Shaft joint flange part,
23... annular groove. 24... Pin, 25... Side wall of the annular groove.
Claims (1)
は該環状溝の側壁を軸方向に貫通して環状溝の中に複数
個のピンを円周方向に分布して設け。 軸継手フランジ部の外周側の前記ピンに対向する位置に
、軸継手フランジ部の接線方向に揺動して前記ピンに適
宜係脱する駆動レバーを設けて成ることを特徴とするタ
ービン始動装置。[Claims] 1. An annular groove is provided on the outer peripheral surface of the shaft coupling flange portion of the turbine, and a plurality of pins are distributed in the annular groove in the annular groove by passing through the side wall of the annular groove in the axial direction. Set up. A turbine starting device comprising: a drive lever that swings in a tangential direction of the shaft joint flange to engage and disengage the pin as appropriate, at a position facing the pin on the outer peripheral side of the shaft joint flange.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6121778A JPS58566B2 (en) | 1978-05-23 | 1978-05-23 | turbine starting device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6121778A JPS58566B2 (en) | 1978-05-23 | 1978-05-23 | turbine starting device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS54152701A JPS54152701A (en) | 1979-12-01 |
| JPS58566B2 true JPS58566B2 (en) | 1983-01-07 |
Family
ID=13164803
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP6121778A Expired JPS58566B2 (en) | 1978-05-23 | 1978-05-23 | turbine starting device |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS58566B2 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP6266406B2 (en) * | 2014-03-28 | 2018-01-24 | 三菱日立パワーシステムズ株式会社 | Turning device and operation method of turning device |
-
1978
- 1978-05-23 JP JP6121778A patent/JPS58566B2/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| JPS54152701A (en) | 1979-12-01 |
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