JPS6010196B2 - Bearing lubricator - Google Patents

Bearing lubricator

Info

Publication number
JPS6010196B2
JPS6010196B2 JP12456480A JP12456480A JPS6010196B2 JP S6010196 B2 JPS6010196 B2 JP S6010196B2 JP 12456480 A JP12456480 A JP 12456480A JP 12456480 A JP12456480 A JP 12456480A JP S6010196 B2 JPS6010196 B2 JP S6010196B2
Authority
JP
Japan
Prior art keywords
cylinder
oil
shaft
movable
boss chamber
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
JP12456480A
Other languages
Japanese (ja)
Other versions
JPS5749099A (en
Inventor
裕志 高橋
裕康 阿南
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.)
Hitachi Sanki Engineering Co Ltd
Hitachi Ltd
Original Assignee
Hitachi Sanki Engineering Co Ltd
Hitachi 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 Hitachi Sanki Engineering Co Ltd, Hitachi Ltd filed Critical Hitachi Sanki Engineering Co Ltd
Priority to JP12456480A priority Critical patent/JPS6010196B2/en
Publication of JPS5749099A publication Critical patent/JPS5749099A/en
Publication of JPS6010196B2 publication Critical patent/JPS6010196B2/en
Expired legal-status Critical Current

Links

Description

【発明の詳細な説明】 本発明は軸流または斜流形の可動翼ポンプ、特にその可
動翼軸を軸受潤滑装置に関するものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an axial flow or mixed flow type movable vane pump, and particularly to a bearing lubrication device for the movable vane shaft thereof.

従来のこの種可動翼ポンプは第1図に示すように、コン
トローラ部1「モータ2、油圧サーボシリンダー3、モ
−夕2により駆動されるポンプ鼠4、油圧サーボシリン
ダー3により操作される操作ロッド5、ポンプ軸4に駆
動されると共に、操作ロッドもこより回動される可動翼
6を内蔵するケーシング7およびケーシング7に揚水管
8を介して連結された吐出ペンド9により構成されてい
る。
As shown in FIG. 1, a conventional movable vane pump of this type includes a controller section 1, a motor 2, a hydraulic servo cylinder 3, a pump rod 4 driven by the motor 2, and an operating rod operated by the hydraulic servo cylinder 3. 5. It is composed of a casing 7 that is driven by the pump shaft 4 and also includes a movable blade 6 that is rotated by the operating rod, and a discharge pend 9 that is connected to the casing 7 via a lift pipe 8.

上記可動翼6の軸6aは第2図に示すように中空状のポ
ンプ藤4の下端に固定されたィンベラハブ10に回敷自
在に枢着されており、この軸6aと操作ロッド5の下端
に固定されたスパィダ11はアーム12、継手13およ
びターンバックル14を介して連結されている。
As shown in FIG. 2, the shaft 6a of the movable blade 6 is rotatably pivoted to an invera hub 10 fixed to the lower end of the hollow pump ratchet 4, and the shaft 6a and the lower end of the operating rod 5 The fixed spider 11 is connected via an arm 12, a joint 13 and a turnbuckle 14.

前記可動翼軸6a、スパイダ11、アーム12、継手1
3およびターンバックル14はインベラハブ10とイン
ベラキヤップ15とにより形成され「かつ油の充満した
インベラボス室16内に収納されている。上記操作ロッ
ド5の上端はポンプ軸4の中空部を貫通して油圧サーボ
シリンダー3内の油圧ピストン18に連続されている(
第3図参照)。
The movable wing shaft 6a, spider 11, arm 12, joint 1
3 and turnbuckle 14 are formed by an invera hub 10 and an invera cap 15 and are housed in an invera boss chamber 16 filled with oil. It is connected to the hydraulic piston 18 in the hydraulic servo cylinder 3 (
(See Figure 3).

この油圧ピストン18の上、下側室はそれぞれ操作油通
路(図示せず)を介して前記モータ2の軸(図示せず)
の中空部に蓮適している。また油圧サーボシリンダー3
への操作油の供給装置としては、第4図に示すように前
記シリンダー3に蓮通する圧油室19および油圧ピスト
ン18の位置をフィードバック制御する復帰レバー20
が設けられている。上述した構造では、操作ロッド5の
往復運動を可動翼6の軸6aに伝達し、その軸6aを回
動させる機構すなわちスパイダ11、ターンバックル1
4、継手量3およびアーム12は可動翼軸6aと共に「
油の充満したィンベラボス室16内に収納されているた
め、錆の発生および異物などの侵入する恐れがない。
The upper and lower chambers of this hydraulic piston 18 are connected to the shaft (not shown) of the motor 2 through operating oil passages (not shown), respectively.
The hollow part of the lotus is suitable. Also hydraulic servo cylinder 3
As shown in FIG. 4, the system for supplying operating oil to the cylinder 3 includes a pressure oil chamber 19 that communicates with the cylinder 3 and a return lever 20 that feedback controls the position of the hydraulic piston 18.
is provided. In the above structure, a mechanism for transmitting the reciprocating motion of the operating rod 5 to the shaft 6a of the movable wing 6 and rotating the shaft 6a, that is, a spider 11 and a turnbuckle 1 are provided.
4, the joint amount 3 and the arm 12 together with the movable blade shaft 6a
Since it is housed in the oil-filled interior boss chamber 16, there is no risk of rust or foreign matter entering.

しかし可動翼軸6aはその軸受17a,17bが水圧モ
ーメントを受けるばかりでなく、可動翼6の角度調節が
断続的に行われ、これに伴う可動翼軸6aの回動も断続
的に行われる。
However, the bearings 17a, 17b of the movable blade shaft 6a are not only subjected to a hydraulic moment, but also the angle adjustment of the movable blade 6 is performed intermittently, and the corresponding rotation of the movable blade shaft 6a is also performed intermittently.

このため可動翼軸6aは高荷重でかつ低速回転するので
、その軸受17a,17bは油膜を形成し‘こくいから
暁付きなどの事故を起す恐れがある。本発明は上記欠点
を解消し、可動翼軸の軸受の摩耗を防止し、可動翼を円
滑に回動させて、ポンプの信頼性の向上をはかることを
目的とするもので、ィンベラハブのィンベラボス室に対
向する面にシリンダーを取付け、このシリンダー内に可
動翼軸用操作ロッドに取付けたピストンを収納すると共
に、そのシリンダーを吸油弁を介してィンベラボス室に
、吐油弁および可榛管を介して可動翼軸に設けた軸受用
油路にそれぞれ運通させたことを特徴とするものである
For this reason, the movable blade shaft 6a is subjected to a high load and rotates at a low speed, so that the bearings 17a and 17b form an oil film and become stiff, which may cause an accident such as a splashing. The present invention aims to eliminate the above-mentioned drawbacks, prevent wear of the bearing of the movable vane shaft, rotate the movable vane smoothly, and improve the reliability of the pump. A cylinder is installed on the surface facing the cylinder, and the piston attached to the operating rod for the movable blade shaft is housed in this cylinder, and the cylinder is connected to the Invera boss chamber through the oil intake valve and through the oil discharge valve and flexible pipe. It is characterized in that the oil passages for the bearings are provided in the movable blade shafts.

以下本発明の一実施例を図面について説明する。An embodiment of the present invention will be described below with reference to the drawings.

第5図に示す符号のうち第2図に示す符号と同一のもの
は同じ符号を示す。第5図ないし第7図において、21
‘よインベラハブ10のインベラボス室16に対面する
面、すなわち操作ロッド5が貫通するインベラハブ量0
の下面に固定されたシリンダー、22はシリンダー21
内に摺動自在に収納されたピストンで、このピストン2
2は操作ロッド5に固定されている。23,25はシリ
ンダー21内の上部に設けられた吸油弁および吐油弁、
24,26もまシリンダー21内の下部に設けられた吸
油弁および吐油弁である。
Among the symbols shown in FIG. 5, the same symbols as those shown in FIG. 2 indicate the same symbols. In Figures 5 to 7, 21
The surface of the invera hub 10 facing the invera boss chamber 16, that is, the amount of invera hub that the operating rod 5 penetrates is 0.
Cylinder fixed to the bottom surface of the cylinder, 22 is the cylinder 21
This piston 2 is a piston that is slidably housed inside.
2 is fixed to the operating rod 5. 23 and 25 are oil intake valves and oil discharge valves provided in the upper part of the cylinder 21;
24 and 26 are oil intake valves and oil discharge valves provided at the lower part of the cylinder 21.

前記シリンダー21は吸油弁23,24を介してィンベ
ラボス室16に、吐油弁25,26を介して可操管27
にそれぞれ連通されている。28は可動翼髄6a内に設
けられ、かつ可榛管27を介してシリンダー21に蓮通
する軸受用油路で「その一端は軸受17aに、池端は軸
受富7bにそれぞれ閉口している。
The cylinder 21 is connected to the inbera boss chamber 16 via oil intake valves 23 and 24, and to the adjustable pipe 27 via oil discharge valves 25 and 26.
are connected to each other. Reference numeral 28 denotes a bearing oil passage which is provided in the movable blade core 6a and passes through the cylinder 21 via the flexible tube 27, and its one end is closed to the bearing 17a, and the end thereof is closed to the bearing well 7b.

その他の構造は従来例(第1図〜第4図)を同一である
から説明を省略する。次に上記のような構成からなる本
実施例の作用について説明する。
The rest of the structure is the same as that of the conventional example (FIGS. 1 to 4), so a description thereof will be omitted. Next, the operation of this embodiment configured as described above will be explained.

可動翼6の角度を変更するために操作ロッド5を下降さ
せると、この操作ロッド5に固定されてピストン22も
同様に下降するので、シリンダー21内の上部の吸油弁
23は開き、吐油弁25は閉じると共に、下部の吸油弁
24は閉じ、吐油弁26は開く。
When the operating rod 5 is lowered to change the angle of the movable blade 6, the piston 22 fixed to the operating rod 5 also descends in the same way, so the upper oil intake valve 23 in the cylinder 21 opens and the oil discharge valve opens. 25 is closed, the lower oil intake valve 24 is closed, and the oil discharge valve 26 is opened.

このためピストン22の下側室内の油は可提督27を介
して可動翼軸6a内の油路28に流入し、さらに可動翼
軸6aの軸受17a,17bの摺動面へ強制的に供給さ
れる。前記ピストン22が上昇する場合も、上記に準じ
て軸受17a,17bの摺動面へ強制的に油を供給する
ことができる。以上説明したように、本発明によれば操
作ロッドの往復動により「可動翼の回動に応じて強制的
に潤滑油を軸受へ供給することができるので、軸受の摩
耗を防止して可動翼の回転を円滑に行い、ポンプの信頼
性を向上させることができる。
Therefore, the oil in the lower chamber of the piston 22 flows into the oil passage 28 in the movable wing shaft 6a via the rotor 27, and is further forcibly supplied to the sliding surfaces of the bearings 17a, 17b of the movable wing shaft 6a. Ru. Even when the piston 22 rises, oil can be forcibly supplied to the sliding surfaces of the bearings 17a and 17b in the same manner as described above. As explained above, according to the present invention, lubricating oil can be forcibly supplied to the bearings in accordance with the rotation of the movable blades by the reciprocating movement of the operating rod, thereby preventing wear on the bearings. The pump can rotate smoothly and improve the reliability of the pump.

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

第1図は従来の可動翼ポンプの縦断面図、第2図は第1
図のA部の詳細図、第3図は第1図の油圧サーボシリン
ダーの詳細断面図、第4図は可動翼の操作説明図、第5
図は本発明に係わる可動翼軸の軸受潤滑装置の一実施例
を示す断面図、第6図および第7図は第5図のB,C部
の拡大詳細図である。 母‘・…・ポンプ軸「 5・・・・・・操作ロッドL
6a…・・・可動翼軸、10・・・・・・ィンベラハブ
、16・・・・・・ィンベラボス室、竃7a,17b・
…・・軸受、21……シリンダー、22……ピストン、
23,24……吸油弁、25,26・・…・吐油弁、2
7・・・…可孫管「 28・・・・・・軸受用油路。 菊′図 菊Z図 黍3図 兼4図 繋5図 第6図 第7図
Figure 1 is a vertical cross-sectional view of a conventional movable vane pump, and Figure 2 is a vertical cross-sectional view of a conventional movable vane pump.
3 is a detailed sectional view of the hydraulic servo cylinder in FIG. 1, 4 is an explanatory diagram of the operation of the movable blade,
The figure is a sectional view showing one embodiment of the bearing lubrication device for a movable blade shaft according to the present invention, and FIGS. 6 and 7 are enlarged detailed views of sections B and C in FIG. 5. Mother'... Pump shaft 5... Operating rod L
6a...Movable blade shaft, 10...Imbera hub, 16...Imbera boss chamber, stoves 7a, 17b.
...Bearing, 21...Cylinder, 22...Piston,
23, 24... Oil suction valve, 25, 26... Oil discharge valve, 2
7...Kazuno pipe 28...Oil passage for bearing.

Claims (1)

【特許請求の範囲】[Claims] 1 ポンプ軸を貫通する操作ロツドにより、インペラボ
ス室内に設けた可動翼軸を操作するように構成した可動
翼ポンプにおいて、インペラハブの前記インペラボス室
に対向する面にシリンダーを取付け、このシリンダー内
に前記操作ロツドに取付けたピストンを収納すると共に
、そのシリンダーを吸油弁を介してインペラボス室に、
吐油弁および可撓管を介して前記可動翼軸に設けた軸受
用油路にそれぞれ連通させたことを特徴とする軸受潤滑
装置。
1. In a movable vane pump configured to operate a movable vane shaft provided in an impeller boss chamber by an operating rod penetrating the pump shaft, a cylinder is attached to the surface of the impeller hub facing the impeller boss chamber, and a cylinder is installed within the cylinder to operate the movable vane shaft provided in the impeller boss chamber. In addition to housing the piston attached to the rod, the cylinder is inserted into the impeller boss chamber via an oil intake valve.
A bearing lubricating device characterized in that the oil passages for a bearing provided on the movable blade shaft are connected to each other via an oil discharge valve and a flexible pipe.
JP12456480A 1980-09-10 1980-09-10 Bearing lubricator Expired JPS6010196B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12456480A JPS6010196B2 (en) 1980-09-10 1980-09-10 Bearing lubricator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12456480A JPS6010196B2 (en) 1980-09-10 1980-09-10 Bearing lubricator

Publications (2)

Publication Number Publication Date
JPS5749099A JPS5749099A (en) 1982-03-20
JPS6010196B2 true JPS6010196B2 (en) 1985-03-15

Family

ID=14888596

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12456480A Expired JPS6010196B2 (en) 1980-09-10 1980-09-10 Bearing lubricator

Country Status (1)

Country Link
JP (1) JPS6010196B2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2742239A1 (en) * 2011-08-10 2014-06-18 Mekorot Water Company Ltd. Well pump system

Also Published As

Publication number Publication date
JPS5749099A (en) 1982-03-20

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