JPS5820901A - Rotary blade type expansion machine - Google Patents

Rotary blade type expansion machine

Info

Publication number
JPS5820901A
JPS5820901A JP12027981A JP12027981A JPS5820901A JP S5820901 A JPS5820901 A JP S5820901A JP 12027981 A JP12027981 A JP 12027981A JP 12027981 A JP12027981 A JP 12027981A JP S5820901 A JPS5820901 A JP S5820901A
Authority
JP
Japan
Prior art keywords
blade
groove
back pressure
pressure
cylinder
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.)
Pending
Application number
JP12027981A
Other languages
Japanese (ja)
Inventor
Yuki Koishi
小石 勇喜
Hiroshi Uno
浩 宇野
Junichi Jiyakudo
雀堂 純一
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.)
Panasonic Holdings Corp
Original Assignee
Matsushita Electric Industrial 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 Matsushita Electric Industrial Co Ltd filed Critical Matsushita Electric Industrial Co Ltd
Priority to JP12027981A priority Critical patent/JPS5820901A/en
Publication of JPS5820901A publication Critical patent/JPS5820901A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C21/00Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/08Rotary pistons
    • F01C21/0809Construction of vanes or vane holders
    • F01C21/0818Vane tracking; control therefor
    • F01C21/0854Vane tracking; control therefor by fluid means
    • F01C21/0863Vane tracking; control therefor by fluid means the fluid being the working fluid

Abstract

PURPOSE:To prevent reliably a separation of the edge of a blade from the internal circumferential surface of a cylinder, by forming a pressure equalizing groove on a high pressure side surface of a blade provided with a pressurizing device of back pressure. CONSTITUTION:Back pressure grooves 12 and 13 which lead back pressure to a blade groove 5 and are confronted with each other are formed on a front and a rear walls 2 and 3 of a cylinder 1, and a pressure equalizing pipe 7 which connects the blade groove 5 with an expansion space is formed on a high pressure side surface of a blade 6. In this constitution, high pressure actuation gas is filled evenly in the blade groove 5 through the back pressure grooves 12 and 13 and the blade 6 is pushed forcibly against the internal circumferential surface of the cylinder 1, in the vicinity of a rotary position P1 where a separation phenomenon is easy to occur. Then, when the blade 6 advances in a direction of a position P2, the pressure equalizing groove 7 of the blade 6 is opened into the expansion space 16 and a high pressure working fluid in the blade groove 5 is made to flow into the expansion space 16.

Description

【発明の詳細な説明】 回転子に複数の羽根溝を設け、この羽根溝に羽根を挿入
し、この羽根付回転子をシリンダ内に偏心させて支持し
て、この回転子を回転させる従来の容積型回転羽根式膨
張機では、回転子の回転中に羽根の先端がシリンダの内
周壁から遊離する現象(羽根の遊離現象)を防止する手
段として、羽根の底部に膨張機へ流入する高圧の作動気
体の一部を導入して、羽根の底部を背圧付勢する手段が
とられているが、低速回転時に羽根自体の遠心力が力学
的に十分得られず、膨張機を低速回転数か本発明は、上
記の問題点を改善するもので、高圧の作動気体の圧力を
羽根の背圧付勢力とする手段を改善するものであり、膨
張機の低速回転時においても、充分な羽根背圧付勢力を
得るようにすることを目的とする。
[Detailed description of the invention] In the conventional method, a rotor is provided with a plurality of blade grooves, blades are inserted into the blade grooves, and the rotor with blades is eccentrically supported in a cylinder to rotate the rotor. In positive displacement rotary vane type expanders, high pressure flowing into the expander is installed at the bottom of the vanes as a means of preventing the phenomenon in which the tips of the vanes come loose from the inner circumferential wall of the cylinder during rotation of the rotor (vane detachment phenomenon). Measures have been taken to introduce part of the working gas to apply back pressure to the bottom of the blade, but the centrifugal force of the blade itself is not dynamically sufficient at low speed rotation, and the expander is forced to rotate at low speed. The present invention is intended to improve the above-mentioned problems, and improves the means for using the pressure of high-pressure working gas as a back pressure urging force for the blades, so that even when the expander rotates at low speed, the blades can be sufficiently The purpose is to obtain back pressure urging force.

以下本発明をその一実施例を示す図面を参考に説明する
The present invention will be explained below with reference to the drawings showing one embodiment thereof.

1はシリンダ、2は前壁、3は後壁、4は回転子で、回
転子4はシリンダ内に偏心として回転目−在にと9つけ
られている。回転子4には羽根溝5が形成され、羽根溝
6に羽根6が挿入されている。
1 is a cylinder, 2 is a front wall, 3 is a rear wall, 4 is a rotor, and the rotor 4 is eccentrically mounted in the cylinder so as to rotate. A blade groove 5 is formed in the rotor 4, and a blade 6 is inserted into the blade groove 6.

羽根6の一面には圧力均衡溝7が形成されている。A pressure balancing groove 7 is formed in one surface of the blade 6.

またシリンダ1には流入頭部8と流入孔9が設けられ、
後壁3には背圧流入部10と背圧連通孔11および円弧
状の後壁背圧力溝12、さらに排出孔14と排出頭部1
7が設けられ、前壁2には、前記後壁背圧力溝12に対
応する部分に円弧状の前壁背圧力溝13が設けられ、シ
リンダ1、前壁2、後壁3で構成される空間で回転子4
が回転し、その際羽根溝6の底部は後壁背圧力溝12と
前壁背圧力溝13に連通し得る。
The cylinder 1 is also provided with an inflow head 8 and an inflow hole 9.
The rear wall 3 includes a back pressure inlet 10, a back pressure communication hole 11, an arcuate rear wall back pressure groove 12, and a discharge hole 14 and a discharge head 1.
7, and the front wall 2 is provided with an arc-shaped front wall back pressure groove 13 in a portion corresponding to the rear wall back pressure groove 12, and is composed of a cylinder 1, a front wall 2, and a rear wall 3. rotor 4 in space
rotates, the bottom of the vane groove 6 being able to communicate with the rear wall backpressure groove 12 and the front wall backpressure groove 13.

高圧の作動気体は分岐点Aにおいて分流し、膨張過程を
生ずるだめの主流は流入頭部8からシリンダ1の流入孔
9を通って、シリンダ1、前壁2、後壁3、羽根6で囲
まれる膨張空間15に入り、回転子4と外部出力軸16
を矢印M方向に回転させ、外部出力軸16に動力を一一
一発生させた後排出孔″を通−て排出頭部”71り外部
に出る・一方分岐点Aにおいて分流し、羽根6の底部に
付12を通り、羽根溝5の底部を通って前壁2の前壁背
圧力溝13へ導入される。前壁背圧力溝13と後壁背圧
力溝12に導入された高圧の作動気体は羽根6の遊離現
象を防ぐための羽根6への背圧力として作用する。また
背圧流入部1oからの高圧の作動気体は、羽根6に対す
る背圧付勢力のみではなく、その一部が羽根6の圧力均
衡溝を介して膨張空間15へ流入し、これによって、シ
リンダ1の流入孔9で生ずる流体抵抗に起因する作動気
体の流量減少を補い、膨張機の効率の低下を防ぐ作用を
する。そして膨張過程を終了した作動気体は低圧となっ
て、排出頭部17を通って膨張機外に出る。
The high-pressure working gas is separated at the branch point A, and the main flow of the reservoir that causes the expansion process passes from the inlet head 8 through the inlet hole 9 of the cylinder 1 and is surrounded by the cylinder 1, the front wall 2, the rear wall 3, and the vane 6. The rotor 4 and external output shaft 16
is rotated in the direction of arrow M to generate power on the external output shaft 16, and then exits to the outside through the discharge head 71 through the discharge hole. It passes through the attachment 12 at the bottom and is introduced through the bottom of the vane groove 5 into the front wall back pressure groove 13 of the front wall 2. The high pressure working gas introduced into the front wall back pressure groove 13 and the rear wall back pressure groove 12 acts as a back pressure on the blade 6 to prevent the blade 6 from coming loose. Further, the high pressure working gas from the back pressure inflow portion 1o not only exerts a back pressure urging force on the blade 6, but also a part of it flows into the expansion space 15 through the pressure balancing groove of the blade 6, thereby causing the cylinder 1 It compensates for the decrease in the flow rate of the working gas caused by the fluid resistance that occurs in the inflow hole 9, and serves to prevent a decrease in the efficiency of the expander. After completing the expansion process, the working gas has a low pressure and exits the expander through the discharge head 17.

羽根6は回転位置P1付近で遊離現象を生じ易いが、後
壁背圧力溝12とこれから羽根溝6を経て前壁背圧力溝
13に均等な高圧の作動気体が充満し、羽根6の底部に
背圧付勢力を作用させ、羽根6の先端とシリンダ1の内
周面の間に互いに反力が発生し、回転子4の低速回転時
の遊離現象を防      1・ぐ。次に羽根6の回転
位置がPlからP2付近まで進むと、羽根6は遊離現象
の生じやすい範囲をはずれる。このとき羽根6の高圧側
側面に設けた圧力均衡溝7が膨張空間15に開口して、
高圧の作動気体を膨張空間15に開口して高圧の作動気
体を流入させる。このように、高圧作動気体は、羽根6
の遊離現象範囲を超えた回転角の位置で、羽根6の圧力
均衡溝7を通じて膨張空間16に開口し、吸入過程(膨
張空間16がまた流入孔9VC開口している回転角度の
範囲)の終了と同時に羽根溝5の底部と前壁背圧力溝1
3および後壁背圧力溝12との連通関係が遮断されて、
背圧流入部10からの作動気体が膨張空間15へ導入さ
れることを停止する。また羽根6が回転位置P3からP
4にある場合には、羽根溝6の底部に残留した高圧の作
動気体が羽根6の先端を過剰にシリンダ1の内面に押し
付けて機械損失をもたらすことのないよう、羽根6の圧
力均衡溝7を通じて羽根溝5の底部の高圧の作動気体を
逃がすのである。
Although the blade 6 is prone to release phenomenon near the rotational position P1, the rear wall back pressure groove 12 and from there, the front wall back pressure groove 13 via the blade groove 6 are filled with even high-pressure working gas, and the bottom of the blade 6 is By applying a back pressure biasing force, a reaction force is generated between the tips of the vanes 6 and the inner circumferential surface of the cylinder 1, thereby preventing the rotor 4 from coming loose when rotating at low speed. Next, when the rotational position of the blade 6 advances from Pl to around P2, the blade 6 leaves the range where the separation phenomenon is likely to occur. At this time, the pressure balancing groove 7 provided on the high-pressure side side surface of the blade 6 opens into the expansion space 15.
The high-pressure working gas is opened into the expansion space 15 and the high-pressure working gas is introduced into the expansion space 15 . In this way, the high pressure working gas is
At a rotational angle position exceeding the release phenomenon range, the pressure balancing groove 7 of the blade 6 opens into the expansion space 16, and the suction process (the rotational angle range in which the expansion space 16 also opens the inflow hole 9VC) ends. At the same time, the bottom of the blade groove 5 and the front wall back pressure groove 1
3 and the rear wall back pressure groove 12 are cut off,
The working gas from the back pressure inlet 10 is stopped from being introduced into the expansion space 15. Also, the blade 6 moves from the rotational position P3 to P
4, the pressure balancing groove 7 of the blade 6 is installed to prevent the high-pressure working gas remaining at the bottom of the blade groove 6 from excessively pressing the tip of the blade 6 against the inner surface of the cylinder 1 and causing mechanical loss. The high pressure working gas at the bottom of the blade groove 5 is released through the blade groove 5.

上記実施例から明らかなように、本発明の回転羽根式膨
張機では、回転子の回転角度に関係なく常に後壁背圧力
溝および回転子の羽根溝を通じて前壁背圧力溝に高圧の
作動気体が滞留しており、羽根°溝の底部が後壁背圧力
溝に開口する、羽根の遊離現象範囲の開始回転角時に遅
滞なく羽根底部へ背圧付勢力を与え、かつ従来では後壁
背圧力溝からの距離の関係で背圧付勢力の伝わり難かっ
た前壁付近の羽根底部へも均等に背圧力を付勢すること
ができ、低速回転時の羽根の遊離現象を防ぐことができ
て、膨張機の効率が改善されると共に、羽根に、前壁と
後壁の両側面から対称的に圧力が付加されて羽根へ偏向
荷重が加わらず、したがって背圧力溝の開口回転角時(
背圧力として作用する角度範囲)での羽根の摩耗が改善
され、さらに前壁背圧力溝の容積の一部が高圧の作動気
体に伴って循環する潤滑油の滞留機能を果し、前壁側の
膨張機構部品表面の潤滑作用を促進する効果を奏する。
As is clear from the above embodiments, in the rotary vane expander of the present invention, high-pressure working gas is always supplied to the front wall back pressure groove through the rear wall back pressure groove and the rotor blade groove, regardless of the rotation angle of the rotor. stagnates, and when the bottom of the blade groove opens into the rear wall back pressure groove, a back pressure biasing force is applied to the blade bottom without delay at the starting rotation angle of the blade release phenomenon range, and conventionally, the rear wall back pressure It is possible to apply back pressure evenly to the bottom of the blade near the front wall, where the back pressure force is difficult to transmit due to the distance from the groove, and it is possible to prevent the blade from coming loose during low speed rotation. In addition to improving the efficiency of the expander, pressure is applied to the blades symmetrically from both sides of the front and rear walls, so that no deflection load is applied to the blades, so that at the opening rotation angle of the back pressure groove (
In addition, part of the volume of the front wall back pressure groove serves as a retention function for the lubricating oil that circulates with the high pressure working gas, and the front wall side This has the effect of promoting lubrication on the surfaces of the expansion mechanism parts.

【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を示す回転羽根式膨張機の側
断面図、第2図は第1図のn −n’線による正面図、
第3図は第1図のm −m’線による正面図、第4図は
同膨張機の羽根の斜視図である。 1・・・・・・シリンダ、2・・・・・・前壁、3・・
・・・・後壁、4・・・・・回転子、5・・・・・・羽
根溝、6 ・・・・・羽根、7・・・・・・圧力均衡溝
、9・・・・・流入孔、11・・・・・背圧連通孔、1
2・・・・・・後壁背圧力溝(背圧力溝)、13・・・
・・・前壁背圧力溝(背圧力溝)、16・・・・・・膨
張空間。 代理人の氏名 弁理士 中 尾 敏 男 ほか1名第1
図       へ m’−1 第2図
FIG. 1 is a side sectional view of a rotary vane type expander showing an embodiment of the present invention, FIG. 2 is a front view taken along line n-n' in FIG. 1,
FIG. 3 is a front view taken along line m-m' in FIG. 1, and FIG. 4 is a perspective view of the blades of the expander. 1...Cylinder, 2...Front wall, 3...
... Rear wall, 4 ... Rotor, 5 ... Vane groove, 6 ... Vane, 7 ... Pressure balance groove, 9 ...・Inflow hole, 11... Back pressure communication hole, 1
2... Rear wall back pressure groove (back pressure groove), 13...
... Front wall back pressure groove (back pressure groove), 16... Expansion space. Name of agent: Patent attorney Toshio Nakao and 1 other person No. 1
Figure m'-1 Figure 2

Claims (1)

【特許請求の範囲】[Claims] シリンダの両端に前壁と後壁をとりつけてシリンダ内部
の空間を形成し、この字跡に、羽根溝を有してこの羽根
溝に羽根を挿入した回転子を配設すると共に、この空間
に高圧作動気体を流入させる流入孔を設け、前壁あるい
は後壁の一方に背圧連通孔と、この背圧連通孔から前記
羽根溝の底部へ高圧作動気体の一部を導く円弧状の背圧
力溝を設け、他方にこの背圧力溝と対向する円弧状の他
の背圧力溝を設け、かつ羽根の高圧側側面に圧力均衡溝
を形成し、前記背圧連通孔からの作動気体を羽根の底部
付勢用および膨張用作動気体とした回転羽根式膨張機。
A front wall and a rear wall are attached to both ends of the cylinder to form a space inside the cylinder, and a rotor having blade grooves and blades inserted into the blade grooves is disposed in this trace, and a high pressure is placed in this space. An inflow hole through which working gas flows is provided, a back pressure communication hole is provided on one of the front wall or the rear wall, and an arcuate back pressure groove that guides a portion of the high pressure working gas from the back pressure communication hole to the bottom of the blade groove. , and another arc-shaped back pressure groove facing this back pressure groove is provided on the other side, and a pressure balancing groove is formed on the high-pressure side side surface of the blade, and the working gas from the back pressure communication hole is directed to the bottom of the blade. A rotary vane expander that uses working gas for urging and expansion.
JP12027981A 1981-07-30 1981-07-30 Rotary blade type expansion machine Pending JPS5820901A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12027981A JPS5820901A (en) 1981-07-30 1981-07-30 Rotary blade type expansion machine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12027981A JPS5820901A (en) 1981-07-30 1981-07-30 Rotary blade type expansion machine

Publications (1)

Publication Number Publication Date
JPS5820901A true JPS5820901A (en) 1983-02-07

Family

ID=14782300

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12027981A Pending JPS5820901A (en) 1981-07-30 1981-07-30 Rotary blade type expansion machine

Country Status (1)

Country Link
JP (1) JPS5820901A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4775504A (en) * 1985-08-22 1988-10-04 Kurosaki Refractories Co., Ltd. Process for producing refractory plate for sliding nozzle

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4775504A (en) * 1985-08-22 1988-10-04 Kurosaki Refractories Co., Ltd. Process for producing refractory plate for sliding nozzle

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