JPH09105561A - Stirling machine - Google Patents

Stirling machine

Info

Publication number
JPH09105561A
JPH09105561A JP26282295A JP26282295A JPH09105561A JP H09105561 A JPH09105561 A JP H09105561A JP 26282295 A JP26282295 A JP 26282295A JP 26282295 A JP26282295 A JP 26282295A JP H09105561 A JPH09105561 A JP H09105561A
Authority
JP
Japan
Prior art keywords
gas
cylinder
space
annular
piston
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
JP26282295A
Other languages
Japanese (ja)
Other versions
JP3258872B2 (en
Inventor
Takashi Nakazato
孝 中里
Takayuki Inoue
貴至 井上
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.)
Sanyo Electric Co Ltd
Original Assignee
Sanyo Electric 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 Sanyo Electric Co Ltd filed Critical Sanyo Electric Co Ltd
Priority to JP26282295A priority Critical patent/JP3258872B2/en
Publication of JPH09105561A publication Critical patent/JPH09105561A/en
Application granted granted Critical
Publication of JP3258872B2 publication Critical patent/JP3258872B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02GHOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS; USE OF WASTE HEAT OF COMBUSTION ENGINES; NOT OTHERWISE PROVIDED FOR
    • F02G2243/00Stirling type engines having closed regenerative thermodynamic cycles with flow controlled by volume changes
    • F02G2243/30Stirling type engines having closed regenerative thermodynamic cycles with flow controlled by volume changes having their pistons and displacers each in separate cylinders

Landscapes

  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Abstract

PROBLEM TO BE SOLVED: To provide a high performance Stirling machine in which pressure loss of working gas on a gas flow passage between a compression space and an expansion space is reduced, and heat efficiency is increased. SOLUTION: An annular spacer 20 having an inclined upper surface is disposed in a gas inlet space 16 located at the bottom of an annular empty chamber 15 formed in the outer periphery of a second cylinder 12. With use of the spacer 20, inflow gas into the gas inlet space 16 smoothly horizontally diffuses, and flows through a heat regenerator 8 with less resistance upwardly of the annular empty chamber 15 as a uniform gas flow whereby an effective gas amount flowing into an expansion space is increased and hence terminal efficiency at the heat regenerator 8 is improved.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は、圧縮空間と膨張空
間との間のガス流通経路における作動ガスの圧損を低減
し、性能を向上させたスターリング機器に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a Stirling machine having improved performance by reducing pressure loss of a working gas in a gas flow path between a compression space and an expansion space.

【0002】[0002]

【従来の技術】図9は、スターリング機器の一例を示す
概略断面図であって、1は第1シリンダ11に内挿され
た第1ピストン、2は第2シリンダ12に内挿された第
2ピストン、3は第1ピストンと第2ピストンを或る位
相差を持って往復運動させる駆動部、4は第1ピストン
1の前方に形成されるガス圧縮空間、5は第2ピストン
2の前方に形成されるガス膨張空間を示しておる。
2. Description of the Related Art FIG. 9 is a schematic sectional view showing an example of a Stirling machine, where 1 is a first piston inserted in a first cylinder 11 and 2 is a second piston inserted in a second cylinder 12. A piston, 3 is a drive unit that reciprocates the first piston and the second piston with a certain phase difference, 4 is a gas compression space formed in front of the first piston 1, and 5 is in front of the second piston 2. The gas expansion space formed is shown.

【0003】6はガス圧縮空間4とガス膨張空間5とを
連通させるガス流路で、このガス流路6には、ガス圧縮
空間4側にギャップ式熱交換器7を配設する一方、ガス
膨張空間5側に熱再生器8と熱交換器(放熱フィン)9
とを配設している。
Reference numeral 6 denotes a gas flow passage which connects the gas compression space 4 and the gas expansion space 5 to each other. In the gas flow passage 6, a gap type heat exchanger 7 is arranged on the gas compression space 4 side, while A heat regenerator 8 and a heat exchanger (radiation fin) 9 are provided on the expansion space 5 side.
And are arranged.

【0004】ここで、第2シリンダ12は、内側筒体1
3と外側中空筒14から成り、内側筒体13と外側中空
筒14との間の形成される環状空間15内に前記熱再生
器8が収納配設されている。
The second cylinder 12 is the inner cylinder 1
3 and the outer hollow cylinder 14, and the heat regenerator 8 is housed in an annular space 15 formed between the inner cylinder 13 and the outer hollow cylinder 14.

【0005】そして前記環状空間15の底部には、ガス
流路6からの作動ガスが最初に流入するガス入口空間1
6が環状の空胴となって連設形成されており、そしてそ
のガス入口空間16の底面の一カ所にガス入口17が開
口形成されている。従って、このガス入口17から流入
した作動ガスは、そのガス入口空間16から立ち昇って
熱再生器8を通過してガス膨張空間5に流入するように
なっている。
At the bottom of the annular space 15, the gas inlet space 1 into which the working gas from the gas passage 6 first flows.
6 are formed as a ring-shaped cavity and are continuously formed, and a gas inlet 17 is formed at one location on the bottom surface of the gas inlet space 16. Therefore, the working gas flowing from the gas inlet 17 rises from the gas inlet space 16, passes through the heat regenerator 8, and flows into the gas expansion space 5.

【0006】また第1シリンダ11側に設けられるギャ
ップ式熱交換器7は、そのシリンダの内側筒体の外周壁
と放熱フィンを有する外側筒体の内周壁との間にギャッ
プ部19を設けており、このギャップ部19を圧縮作動
ガスが通過する際に熱を外部へ放出するようにしてい
る。なお10は第ピストン1と第2ピストン2との後方
空間の背圧調整用の流路を示している。
The gap type heat exchanger 7 provided on the first cylinder 11 side has a gap portion 19 provided between the outer peripheral wall of the inner cylinder of the cylinder and the inner peripheral wall of the outer cylinder having the heat radiation fins. Therefore, when the compressed working gas passes through the gap portion 19, heat is released to the outside. Reference numeral 10 denotes a flow path for adjusting back pressure in the rear space between the first piston 1 and the second piston 2.

【0007】上記構成で、まず駆動部3が駆動すると第
1ピストン1がガス圧縮空間4側に移動してガス圧縮空
間4に充満するヘリウムや窒素等の液化しにくい作動ガ
スが圧縮される。圧縮された作動ガスは、ギャップ式熱
交換器7で外気と熱交換され冷却される。そしてさらに
ガス流路6を介して作動ガスは、熱再生器8に流入す
る。熱再生器8に流入した作動ガスは、内部の充填材を
通過する際に蓄熱され、作動ガスはガス膨張空間5へ流
入される。
With the above structure, first, when the drive unit 3 is driven, the first piston 1 moves to the gas compression space 4 side and the working gas such as helium and nitrogen which fills the gas compression space 4 and is difficult to liquefy is compressed. The compressed working gas is cooled by exchanging heat with the outside air in the gap type heat exchanger 7. Then, the working gas further flows into the heat regenerator 8 via the gas flow path 6. The working gas that has flowed into the heat regenerator 8 stores heat when passing through the filler inside, and the working gas flows into the gas expansion space 5.

【0008】その後、ガス膨張空間5の第2ピストン2
が第1ピストン1とある位相差を持って降下してくる。
これによって、ガス膨張空間5が拡張されて熱再生器8
からガス膨張空間5へ流入した高圧の作動ガスが急膨張
して、作動ガスの圧力が急降下するため作動ガスが低温
となる。やがて、第2ピストン2が上昇を開始し、第1
ピストン1が後退すると、低温となる作動ガスが熱再生
器8を通ってガス圧縮空間4へ戻る。このとき、熱再生
器8では冷熱の蓄熱がされる。
After that, the second piston 2 in the gas expansion space 5
Comes down with a certain phase difference from the first piston 1.
As a result, the gas expansion space 5 is expanded and the heat regenerator 8 is expanded.
The high-pressure working gas that has flowed into the gas expansion space 5 rapidly expands, and the pressure of the working gas sharply drops, so that the working gas becomes a low temperature. Eventually, the second piston 2 starts to rise, and the first piston 2
When the piston 1 retracts, the working gas having a low temperature returns to the gas compression space 4 through the heat regenerator 8. At this time, cold heat is stored in the heat regenerator 8.

【0009】上記した工程によって、1つの熱サイクル
が終了し、この工程が駆動部の往復運動にによって繰り
返され、これにより、徐々に、ガス膨張空間の周辺の温
度が低温とされる。
By the above-mentioned steps, one thermal cycle is completed, and this step is repeated by the reciprocating movement of the driving part, whereby the temperature around the gas expansion space is gradually lowered.

【0010】[0010]

【発明が解決しようとする課題】ところで、熱再生器の
熱効率は、第1シリンダのガス圧縮空間4から第2シリ
ンダのガス膨張空間5へ流入し、膨張に作用する有効ガ
ス量が多いほど高いものとなる。従って熱再生器8を配
設している環状空間15を作動ガスがどの部分でも抵抗
差がなく、即ち圧損が無く熱再生器8を通過し、均一に
ガスが流れることが望ましい。
By the way, the thermal efficiency of the heat regenerator increases as the amount of effective gas flowing from the gas compression space 4 of the first cylinder into the gas expansion space 5 of the second cylinder and acting on expansion increases. Will be things. Therefore, it is desirable that the working gas passes through the annular space 15 in which the heat regenerator 8 is disposed without any resistance difference, that is, without pressure loss, and passes through the heat regenerator 8 to uniformly flow the gas.

【0011】しかし、上述した従来の第2シリンダ12
の構造であると、環状空間へは作動ガスは位置的に見て
片方に寄った一個のガス入口17から入り、そのガスが
環状の空間を全周方向に拡散し、その後空間底面と鉛直
な環状空間15の内面に沿うよう方向を転換して上方へ
と流れるが、ガス入口17から遠い場所ほど届くガス量
が減り、かつその場所でガスが方向を転換する際、環状
空間の鉛直な内面と底面とのなす角度が直角なためガス
にとって大きい流通抵抗となって、熱再生器8を通過す
るガスは弱いガス流になってしまい、ガス膨張空間5に
流入する総ガス量が減り、熱効率が低いものとなる問題
があった。
However, the conventional second cylinder 12 described above is used.
With this structure, the working gas enters the annular space through one gas inlet 17 which is close to one side in terms of position, the gas diffuses in the entire circumferential direction of the annular space, and then the space bottom surface and the vertical direction. Although the direction is changed so as to follow the inner surface of the annular space 15 and flows upward, when the distance from the gas inlet 17 decreases, the amount of gas reaching the area decreases, and when the gas changes direction at that location, the vertical inner surface of the annular space Since the angle between the bottom surface and the bottom surface is a right angle, the flow resistance becomes large for the gas, and the gas passing through the heat regenerator 8 becomes a weak gas flow, so that the total amount of gas flowing into the gas expansion space 5 is reduced and the thermal efficiency is reduced. There was a problem that was low.

【0012】本発明は、上記問題に鑑みて成されたもの
で、作動ガスをガス膨張空間にスムーズに流し、有効ガ
ス量が多くなって熱効率を向上させ性能を高められるス
ターリング機器を提供することを目的とする。
The present invention has been made in view of the above problems, and provides a Stirling machine capable of smoothly flowing a working gas into a gas expansion space, increasing an effective gas amount, improving thermal efficiency, and enhancing performance. With the goal.

【0013】[0013]

【課題を解決するための手段】上記目的を達成するた
め、本発明の請求項1記載のスターリング機器は、第1
シリンダにおける第1ピストン前方のガス圧縮空間と第
2シリンダにおける第2ピストン前方のガス膨張空間と
がガス流路で連通し、前記第1ピストンと第2ピストン
が或る位相差を持って往復動駆動することにより、第1
シリンダから第2シリンダに流入した圧縮作動ガスが膨
張して冷却され、その膨張作動ガスが第1シリンダに戻
る熱サイクルが繰返されて、前記第2シリンダの外周壁
と放熱フィンを有する外側中空筒との間に形成された環
状空室に収設された円筒状の熱再生器に冷熱が蓄熱され
るスターリング機器において、前記ガス流路からのガス
流入口が開口している前記環状空室の内底部に、流入し
た作動ガスが前記環状空室の底部全周域に均一に拡散し
かつ前記熱再生器へと均一な流れとなって上昇通過して
前記ガス膨張空間に流入するようなガス流を形成させる
環状のスペーサを配したことを特徴とするスターリング
機器。
In order to achieve the above object, a Stirling machine according to claim 1 of the present invention is provided with a first Stirling machine.
A gas compression space in front of the first piston in the cylinder and a gas expansion space in front of the second piston in the second cylinder communicate with each other through a gas flow path, and the first piston and the second piston reciprocate with a certain phase difference. First by driving
The compressed working gas that has flowed from the cylinder to the second cylinder is expanded and cooled, and the expanded working gas is returned to the first cylinder to repeat the heat cycle, and the outer hollow cylinder having the outer peripheral wall of the second cylinder and the heat radiation fins. In a Stirling machine in which cold heat is stored in a cylindrical heat regenerator housed in an annular space formed between and, in the annular space where the gas inlet from the gas flow path is open A gas in which the working gas that has flowed into the inner bottom is uniformly diffused in the entire peripheral region of the bottom of the annular cavity and flows into the gas expansion space as a uniform flow to the heat regenerator. A Stirling machine having an annular spacer for forming a flow.

【0014】また、請求項2記載のスターリング機器
は、前記環状空室の内底部に配される前記環状のスペー
サは、一端部に前記ガス流入口と連通するガス流通孔を
有するか若しくは前記ガス流入口と対応する端部が切徐
された形状に形成され、かつ前記ガス流入口と反対側端
に向い漸次高さが高くなる一定角度の傾斜した上面に形
成したものである。
According to a second aspect of the present invention, in the Stirling machine, the annular spacer disposed on the inner bottom of the annular space has a gas flow hole communicating with the gas inlet at one end or the gas. The end corresponding to the inflow port is formed in a cut-off shape, and is formed on the upper surface inclined at a constant angle so that the height gradually increases toward the end opposite to the gas inflow port.

【0015】さらにまた、請求項3記載のスターリング
機器は、前記環状空室の内底部に配される前記環状のス
ペーサは、内側に凹んだ湾曲した傾斜上面に形成されて
いるものである。
Furthermore, in the Stirling machine according to a third aspect of the present invention, the annular spacer arranged on the inner bottom portion of the annular space is formed on a curved inclined upper surface that is recessed inward.

【0016】[0016]

【発明の実施の形態】以下、本発明の実施例を図面に基
づき説明する。なお図9に示す従来装置と同一又は同等
の構成部は同一番号で示す。
BEST MODE FOR CARRYING OUT THE INVENTION Embodiments of the present invention will be described below with reference to the drawings. The same or equivalent components as those of the conventional device shown in FIG. 9 are designated by the same reference numerals.

【0017】図1において、熱再生器8を配設する第2
シリンダ12における環状空室15の下部、すなわち図
番16で示すガス入口空間の内部に、図2に示すように
全体が環形で、かつ高さが一方に向かって徐々に高くな
るように上面21を斜めにカットした形状のスペーサー
20を配設する。このスペーサー20は、高温の作動ガ
スに耐えられるように耐熱性の部材例えば樹脂の成形品
で形成されていると共に、低い方の部分にはガス流通孔
22が設けられている。
Referring to FIG. 1, a second heat regenerator 8 is provided.
In the lower part of the annular vacant chamber 15 in the cylinder 12, that is, inside the gas inlet space shown in FIG. 16, an upper surface 21 having a ring shape as a whole and gradually increasing in height toward one side as shown in FIG. A spacer 20 having an obliquely cut shape is arranged. The spacer 20 is formed of a heat-resistant member such as a molded product of resin so as to withstand a high-temperature working gas, and a gas passage hole 22 is provided in the lower portion.

【0018】従って、スペーサー20はこのガス流通孔
22をガス入口17と一致させる向きにして、ガス入口
空間16内に配し、接着剤等によりガス入口空間16の
底に強固に装着固定されている。
Therefore, the spacer 20 is arranged in the gas inlet space 16 with the gas passage hole 22 aligned with the gas inlet 17, and is firmly attached and fixed to the bottom of the gas inlet space 16 by an adhesive or the like. There is.

【0019】こうしたスペーサー20がガス入口部分で
ある第2シリンダ12内の底部(ガス入口空間16)に
配されていると、ガス流路6からの作動ガスがガス入口
17からガス流通孔22を通りガス入口空間16に出る
と、そのガスはスペーサー20の傾斜上面21に沿い抵
抗なく流れ、ガス流通孔22と反対側のガス入口空間1
6の領域の方へもスムースに回り込んで行き、ガス入口
空間16全体に十分に拡散する。
When such a spacer 20 is arranged in the bottom portion (gas inlet space 16) in the second cylinder 12 which is the gas inlet portion, the working gas from the gas flow path 6 passes from the gas inlet 17 to the gas flow hole 22. When passing through the gas inlet space 16, the gas flows along the inclined upper surface 21 of the spacer 20 without resistance, and the gas inlet space 1 on the opposite side of the gas flow hole 22 is provided.
It smoothly wraps around to the area 6 and diffuses sufficiently into the entire gas inlet space 16.

【0020】こうして横(水平向き)へ流れガス入口空
間16に拡散したガスは、その後、第2シリンダの内側
面に沿い立ち昇るように水平から垂直方向へと流れる向
きが変わる。この時この流れが変更する地点の角度が、
本発明では、図4に示すように、スペーサー20の傾斜
上面21と第2シリンダの内側面24とで鈍角βとなっ
ているため、従来の水平なシリンダ底面と垂直な内面と
による直角になっていた場合より、抵抗が少なくなりガ
スの流れが良くなり、熱再生器8をガスが圧損を受けず
に均一に通過するようになっって、シリンダのガス膨張
空間5に十分な量のガスを送給することができるように
なる。よって、スタリーング機器の性能が高まり、熱再
生器8の熱効率を向上させることができるようになる。
The gas that has flowed laterally (horizontally) in this way and then diffused into the gas inlet space 16 changes its direction from horizontal to vertical so as to rise along the inner surface of the second cylinder. At this time, the angle of the point where this flow changes
In the present invention, as shown in FIG. 4, since the obtuse angle β is formed between the inclined upper surface 21 of the spacer 20 and the inner side surface 24 of the second cylinder, a right angle is formed by the conventional horizontal cylinder bottom surface and the vertical inner surface. The resistance is reduced and the gas flow is improved, and the gas passes uniformly through the heat regenerator 8 without pressure loss, so that a sufficient amount of gas can be supplied to the gas expansion space 5 of the cylinder. Will be able to send. Therefore, the performance of the staring device is improved, and the thermal efficiency of the heat regenerator 8 can be improved.

【0021】またスペーサーの上面を、図5に示すよう
に下に凸の曲線を描くような内側(下方)に湾曲した傾
斜上面21bに形成したスペーサー20Bを使用する
と、ガス流に対する抵抗が更に少なくすることができる
ので、もっと効果的にガスの拡散及び上昇を推進できる
ようになり、熱効率の改善により有効となる。またこの
湾曲度合いをシリンダの内径、ピストンの駆動力等構造
上の要素と関連させて適正に設定することで、最高の出
力を得られるようになることは言うまでもない。
Further, when the spacer 20B formed on the upper surface of the spacer on the inclined upper surface 21b curved inward (downward) so as to draw a downward convex curve as shown in FIG. 5 is used, the resistance against gas flow is further reduced. Therefore, it becomes possible to promote the diffusion and rise of gas more effectively, and it becomes more effective by improving the thermal efficiency. Further, it goes without saying that the maximum output can be obtained by appropriately setting the degree of curvature in association with structural elements such as the inner diameter of the cylinder and the driving force of the piston.

【0022】図6乃至図8は、他の実施例に係るスペー
サー20Cを示し、第1実施例のスペーサー20のよう
にガス導入のためのガス流通孔22を備えさせるのでは
なく、ガス流路6のガス入口17と対応する側の端部2
6を広く切徐した形のスペーサー20Cとしたものであ
る。
FIGS. 6 to 8 show a spacer 20C according to another embodiment, which is different from the spacer 20 of the first embodiment in that a gas passage hole 22 for introducing gas is not provided, but a gas passage. 6, the end 2 on the side corresponding to the gas inlet 17
6 is a spacer 20C having a shape in which 6 is widely cut.

【0023】このスペーサー20Cでは、端部26を切
り落してガス導入を可能としており、第1実施例のスペ
ーサー20のようにガス流通孔22を形成せずともよい
ので、加工等が容易になりコスト的にも安いものとでき
る。
In this spacer 20C, the gas can be introduced by cutting off the end portion 26, and it is not necessary to form the gas circulation hole 22 unlike the spacer 20 of the first embodiment, so that the processing is facilitated and the cost is reduced. It can be cheap.

【0024】[0024]

【発明の効果】以上のように請求項1の発明によれば、
筒状の熱再生器を配設したシリンダ外周の環状空室に、
偏在位置するガス入口から流入した作動ガスをガス入口
と遠い側まで十分に誘導して、環状空室をシリンダの作
動空間へと均一に流れるガス流を形成できるようなスペ
ーサを配したので、流通抵抗を受けて流量の減る心配の
熱再生器も、ガスは均一な流れとなって通過し、ガス作
動空間へ送り込まれる有効ガス量は十分となり、熱再生
器での蓄熱度も高められて、熱効率を向上できるスタリ
ーング機器を提供できる。
As described above, according to the first aspect of the present invention,
In the annular space around the cylinder where the tubular heat regenerator is placed,
Since the working gas flowing from the unevenly located gas inlets is sufficiently guided to the side far from the gas inlets, and the spacer is arranged so as to form a gas flow that uniformly flows into the working space of the cylinder, the spacer is arranged. Even in the heat regenerator, which is concerned that the flow rate will decrease due to resistance, the gas passes through as a uniform flow, the amount of effective gas sent to the gas working space is sufficient, and the heat storage degree in the heat regenerator is also increased. It is possible to provide a staring device that can improve thermal efficiency.

【0025】また、具体的には請求項2の発明のよう
に、このスペーサは環状でかつ傾斜した上面を持つスペ
ーサとすることで、簡単にガス流を均一に流せるものと
なり、構成的にも複雑にならず、低コストで実現でき
る。
Further, specifically, as in the second aspect of the invention, the spacer is annular and has an inclined upper surface, so that the gas flow can be easily and uniformly flown, and also in terms of constitution. It is not complicated and can be realized at low cost.

【0026】更に、このスペーサの傾斜上面を内側に凹
む湾曲状にすれば、一段に均一なガス流を形成できるよ
うになり、さらなる熱効率の向上、及び性能をアップさ
せたスタリーング機器を提供できるようになる。
Further, if the inclined upper surface of the spacer is curved inwardly, a more uniform gas flow can be formed, and it is possible to provide a staring machine with further improved thermal efficiency and performance. become.

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

【図1】本発明に係るスタリーング機器の概略断面図。FIG. 1 is a schematic sectional view of a staring machine according to the present invention.

【図2】本発明の熱再生器に均一に流すガス流を形成せ
るスペーサの斜視図。
FIG. 2 is a perspective view of a spacer for forming a gas flow that evenly flows in the heat regenerator of the present invention.

【図3】上記スペーサの縦断側面図。FIG. 3 is a vertical sectional side view of the spacer.

【図4】上記スペーサの平面図。FIG. 4 is a plan view of the spacer.

【図5】上面を下方に湾曲した傾斜面とした他の実施例
に係るスペーサの側面図。
FIG. 5 is a side view of a spacer according to another embodiment in which an upper surface has an inclined surface curved downward.

【図6】別の実施例に係るスペーサの斜視図。FIG. 6 is a perspective view of a spacer according to another embodiment.

【図7】同スペーサの縦断側面図。FIG. 7 is a vertical sectional side view of the spacer.

【図8】同スペーサの平面図。FIG. 8 is a plan view of the spacer.

【図9】従来のスタリーング機器の概略断面図。FIG. 9 is a schematic sectional view of a conventional staring machine.

【符号の説明】[Explanation of symbols]

1 第1ピストン 2 第2ピストン 6 ガス流路 8 熱再生器 12 第2シリンダ 15 環状空間 16 ガス入口空間 17 ガス入口 20,20B,20C スペーサ 1 1st piston 2 2nd piston 6 Gas flow path 8 Heat regenerator 12 2nd cylinder 15 Annular space 16 Gas inlet space 17 Gas inlet 20, 20B, 20C Spacer

Claims (3)

【特許請求の範囲】[Claims] 【請求項1】 第1シリンダにおける第1ピストン前方
のガス圧縮空間と第2シリンダにおける第2ピストン前
方のガス膨張空間とがガス流路で連通し、前記第1ピス
トンと第2ピストンが或る位相差を持って往復動駆動す
ることにより、第1シリンダから第2シリンダに流入し
た圧縮作動ガスが膨張して冷却され、その膨張作動ガス
が第1シリンダに戻る熱サイクルが繰返されて、前記第
2シリンダの外周壁と放熱フィンを有する外側中空筒と
の間に形成された環状空室に収設した円筒状の熱再生器
に冷熱が蓄熱されるスターリング機器において、 前記ガス流路からのガス流入口が開口している前記環状
空室の内底部に、流入した作動ガスが前記環状空室の底
部全周域に均一に拡散しかつ前記熱再生器へと均一な流
れとなって上昇通過して前記ガス膨張空間に流入するよ
うなガス流を形成させる環状のスペーサを配したことを
特徴とするスターリング機器。
1. A gas compression space in front of the first piston in the first cylinder and a gas expansion space in front of the second piston in the second cylinder communicate with each other through a gas flow path, and the first piston and the second piston are provided. By reciprocatingly driving with a phase difference, the compressed working gas flowing from the first cylinder into the second cylinder is expanded and cooled, and the thermal cycle in which the expanded working gas returns to the first cylinder is repeated, In a Stirling machine in which cold heat is stored in a cylindrical heat regenerator housed in an annular space formed between an outer peripheral wall of a second cylinder and an outer hollow cylinder having a heat radiation fin, The working gas that has flowed into the inner bottom portion of the annular cavity where the gas inlet is open diffuses uniformly throughout the entire bottom area of the annular cavity and rises to the heat regenerator as a uniform flow. Pass through Stirling devices, characterized in that arranged annular spacers to form a gas stream so as to flow into the serial gas expansion space.
【請求項2】 前記環状空室の内底部に配される前記環
状のスペーサは、一端部に前記ガス流入口と連通するガ
ス流通孔を有するか若しくは前記ガス流入口と対応する
端部が切徐された形状に形成され、かつ前記ガス流入口
と反対側端に向い漸次高さが高くなる一定角度の傾斜し
た上面に形成されていることを特徴とする前記請求項1
記載のスターリング機器。
2. The annular spacer disposed on the inner bottom portion of the annular space has a gas flow hole communicating with the gas inlet port at one end or an end portion corresponding to the gas inlet port is cut off. The said upper surface is formed in a gradual shape, and is formed on an upper surface inclined at a constant angle whose height gradually increases toward the end opposite to the gas inlet.
Stirling equipment as described.
【請求項3】 前記環状空室の内底部に配される前記環
状のスペーサは、内側に凹んだ湾曲した傾斜上面に形成
されていることを特徴とする前記請求項2記載のスター
リング機器。
3. The Stirling machine according to claim 2, wherein the annular spacer disposed on the inner bottom portion of the annular space is formed on a curved inclined upper surface that is recessed inward.
JP26282295A 1995-10-11 1995-10-11 Stirling equipment Expired - Fee Related JP3258872B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP26282295A JP3258872B2 (en) 1995-10-11 1995-10-11 Stirling equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP26282295A JP3258872B2 (en) 1995-10-11 1995-10-11 Stirling equipment

Publications (2)

Publication Number Publication Date
JPH09105561A true JPH09105561A (en) 1997-04-22
JP3258872B2 JP3258872B2 (en) 2002-02-18

Family

ID=17381101

Family Applications (1)

Application Number Title Priority Date Filing Date
JP26282295A Expired - Fee Related JP3258872B2 (en) 1995-10-11 1995-10-11 Stirling equipment

Country Status (1)

Country Link
JP (1) JP3258872B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013181873A1 (en) * 2012-06-06 2013-12-12 镇江市博林光电科技有限公司 Stirling engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013181873A1 (en) * 2012-06-06 2013-12-12 镇江市博林光电科技有限公司 Stirling engine

Also Published As

Publication number Publication date
JP3258872B2 (en) 2002-02-18

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