JPH03217765A - Cryogenic refrigerator using expansion turbine - Google Patents
Cryogenic refrigerator using expansion turbineInfo
- Publication number
- JPH03217765A JPH03217765A JP1256690A JP1256690A JPH03217765A JP H03217765 A JPH03217765 A JP H03217765A JP 1256690 A JP1256690 A JP 1256690A JP 1256690 A JP1256690 A JP 1256690A JP H03217765 A JPH03217765 A JP H03217765A
- Authority
- JP
- Japan
- Prior art keywords
- expansion turbine
- inlet valve
- cooled
- heat exchanger
- expansion
- 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
Links
Landscapes
- Separation By Low-Temperature Treatments (AREA)
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明は膨張タービンを有する極低温冷凍装置に係り、
特に膨張タービンの急激な圧力変動ガタの保護に好適な
極低温冷凍装置に関するものである。[Detailed Description of the Invention] [Industrial Application Field] The present invention relates to a cryogenic refrigeration system having an expansion turbine;
In particular, the present invention relates to a cryogenic refrigeration system suitable for protecting an expansion turbine from sudden pressure fluctuations.
画低温冷凍装置、例えばヘリウム冷凍装置では、寒冷を
発生する膨張機としてガス軸受式の膨張タービンが使用
されている。この膨張タービンは効率を確保するために
、数万〜数十万rpmの高速回転を行っている。ガス軸
受式のために軸受の負荷容量は大きくなく、膨張タービ
ン入口圧力と出口圧力とに急激な変動が生じた場合には
、アンバランスが生じて軸受が接触焼損したり、過回転
による破損が生じたりする。BACKGROUND ART In a low-temperature refrigeration system, such as a helium refrigeration system, a gas bearing type expansion turbine is used as an expander that generates cold. This expansion turbine rotates at a high speed of tens of thousands to hundreds of thousands of rpm to ensure efficiency. Because it is a gas bearing type, the load capacity of the bearing is not large, and if there is a sudden change in the expansion turbine inlet pressure and outlet pressure, an imbalance may occur and the bearing may burn out due to contact or damage due to overspeed. Occurs.
なお、この種の装置として関連するものには、例えば、
日本工業出版「ターボ機械 第11啓第7号(1983
.7)「He液化冷凍機用膨張タービン」が有る。Note that related devices of this type include, for example,
Nihon Kogyo Shuppan “Turbo Machinery No. 11 Kei No. 7 (1983)
.. 7) There is an "expansion turbine for He liquefaction refrigerators."
上記従来技術は,膨侭タービンに過大な負荷変動を与え
ないようにする配慮に欠け、誤操作,誤作動,停電等の
異常詩に、膨張タービンを保護できないという問題があ
った。The above-mentioned conventional technology lacks consideration to prevent excessive load fluctuations from being applied to the expansion turbine, and has the problem of not being able to protect the expansion turbine from abnormalities such as erroneous operation, malfunction, and power outage.
本発明の目的は、信頼性の高い膨張タービンを有する極
低温冷凍装置を提供することにある。An object of the present invention is to provide a cryogenic refrigeration system having a highly reliable expansion turbine.
上記目的を達成するために、膨張タービン入口弁に級や
かに開く手攻(例えば、スピードコントローラ)を付属
させるか、または膨張タービン出口弁に緑やかに開閉す
る手段(例えば、スピードコントローラ)を付属させる
か、さらにこれらを共に付属させたものである。In order to achieve the above object, the expansion turbine inlet valve is equipped with a graceful opening mechanism (for example, a speed controller), or the expansion turbine outlet valve is equipped with a graceful opening and closing mechanism (for example, a speed controller). or both together.
また、上記目的を達成するために、コールドボブクス入
口弁着二緩やかに開く手段(例えば、スピドコントロー
ラ)を付属させたものである。Further, in order to achieve the above object, a means (for example, a speed controller) for gently opening the cold box inlet valve is attached.
急開防止手段付膨張タービン入口弁は、誤操作,誤動作
等によって、急開信号を受けた場合でも制限された一定
の速度でしか開しない。急開急閉防止手段付膨張タービ
ン出口弁は、同様に、制限された一定の速度でしか開閉
しない。これにより、膨張タービンに過大な圧力(負荷
)変動を与えるのを防止できる。The expansion turbine inlet valve with a sudden opening prevention means opens only at a limited and constant speed even if it receives a sudden opening signal due to erroneous operation or malfunction. The expansion turbine outlet valve with rapid opening/closing prevention means similarly opens and closes only at a limited and constant speed. This can prevent excessive pressure (load) fluctuations from being applied to the expansion turbine.
また、コールドボックス入口弁に急開防止手段を付属さ
せることにより、コールドボックス入口弁は急開しなく
なり、コールドボックスへの流量は、徐々に増加し、高
圧ラインの圧力は、ヘリウム圧縮機吐出側に設置される
圧力制御装置により、安定した圧力となり得る。このた
め、高圧ラインより供給されるタービン軸受ガス供給圧
力も安定するので、タービン軸受の損傷も防止できる。In addition, by attaching a sudden opening prevention means to the cold box inlet valve, the cold box inlet valve will not open suddenly, the flow rate to the cold box will gradually increase, and the pressure in the high pressure line will be reduced to the helium compressor discharge side. The pressure control device installed in the chamber ensures stable pressure. Therefore, the turbine bearing gas supply pressure supplied from the high pressure line is also stabilized, so that damage to the turbine bearing can be prevented.
以下、本発明の一実施例を第1図により説明する。 An embodiment of the present invention will be described below with reference to FIG.
第1図において、lは圧縮機(図示省略)から導入する
高圧ライン、2は圧縮機へ戻る低圧ライン, 10はコ
ールドボックス,lla〜llfは第1〜第6の熱交換
器、12a,12bは第1,i!2の急開防止機構付膨
張タービン入口弁、13a〜13 cは第1〜第3の膨
張タービン、14は急開急閉防止機構付膨張タービン出
口弁、Iは冷却負荷である。In FIG. 1, l is a high pressure line introduced from a compressor (not shown), 2 is a low pressure line returning to the compressor, 10 is a cold box, lla to llf are first to sixth heat exchangers, 12a, 12b is the first, i! 2 is an expansion turbine inlet valve with a sudden opening prevention mechanism, 13a to 13c are first to third expansion turbines, 14 is an expansion turbine outlet valve with a sudden opening and closing prevention mechanism, and I is a cooling load.
次に、上記のように構成された本発明の実施例の動作に
ついて説明する。高圧ラインlでコールドボックス10
に導入された高圧ヘリウムは、第1の熱交換器USで冷
却された後、一部は!!l1の急開防止機構付膨張ター
ビン入口弁12aを通り、第1の膨張タービン13aに
導入され断熱膨張することによって寒冷を発生し、第3
の熱交換器UCで冷却された後、第2の膨張タービン1
3 bで低圧圧力まで断熱膨張して低圧ライン2に合流
する。第1の熱交換器11 aで冷却された残りのヘリ
ウムは、第2〜第5の熱交換器1l b = 11 @
で冷却された後、第2の急開防止機構付膨張タービン入
口弁12bを通り第3の膨張タービン13 cで、この
場合、約4itmまで断熱膨帳して寒冷を発生した後、
!!6の熱交換器11fで冷却され、最終的に急開急閉
防止機構付膨張タービン出口弁14で低圧圧力までジュ
ールトムソン膨張して一部液化ヘリウムを生成して、冷
却負荷四の熱負荷を吸収する。冷却負荷加から戻った極
低温ヘリウムは第6〜第1の熱交換器11f〜llaで
寒冷回収された後、低圧ラインを通り圧縮機に戻る。Next, the operation of the embodiment of the present invention configured as described above will be explained. Cold box 10 with high pressure line l
After being cooled in the first heat exchanger US, some of the high-pressure helium introduced into the! ! It passes through the expansion turbine inlet valve 12a with a sudden opening prevention mechanism of l1, is introduced into the first expansion turbine 13a, and is adiabatically expanded to generate cooling.
after being cooled by the heat exchanger UC of the second expansion turbine 1
At step 3b, it expands adiabatically to a low pressure and joins the low pressure line 2. The remaining helium cooled by the first heat exchanger 11 a is transferred to the second to fifth heat exchangers 1 l b = 11 @
After being cooled, it passes through the second expansion turbine inlet valve 12b with a rapid opening prevention mechanism and is adiabatic expanded to about 4 itm in this case in the third expansion turbine 13c to generate cold.
! ! The helium is cooled by the heat exchanger 11f of No. 6, and is finally Joule-Thomson expanded to a low pressure at the expansion turbine outlet valve 14 with a rapid opening/quick closing prevention mechanism to partially generate liquefied helium, thereby reducing the heat load of cooling load No. 4. Absorb. The cryogenic helium returned from the application of the cooling load is cooled and recovered in the sixth to first heat exchangers 11f to lla, and then returns to the compressor through the low pressure line.
本実施例によれば、誤操作,誤作動等の時も、膨張ター
ビンに過大な負荷変動を与えるのを防止でき信頼性が向
上する効果がある。According to this embodiment, even in the event of an erroneous operation or malfunction, it is possible to prevent excessive load fluctuations from being applied to the expansion turbine, thereby improving reliability.
なお、本一実施例では、膨張タービンの入口および出口
に急開または急閉防止機構を設けたが、これらのうちい
ずれか一つでも効果がある。In this embodiment, a mechanism for preventing sudden opening or closing is provided at the inlet and outlet of the expansion turbine, but any one of these mechanisms is also effective.
次に、本発明の第2の実施例を第2図により説明する。Next, a second embodiment of the present invention will be described with reference to FIG.
圧縮機3より圧縮したヘリウムガスは、高圧ラインl,
コールドボックス入口弁9を介して、コールドボックス
10に導かれる。The helium gas compressed by the compressor 3 is transferred to the high pressure line l,
It is led to a cold box 10 via a cold box inlet valve 9.
コールドボックス10へ導かれたヘリウムガスは、熱交
換器11 aで低圧ライン2の戻りガスと熱文換し、冷
却された後、膨張タービン13a,13bで断熱膨張し
低温ガスとなり、低圧ライン2に合流して戻りガスとな
る。また,JT弁16に向うガスは、熱交換器1l b
− 11 eによって戻りガスと熱交換し、冷却され
、JT弁16で膨張し一部が液化する。The helium gas led to the cold box 10 undergoes thermal exchange with the return gas of the low pressure line 2 in the heat exchanger 11a, is cooled, and is then adiabatically expanded in the expansion turbines 13a, 13b to become low-temperature gas. It merges with the gas and becomes return gas. In addition, the gas heading to the JT valve 16 is transferred to the heat exchanger 1l b
- 11e exchanges heat with the return gas, is cooled, expands with the JT valve 16, and partially liquefies.
液化したヘリウムは、冷却負荷Iで熱負荷を受けガス化
し、液化しなかったガスと共に、戻りガスとなり、熱交
換器11 e〜111で熱回収され、圧縮機3の収入側
に戻る。The liquefied helium is gasified under the heat load of the cooling load I, becomes a return gas together with the gas that has not been liquefied, is heat-recovered in the heat exchangers 11e to 111, and returns to the input side of the compressor 3.
また、本装置では、圧縮機3の吐出圧力制御のため高圧
圧力調整計7.圧力調整弁5で制御している。Additionally, in this device, a high pressure regulator 7. is used to control the discharge pressure of the compressor 3. It is controlled by a pressure regulating valve 5.
また、タービン軸受ガス供給ライン15は、高圧ライン
lより接続しており、タービン軸受ガス供給弁16.
18によりあらかじめ設定した圧力で膨張タービン13
a,13bに軸受ガスを供給する。Further, the turbine bearing gas supply line 15 is connected to the high pressure line l, and the turbine bearing gas supply valve 16.
Expansion turbine 13 at a preset pressure by 18
Bearing gas is supplied to a and 13b.
軸受ガス出口ラインは調整弁17.19により、タービ
ン軸受室の圧力を保持される。The bearing gas outlet line is maintained at the pressure in the turbine bearing chamber by a regulating valve 17.19.
上記の構成の装置において、コールドボックス入口弁9
を急開した場合,、多大な流量がコールドボックスlO
側へ供給され、圧縮機3の吐出力圧力が高圧圧力調整計
7,圧力調整弁5だけでは追従できず、圧力低下を伴う
。このため、タービン軸受ガス供給圧力も低下し、ター
ビンの軸受の損傷につながる。このため、コールドボッ
クス入口弁7にスピードコントローラを設置し、急激な
圧力低下が生じないようにし、タービン軸受ガス圧力の
安定性を計る。In the apparatus configured as described above, the cold box inlet valve 9
If the cold box is opened suddenly, a large amount of flow will flow into the cold box.
The discharge output pressure of the compressor 3 cannot be followed by the high pressure regulator 7 and the pressure regulating valve 5 alone, resulting in a pressure drop. As a result, the turbine bearing gas supply pressure also decreases, leading to damage to the turbine bearings. For this reason, a speed controller is installed at the cold box inlet valve 7 to prevent a sudden pressure drop and to measure the stability of the turbine bearing gas pressure.
本実施例によれば起a時の高圧ラインの圧力を一定に保
つことができ、タービンの軸受ガス供給ラインの圧力を
安定させることができる効果がある。According to this embodiment, the pressure in the high pressure line at the time of startup can be kept constant, and the pressure in the turbine bearing gas supply line can be stabilized.
本発明によれば、誤操作、誤動作等の時も膨張タービン
に過大な負荷変動を与えるのを防止できるため、信相性
、操作性を向上できる効果がある。According to the present invention, it is possible to prevent excessive load fluctuations from being applied to the expansion turbine even in the event of an erroneous operation or malfunction, thereby improving reliability and operability.
第1図は本発明の一実施例である膨張タービンを有する
極低温冷凍装置を示す系統図、第2図は本発明の第2の
実施例である膨張タービンを有する極低温冷凍装置を示
す系統図である。
9・・・・・・コールドボックス入口弁、12a,12
b・・・急開防止機構付膨張タービン入口弁、13 a
ないし13c・・・・・・膨張タービン、14・・・・
・・急開急閉防止機構′4l図
/4−−−−−1−ど翔口汁FIG. 1 is a system diagram showing a cryogenic refrigeration system having an expansion turbine which is an embodiment of the present invention, and FIG. 2 is a system diagram showing a cryogenic refrigeration system having an expansion turbine which is a second embodiment of the present invention. It is a diagram. 9...Cold box inlet valve, 12a, 12
b... Expansion turbine inlet valve with sudden opening prevention mechanism, 13 a
or 13c...expansion turbine, 14...
・・Sudden opening/sudden closing prevention mechanism'4l diagram/4-----1-Dosho mouth juice
Claims (1)
冷凍装置において、膨張タービン入口弁に緩やかに開く
手段を設けたことを特徴とする膨張タービンを有する極
低温冷凍装置。 2、膨張タービンと膨張タービン出口弁を有する極低温
冷凍装置において、膨張タービン出口弁に緩やかに開閉
する手段を設けたことを特徴とする膨張タービンを有す
る極低温冷凍装置。 3、膨張タービンと膨張タービン入口弁と膨張タービン
出口弁を有する極低温冷凍装置において、膨張タービン
入口弁に緩やかに開く手段を設け、膨張タービン出口弁
に緩やかに開閉する手段を設けたことを特徴とする膨張
タービンを有する極低温冷凍装置。 4、膨張タービンを有する極低温装置において、コール
ドボックス入口弁に緩やかに開く手段を設けたことを特
徴とする膨張タービンを有する極低温冷凍装置。[Scope of Claims] 1. A cryogenic refrigeration system having an expansion turbine and an expansion turbine inlet valve, characterized in that the expansion turbine inlet valve is provided with means for gently opening it. 2. A cryogenic refrigeration system having an expansion turbine and an expansion turbine outlet valve, characterized in that the expansion turbine outlet valve is provided with means for gently opening and closing the expansion turbine. 3. A cryogenic refrigeration system having an expansion turbine, an expansion turbine inlet valve, and an expansion turbine outlet valve, characterized in that the expansion turbine inlet valve is provided with means for gently opening, and the expansion turbine outlet valve is provided with means for gently opening and closing. A cryogenic refrigeration system with an expansion turbine. 4. A cryogenic refrigeration apparatus having an expansion turbine, characterized in that the cold box inlet valve is provided with means for gently opening.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1256690A JPH03217765A (en) | 1990-01-24 | 1990-01-24 | Cryogenic refrigerator using expansion turbine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1256690A JPH03217765A (en) | 1990-01-24 | 1990-01-24 | Cryogenic refrigerator using expansion turbine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH03217765A true JPH03217765A (en) | 1991-09-25 |
Family
ID=11808906
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP1256690A Pending JPH03217765A (en) | 1990-01-24 | 1990-01-24 | Cryogenic refrigerator using expansion turbine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH03217765A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH05172413A (en) * | 1991-12-20 | 1993-07-09 | Kobe Steel Ltd | Cooling system |
-
1990
- 1990-01-24 JP JP1256690A patent/JPH03217765A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH05172413A (en) * | 1991-12-20 | 1993-07-09 | Kobe Steel Ltd | Cooling system |
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