JP4242645B2 - Transport line and transport method for moving cryogenic fluid - Google Patents
Transport line and transport method for moving cryogenic fluid Download PDFInfo
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- JP4242645B2 JP4242645B2 JP2002542800A JP2002542800A JP4242645B2 JP 4242645 B2 JP4242645 B2 JP 4242645B2 JP 2002542800 A JP2002542800 A JP 2002542800A JP 2002542800 A JP2002542800 A JP 2002542800A JP 4242645 B2 JP4242645 B2 JP 4242645B2
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C9/00—Methods or apparatus for discharging liquefied or solidified gases from vessels not under pressure
- F17C9/02—Methods or apparatus for discharging liquefied or solidified gases from vessels not under pressure with change of state, e.g. vaporisation
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C6/00—Methods and apparatus for filling vessels not under pressure with liquefied or solidified gases
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C9/00—Methods or apparatus for discharging liquefied or solidified gases from vessels not under pressure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
- F17C2205/03—Fluid connections, filters, valves, closure means or other attachments
- F17C2205/0302—Fittings, valves, filters, or components in connection with the gas storage device
- F17C2205/0323—Valves
- F17C2205/0326—Valves electrically actuated
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
- F17C2205/03—Fluid connections, filters, valves, closure means or other attachments
- F17C2205/0302—Fittings, valves, filters, or components in connection with the gas storage device
- F17C2205/0323—Valves
- F17C2205/0329—Valves manually actuated
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
- F17C2205/03—Fluid connections, filters, valves, closure means or other attachments
- F17C2205/0302—Fittings, valves, filters, or components in connection with the gas storage device
- F17C2205/0323—Valves
- F17C2205/0332—Safety valves or pressure relief valves
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
- F17C2205/03—Fluid connections, filters, valves, closure means or other attachments
- F17C2205/0302—Fittings, valves, filters, or components in connection with the gas storage device
- F17C2205/0352—Pipes
- F17C2205/0355—Insulation thereof
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
- F17C2205/03—Fluid connections, filters, valves, closure means or other attachments
- F17C2205/0302—Fittings, valves, filters, or components in connection with the gas storage device
- F17C2205/0352—Pipes
- F17C2205/0358—Pipes coaxial
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
- F17C2205/03—Fluid connections, filters, valves, closure means or other attachments
- F17C2205/0302—Fittings, valves, filters, or components in connection with the gas storage device
- F17C2205/0352—Pipes
- F17C2205/0364—Pipes flexible or articulated, e.g. a hose
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
- F17C2205/03—Fluid connections, filters, valves, closure means or other attachments
- F17C2205/0302—Fittings, valves, filters, or components in connection with the gas storage device
- F17C2205/037—Quick connecting means, e.g. couplings
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2221/00—Handled fluid, in particular type of fluid
- F17C2221/01—Pure fluids
- F17C2221/014—Nitrogen
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/01—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
- F17C2223/0146—Two-phase
- F17C2223/0153—Liquefied gas, e.g. LPG, GPL
- F17C2223/0161—Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2265/00—Effects achieved by gas storage or gas handling
- F17C2265/01—Purifying the fluid
- F17C2265/015—Purifying the fluid by separating
- F17C2265/017—Purifying the fluid by separating different phases of a same fluid
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2270/00—Applications
- F17C2270/02—Applications for medical applications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2270/00—Applications
- F17C2270/05—Applications for industrial use
- F17C2270/0545—Tools
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Thermal Insulation (AREA)
- Rigid Pipes And Flexible Pipes (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Pipeline Systems (AREA)
Abstract
Description
【0001】
発明の背景
超低温流体を搬送する多くの場合では、できる限り完全な液体状態で流体を移動することが重要である。従来は、流体をまず相分離したり、熱交換器で過冷したり、真空ジャケッティングによりラインを断熱状態に保ったりすることが必要であった。さもなければ、搬送ラインの熱漏れはボイルオフを招来し、ひいては搬送ライン内における波動、不安定さ、脈動等、一般的に望ましくない流れの原因となる。長い搬送ラインでは、特に熱漏れが問題となる。
【0002】
本発明は、超低温流体の第一部分が内方の管内を流れ、第二部分が内方の管と外方の管との間の環体内を流れ、外方の管における環体が内方の管よりも圧力が低く同軸、又は“チューブインチューブ”構造の超低温搬送ラインに関するものである。この圧力の違いにより、容易に環体内の流体により内方の管内(煮沸など)にある液体の冷却が可能になり、飽和液体状態に留められる。液体をさらに冷却し、冷却“クッション”として熱漏れに対応可能にする事が望ましい。
【0003】
また、多くの超低温流体搬送装置では搬送ラインが軽量で可撓性を有することが重要である。これは導入時、操作時、保守時に最大の自由度を提供し、ラインが繰り返し曲がることを防げるようにする。本発明は第二に可撓性材料(ポリマー物質など)からラインの少なくとも一部分を形成する超低温搬送ラインに関するものである。
【0004】
従来の技術では超低温搬送ラインのこれら双方の重要な問題が解決されていない。
米国特許第3696627号(ロングスワース(Longsworth))の超低温搬送システムは、堅固な同軸パイピングの構成により超低温流の過冷や安定化を開示している。米国特許第4296610号(デービス(Davis))、米国特許第4336689号(デービス(Davis))、米国特許第4715187号(スターンズ(Stearns))及び、米国特許第5477691号(ホワイト(White))でも同様のシステムを開示している。
【0005】
チャン等(Chang et al)が開示した非金属、可撓超低温搬送ラインは超低温を冷凍手術システム内のクリオプローブを冷却する超低温システムに使用している(“高パフォーマンスマルチプルーブ冷凍手術デバイスの開発”バイオメディカル インストゥルメンション アンド テクノロジー(Biomedical Instrumentation and Techology)、 9月/10月 1994年 383−390ページ)。チャンの可撓性を有するライン設計に起因する熱漏れボイルオフのため、本質的に防熱が弱いこともあいまって、これらのラインは短くする必要があり、適切に稼動させるため十分に過冷された(−214℃)超低温液体で充満される必要がある。これは複雑にして高価な超低温の貯蔵装置と、供給装置と制御システムを上流側に必要とする。
【0006】
また超低温搬送ラインが機械加工に使用されることも知られている。機械加工においては、起寒剤は切削工具や被加工物のインターフェースとして使用される。例として、米国特許第2635399号(ウエスト(West))、米国特許第5103701号(ランデン(Lundin))、米国特許第5509335号(エマーソン(Emerson))、米国特許第5592863号(ジャスコウィック(Jaskowiak))、米国特許第5761974号(ワグナー(Wagner))、米国特許第5901623号(ホン(Hong))がある。チャンと同様に、これらのラインは短く、熱漏れボイルオフの防止のために過冷超低温液体を流す必要があり、従って上流に高価な過冷システムを必要とする。
【0007】
米国特許第3433028号(クレー(Klee))は、純単層内において超低温流体を一定の距離にわたって運ぶ同軸システムを開示している。大きさが決定された、超低温搬送内部ラインの入口オリフィスを使用することにより、外部熱漏れの影響を受ける場合、液体は蒸発するために外部ラインへ通過することが許容される。同軸ラインの出口端に設置された温度センサよりなるフロー制御ユニットは、内部ライン内の液体の沸点よりも高いことを必要とする温度(通常、50−100°F)になると、外部ラインの蒸気の流れを止める。その結果、外部ラインの圧力が超低温ソースの圧力に近づいてくる。また、外部ラインの蒸気は常に内部ラインの液体よりも暖かくなる。さらに、蒸発するために外部ラインへ通過する液体の量は、入口に設けた非可変的に設けられたオリフィスにより常に制限されるため、高い熱漏れは完全に防ぐことができない。これらの操作原理において、ラインの設置工事中に耐高圧材、非可撓性金属管材、や断熱素材の使用を必要とする。
【0008】
日本国特許出願公開06210105号は非超低温のガス抜き用ポリマー同軸搬送ラインを開示している。このチューブの素材の特性では、超低温にて使用される搬送ラインの使用が困難である。
【0009】
発明の概要
本発明は超低温流体の搬送方法及び搬送装置に関する。ポリマー同軸搬送ラインは内方の導管を超低温流体の第一部分が流れるように使用され、超低温流体の第二部分が内方の導管と外方の導管との間の環体内を流れる。環体内の圧力は内方の導管内の圧力よりも低い。一実施例においては、内方の導管はほぼ非孔質であり、搬送ラインの上流には流れ制御手段が設けられている。流れ制御手段は、超低温流体の第一の部分と第二の部分の少なくとも一部を内方の導管と環体とに分配をする。第二の実施例では、内方の導管の少なくとも一部分は、超低温流体の第一部分の気体浸透や液体浸透に対応するように浸透性を有し、第一部分の気体部及び液状部が環体に浸透して第二部分の少なくとも一部を構成する。
【0010】
本発明の詳細な説明
本発明のポリマー同軸搬送ラインは、図1に示すように、流れ制御ボックス20の下流側に搬送ライン22が配置されている。搬送ライン22において、内方の管72の周囲に外方の管74が配置されている。外方の管74の周囲には断熱材70が設けられ、同断熱材70の周囲には可撓保護ケース68が設けられている。超低温流体の第一部分は内方の管内を流れ、第二部分は内方の管と外方の管の間の環体内を流れる。第一部分は第二部分より高い圧力を有する。
【0011】
搬送ラインの少なくも一部分はポリマー物質など、可撓性材料で形成される。ほぼ全ての内方の管と、ほぼ全ての外方の管を可撓性のあるポリマー物質にて形成することも可能である。さらに、ほぼ全ての外方の管を可撓性に富むポリマー物質で形成し、ほぼ全ての内方の管を、超低温下で脆くならず、かつ可撓性を備えた非ポリマー物質、例えば、(i)銅やその合金、(ii)アルミニウムやその合金、(iii)ニッケルやその合金(iv)オーステナイトステンレス鋼、(v)高濃度のグラファイト(vi)セラミックファイバー編みこみ製品から形成することも可能である。さらに、ほぼ全ての内方の管と、ほぼ全ての外方の管を(i)銅やその合金、(ii)アルミニウムやその合金、(iii)ニッケルやその合金(iv)オーステナイトステンレス鋼、(v)高濃度のグラファイト(vi)セラミックファイバー編みこみ管状製品などから選択された可撓性非ポリマー物質から形成することも可能である。加えて、ほぼ全ての外方の管を可撓性を有する断熱材料で形成することも可能である。さらに、内方の導管及び外方の導管のうちの少なくとも一方がほぼ四辺形、多辺形、楕円形、他の一般的な幾何学的な断面を有する形状にしてもよい。
【0012】
内方の管はほぼ非浸透性を有することができ、このため環体内における流体の第二部分は内方の管を通じた浸透の結果ではない。又は、内方の管の少なくとも一部分には複数の穴が形成可能であり、及び/又は、気体浸透及び液体浸透が可能なように浸透性を有することができ、第一の部分の気体状部及び液状部が環体に浸透し、第二の部分の少なくとも一部を形成する。また、内方の管の複数の部分は、より詳細に述べるならば内方の管の長さ方向において等間隔をおいて配置された複数の部分は、それら浸透性が増強され得る。
【0013】
搬送ラインの上流には、超低温流体の第一部分と第二部分の少なくとも一部を内方の導管と環体に対して分配する流れ制御手段、例えば図1に示す流れ制御ボックス20が有効に配置されている。流れ制御手段は、一般に環体に分配される流体の第二部分の圧力を減少する手段(バルブなど)と一体化され、流体の第二部分の少なくとも少量が液体として環体内に分配される。この差圧により、環体内の液体が内方の管の内部の流体を冷却できる。内方の管が少なくとも部分的に浸透性を有する場合、内方の管から環体気体内への浸透は流れ制御ボックスによって実行される流体分配の少なくとも一部分を補完することができる。流れ制御ボックスの連結部及び内部コンポーネントは3つのオン/オフ(ソレノイド)バルブ61,62,63と手動計量バルブ64を備え、これらのバルブは入口30を介して流れ制御ボックスに連通し、超低温の流れの受け入れ、圧力を制御する。流れ制御ボックス20内部の主要コンポーネントは3方向連結器66であり、これは内方の管と環体にそれぞれ超低温流体の第一部分と第二部分を導入する。ねじ連結部78は3方向連結器66を外方の管74に連結する。任意の直線クランプ部材76は、外方の管をねじ連結部に固定するために使用され得る。流れ制御ボックス20は断熱ケーシングを有し、断熱フィルターを任意に備える。圧力リリーフ弁84を設けてもよい。オン/オフバルブ62、63はその内壁又はバルブシートに開口が形成され、バイパスオリフィス(86,88)が設けられている。
【0014】
環体内における流体の第二部分の少なくとも少量は内方の管内の液体と共に搬送目的箇所及び/又は冷却対象に搬送される。任意に、環体内の流体の第二部分の少なくとも少量が搬送目的箇所及び/又は冷却対象から発散される。前者の場合、搬送ラインの内方の導管と連通する内方管と、搬送ラインの環体と連通する外方管とからなる同軸ノズルの使用により達成される。後者の場合、環体の流体全てが発散され、このことは、環体内の流れの方向が内方の管の流れの方向と同一であるという制限がなくなるだろう。任意のノズルが搬送ラインのインターフェースとノズルとの間の漏れを防止するために熱収縮コネクタを含むことが望ましい。
【0015】
本発明の搬送ラインに適したポリマー物質として、炭素系ポリマー、フッ化炭素系ポリマー、コポリマー及びその混合物、例えばテフロン(E.I.デュポン社の商標名)が挙げられる。
【0016】
本発明における搬送ラインで搬送され得る超低温流体の例としては、窒素、アルゴン、これらの混合物が挙げられる。
本発明における超低温流体を搬送する装置と方法は、搬送目的箇所や冷却対象が、比較的流速が低く、液体の高い応答性を必要とする時、特に使用に適している。このような本発明の搬送ラインが使用される搬送目的箇所及び/又は冷却対象の例として以下に示すものが挙げられる。
【0017】
(i)ストレススクリーニング電子コンポーネントに使用される環境試験チャンバー
(ii)収縮させた後に締りばめされたコンポーネント
(iii )生物学的な保存に使用される標本保存用コンテナ
(iv)窒素飛沫ディスペンサー
(v)機械加工に使用される切削工具及び/又は被加工物
( vi )冷凍手術システムのクリオプローブ
【図面の簡単な説明】
【図1】 本発明の一実施の形態を示す概略図[0001]
Background of the Invention In many cases of transporting cryogenic fluids, it is important to move the fluid in as complete a liquid state as possible. In the past, it was necessary to phase-separate the fluid first, to supercool it with a heat exchanger, or to keep the line in an adiabatic state by vacuum jacketing. Otherwise, heat leaks in the transfer line can result in boil-off and, in turn, cause generally undesired flows such as waves, instabilities, and pulsations in the transfer line. In long transport lines, heat leakage is a problem.
[0002]
In the present invention, the first portion of the cryogenic fluid flows through the inner tube, the second portion flows through the annulus between the inner tube and the outer tube, and the annulus in the outer tube is the inner tube. The present invention relates to an ultra-low temperature conveying line having a pressure lower than that of a tube and having a coaxial or “tube-in-tube” structure. Due to the difference in pressure, the fluid in the inner tube (such as boiling) can be easily cooled by the fluid in the annulus and can be kept in a saturated liquid state. It is desirable to further cool the liquid so that it can respond to heat leaks as a cooling “cushion”.
[0003]
In many ultra-low temperature fluid transfer devices, it is important that the transfer line is lightweight and flexible. This provides maximum freedom during introduction, operation and maintenance, and prevents the line from bending repeatedly. The present invention secondly relates to a cryogenic transfer line that forms at least a portion of the line from a flexible material (such as a polymer material ).
[0004]
The prior art has not solved both of these important problems in the cryogenic transfer line.
U.S. Pat. No. 3,696,627 (Longsworth) ultracold transport system discloses supercooling and stabilization of a cryogenic flow with a rigid coaxial piping configuration. The same applies to U.S. Pat. No. 4,296,610 (Davis), U.S. Pat. No. 4,336,689 (Davis), U.S. Pat. No. 4,715,187 (Stearns), and U.S. Pat. No. 5,477,691 (White). The system is disclosed.
[0005]
The non-metallic, flexible cryogenic transfer line disclosed by Chang et al. Uses ultra-low temperatures for cryogenic systems that cool cryoprobes in cryosurgical systems (“Development of high performance multiple probe cryosurgical devices”) Biomedical Instrumentation and Technology, September / October 1994, pages 383-390). Due to heat leak boil-off due to Chang's flexible line design, these lines need to be shortened, coupled with their inherently poor thermal insulation, and are sufficiently subcooled to operate properly (−214 ° C.) Need to be filled with ultra low temperature liquid. This requires a complex and expensive ultra-low temperature storage device, a supply device and a control system upstream.
[0006]
It is also known that ultra-low temperature transfer lines are used for machining. In machining, cryogens are used as interfaces for cutting tools and workpieces. Examples include U.S. Pat. No. 2,635,399 (West), U.S. Pat. No. 5,107,701 (Lundin), U.S. Pat. No. 5,509,335 (Emerson), U.S. Pat. No. 5,592,863 (Jaskowiac). ), US Pat. No. 5,761,974 (Wagner), US Pat. No. 5,901,623 (Hong). Like Chang, these lines are short and require a supercooled cryogenic liquid to flow to prevent heat leak boil-off, thus requiring an expensive supercooling system upstream.
[0007]
U.S. Pat. No. 3,433,028 (Klee) discloses a coaxial system that carries cryogenic fluid over a distance in a pure monolayer. By using the inlet orifice of the sized cryogenic transfer inner line , when affected by external heat leakage, the liquid is allowed to pass to the external line to evaporate. A flow control unit consisting of a temperature sensor installed at the outlet end of the coaxial line will cause the vapor in the external line to reach a temperature (usually 50-100 ° F.) that needs to be higher than the boiling point of the liquid in the internal line. Stop the flow. As a result, the pressure in the external line approaches the pressure in the cryogenic source. Also, the external line vapor is always warmer than the internal line liquid. Furthermore, the amount of liquid that passes to the external line to evaporate is always limited by a non-variably provided orifice at the inlet, so high heat leakage cannot be completely prevented. These operating principles require the use of high pressure resistant materials, inflexible metal tubing, and insulation materials during line installation work.
[0008]
Japanese Patent Application No. 06210105 discloses a non-ultra low temperature degassing polymer coaxial transport line. Due to the properties of the tube material, it is difficult to use a transfer line that is used at ultra-low temperatures.
[0009]
The present invention relates to the transport method and conveying apparatus for the cryogenic fluid. The polymer coaxial transport line is used such that the first portion of the cryogenic fluid flows through the inner conduit and the second portion of the cryogenic fluid flows through the annulus between the inner and outer conduits. The pressure in the annulus is lower than the pressure in the inner conduit. In one embodiment, the inner conduit is substantially non-porous and a flow control means is provided upstream of the transfer line. The flow control means distributes at least a portion of the first and second portions of the cryogenic fluid into the inner conduit and the annulus . In the second embodiment, at least a portion of the inner conduit is permeable to accommodate gas permeation and liquid permeation of the first portion of the cryogenic fluid, with the gas and liquid portions of the first portion being in the annulus. Permeates and constitutes at least part of the second part.
[0010]
DETAILED DESCRIPTION OF THE INVENTION The polymer coaxial conveyance line of the present invention has a conveyance line 22 disposed on the downstream side of the
[0011]
At least a portion of the transport line is formed of a flexible material, such as a polymer material . It is also possible to form almost all inner tubes and almost all outer tubes from flexible polymeric materials . Furthermore, almost all outer tubes are formed of a flexible polymeric material , and almost all inner tubes are not brittle under ultra-low temperatures and are flexible non- polymeric materials , for example, (I) Copper and alloys thereof, (ii) Aluminum and alloys thereof, (iii) Nickel and alloys thereof (iv) Austenitic stainless steel, (v) High concentration graphite (vi) Ceramic fiber braided products Is possible. In addition, almost all inner tubes and almost all outer tubes are (i) copper and its alloys, (ii) aluminum and its alloys, (iii) nickel and its alloys (iv) austenitic stainless steel, ( v) It can also be formed from flexible non- polymeric materials selected from high concentrations of graphite (vi) ceramic fiber braided tubular products and the like. In addition, almost all outer tubes can be formed of a flexible insulating material. Furthermore, at least one of the inner conduit and the outer conduit may have a substantially quadrilateral, polygonal, elliptical, or other general geometric cross-sectional shape.
[0012]
Inner tubes can have a substantially non-permeable, a second portion of the fluid at this end ring body is not the result of penetration through the inner tube. Or, at least a portion of the inner tube may be formed a plurality of holes, and / or can have a permeability to allow gas permeation and liquid permeation, gaseous portion of the first portion And the liquid part penetrates into the ring body and forms at least a part of the second part. Further, the plurality of portions of the inner tube, which will be described in more detail, can have their permeability enhanced by a plurality of portions arranged at equal intervals in the length direction of the inner tube.
[0013]
Effectively disposed upstream of the transfer line is a flow control means for distributing at least a portion of the first and second portions of the cryogenic fluid to the inner conduit and ring, for example, the
[0014]
At least a small amount of the second portion of the fluid in the annulus is transported along with the liquid in the inner tube to the transport destination and / or to be cooled. Optionally, at least a small amount of the second part of the fluid in the annulus is emitted from the delivery destination and / or the object to be cooled. In the former case, this is achieved by using a coaxial nozzle comprising an inner pipe communicating with the inner conduit of the transport line and an outer pipe communicating with the ring of the transport line. In the latter case, all the fluid in the annulus will diverge, which will eliminate the restriction that the flow direction in the annulus is the same as the flow direction in the inner tube . It is desirable for any nozzle to include a heat shrink connector to prevent leakage between the transport line interface and the nozzle .
[0015]
As polymeric substances suitable for conveying line of the present invention, the carbon-based polymer over, fluorocarbon polymer - over, copolymer over and mixtures thereof, for example, Teflon (E. I. Du Pont trade name) and the like.
[0016]
Examples of the cryogenic fluid that can be transported on the transport line in the present invention include nitrogen, argon, and mixtures thereof.
The apparatus and method for transporting a cryogenic fluid in the present invention are particularly suitable for use when the transport destination and the object to be cooled have a relatively low flow rate and require high liquid responsiveness. Such transfer line of the present invention include those shown below as an example of a target site feed transportable that is used and / or cooling target.
[0017]
(I) Environmental test chambers used for stress screening electronic components (ii) Components that have been crimped after shrinking (iii) Containers for specimen storage used for biological preservation (iv) Nitrogen spray dispensers ( v) Cutting tools and / or workpieces used for machining
( Vi ) Cryoprobe of cryosurgery system [Brief description of the drawings]
FIG. 1 is a schematic diagram showing an embodiment of the present invention.
Claims (12)
(a)前記超低温流体の第1部分が通るように構成される内方導管(72)と;
(b)前記内方導管(72)を包囲する外方導管(74)であって、前記外方導管(74)は前記内方導管(72)との間に前記超低温流体の第2部分が通る環体を区画形成することと;
(c)前記内方導管(72)に前記第1部分を流し、前記環体に前記第2部分を流すように分配する流れ制御手段と
を備え、
前記流れ制御手段は、
(i) 前記超低温流体の受入れに適した流路入口(30)と;
(ii)3方向連結器(66)と;
(iii) 前記流路入口(30)から前記3方向連結器(66)まで延びる第1流路であって、前記第1流路は前記3方向連結器(66)によって前記内方導管(72)に連結され、前記第1流路は前記流路入口(30)から前記3方向連結器(66)に向かって順に第1分岐部と第1結合部を有することと;
(iv) 前記第1分岐部と前記第1連結部の間において前記第1流路に設けられる第1オンオフバルブ(63)であって、前記第1オンオフバルブ(63)は第1バイパスオリフィス(86)を有し、前記第1バイパスオリフィス(86)は前記第1オンオフバルブ(63)の閉じ状態において前記第1流路を絞ることと;
(v) 前記第1分岐部において前記第1流路から分岐して前記3方向連結器(66)まで延びる第2流路であって、前記第2流路は前記3方向連結器(66)によって前記環体に連結され、前記3方向連結器は前記第1部分を前記内方導管に導入し、前記第2部分を前記外方導管に導入し、前記第2流路は前記第1分岐部と前記3方向連結器(66)の間に第2分岐部を有することと;
(vi) 前記第1分岐部と前記第2分岐部の間において前記第2流路に設けられる第2オンオフバルブ(62)であって、前記第2オンオフバルブ(62)は第2バイパスオ
リフィス(88)を有し、前記第2バイパスオリフィス(88)は前記第2オンオフバルブ(62)の閉じ状態において前記第2流路を絞ることと;
(vii) 前記第2分岐部において前記第2流路から分岐して、前記第1結合部において前記第1流路に連結される第3流路と;
(viii) 前記第3流路に設けられる手動計量バルブ(64)と
を備え、
前記流路入口(30)から前記第1流路に受入れた前記超低温流体を前記第1部分と前記第2部分に分配し、前記第2部分の少なくとも一部の圧力を減少させ、前記環体内の前記第2部分の少なくとも少量は液体として前記環体内に分配されつつ前記内方導管(72)内の前記第1部分を冷却し、前記第2部分の少なくとも一部は前記搬送目的箇所と前記冷却対象のうちの少なくとも一方に搬送されるように、前記第2オンオフバルブ(62)の閉じ状態において前記手動計量バルブ(64)が調整されることによって前記超低温流体の流れは圧力調整される、搬送ライン。An ultra-low temperature fluid transfer line, wherein the transfer line is used to deliver at least a part of the ultra-low temperature fluid to at least one of a transfer destination and a cooling target, and at least a part of the transfer line is flexible. Formed of a conductive material, the transport line is
(A) an inner conduit (72) configured to pass a first portion of the cryogenic fluid;
(B) an outer conduit (74) surrounding the inner conduit (72), the second portion of the cryogenic fluid being between the outer conduit (74) and the inner conduit (72). Compartmentalizing the passing ring;
(C) flow control means for distributing the first portion through the inner conduit (72) and distributing the second portion through the annular body;
The flow control means includes
(I) a flow path inlet (30) suitable for receiving said cryogenic fluid;
(Ii) a three-way coupler (66);
(Iii) a first flow path extending from the flow path inlet (30) to the three-way coupler (66), wherein the first flow path is connected to the inner conduit (72) by the three-way coupler (66). The first flow path has a first branch part and a first coupling part in order from the flow path inlet (30) toward the three-way coupler (66);
(Iv) A first on / off valve (63) provided in the first flow path between the first branch portion and the first connecting portion, wherein the first on / off valve (63) is a first bypass orifice (63). 86), and the first bypass orifice (86) restricts the first flow path in the closed state of the first on-off valve (63);
(V) a second flow path that branches from the first flow path at the first branch portion and extends to the three-way coupler (66), wherein the second flow path is the three-way coupler (66). The three-way coupler introduces the first part into the inner conduit, the second part into the outer conduit, and the second flow path is connected to the first branch. And having a second branch between the three-way connector (66);
(Vi) A second on / off valve (62) provided in the second flow path between the first branch portion and the second branch portion, wherein the second on / off valve (62) is a second bypass valve.
The second bypass orifice (88) restricts the second flow path in the closed state of the second on / off valve (62);
(Vii) a third flow path branched from the second flow path at the second branch portion and connected to the first flow path at the first coupling portion;
(Viii) a manual metering valve (64) provided in the third flow path;
With
Distributing the cryogenic fluid received in said first flow path from the flow path inlet (30) to said second portion and said first portion, reducing at least a portion of the pressure of said second portion, said ring body At least a small amount of the second part is distributed as a liquid in the annulus and cools the first part in the inner conduit (72), and at least a part of the second part includes the transport destination and the part. The flow of the cryogenic fluid is adjusted by adjusting the manual metering valve (64) in a closed state of the second on / off valve (62) so as to be conveyed to at least one of the objects to be cooled. Conveying line.
前記同軸ノズルは、
前記内方導管(72)に連通する内方通路と、
前記環体に連通する外方通路と
を備える、請求項1に記載の搬送ライン。At least a small amount of the second portion of the fluid in the annular body is transported to the at least one of the transport destination and the object to be cooled together with the liquid flow in the inner conduit (72) by the action of the coaxial nozzle,
The coaxial nozzle is
An inner passage communicating with the inner conduit (72);
The conveyance line according to claim 1, further comprising an outer passage communicating with the ring body.
(i)ストレススクリーニング電子コンポーネントに使用される環境試験チャンバー、
(ii)収縮させた後に締りばめされたコンポーネント、
(iii )生物学的な保存用に使用される標本保存用コンテナ、
(iv)窒素飛沫ディスペンサー、
(v)機械加工に使用される切削工具と被加工物のうちの少なくとも一方、および
(vi)冷凍手術システムのクリオプローブ
のうちから選択される、請求項1に記載の搬送ライン。At least one of the transfer destination and the cooling object is (i) an environmental test chamber used for a stress screening electronic component;
(Ii) components that have been crimped after being shrunk;
(Iii) specimen storage containers used for biological storage;
(Iv) Nitrogen splash dispenser,
The transfer line according to claim 1, selected from (v) at least one of a cutting tool and a workpiece used for machining, and (vi) a cryoprobe of a cryosurgical system.
ほぼ全ての前記内方導管(72)は、(i)銅やその合金、(ii)アルミニウムやその合金、(iii)ニッケルやその合金、(iv)オーステナイトステンレス鋼、(v)高濃度のグラファイト(dense graphite)、および(vi)セラミックファイバー
編込管状製品から選択された可撓性を有する非ポリマー物質によって形成された、請求項1に記載の搬送ライン。Almost all the outer conduit (74) is formed by a flexible polymeric material;
Almost all the inner conduits (72) consist of (i) copper and its alloys, (ii) aluminum and its alloys, (iii) nickel and its alloys, (iv) austenitic stainless steel, and (v) high-concentration graphite. The delivery line of claim 1 formed by a flexible non-polymeric material selected from (dense graphite) and (vi) a ceramic fiber braided tubular product.
ほぼ全ての前記内方導管(72)は、(i)銅やその合金、(ii)アルミニウムやその合金、(iii)ニッケルやその合金、(iv)オーステナイトステンレス鋼、(v)高濃度のグラファイト、および(vi)セラミックファイバー編込管状製品から選択された可撓性を有する非ポリマー物質から形成される、請求項1に記載の搬送ライン。Almost all the outer conduit (74) is formed by a flexible insulating material;
Almost all the inner conduits (72) consist of (i) copper and its alloys, (ii) aluminum and its alloys, (iii) nickel and its alloys, (iv) austenitic stainless steel, and (v) high-concentration graphite. And (vi) the transfer line of claim 1 formed from a flexible non-polymeric material selected from ceramic fiber braided tubular products.
前記第1部分を前記内方導管(72)に流すとともに前記第2部分を前記環体に流すことと、
前記流路入口(40)から前記第1流路に受入れた前記超低温流体を前記第1部分と前 記第2部分に分配し、前記第2部分の少なくとも一部の圧力を減少させ、前記環体内の前記第2部分の少なくとも少量は液体として前記環体内に分配されつつ前記内方導管(72)内の前記第1部分を冷却し、前記第2部分の少なくとも一部は前記搬送目的箇所と前記冷却対象のうちの少なくとも一方に搬送されるように、前記オンオフバルブ(62)の閉じ状態において前記手動計量バルブ(64)を調整することと
を備える、方法。A method for transporting the cryogenic fluid using the transport line according to any one of claims 1 to 11, wherein the method comprises:
Flowing the first portion through the inner conduit (72) and flowing the second portion through the annulus;
Distributing the cryogenic fluid received in said first flow path from the flow path inlet (40) to said first portion and before Symbol second portion reduces at least a portion of the pressure of said second portion, said ring At least a small amount of the second part in the body is distributed as a liquid in the annulus and cools the first part in the inner conduit (72), and at least a part of the second part is separated from the transport destination point. Adjusting the manual metering valve (64) in a closed state of the on-off valve (62) to be conveyed to at least one of the objects to be cooled .
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US09/911,027 US6513336B2 (en) | 2000-11-14 | 2001-07-23 | Apparatus and method for transferring a cryogenic fluid |
PCT/US2001/047516 WO2002040915A2 (en) | 2000-11-14 | 2001-11-08 | Apparatus and method for transferring a cryogenic fluid |
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---|---|---|---|---|
CH260393A (en) * | 1946-04-10 | 1949-03-15 | Rateau Soc | Thermal insulation device for low temperature and low density gas pipelines, in particular for cold and expanded air pipelines of aircraft engine test benches. |
US3433028A (en) * | 1966-09-02 | 1969-03-18 | Air Prod & Chem | Cryogenic fluid conveying system |
US3706208A (en) * | 1971-01-13 | 1972-12-19 | Air Prod & Chem | Flexible cryogenic liquid transfer system and improved support means therefor |
US3696627A (en) * | 1971-01-18 | 1972-10-10 | Air Prod & Chem | Liquid cryogen transfer system |
FR2624949B1 (en) * | 1987-12-22 | 1990-06-15 | Commissariat Energie Atomique | LIQUEFIED GAS TRANSFER LINE COMPRISING AT LEAST ONE BYPASS OF THE VAPORS OF THIS GAS |
US5477691A (en) * | 1994-09-30 | 1995-12-26 | Praxair Technology, Inc. | Liquid cryogen delivery system |
GB0004174D0 (en) * | 2000-02-22 | 2000-04-12 | Gore & Ass | Cryogenic fluid transfer tube |
-
2001
- 2001-11-08 AT AT01990051T patent/ATE287064T1/en not_active IP Right Cessation
- 2001-11-08 CA CA002428777A patent/CA2428777C/en not_active Expired - Lifetime
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- 2001-11-08 EP EP01990051A patent/EP1334306B1/en not_active Expired - Lifetime
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- 2001-11-08 JP JP2002542800A patent/JP4242645B2/en not_active Expired - Fee Related
- 2001-11-08 CN CN01818843.5A patent/CN1237303C/en not_active Expired - Lifetime
- 2001-11-08 AU AU2002228925A patent/AU2002228925B9/en not_active Expired
- 2001-11-08 WO PCT/US2001/047516 patent/WO2002040915A2/en active IP Right Grant
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TW536601B (en) | 2003-06-11 |
WO2002040915A3 (en) | 2003-05-01 |
CA2428777C (en) | 2006-09-12 |
DE60108415D1 (en) | 2005-02-17 |
AU2892502A (en) | 2002-05-27 |
DE60108415T2 (en) | 2005-12-22 |
EP1334306B1 (en) | 2005-01-12 |
ATE287064T1 (en) | 2005-01-15 |
CN1237303C (en) | 2006-01-18 |
BR0115316A (en) | 2003-10-21 |
AU2002228925B9 (en) | 2005-09-08 |
AU2002228925B2 (en) | 2005-04-21 |
MXPA03004259A (en) | 2004-12-03 |
BR0115316B1 (en) | 2011-04-05 |
CA2428777A1 (en) | 2002-05-23 |
CN1474920A (en) | 2004-02-11 |
JP2004514095A (en) | 2004-05-13 |
EP1334306A2 (en) | 2003-08-13 |
WO2002040915A2 (en) | 2002-05-23 |
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