JPS6314586B2 - - Google Patents
Info
- Publication number
- JPS6314586B2 JPS6314586B2 JP55077600A JP7760080A JPS6314586B2 JP S6314586 B2 JPS6314586 B2 JP S6314586B2 JP 55077600 A JP55077600 A JP 55077600A JP 7760080 A JP7760080 A JP 7760080A JP S6314586 B2 JPS6314586 B2 JP S6314586B2
- Authority
- JP
- Japan
- Prior art keywords
- helium
- liquid
- rotor
- phase
- bath
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 239000001307 helium Substances 0.000 claims description 66
- 229910052734 helium Inorganic materials 0.000 claims description 66
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 claims description 65
- 239000012071 phase Substances 0.000 claims description 37
- 239000007788 liquid Substances 0.000 claims description 33
- 239000007789 gas Substances 0.000 claims description 20
- 238000009835 boiling Methods 0.000 claims description 7
- 239000007791 liquid phase Substances 0.000 claims description 7
- 238000000034 method Methods 0.000 claims description 7
- 230000005501 phase interface Effects 0.000 claims 1
- 238000001816 cooling Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 230000001133 acceleration Effects 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 230000001360 synchronised effect Effects 0.000 description 2
- 238000004804 winding Methods 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000014509 gene expression Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 150000002371 helium Chemical class 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000010587 phase diagram Methods 0.000 description 1
- 230000010363 phase shift Effects 0.000 description 1
- 238000005086 pumping Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 229920006395 saturated elastomer Polymers 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K9/00—Arrangements for cooling or ventilating
- H02K9/19—Arrangements for cooling or ventilating for machines with closed casing and closed-circuit cooling using a liquid cooling medium, e.g. oil
- H02K9/193—Arrangements for cooling or ventilating for machines with closed casing and closed-circuit cooling using a liquid cooling medium, e.g. oil with provision for replenishing the cooling medium; with means for preventing leakage of the cooling medium
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K9/00—Arrangements for cooling or ventilating
- H02K9/19—Arrangements for cooling or ventilating for machines with closed casing and closed-circuit cooling using a liquid cooling medium, e.g. oil
- H02K9/20—Arrangements for cooling or ventilating for machines with closed casing and closed-circuit cooling using a liquid cooling medium, e.g. oil wherein the cooling medium vaporises within the machine casing
-
- 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
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K55/00—Dynamo-electric machines having windings operating at cryogenic temperatures
- H02K55/02—Dynamo-electric machines having windings operating at cryogenic temperatures of the synchronous type
- H02K55/04—Dynamo-electric machines having windings operating at cryogenic temperatures of the synchronous type with rotating field windings
-
- 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
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/068—Special properties of materials for vessel walls
- F17C2203/0687—Special properties of materials for vessel walls superconducting
-
- 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
-
- 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
- F17C2221/016—Noble gases (Ar, Kr, Xe)
- F17C2221/017—Helium
-
- 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
-
- 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
- F17C2250/00—Accessories; Control means; Indicating, measuring or monitoring of parameters
- F17C2250/04—Indicating or measuring of parameters as input values
- F17C2250/0404—Parameters indicated or measured
- F17C2250/0408—Level of content in the vessel
- F17C2250/0413—Level of content in the vessel with floats
-
- 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
- F17C2250/00—Accessories; Control means; Indicating, measuring or monitoring of parameters
- F17C2250/06—Controlling or regulating of parameters as output values
- F17C2250/0605—Parameters
- F17C2250/061—Level of content in the vessel
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E40/00—Technologies for an efficient electrical power generation, transmission or distribution
- Y02E40/60—Superconducting electric elements or equipment; Power systems integrating superconducting elements or equipment
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Superconductive Dynamoelectric Machines (AREA)
- Motor Or Generator Cooling System (AREA)
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明は、超電導発電機回転子内の低圧で沸騰
するヘリウム浴へ周囲圧力下にあるヘリウム貯蔵
タンクからヘリウムを補給するための方法に関す
る。DETAILED DESCRIPTION OF THE INVENTION Field of the Invention The present invention relates to a method for replenishing a low-pressure boiling helium bath in a superconducting generator rotor with helium from a helium storage tank at ambient pressure.
回転する超電導界磁巻線を備えた回転電機の運
転時の高信頼度を得るためには、冷却装置の故障
時にも回転電機の支障のない運転が保証されるよ
うに液体ヘリウムの供給が行われることが必要で
ある。この回転電機を冷却装置から切り離すこと
は、液体ヘリウム貯蔵タンクを間に接続すること
によつて簡単に保証される。この貯蔵タンク内に
おける圧力は大気圧下にあるか、また周囲雰囲気
内の不純物から液体ヘリウムが汚染されるのを避
けるために僅かの過圧状態におかれることが好ま
しい。
In order to achieve high reliability during operation of a rotating electric machine equipped with a rotating superconducting field winding, liquid helium must be supplied to ensure trouble-free operation of the rotating electric machine even in the event of a failure of the cooling system. It is necessary to be informed. The disconnection of this rotating electrical machine from the cooling system is simply ensured by connecting a liquid helium storage tank between them. The pressure in this storage tank is preferably atmospheric or slightly overpressured to avoid contamination of the liquid helium from impurities in the surrounding atmosphere.
超電導回転子巻線は、高い電流密度を得るため
に、数十分の1barの低減された圧力下で沸騰し、
それによりT<4.2Kの沸騰温度を持つヘリウム
で冷却されることが好ましい。回転子におけるこ
の低圧は排出ガス流の望ましい案内によつて簡単
に維持することができ、排出ガスは損失熱を吸収
後大気圧力で回転子より出る。回転子の冷却部に
おける低圧を得るために付加的なポンプは不要で
ある。 The superconducting rotor windings are boiled under a reduced pressure of a few tenths of bar to obtain high current densities.
It is thereby preferably cooled with helium having a boiling temperature of T<4.2K. This low pressure in the rotor can be easily maintained by the desired guidance of the exhaust gas flow, which leaves the rotor at atmospheric pressure after absorbing the lost heat. No additional pumps are required to obtain the low pressure in the rotor cooling section.
到来するヘリウムを絞り弁によつて回転子中に
存在する低圧に弛緩(ジユール・トムソン弛緩)
させることは既に提案されている(A.Bejan,
“Improved Thermal Design of the Cryogenic
Cooling System for a Superconducting
Synchroneous Generator”,Thesis MIT
(1974);米国特許第4056745号明細書)。この弁は
回転子に必要なヘリウム流に応じて積極的に調節
されなければならない。 The incoming helium is relaxed by a throttle valve to the low pressure present in the rotor (Joule-Thomson relaxation).
It has already been proposed to do so (A. Bejan,
“Improved Thermal Design of the Cryogenic
Cooling System for a Superconducting
Synchronous Generator”,Thesis MIT
(1974); U.S. Pat. No. 4,056,745). This valve must be actively adjusted depending on the helium flow required by the rotor.
他の提案(米国特許第4085529号および第
4082967号明細書)においては、回転子に流入す
るヘリウム流が移送管内の熱損失により比較的大
きなガス成分を持つことに基づいている。その場
合回転する供給管は供給管の少なくとも半径方向
にある部分で液体とガスとが空間的に分離するよ
うに構成される。この供給管における半径方向の
圧力変化は回転に基づく蒸気圧縮によつて与えら
れる。この供給管は、低圧で沸騰する液体内の、
液圧が気柱内における圧力と等しい所で開口す
る。この補給システムは蒸気成分が少なすぎるこ
とがない限り自己調節を行う。又大きなヘリウム
流の場合にも安定な運転を保証するためには、必
要ならば移相管の加熱によつて必要な蒸気成分を
発生させることが行われる。 Other proposals (U.S. Pat. No. 4,085,529 and No.
No. 4,082,967), it is based on the fact that the helium flow entering the rotor has a relatively large gas content due to heat losses in the transfer tubes. The rotating supply pipe is then constructed in such a way that liquid and gas are spatially separated in at least a radial section of the supply pipe. The radial pressure variation in this supply tube is provided by rotation-based vapor compression. This supply tube is used to store liquids in boiling water at low pressure.
It opens where the liquid pressure is equal to the pressure in the air column. This replenishment system is self-regulating as long as the vapor content does not become too low. In order to ensure stable operation even in the case of large helium flows, it is necessary to generate the necessary vapor components by heating the phase shift tube, if necessary.
他の方法は“Cryogenics”17,429(1977)に
記載されている。この場合には液体は放射方向の
供給管を通して導入され、低圧で沸騰するヘリウ
ム中へ、等しい液圧が存在する個所で給入され
る。その給入が行われる半径は気体−液体混合物
を供給する場合よりも大きい。それは例えば50Hz
の回転子の場合には例えば0.33mより大きくなけ
ればならない。別の欠点は放射方向の供給管を通
して純粋な液体のみが運ばれることである。 Other methods are described in "Cryogenics" 17 , 429 (1977). In this case, the liquid is introduced through radial supply pipes and is fed into the boiling helium at low pressure at the point where equal liquid pressure is present. The radius over which the feeding takes place is larger than when feeding a gas-liquid mixture. It is for example 50Hz
For example, in the case of a rotor of Another drawback is that only pure liquid is conveyed through the radial supply tubes.
本発明の目的は低減された圧力のもとで沸騰し
回転するヘリウム浴の補給を、供給すべきヘリウ
ムの蒸気成分に関係なく、また供給を受ける回転
子の大きさにも無関係に可能にする補給方法を提
供することにある。
The object of the invention is to enable the replenishment of boiling and rotating helium baths under reduced pressure, independent of the vapor composition of the helium to be supplied and independent of the size of the rotor receiving the supply. The purpose is to provide a replenishment method.
この目的は本発明によれば、回転子内の低圧で
沸騰するヘリウム浴へ周囲圧力下にあるヘリウム
貯蔵タンクから液体ヘリウムを供給し、ヘリウム
貯蔵タンクからヘリウム浴へ流れる間に一部が気
相に変化したヘリウムの液相と気相とを回転子に
固定した相分離器において分離し、分離した気相
は相分離器から外部へ引き出し、液相のみを回転
軸から距離をおいて回転子内のヘリウム浴へ導く
ことにより達成される。
This purpose, according to the invention, is to supply liquid helium from a helium storage tank at ambient pressure to a boiling helium bath at low pressure in the rotor, so that during the flow from the helium storage tank to the helium bath, a portion of the liquid helium is in the gas phase. The liquid and gas phases of the helium that has changed into This is achieved by introducing the helium bath into a helium bath.
液相のヘリウムのヘリウム浴への導入は、ヘリ
ウム浴の液相気相境界面より回転子の回転軸に対
し遠い位置で行うと有利である。 The introduction of liquid helium into the helium bath is advantageously carried out at a position farther from the axis of rotation of the rotor than the liquid-vapor interface of the helium bath.
本発明においては、ヘリウム貯蔵タンクから液
体ヘリウムが相分離器へ供給されるが、この液体
ヘリウムの一部は相分離器へ流れる間に気相に変
化する。相分離器において回転子の回転による遠
心作用によりこの気相と液相とは分離され、気相
は直ちに相分離器から外部へ引き出され、液相の
みが回転子内のヘリウム浴の液相部分に供給され
る。
In the present invention, liquid helium is supplied from a helium storage tank to a phase separator, and a portion of the liquid helium is converted into a gas phase while flowing to the phase separator. In the phase separator, the gas phase and liquid phase are separated by the centrifugal action caused by the rotation of the rotor, and the gas phase is immediately drawn out from the phase separator to the outside, leaving only the liquid phase in the liquid phase portion of the helium bath inside the rotor. supplied to
以下第1図および第2図により本発明を一実施
例について説明する。第1図は発電機の一部を概
略的に示している。
An embodiment of the present invention will be described below with reference to FIGS. 1 and 2. FIG. 1 schematically shows part of the generator.
液体ヘリウムは、真空外被10によつて絶縁さ
れている静止した導管1(第1図)を通して、圧
力p0(p01bar)のもとにあるヘリウム貯蔵タン
ク(図示せず)から流れ出し、回転子9と結合さ
れている相分離器2に流入する。相分離器2は主
として、周辺に少なくとも1つの出口3を備えた
異なる導管4および12のための分岐部11から
なる。相分離器2の中心を通る回転軸8の周りの
回転によつて供給導管1内に生じる気相成分が液
体から分離され、その結果液体は相分離器2の周
辺に沿う領域13に集まる。もし回転数が十分高
いと、分離は水平方向にある回転軸8においても
起こる。例えば50Hzの同期発電機の運転回転数に
おける遠心加速度は、回転軸から1cmの距離のと
ころで既に重力加速度の100倍以上大きくなる。 Liquid helium flows out of a helium storage tank (not shown) under pressure p 0 (p 0 1 bar) through a stationary conduit 1 (FIG. 1) insulated by a vacuum jacket 10; It flows into a phase separator 2 which is connected to a rotor 9. The phase separator 2 mainly consists of branches 11 for different conduits 4 and 12 with at least one outlet 3 on the periphery. Due to the rotation about the axis of rotation 8 passing through the center of the phase separator 2, the gas phase components occurring in the supply conduit 1 are separated from the liquid, so that the liquid collects in a region 13 along the periphery of the phase separator 2. If the rotational speed is high enough, separation also occurs at the horizontal axis of rotation 8. For example, the centrifugal acceleration at the operating speed of a synchronous generator of 50 Hz is already more than 100 times greater than the gravitational acceleration at a distance of 1 cm from the rotation axis.
液体は導管4,12を通して、供給すべきヘリ
ウム浴5内へ案内される。このヘリウム浴5内の
ヘリウムは回転軸8の近くにおいて圧力p0よりも
小さい圧力p1で沸騰し、回転子内の液相の浴と、
気相との境界面は軸8より距離R1のところにあ
る。 The liquid is conducted through conduits 4, 12 into the helium bath 5 to be supplied. The helium in this helium bath 5 boils near the rotating shaft 8 at a pressure p 1 smaller than the pressure p 0 , and the liquid phase bath in the rotor and
The interface with the gas phase is located at a distance R 1 from the axis 8.
相分離器において生じる蒸気そのものは、外被
10の周りにある同軸外管6を通して相分離器2
から排出される。相分離器2の蒸気室11におけ
る気体−液体境界面の半径R0は、レベル調節器
7によつて所定値に保持される。相分離器2にお
ける液体レベルは積極的に調節されなければなら
ない。この種のレベル調節器7はよく知られてい
る。レベル調節器7としては例えば温度センサ
(炭素抵抗式温度計または超電導検出器)が用い
られる。レベル平衡はヘリウム貯蔵器内の圧力を
変えるか、同軸外管6のガス出力の圧力を変える
ことによつて行うことができる。これは非回転シ
ステムにおけると同様の技術を使用することがで
きる。 The steam itself generated in the phase separator passes through the coaxial outer tube 6 around the jacket 10 to the phase separator 2.
is discharged from. The radius R 0 of the gas-liquid interface in the vapor chamber 11 of the phase separator 2 is maintained at a predetermined value by the level regulator 7 . The liquid level in the phase separator 2 must be actively regulated. Level regulators 7 of this type are well known. As the level regulator 7, for example, a temperature sensor (carbon resistance thermometer or superconducting detector) is used. Level balancing can be achieved by varying the pressure within the helium reservoir or by varying the pressure of the gas output of the coaxial outer tube 6. This can use similar techniques as in non-rotating systems.
補給すべき浴5内においては導管4および12
の供給点14のところでヘリウム浴5におけると
同じ液圧が存在するように回転軸8より距離R1
のところに相境界が生じる。供給点14は回転軸
8より距離R2のところにある。 In the bath 5 to be replenished, the conduits 4 and 12
At a distance R 1 from the axis of rotation 8 such that the same liquid pressure as in the helium bath 5 exists at the supply point 14 of
A phase boundary occurs at this point. The feed point 14 is located at a distance R 2 from the axis of rotation 8 .
第2図には放射方向の導管4,12(これは円
筒状の供給管であつてもよい)およびヘリウム浴
5における圧力が、回転軸8からの距離Rによつ
て、また相境界の距離R0,R1によつてどのよう
に変化するかが示されている。この例は50Hzの回
転数と1mの直径を有する大形超電導ターボ回転
子9における典型的な関係を示す。回転子9の回
転軸8に沿つて、例えば自動ポンプ効果によつて
排気回路において調整可能な0.41barの圧力が存
在するものと仮定されている。 FIG. 2 shows that the pressure in the radial conduits 4, 12 (which may be cylindrical supply pipes) and the helium bath 5 is determined by the distance R from the axis of rotation 8 and by the distance of the phase boundary. It shows how it changes depending on R 0 and R 1 . This example shows a typical relationship for a large superconducting turbo rotor 9 with a rotation speed of 50 Hz and a diameter of 1 m. It is assumed that along the axis of rotation 8 of the rotor 9 there is a pressure of 0.41 bar which can be adjusted in the exhaust circuit, for example by a self-pumping effect.
破線カーブaはp0=1barの圧力変化を示し、実
線カーブは圧力p1=0.41barに対応する。その他
のカーブは半径R0およびR1の外側でこれらの蒸
気空間に接する液体における圧力を示す。これら
のカーブ群は半径R0,R1およびR2がどの境界で
変化し得るかを示す。 The dashed curve a shows a pressure change of p 0 =1 bar, the solid curve corresponds to a pressure p 1 =0.41 bar. The other curves show the pressure in the liquid bordering these vapor spaces outside the radii R 0 and R 1 . These curves show at which boundaries the radii R 0 , R 1 and R 2 can change.
蒸気半径および供給半径がどの範囲で変化し得
るかを示すために第2図には3つの例が示されて
いる。それぞれ、ヘリウム浴5内ではR1=0.1m
の蒸気半径が生じることが要求される。R2A=
0.2m、R2B=0.35mまたはR2C=0.45mの個所で供
給が行われる場合に、相分離器2内の気体−液体
境界面は半径R0A,R0BまたはR0Cに調整されなけ
ればならない。 Three examples are shown in FIG. 2 to illustrate the range in which the steam radius and feed radius can vary. R 1 = 0.1m in helium bath 5, respectively.
is required to produce a vapor radius of . R2A =
0.2 m, R 2B = 0.35 m or R 2C = 0.45 m, the gas-liquid interface in phase separator 2 must be adjusted to radius R 0A , R 0B or R 0C . No.
第2図に示されている結果をもたらす計算の場
合には、ヘリウムの熱力学的な状態が遠心力によ
る圧縮の際に激しく変化することが考慮されなけ
ればならない。 In the calculations leading to the results shown in FIG. 2, it must be taken into account that the thermodynamic state of helium changes dramatically during centrifugal compression.
ヘリウムは供給導管4および/または12にお
ける熱の吸収または放出は全くない。即ちこれら
の導管は特に熱伝導率の悪い材料(特殊鋼)から
作られなければならない。単一相の液体における
圧力上昇は、状態変化
h(R)−h(O)=1/2ω2R2 (1)
および
s=一定 (2)
から計算される。ただし、hは固有エンタルピで
あり、sは固有エントロピである。蒸気は状態図
における相境界にそつて圧縮されるので、相境界
における蒸気圧力は次式によつて与えられる。 Helium absorbs or releases no heat in the supply conduits 4 and/or 12. This means that these conduits must be made of a material with particularly poor thermal conductivity (special steel). The pressure rise in a single phase liquid is calculated from the change of state h(R) - h(O) = 1/2ω 2 R 2 (1) and s = constant (2). However, h is the characteristic enthalpy and s is the characteristic entropy. Since steam is compressed along the phase boundary in the phase diagram, the steam pressure at the phase boundary is given by:
∫p(r1) p(r0)1/ρsdp=1/2ω2(r1 2−r0 2) (3)
がなりたつ。ただしρsは飽和蒸気の密度、r1は相
境界の半径(=R1),r0は浴からの蒸気出力の半
径(0)、p(r1)、p(r0)は対応する圧力であ
る。関係式(1),(2),(3)は実験的にも確認されてい
る。∫ p(r1) p(r0) 1/ρsdp=1/2ω 2 (r 1 2 − r 0 2 ) (3) holds. where ρs is the density of saturated steam, r 1 is the radius of the phase boundary (= R 1 ), r 0 is the radius of the steam output from the bath (0), and p (r 1 ) and p (r 0 ) are the corresponding pressures. It is. Relational expressions (1), (2), and (3) have also been confirmed experimentally.
本発明においては、ヘリウム貯蔵タンクより流
入するヘリウムの液体およびガスが回転子9内に
組み込まれた相分離器2において分離されるもの
であるが、液体は適当な個所即ち導管4および/
または12の所で回転子9に供給され、ガスは別
の管6を通して戻される。この供給点は広い範囲
で自由に選ぶことができる。本方法はヘリウムの
ガス成分の量に関係なく機能する。 In the present invention, the helium liquid and gas flowing from the helium storage tank are separated in a phase separator 2 built into the rotor 9;
or 12 to the rotor 9, and the gas is returned through another tube 6. This feeding point can be freely selected within a wide range. The method works regardless of the amount of helium gaseous component.
本発明によれば、ヘリウム貯蔵タンクから供給
される液体ヘリウムに含まれる気相のヘリウムは
回転子内に組み込まれた相分離器において分離さ
れ、液相のヘリウムのみが回転子内のヘリウム浴
の中心軸より離れたところ、すなわち液相部分に
供給されるものであるから、相分離器内の蒸気室
と回転子内のヘリウム浴の気相部分とが直接結合
されず両者の間にヘリウムの液柱が存在するた
め、静止部分と回転部分との間に圧力差がなく、
ヘリウムガスの洩れによる障害を防止することが
でき、高い運転信頼性が得られ、種々の回転子構
造にも適応させることができるという効果が得ら
れるものである。
According to the present invention, the gas phase helium contained in the liquid helium supplied from the helium storage tank is separated in the phase separator built into the rotor, and only the liquid phase helium is contained in the helium bath inside the rotor. Since it is supplied away from the central axis, that is, to the liquid phase, the vapor chamber in the phase separator and the gas phase of the helium bath in the rotor are not directly connected, and there is no helium between them. Due to the presence of a liquid column, there is no pressure difference between the stationary and rotating parts.
This has the following effects: troubles due to helium gas leakage can be prevented, high operational reliability can be obtained, and it can be adapted to various rotor structures.
第1図は本発明装置の実施例の示す概略構成
図、第2図は本発明の作用説明図である。
1……供給導管、2……相分離器、3……出
口、4,12……導管、5……ヘリウム浴、6…
…同軸外管、7……レベル調節器、8……回転
軸、9……回転子。
FIG. 1 is a schematic diagram showing an embodiment of the apparatus of the present invention, and FIG. 2 is an explanatory diagram of the operation of the present invention. 1... Supply conduit, 2... Phase separator, 3... Outlet, 4, 12... Conduit, 5... Helium bath, 6...
... Coaxial outer tube, 7 ... Level adjuster, 8 ... Rotating shaft, 9 ... Rotor.
Claims (1)
圧力下にあるヘリウム貯蔵タンクから液体ヘリウ
ムを供給し、ヘリウム貯蔵タンクからヘリウム浴
へ流れる間に一部が気相に変化したヘリウムの液
相と気相とを回転子に固定した相分離器において
分離し、分離した気相は相分離器から外部へ引き
出し、液相のみを回転軸から距離をおいて回転子
内のヘリウム浴へ導くことを特徴とする超電導回
転子のヘリウム補給方法。 2 液相のヘリウムのヘリウム浴への導入は、ヘ
リウム浴の液相気相境界面より回転子の回転軸に
対し遠い位置で行うことを特徴とする特許請求の
範囲第1項記載の方法。[Claims] 1. Liquid helium is supplied from a helium storage tank under ambient pressure to a helium bath boiling at low pressure in the rotor, and a portion of the liquid helium changes into a gas phase while flowing from the helium storage tank to the helium bath. The liquid and gas phases of helium are separated in a phase separator fixed to the rotor, the separated gas phase is drawn out from the phase separator, and only the liquid phase is separated from the rotor at a distance from the rotation axis. A helium replenishment method for a superconducting rotor characterized by introducing helium into a helium bath. 2. The method according to claim 1, wherein the introduction of liquid helium into the helium bath is carried out at a position farther from the rotation axis of the rotor than the liquid-gas phase interface of the helium bath.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19792923496 DE2923496A1 (en) | 1979-06-09 | 1979-06-09 | METHOD AND DEVICE FOR REFILLING HELIUM INTO THE ROTOR OF A SUPRAL-CONDUCTING GENERATOR |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS563550A JPS563550A (en) | 1981-01-14 |
| JPS6314586B2 true JPS6314586B2 (en) | 1988-03-31 |
Family
ID=6072907
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP7760080A Granted JPS563550A (en) | 1979-06-09 | 1980-06-09 | Method and device for supplying helium to rotor for superconductive generator |
Country Status (5)
| Country | Link |
|---|---|
| JP (1) | JPS563550A (en) |
| CH (1) | CH649661A5 (en) |
| DE (1) | DE2923496A1 (en) |
| FR (1) | FR2458935A1 (en) |
| GB (1) | GB2054278B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2947592C2 (en) * | 1979-11-26 | 1983-06-30 | Siemens AG, 1000 Berlin und 8000 München | Refill device for the cooling arrangement of a superconducting field winding in the rotor of an electrical machine |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4000777A (en) * | 1972-11-23 | 1977-01-04 | Nikolaus Laing | Rotary heat exchanger |
| US4123677A (en) * | 1975-04-30 | 1978-10-31 | General Electric Company | Self-regulating transport mechanism for super-conductive rotor refrigerant |
| DE2530100A1 (en) * | 1975-07-05 | 1977-02-03 | Kernforschung Gmbh Ges Fuer | Cooling for rotating magnet with superconducting windings - using convection generated in closed cooling channels forming thermosiphon |
| US4048529A (en) * | 1975-11-26 | 1977-09-13 | Gen Electric | Flow control device for superconductive rotor refrigerant |
| US4056745A (en) * | 1976-01-08 | 1977-11-01 | Westinghouse Electric Corporation | Cryogen transfer coupling with adjustable throttle valve for rotating machinery |
| US4082967A (en) * | 1976-03-31 | 1978-04-04 | General Electric Company | Uniformly-cooled superconducting rotor |
| US4085529A (en) * | 1976-11-19 | 1978-04-25 | Merrifield Fred C | Snowshoe |
| US4176291A (en) * | 1977-05-27 | 1979-11-27 | Electric Power Research Institute, Inc. | Stored field superconducting electrical machine and method |
-
1979
- 1979-06-09 DE DE19792923496 patent/DE2923496A1/en active Granted
-
1980
- 1980-05-29 GB GB8017606A patent/GB2054278B/en not_active Expired
- 1980-06-06 CH CH4374/80A patent/CH649661A5/en not_active IP Right Cessation
- 1980-06-09 JP JP7760080A patent/JPS563550A/en active Granted
- 1980-06-09 FR FR8012793A patent/FR2458935A1/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| GB2054278B (en) | 1984-05-02 |
| GB2054278A (en) | 1981-02-11 |
| DE2923496C2 (en) | 1989-09-28 |
| FR2458935A1 (en) | 1981-01-02 |
| JPS563550A (en) | 1981-01-14 |
| CH649661A5 (en) | 1985-05-31 |
| DE2923496A1 (en) | 1980-12-11 |
| FR2458935B1 (en) | 1984-04-27 |
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