US3529429A - Transfer system for cryogenic liquids - Google Patents

Transfer system for cryogenic liquids Download PDF

Info

Publication number
US3529429A
US3529429A US3529429DA US3529429A US 3529429 A US3529429 A US 3529429A US 3529429D A US3529429D A US 3529429DA US 3529429 A US3529429 A US 3529429A
Authority
US
United States
Prior art keywords
coil
connector
cooling
liquid
transfer system
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 - Lifetime
Application number
Inventor
Abraham Harel
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.)
US Air Force
Original Assignee
US Air Force
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 US Air Force filed Critical US Air Force
Application granted granted Critical
Publication of US3529429A publication Critical patent/US3529429A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C9/00Methods or apparatus for discharging liquefied or solidified gases from vessels not under pressure
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2201/00Vessel construction, in particular geometry, arrangement or size
    • F17C2201/01Shape
    • F17C2201/0138Shape tubular
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2223/00Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/01Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
    • F17C2223/0146Two-phase
    • F17C2223/0153Liquefied gas, e.g. LPG, GPL
    • F17C2223/0161Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2227/00Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
    • F17C2227/03Heat exchange with the fluid
    • F17C2227/0337Heat exchange with the fluid by cooling
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2227/00Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
    • F17C2227/04Methods for emptying or filling

Definitions

  • a cooling system has the cooling liquid, for example liquid-nitrogen or liquid helium, from a pressure tank, supplied through a T connector to the center of a helical coil.
  • the axis of the coil is substantially vertical so that the gas formed in the coil will rise to the top turns of the coil.
  • the output is taken otf a second T connector at the top of the coil.
  • a second coil providing a high impedance path is connected between the bottom of the cooling coil and the top of the cooling coil through the second T connector.
  • Coils containing liquid nitrogen or other cryogenic liquids are widely used in vacuum systems such as in forming baffies for oil diffusion pumps and cryogenic pumps or meissner traps.
  • the cooling liquid must be transferred from a pressurized tank into the coils.
  • a common problem with these systems is that the liquid coolant warms up in the coils and in the pipes which lead from the tank to the coil. During the refilling process a burst of warm gas from the pipes leading to the coil will cause the liquid coolant remaining in the coil to be ejected thus permitting the entire coil to warm up and cause a pressure rise in the vacuum system. This also causes a waste of liquid coolant.
  • the liquid coolant is fed at the center of a helical cooling coil through an input T connector.
  • the axis of the cooling coil is vertical to permit the gas to rise to the top turns by gravity.
  • the output at the top of the coil also has a T connector.
  • a high impedance passage is provided between the output T connector at the top of the cooling coil and the bottom of the cooling coil.
  • FIG. 1 is a top plan view of the liquid-nitrogen transfer system of the invention.
  • FIG. 2 is a front end view of the device of FIG. 1.
  • FIG. 1 of the drawing shows a cooling coil for cooling a vacuum system apparatus, not shown, on a support 131.
  • the coil 10 may be used to cool a bafile for an oil-diffusion pump, a meissner trap, or other apparatus.
  • Liquid coolant supplied from supply 12 at input 14 is fed to a T connector 16 through tube 17.
  • the coil 10 is cut in the center into a top coil section 18 and a bottom coil section 119 with the two cut ends being connected to the T connector 16 at 20 and 21.
  • a second T connector 23 is provided between the top of coil 10 at 24 and outlet 25 at 26.
  • a high im- 3,529,429 Patented Sept. 22, 1970 pedance coil 27 is connected between the T connector 23 at 28 and the bottom of coil section 19 at 29.
  • liquid coolant for example liquid nitrogen continuously converts to gas in the coil 10 and the gas accumulates in the top section 18 of the coil 10 and the liquid remains in the bottom section 19.
  • liquid coolant for example liquid nitrogen continuously converts to gas in the coil 10 and the gas accumulates in the top section 18 of the coil 10 and the liquid remains in the bottom section 19.
  • the coil is about one-half full with liquid nitrogen, it is refilled.
  • the initial surge of warm gas from the feed line passes through the gas-filled top section 18 since it presents a much lower impedance than the liquid-filled bottom section 19 which is terminated by a high impedance passage to the exit.
  • the high impedance passage 27 keeps the liquid nitrogen from being ejected from the bottom section 19 of coil 10 during refilling.
  • An apparatus for supplying a liquid coolant from a pressurized liquid coolant supply to a cooling coil for use in a vacuum system comprising a plural turn tubular cooling coil having its axis in a substantially vertical direction; means for supplying said liquid coolant to the center porton of said coil; output means connected to the top of said cooling coil and a high impedance means connected between the output means at the top of said cooling coil and the bottom of said cooling coil.
  • cooling coil is cut in the middle to form a top section and a bottom section; said means for supplying liquid coolant to the cooling coil being a T connector .with the cut ends being connected to two arms of the T connector; and the input being connected to the third arm of the T connector.
  • said high impedance means is a plural turn tubular coil connected between the top of said cooling coil and the bottom of said cooling coil.
  • the device as recited in claim 3 including a second T connector with the end of the top section of said coil being connected to one arm of said T connector; the top end of said high impedance coil being connected to another arm of said T connector and the output means being connected to the third arm of said T connector.

Description

Sept. 22, 1970 A. HAREL v TRANSFER SYSTEM FOR CRYOGENIC LIQUIDS Filed Oct. 16, 1968 2 Sheets-Sheet 1 NVENTOR.
Sept. 22, 1970 A. HAREL "3,529,429
TRANSFER SYSTEM FOR CRYOGENIC LIQUIDS Filed Oct. 16, 1968 2 Sheets-Sheet 2 United States Patent O 3,529,429 TRANSFER SYSTEM FOR CRYOGENIC LIQUIDS Abraham Hare], Trenton, N.J., assignor, by mesne assignments, to the United States of America as represented by the Secretary of the Air Force Filed Oct. 16, 1968, Ser. No. 768,147 Int. Cl. Btlld 5/00 U.S. Cl. 62-555 4 Claims ABSTRACT OF THE DISCLOSURE A cooling system has the cooling liquid, for example liquid-nitrogen or liquid helium, from a pressure tank, supplied through a T connector to the center of a helical coil. The axis of the coil is substantially vertical so that the gas formed in the coil will rise to the top turns of the coil. The output is taken otf a second T connector at the top of the coil. A second coil providing a high impedance path is connected between the bottom of the cooling coil and the top of the cooling coil through the second T connector.
BACKGROUND OF THE INVENTION Coils containing liquid nitrogen or other cryogenic liquids are widely used in vacuum systems such as in forming baffies for oil diffusion pumps and cryogenic pumps or meissner traps. In these systems the cooling liquid must be transferred from a pressurized tank into the coils. A common problem with these systems is that the liquid coolant warms up in the coils and in the pipes which lead from the tank to the coil. During the refilling process a burst of warm gas from the pipes leading to the coil will cause the liquid coolant remaining in the coil to be ejected thus permitting the entire coil to warm up and cause a pressure rise in the vacuum system. This also causes a waste of liquid coolant.
SUMMARY OF THE INVENTION According to this invention the liquid coolant is fed at the center of a helical cooling coil through an input T connector. The axis of the cooling coil is vertical to permit the gas to rise to the top turns by gravity. The output at the top of the coil also has a T connector. A high impedance passage is provided between the output T connector at the top of the cooling coil and the bottom of the cooling coil.
BRIEF DESCRIPTION OF THE DRAWINNG FIG. 1 is a top plan view of the liquid-nitrogen transfer system of the invention; and
FIG. 2 is a front end view of the device of FIG. 1.
DESCRIPTION OF THE PREFERRED EMBODIMENT Reference is now made to FIG. 1 of the drawing which shows a cooling coil for cooling a vacuum system apparatus, not shown, on a support 131. The coil 10 may be used to cool a bafile for an oil-diffusion pump, a meissner trap, or other apparatus. Liquid coolant supplied from supply 12 at input 14 is fed to a T connector 16 through tube 17. The coil 10 is cut in the center into a top coil section 18 and a bottom coil section 119 with the two cut ends being connected to the T connector 16 at 20 and 21. Through coils 18 and 19 are shown in vertical alignment, they need not be so located as long as coil section 18 is at a higher elevation so that gravity will cause the gases which form in the coil to rise into this section. A second T connector 23 is provided between the top of coil 10 at 24 and outlet 25 at 26. A high im- 3,529,429 Patented Sept. 22, 1970 pedance coil 27 is connected between the T connector 23 at 28 and the bottom of coil section 19 at 29.
When the coil of the invention is in use, liquid coolant, for example liquid nitrogen continuously converts to gas in the coil 10 and the gas accumulates in the top section 18 of the coil 10 and the liquid remains in the bottom section 19. When the coil is about one-half full with liquid nitrogen, it is refilled. With the liquid nitrogen being supplied at the center of the coil, the initial surge of warm gas from the feed line passes through the gas-filled top section 18 since it presents a much lower impedance than the liquid-filled bottom section 19 which is terminated by a high impedance passage to the exit. The high impedance passage 27 keeps the liquid nitrogen from being ejected from the bottom section 19 of coil 10 during refilling. When the warm gas passes through the top section of the coil and the liquid nitrogen from the pressurized supply tank arrives at the coil, it fills the entire coil. Since the warm gas does not eject the liquid nitrogen from the lower half of the coil, this portion remains cold so that a pressure rise in the vacuum system does not result. This system lends itself very well to automatic time-controlled refilling of the coil and such a system has been operated satisfactorily.
There is thus provided a system for transferring a liquid coolant to a cooling coil that does not have the problems of prior art systems.
While one specific embodiment has been described, it is obvious that numerous changes may be made without departing from the general principles and scope of the invention.
IWhat is claimed is:
1. An apparatus for supplying a liquid coolant from a pressurized liquid coolant supply to a cooling coil for use in a vacuum system; comprising a plural turn tubular cooling coil having its axis in a substantially vertical direction; means for supplying said liquid coolant to the center porton of said coil; output means connected to the top of said cooling coil and a high impedance means connected between the output means at the top of said cooling coil and the bottom of said cooling coil.
'2. The device as recited in claim 1 wherein said cooling coil is cut in the middle to form a top section and a bottom section; said means for supplying liquid coolant to the cooling coil being a T connector .with the cut ends being connected to two arms of the T connector; and the input being connected to the third arm of the T connector.
3. The device as recited in claim 2 wherein said high impedance means is a plural turn tubular coil connected between the top of said cooling coil and the bottom of said cooling coil.
4. The device as recited in claim 3 including a second T connector with the end of the top section of said coil being connected to one arm of said T connector; the top end of said high impedance coil being connected to another arm of said T connector and the output means being connected to the third arm of said T connector.
References Cited UNITED STATES PATENTS 3,279,214 10/1966 Klipping et al. 6255.5 3,396,548 8/1968 Mahe 6255.5
FOREIGN PATENTS 1,049,l,705 11/ 1966 Great Britain.
WILLIAM J. WYE, Primary Examiner U.S. Cl. X.R. 62-5 14
US3529429D 1968-10-16 1968-10-16 Transfer system for cryogenic liquids Expired - Lifetime US3529429A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US76814768A 1968-10-16 1968-10-16

Publications (1)

Publication Number Publication Date
US3529429A true US3529429A (en) 1970-09-22

Family

ID=25081681

Family Applications (1)

Application Number Title Priority Date Filing Date
US3529429D Expired - Lifetime US3529429A (en) 1968-10-16 1968-10-16 Transfer system for cryogenic liquids

Country Status (1)

Country Link
US (1) US3529429A (en)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3279214A (en) * 1963-11-02 1966-10-18 Max Planck Gesellschaft Pump
GB1049705A (en) * 1963-05-27 1966-11-30 Max Planck Gesellschaft Apparatus for the generation of a vacuum
US3396548A (en) * 1965-09-08 1968-08-13 Philips Corp Vacuum device

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1049705A (en) * 1963-05-27 1966-11-30 Max Planck Gesellschaft Apparatus for the generation of a vacuum
US3279214A (en) * 1963-11-02 1966-10-18 Max Planck Gesellschaft Pump
US3396548A (en) * 1965-09-08 1968-08-13 Philips Corp Vacuum device

Similar Documents

Publication Publication Date Title
JP2933718B2 (en) Liquid cooling system using air purge mechanism
US3502103A (en) Inlet device for introducing water and oil in a pipeline
US3495612A (en) Water pumping and control system
JP4783720B2 (en) Fuel tank
US3630039A (en) Individual cooling device
JPS598719B2 (en) Cryogenic agent delivery device configured in a closed loop
US3529429A (en) Transfer system for cryogenic liquids
US2969924A (en) Fuel nozzles for large flow range
US3316931A (en) Cryogenic transfer method and apparatus
US5454532A (en) Aircraft deicer pumping system
GB1227444A (en)
GB1230790A (en)
JPH03181699A (en) Method for maintaining pressure at value lower than given limit during filling of storage facility for storing fluid having liquid phase and gas phase and recondensing facility thereof
US2938464A (en) Air charger
US3588312A (en) Method and device for circulating a cryogenic liquid within a body immersed in the cryogenic liquid
US2625007A (en) Rocket motor cooling system
US3111819A (en) Evaporator with oil return means
US2966039A (en) Carbon dioxide discharge device
US2362968A (en) System for converting a liquefied gas into vapor
US3472038A (en) Apparatus and method for transferring heat from a lower temperature level to a higher temperature level
US3063213A (en) Apparatus for handling small articles
GB1119396A (en) A method of pumping wax-bearing oil through a pipeline
US3369526A (en) Supercritical pressure boiler
US1958420A (en) Method of and apparatus for liquefying and recovering explosives from a container
JPS60190134A (en) Liquid-cooled stator winding