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Publication numberUS3302417 A
Publication typeGrant
Publication dateFeb 7, 1967
Filing dateJun 29, 1965
Priority dateJun 29, 1965
Publication numberUS 3302417 A, US 3302417A, US-A-3302417, US3302417 A, US3302417A
InventorsKenneth W Cowans
Original AssigneeHughes Aircraft Co
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Coupling arrangement between cryogenic refrigerator and heat load
US 3302417 A
Abstract  available in
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Claims  available in
Description  (OCR text may contain errors)

Feb. 7, 1967 K. w. COWANS COUPLING ARRANGEMENT BETWEEN GRYOGENIC REFRIGERATOR AND HEAT LOAD 2 Sheets-Sheet 1 Filed June 29, 1965 Kenneih W. Cowuns,

Fig.1.

INVENTOR.

ATTORNEY.

Feb. 7, 1967 K. w. cowANs COUPLING ARRANGEMENT BETWEEN CRYOGENIC REFRIGERATOR AND HEAT LOAD 2 Sheets-Sheet 2 Filed June 29, 1965 Fig. 2.

S n G W O C WT N h E .TV 6N n l n e K ATTORNEY.

United States Patent 3,302,417 COUPLING ARRANGEMENT BETWEEN CRYO- GENIC REFRIGERATOR AND HEAT LOAD Kenneth W. Cowans, Los Angeles, Calif., assignor to Hughes Aircraft Company, Culver City, Calif., a corporation of Delaware Filed June 29, 1965, Ser. No. 467,845 3 Claims. (Cl. 62-49) The invention relates to a coupling arrangement between a cryogenic refrigerating source and a remote low temperature heat load and is particularly adapted to the maintenance of a steady-state temperature condition at the heat load over long periods of operation with a high degree of operating efficiency In the reception, transmission and amplification of various signals, for example, the reception and amplification of radio signals between ground and air stations, it is essential, for satisfactory operation, that the amplifier arrangement be maintained in a steady-state low temperature ambient condition over extended periods of time. It is therefore a first purpose of the invention to provide a cryogenic fluid transfer arrangement that will provide such steady-state ambient condition over a reasonably long period of time. Additionally, the arrangement disclosed is readily adapted to the incorporation of a redundant or secondary power system which further enhances service time operation in the event of accidental primary power system shutdown.

A major problem presented in the design of systems of the type hereunder consideration involves the effective utilization of refrigerating capacity from the standpoint of cryogenic efficiency and work output and the resulting in service, economical operation. Secondarily, of course, economical system manufacture is of major importance.

A major problem with regard to such systems has been the design of components that, when integrated within the over-all system, accomplishes maximum refrigeration with a minimum of work input and within practical parameters. The problem of an efiicient system is magnified, where, the ultimate refrigerating effect requires temperature reductions from an ambient in the range of 320 K. to an operating temperature in the range of 4 K.

With this in mind, the disclosed invention incorporates a cryogenic refrigerator and a coupling or transfer circuit combined with a heat load encapsulating Dewar in a combination adapted to produce the intended result in a highly efficient manner. The circuit employs a transfer pump which draws a cryogenic material from a load Dewar at essentially ambient temperature. The cryogenic gas from the Dewar is then circulated to a refrigerator where liquefaction is accomplished. The transfer circuit at the cryoengine is isolated from ambient by an evacuated or vacuum vessel, heat transfer being accomplished by direct conduction, that is, the circuit tubing physically contacting the refrigerator cooling sector. Preferably, the engine or refrigerator is multistaged. The transfer tube emanating from the cryoengine is the cold side of the circuit and carries the liquefied cryogenic material. The cold-side tube is again isolated from ambient by disposition thereof within a radiation shielded and evacuated (vacuum) transfer tube container. In the preferred embodiment the vacuum vessel and the vacuum tube container are unitary and the insulating vacuum is common thereto. The cold-side tube and tube container are received within the Dewar and the cold-side tube arranged to deposit the liquid cryogen at the load site. As a result of this structure, heat transfer in relation to the cold-side. tube is negligible and may be practically discounted with reference to the heat balance required to maintain the desired steady-state temperature condition at the load site. To achieve operational efficiency, it is important that structural dimensional integrity employed be accurately maintained during operation. Accordingly, it is desirable that the surface level of the liquid cryogen within the load Dewar be accurately maintained. To accomplish this result the system disclosed incorporates a regulating arrangement which is physically positioned within the Dewar at the desired level of liquid-vapor interface. The regulator is operative to dissipate heat to the Dewar in response to the degree of physical contact between the regulator and liquid cryogen. Specifically, the regulator comprises a resistance element with a constant current applied thereto, the resistance of said element varying in response to physical contact between the element and the cryogenic liquid. Specifically, as the temperature of the regulator is reduced by surface contact with the liquid cryogen, the resistance of the regulator increases and heat dissipation is increased. The dissipated heat stimulates the boiling and vaporization of the liquid cryogen. As a result the liquid interface is maintained at approximately the desired level. The attainment of an accurate located of liquid-vapor interface is an important feature of the invention. The heat load, of course, is continually bathed in the liquid cryogen thus maintaining its optimum operating temperature and an effective thermal balance may be achieved in the vapor aspect of the Dewar as will hereinafter be discussed.

The particular arrangement disclosed has been found to be highly effective in cooling an electronic device such as a preamplifier to an operating range at the approximate temperature of liquid helium. The particular Dewar that will encapsulate the preamplifier requires waveguide structure for signal transmission to and from the preamplifier. The waveguide structure enters the Dewar from an ambient atmosphere and etxends therein to engage the preamplifier. Heat conduction via the structure of the waveguide occurs. Additionally, the cold chamber of the Dewar will be subject to heat ingress by conduction along the Dewar walls and radiation shield and heat radiation from the Dewar walls. The most efficient operation of the system, with a minimum of waste refrigeration, requires that the vaporized cryogen leave the Dewar at approximately ambient temperature. This is most efiiciently accomplished by the absorption of: the noted heat load via warming of the vaporized cryogen by absorbing much of this heat ingress as it is moved to the egress port of the Dewar. Employing the disclosed arrangement, the waveguide structure is cooled continuously along its length to preamplifier operating temperature at the point of juncture therewith which avoids excessive heat impact at the preamplifier.

Thus, through vaporization and warming of the cryogen, a heat balance results assuring that the preamplifier is continuously bathed in liquid cryogen and maintained at its optimum operating temperature.

These and other objects and purposes of the disclosed invention will become apparent in the course of the following description and from an examination of the related drawings, wherein:

FIGURE 1 is a partially schematic, fragmentary perspective view of a typical system employing the invention;

FIG. '2 is a schematic illustration of the system employed and illustrates the invention in essentially flow diagram form; and

FIG. 3 is a fragmentary, partially schematic, vertical, sectional view of the load Dewar arrangement.

Describing the invention in detail and directing attention to the drawings, it will be understood that FIG. 1 discloses a coupling arrangement utilizing an active or primary system indicated generally at 10 and a standby or secondary system indicated generally at 12. The

stand-by or secondary system, of, course, is only employed in the event of accidental failure of the primary system or when the primary system requires purposeful shutdown for service.

The systems 10 and 12 are identical in structure and operation and, accordingly, only the primary system will herein be discussed in detail.

To provide cooling and liquefaction of the cryogen within the transfer circuit, a cryogenic refrigerator indicated generally at 14 is provided. A typical refrigerator that will efiiciently meet service requirement when the cryogen employed is helium may be a Solvay engine in operative series with a Joule-Thomson liquefier although other refrigerators may be employed. Specifically, a four-stage arrangement has been found satisfactory when the final heat load ambient temperature is in a range between 4 and Kelvin. A plurality of leads 16, 16 are operatively associated with the refrigerator 14 and in communication with an appropriate compressor (not shown) in the conventional manner. An encasing vessel 18 surrounds the cooling stages 20, 22, 24 and 26, of the refrigerator 14, and vacuum insulates said stages from ambient.

A transfer circuit pump 28 is provided and has a vapor intake line 30 and a vapor outlet line 32. The pump operates to circulate the cryogen as will hereinafter be described. In order to maximize heat transfer between the refrigerator 14 and the rtansfer line 32 within vacuum vessel 18, the line 32 is arranged to physically contact (bonded to) the respective cooling stages so that efficient heat transfer therebetween may be achieved by direct conduction. This arrangement is illustrated at 34, 34 of FIG. 1.

The load containing Dewar is indicated generally at 36 in FIGS. 1 and 3. It comprises a chamber 38 at the lower aspect there-0f housing the heat load such as an electronic preamplifier 40. The chamber 38 is partially defined by Dewar wall 39 which is surrounded by radiation shield 41. The intervening space is evacuated to offer appropriate vacuum insulation. The upper aspect of the Dewar 36 is closed by cap 42 and contains a cylinder of insulating material 44 such as fiberglass wool therebelow. Means 46 are provided for transmitting an energy signal to the preamplifier 40 and will hereinafter be referred to as the waveguide tubing. The waveguide tubing extends into the Dewar and is operatively associated with preamplifier 40 in chamber 38. The vapor intake line 30 also communicates with chamber 38. It is also desirable to provide a cryogen regenerating supply line 48 in communication with chamber 38. The line 48 may be in communication with a helium supply (not shown) and may have a regulating valve 50 therein so that additional cryogen :may be supplied to the circuit in the event pressure therein falls below a predetermined level.

A cold side liquid helium transfer line or tube 52 emanates from the refrigerator 14 and is in communication with the chamber 38 as at 54. A particular feature of the transfer line 52 is that it is axially disposed within an elongated radiation shielded vacuum container 56. The container 56, being evacuated and closed, insulates the tube 52 from ambient temperature. An additional tube 57, disposed between container 56 and tube 52 and made of copper or like material, may be incorporated and thus provide an effective insulating radiation shield. The container 56 also extends into chamber 38, insulating the cold side tube 52 from heat transfer relation with the Dewar 36. In the disclosed arrangement it has been found desirable that the container 56 physically communicate with the vessel 18 so that the vacuum existent in the vessel and the vacuum existent in the container 56 are identical. With this structure, heat transfer with the cold side tube 52 is negligible and may be disregarded in determining the physical structure required to maintain a steady-state heat balance within the Dewar 36.

Considering system heat balance, attention will first be directed to the Dewar 36. Noting FIG. 2, it will be seen that heat dissipation into the Dewar 36 may be considered to emanate from the operating device or preamplifier 4t} (arrow 43), and from the Dewar walls (arrows 45, 45), the latter resulting from wall radiation and conductive heat down container 56 and down the Dewar walls from ambient. The waveguide tubing or structure also dissipates heat to the internal aspect of the Dewar (arrows 47, 47 Assuming that the surface 60- of the liquid cryogen is maintained in an approximately fixed location, it is desirable that vaporized cryogen leave the Dewar 36 and enter pump intake line 30 at about ambient temperature. Thus, the vaporized cryogen that is boiled off in cooling the preamplifier 40 is warmed to ambient by absorption of the heat dissipated to the Dewar as described above.

To accurately locate the surface or liquid-gas interface 60, the invention provides a regulating device 62 (FIG. 2) which may be a carbon type resistor having associated therewith electrical leads 64, 64. The leads 64, 64 are connected to an electrical power source 65, which applies a constant current to the regulator 62. Regulators of this type have a resistance inversely related to temperature. That is to say, as the temperature level of the carbon resistor is lowered the resistance thereof increases and the heat dissipation thereof increases. Consequently, in the operating system disclosed, as the surface of the carbon resistor 62 is contacted by the liquid helium and cooled, heat dissipation increases in proportion to the degree of surface contact with the liquid helium. The increased heat dissipation has the effect of increasing the boiling or vaporization rate of the liquid helium with the result that the liquid-gaseous interface 60 is accurately maintained at the appropriate level within the Dewar 36.

It is desirable, to avoid heat balance disturbance via convection or acoustic resonance, that the flow of liquid helium to chamber 38 be continuous. To accomplish this result, a small liquid impedance or constriction is provided in the line 52 at the Dewar terminus thereof as at 68. This fluid impedance has the effect of maintaining the line 52 in liquid-full condition. The fiberglass wool 44 in the upper aspect of the Dewar patently inhibits heat balance disturbance due to convection.

In operation, the engine 14 provides the refrigerating effect and acts as a heat sink to cool the helium in the transfer circuit. The preamplifier 40, the systems primary load, ofiers optimum operation in an ambient condition of approximately 4 K., the temperature at which helium liquefies. The engine 14 may be of any conventional type having the capacity to liquefy helium. For example, a three-stage Solvay engine combined with a Joule-Thomson liquefier is effective to create the temperature levels needed. It will be understood that the cryogenic refrigerator or engine 14 employs helium gas to achieve this extremely low temperature but the gas utilized in the engine is independent of the cryogen in the transfer circuit.

Referring to FIG. 2, the transfer pump 28 removes helium gas from the Dewar 36 via line 30 at approximately ambient temperature of 320 K. and at atmospheric pressure. Heat above ambient added to the helium by the work of pump 28 will be dissipated to atmosphere at coil 62. The gas is then pumped via line 32 to stages 20, 22 and 24 of the engine where the temperature of the gas is staged-lowered to K., 50 K. and 15 K., respectively. At stage 26, the Joule-Thomson liquefier, the temperature of the helium in the transfer circuit is lowered to 4 K. and liquefaction results.

The liquid helium is then transferred via line 52 and is deposited in the Dewar chamber 38 at port 54. Within chamber 38 the helium boils as a result of heat absorption and the boiling effect cools the preamplifier as the liquid helium changes to its gaseous stage. The helium gas moves through the Dewar 36 to line 30 and is warmed to approximately ambient temperature as it enters line 30. In warming to ambient temperature in Dewar 36, the helium absorbs the heat load transmitted from ambient to the cold portion of the Dewar 36 by conduction via the Dewar walls, and the waveguide structure and radiation transmitted to the inner portions of the Dewar.

The line 52, being contained in vacuum transfer tube 56, delivers liquid helium to the heat load of the Dewar chamber 36 with negligible effect on the heat balance of the Dewar. The regulator 62 maintains the liquidvapor interface of the helium at the proper level within the Dewar chamber so that a steady-state condition at the amplifier 4-0 is assured.

In the event the primary power source fails, the liquid helium within the Dewar 36 continues to vaporize and the pressure within the transfer circuit will rise beyond the predetermined control level. This pressure rise within the Dewar vessel actuates relief valve 70. A conventional alarm (not shown) may be triggered by relief valve actuation and the redundant power source 12 may be activated to maintain the steady-state condition within the Dewar 36. Cool-down of redundant or standby system 12 occurs before the reservoir of liquid helium in chamber 38 is dissipated. During normal operation of the primary system 10, the redundant system 12 is static.

Means to regenerate the total volume of helium within the transfer circuit are provided. When pressure within the circuit falls below a determined level, the constant pressure valve 50 opens and helium gas is injected into Dewar 36 from a supply source (not shown) via line 48.

It will thus be apparent that the invention discloses a unique refrigerant transfer and coupling arrangement adapted to efiiciently maintain a steady-state temperature condition at the heat load situs. The design is such that it is readily adapted to the incorporation of a redundant system and thus provides fail-safe operation over extended periods of time.

The invention as disclosed is by way of illustration and not limitation and may be modified in various particulars and yet fall within the scope of the appended claims.

What is claimed is:

1. In a refrigerant transporting arrangement for moving a cryogenic refrigerant from a refrigerating device to a remotely located heat load, the combination of,

a casing of the Dewar type internally defining a chamber insulated to resist thermal transfer between the chamber and ambient atmosphere,

said heat load being disposed within said chamber,

a closed circuit refrigerant transport line having a cold segment terminating in an egress port communicating with the chamber,

said transport line including a return segment communicating with the chamber,

housing means encasing said device and said cold segmeat,

said housing means being sealed from ambient atmosphere and evacuated to vacuum insulate said device and said cold segment from said ambient atmosphere, said transport line including a refrigerating segment disposed within said housing means and in heat conductive engagement with said refrigerating device,

said refrigerating device being operative to reduce the temperature of said refrigerant in said last mentioned segment and to liquefy same,

said housing means thermally insulating said cold segment from heat conductive relation with said casing, pump means to continually convey said refrigerant through said closed circuit line,

said egress port being arranged to deposit liquid refrigerant within the chamber to bathe the heat load therein, and liquid level control means within the chamber operative to variably dissipate heat therein in response to the variation in surface contact between the control means and said liquid refrigerant to variably induce the boiling and vaporization of said liquid refrigerant and thereby control the level of the liquid refrigerant within the chamber, the vaporization and warming of said refrigerant being operative to absorb heat impinging on said chamber from said load and from ambient atmosphere,

said return segment conveying vaporized refrigerant from the chamber to the refrigerating device at approximately ambient temperature.

2. An arrangement according to claim 1,

wherein said refrigerating device comprises a refrigerator having a plurality of cold stages,

said housing means enclosing said cold stages,

the latter being disposed in a vacuum,

said refrigerating segment being series-bonded to the respective cold stages of the refrigerator,

said egress port being constricted to assure a liquid full condition in said cold segment.

3. An arrangement according to claim 2 and including passage means establishing communication between a supply source of cryogenic refrigerant and said chamber, and constant pressure valve regulating means within said passage means to accommodate regeneration of said cryogenic refrigerant when the pressure within the chamber falls below a determined level.

References Cited by the Examiner UNITED STATES PATENTS 2,189,122 2/1940 Andrews 62-514 3,125,863 3/1964 Hood 62-45 3,162,716 12/1964 Silver 62-514 X 3,195,322 7/1965 London 62-514 3,199,303 8/1965 Haumann et a1. 62-49 X LLOYD L. KING, Primary Examiner,

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US2189122 *May 18, 1938Feb 6, 1940Research CorpMethod of and apparatus for sensing radiant energy
US3125863 *Aug 10, 1962Mar 24, 1964 Dense gas helium refrigerator
US3162716 *Oct 15, 1962Dec 22, 1964Garrett CorpSuper conductor-power transmission system
US3195322 *Sep 17, 1962Jul 20, 1965Atomic Energy Authority UkRefrigerator employing helium
US3199303 *May 9, 1963Aug 10, 1965Union Carbide CorpOxygen therapy system
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US3430450 *Jul 25, 1967Mar 4, 1969Max Planck GesellschaftApparatus for replenishing liquid helium in a cryostat from a storage vessel
US4296610 *Apr 17, 1980Oct 27, 1981Union Carbide CorporationLiquid cryogen delivery system
US5587228 *Mar 13, 1995Dec 24, 1996The Boeing CompanyMicroparticle enhanced fibrous ceramics
US5632151 *Jun 5, 1995May 27, 1997The Boeing CompanyTransporting refrigerant to work surface through porous felted ceramic mat of ceramic fibers and ceramic microparticles bound with sol-gel binder
US5635454 *Jun 5, 1995Jun 3, 1997The Boeing CompanyFelting mat of ceramic particles from slurry and binding with sol-gel, coating surface, cooling with cryogen
US5640853 *Jun 5, 1995Jun 24, 1997The Boeing CompanyPorous stopper for cryogenic dewar comprising felted mat of ceramic fibers and microparticles bound by sol-gel binder; permitting pressure relief caused by boil-off of cryogen by allowing vapor to escape through pores
US5644919 *Jun 5, 1995Jul 8, 1997The Boeing CompanyCryogenic cold storage device
US5660053 *Jun 5, 1995Aug 26, 1997The Boeing CompanyFor cooling samples on a work surface
US8511100Jun 30, 2005Aug 20, 2013General Electric CompanyCooling of superconducting devices by liquid storage and refrigeration unit
WO2007005091A1 *Apr 25, 2006Jan 11, 2007Gen ElectricSystem and method for cooling superconducting devices
Classifications
U.S. Classification62/49.2, 62/50.2, 62/51.1
International ClassificationF25J1/00, F25B9/14, F25B25/00
Cooperative ClassificationF25B9/14, F25J1/0276, F25B25/005, F25J2290/42
European ClassificationF25J1/02Z4U2, F25B25/00B