[go: up one dir, main page]

US20130081788A1 - Heat exchange apparatus - Google Patents

Heat exchange apparatus Download PDF

Info

Publication number
US20130081788A1
US20130081788A1 US13/702,659 US201113702659A US2013081788A1 US 20130081788 A1 US20130081788 A1 US 20130081788A1 US 201113702659 A US201113702659 A US 201113702659A US 2013081788 A1 US2013081788 A1 US 2013081788A1
Authority
US
United States
Prior art keywords
working fluid
heat pipe
container
weight
alloy
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.)
Abandoned
Application number
US13/702,659
Inventor
Xiao Yang
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.)
Aavid Thermal Corp
Original Assignee
Individual
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 Individual filed Critical Individual
Assigned to THERMAL CORP. reassignment THERMAL CORP. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: YANG, XIAO
Publication of US20130081788A1 publication Critical patent/US20130081788A1/en
Assigned to PINE STREET CAPITAL PARTNERS II, L.P. reassignment PINE STREET CAPITAL PARTNERS II, L.P. SECURITY INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: THERMAL CORP.
Assigned to ANTARES CAPITAL LP, AS AGENT reassignment ANTARES CAPITAL LP, AS AGENT SECURITY INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: THERMAL CORP.
Assigned to THERMAL CORP. reassignment THERMAL CORP. RELEASE OF SECURITY INTEREST RECORDED AT REEL/FRAME 035134/0363 Assignors: PINE STREET CAPITAL PARTNERS II, L.P.
Assigned to ANTARES CAPITAL LP, AS AGENT reassignment ANTARES CAPITAL LP, AS AGENT FIRST LIEN INTELLECTUAL PROPERTY SECURITY AGREEMENT Assignors: AAVID NIAGARA, LLC, AAVID THERMACORE, INC., AAVID THERMAL CORP., AAVID THERMALLOY, LLC, LIFETIME INDUSTRIES, INC., LTI FLEXIBLE PRODUCTS, INC., LTI HOLDINGS, INC., NUVENTIX, INC.
Assigned to ANTARES CAPITAL LP, AS AGENT reassignment ANTARES CAPITAL LP, AS AGENT SECOND LIEN INTELLECTUAL PROPERTY SECURITY AGREEMENT Assignors: AAVID NIAGARA, LLC, AAVID THERMACORE, INC., AAVID THERMAL CORP., AAVID THERMALLOY, LLC, LIFETIME INDUSTRIES, INC., LTI FLEXIBLE PRODUCTS, INC., LTI HOLDINGS, INC., NUVENTIX, INC.
Assigned to THERMAL CORP. reassignment THERMAL CORP. RELEASE OF SECURITY INTEREST RECORDED AT REEL/FRAME 40355/0672 Assignors: ANTARES CAPITAL LP, AS SUCCESSOR TO GENERAL ELECTRIC CAPITAL CORPORATION, AS AGENT
Assigned to ROYAL BANK OF CANADA reassignment ROYAL BANK OF CANADA FIRST LIEN SECURITY INTEREST Assignors: AAVID THERMAL CORP. (F/K/A THERMAL CORP.), AAVID THERMALLOY, LLC, CSI MEDICAL, INC., LIFETIME INDUSTRIES, INC., LTI FLEXIBLE PRODUCTS, INC., NUVENTIX, INC.
Assigned to ROYAL BANK OF CANADA reassignment ROYAL BANK OF CANADA SECOND LIEN SECURITY INTEREST Assignors: AAVID THERMAL CORP. (F/K/A THERMAL CORP.), AAVID THERMALLOY, LLC, CSI MEDICAL, INC., LIFETIME INDUSTRIES, INC., LTI FLEXIBLE PRODUCTS, INC., NUVENTIX, INC.
Assigned to AAVID THERMACORE, INC., LIFETIME INDUSTRIES, INC., LTI FLEXIBLE PRODUCTS, INC., AAVID NIAGARA, LLC, AAVID THERMAL CORP., AAVID THERMALLOY, LLC,, NUVENTIX, INC., LTI HOLDINGS, INC. reassignment AAVID THERMACORE, INC. RELEASE OF FIRST LIEN SECURITY INTEREST IN PATENTS PREVIOUSLY RECORDED AT REEL/FRAME (042477/0565) Assignors: ANTARES CAPITAL LP, AS ADMINISTRATIVE AND COLLATERAL AGENT
Assigned to AAVID THERMACORE, INC., LTI HOLDINGS, INC., AAVID THERMAL CORP., LIFETIME INDUSTRIES, INC., NUVENTIX, INC., AAVID NIAGARA, LLC, AAVID THERMALLOY, LLC, LTI FLEXIBLE PRODUCTS, INC. reassignment AAVID THERMACORE, INC. RELEASE OF SECOND LIEN SECURITY INTEREST IN PATENTS PREVIOUSLY RECORDED AT REEL/FRAME (042477/0643) Assignors: ANTARES CAPITAL LP, AS ADMINISTRATIVE AND COLLATERAL AGENT
Assigned to NUVENTIX, INC., AAVID THERMALLOY, LLC (NOW KNOWN AS BOYD LACONIA, LLC, THERMAL CORP. (NOW KNOWN AS AAVID THERMAL CORP., LIFETIME INDUSTRIES, INC., LTI FLEXIBLE PRODUCTS, INC., CSI MEDICAL, INC. reassignment NUVENTIX, INC. RELEASE (REEL047028/FRAME0743) Assignors: ROYAL BANK OF CANADA
Abandoned legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D15/00Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies
    • F28D15/02Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes
    • F28D15/04Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes with tubes having a capillary structure
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C23/00Alloys based on magnesium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C23/00Alloys based on magnesium
    • C22C23/04Alloys based on magnesium with zinc or cadmium as the next major constituent
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D15/00Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies
    • F28D15/02Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes
    • F28D15/04Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes with tubes having a capillary structure
    • F28D15/046Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes with tubes having a capillary structure characterised by the material or the construction of the capillary structure
    • H10W40/73

Definitions

  • the present invention relates to heat exchange apparatus, and relates particularly, but not exclusively, to light weight heat exchange apparatus for use in aerospace applications.
  • Heat exchange apparatus such as heat pipes are used to rapidly transfer heat from a first location, for example adjacent to heat generating electronic components in a confined environment such as in the aerospace industry where space restrictions make effective heat dissipation difficult, to a second location, spaced from the first location, where the heat can be more effectively dissipated.
  • a heat pipe generally consists of a sealed vessel of thermally conductive material lined with a wick structure wherein the vessel defines a vapour channel in communication with the wick structure.
  • the vessel is evacuated and filled with working fluid at reduced pressure and then sealed, so that the internal pressure in the vessel is set by the vapour pressure of the working fluid.
  • the heat pipe is arranged so that one part is at the first, high temperature location, and another part of the heat pipe is at the second, low temperature location.
  • the application of heat to the first part of the heat pipe causes the working fluid to vaporise, drawing latent heat of vaporisation from the first location into the fluid.
  • the high temperature vapour then flows rapidly along the vapour channel to the cooler second part of the heat pipe, where it condenses on the pipe walls and the latent heat of vaporisation is released at the second location and dissipated.
  • the condensed working fluid is then transported back to the first location by means of capillary action in the wick structure, gravity or both.
  • Heat pipes are found to be extremely effective in improving heat dissipation in confined environments such as aerospace applications.
  • significant cost involved in transporting components in certain aerospace applications, such as placing satellites in orbit there is significant pressure to reduce the weight of components.
  • Heat pipes formed from aluminium alloys, with ammonia used as the working fluid, are known.
  • US 2004/0134643 discloses an attempt to reduce the weight of a heat pipe, in which a light weight heat pipe vessel is formed from magnesium, lined with a protective layer of oxide or nitride, depending on the choice of working fluid.
  • a stable nitride is used as the protective layer if ammonia is used as the working fluid
  • a stable oxide is used as the protective layer if water is used as the working fluid.
  • This arrangement provides the advantage of enabling the weight to be reduced significantly, since magnesium has a density of 1738 kg/m 3 , i.e. about half the density of aluminium, but has similar thermal and mechanical properties.
  • this arrangement suffers from the drawback that corrosion of magnesium often occurs when it comes into contact with certain types of working fluid. It is believed that the following corrosion reactions of magnesium in an aqueous environment occur:
  • the corrosion process is more complex, since in an electrolytic environment, the presence of other metals in magnesium promotes galvanic attack and can increase the corrosion rate significantly.
  • the introduction of metal impurities into the magnesium base metal can occur by means of many different processes, and it is very difficult to remove all of the impurities from the melt when producing pure magnesium. It has been found that the corrosion rate increases significantly when the tolerance limit of a specific impurity is exceeded.
  • some impurities are introduced intentionally to the magnesium melt during the alloying process to improve mechanical properties such as such strength of the alloy.
  • impurities can still be unintentionally introduced to the final product during subsequent machining as a result of improper tool selection.
  • the production of hydrogen gas during the corrosion process produces the disadvantage that because the hydrogen gas is non-condensable, it has a detrimental effect on heat pipe performance if formed inside the heat pipe.
  • the protective layer must be made very robust in order to avoid any fractures through which the working fluid can leak into contact with the magnesium. This significantly increases the complexity, and therefore the cost of manufacture, of the heat pipe, and some customers may nonetheless be reluctant to use the heat pipe in aerospace applications because of the potentially serious consequences of contact between the magnesium and the working fluid.
  • Preferred embodiments of the present invention seek to overcome one or more of the above disadvantages of the prior art.
  • a heat exchange apparatus comprising a container adapted to have at least one working fluid sealed therein, wherein at least one said working fluid is adapted to evaporate as a result of heating of at least one first part of the container and to condense as a result of cooling of at least one second part of the container, the container comprising at least one working fluid contacting portion, formed from at least one material containing at least one alloy including magnesium, 1% to 2.5% by weight manganese, and up to 2.5% by weight zinc, and defining at least one vapour channel adapted to allow at least one said working fluid to move in vapour state from at least one said first part towards at least one said second part, such that working fluid in liquid state is caused to move from at least one said second part towards at least one said first part.
  • the present invention is based on the surprising discovery that certain magnesium alloys are compatible with certain working fluids, for example ethanol, acetone, ammonia, propylene and ethane.
  • certain working fluids for example ethanol, acetone, ammonia, propylene and ethane.
  • This provides the advantage that no protective coating separating the magnesium from the working fluid is necessary, as a result of which the reliability of the heat exchange apparatus is improved, while its manufacture is simplified. This in turn significantly decreases the cost of manufacture of the heat exchange apparatus.
  • At least one said working fluid contacting portion may comprise wick means adapted to transport at least one said working fluid in liquid state from at least one said second part towards at least one said first part.
  • At least one said alloy may further include up to 0.2% by weight one or more metal impurities.
  • At least one said alloy may include up to 0.01% by weight iron.
  • At least one said alloy may include up to 0.005% by weight nickel and/or copper.
  • At least one said alloy may include 1.8% to 2.2% by weight zinc and 0.75% to 1.25% by weight manganese.
  • At least one said working fluid may include at least one alcohol and/or at least one ketone and/or ammonia and/or propylene and/or ethane.
  • At least one said working fluid may comprise ethanol and/or acetone.
  • At least one said working fluid may comprise ammonia.
  • the apparatus may comprise at least one heat pipe.
  • a heat pipe 2 comprises a sealed body 4 formed from a magnesium alloy such as ZM21 (i.e. approximately 2% by weight zinc, 1% by weight manganese and approximately 97% by weight magnesium) defining a grooved wick structure 6 surrounding a vapour transport channel 8 connecting an evaporator portion 10 of the heat pipe 2 to a condenser portion 12 of the heat pipe 2 .
  • the condenser portion 12 is surrounded by cooling fins 14 for effective heat dissipation.
  • the body 4 is evacuated and a working fluid comprising ethanol, acetone, ethanol/acetone mixture or ammonia is sealed inside the body 4 such that the working fluid is at reduced pressure and wets the wick structure 6 .
  • the body 4 is formed by first extruding a tube with a grooved structure which will subsequently form the wick structure 6 .
  • the grooves formed at each end of the tube are then machined away at each end to a depth of approximately 12 mm.
  • the extruded tube is then spun, and then the end is formed over using a number of small incremental movements. Once both ends are completely formed over, the tube should then be hermetically sealed, and a small hole is created at one end and this is used to introduce the working fluid.
  • the hole is then pinned or closed and the tube heated, and the pin is subsequently momentarily removed to expel the non condensable gases and then replaced and welded in place.
  • the alloy ZM21 is compatible with certain working fluids such as acetone, ethanol, acetone/ethanol mixture or ammonia, as a result of which corrosion is avoided and no protective layer is required between the wick structure 6 and the working fluid. This therefore significantly improves the ease of manufacture and reliability of the heat pipe 2 .
  • metal impurities such as iron, nickel, copper or cobalt are often present, up to a total amount of approximately 0.2 weight % of the total alloy. In particular, iron is often present at less than 0.01 weight %, and nickel and copper present at no more than 0.005 weight %.
  • manganese improves the stress corrosion resistance of the alloy and further enhances the anticorrosion and welding properties of the alloy. Furthermore, manganese reacts with iron ions and generates Fe2Mn during the magnesium alloy formation process, which can be removed as slag and minimise contamination by iron. If excessive manganese is introduced into the magnesium alloy, the plasticity of the alloy is reduced. For example, if the manganese increases from 0.4 weight % to 2.5 weight %, the elongation ratio of the alloy decreases from 5% to 3%.
  • the presence of zinc makes the magnesium alloy electrochemically less reactive, thereby minimising the corrosion rate.
  • the presence of more than 2.5 weight % of zinc can have a detrimental effect on the anti-corrosion behaviour of the magnesium alloy.
  • the presence of the zinc assists in overcoming the harmful corrosive effect of iron and nickel impurities that may be present in the magnesium alloy.
  • the following alloys are found to be compatible with the working fluids ethanol, acetone, ethanol/acetone mixture, and ammonia, and the ZM21 alloy can be extruded from unscalped billets at speeds up to four times faster than for comparable magnesium alloys.
  • the evaporator portion 10 of the heat pipe 2 is located in a region where heat is generated but is difficult to dissipate, such as adjacent to electronics in an aerospace application.
  • the condenser portion 12 is located in a region spaced from the evaporator portion 10 and is surrounded by cooling fins 14 such that heat can be significantly more effectively dissipated in the vicinity of the condenser portion 12 than at the evaporator portion 10 .
  • the application of heat to the evaporator portion 10 causes evaporation of the working fluid which draws significant amounts of heat from the evaporator portion 10 in the form of the latent heat of evaporation of the working fluid.
  • the working fluid then travels along the vapour transport channel 8 to the condenser portion 12 where it condenses, and the latent heat of evaporation is released and dissipated by the cooling fins 14 .
  • the wick structure 6 is wet by the working fluid condensing at the condenser portion 12 , and then transports the working fluid back to the evaporator portion 10 as a result of capillary action, gravity or both. As a result, the process continues as long as the temperature difference between the evaporator portion 10 and condenser portion 12 is maintained.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Cooling Or The Like Of Electrical Apparatus (AREA)

Abstract

A heat exchange apparatus comprising a heat pipe (2) having a body (4) containing a working fluid is disclosed. The working fluid is adapted to evaporate as a result of heating of a first part of the body and to condense as a result of cooling of a second part of the body. The container comprises a grooved wick structure (6), adapted to transport the working fluid in liquid state from the second part towards the first part; and a vapour channel (8) adapted to allow the working fluid to move in vapour state from the first location towards the second location. The wick structure is formed from at least one material containing at least one alloy including magnesium, 1% to 2.5% by weight manganese, and up to 2.5% by weight zinc.

Description

  • The present invention relates to heat exchange apparatus, and relates particularly, but not exclusively, to light weight heat exchange apparatus for use in aerospace applications.
  • Heat exchange apparatus such as heat pipes are used to rapidly transfer heat from a first location, for example adjacent to heat generating electronic components in a confined environment such as in the aerospace industry where space restrictions make effective heat dissipation difficult, to a second location, spaced from the first location, where the heat can be more effectively dissipated. A heat pipe generally consists of a sealed vessel of thermally conductive material lined with a wick structure wherein the vessel defines a vapour channel in communication with the wick structure. The vessel is evacuated and filled with working fluid at reduced pressure and then sealed, so that the internal pressure in the vessel is set by the vapour pressure of the working fluid. The heat pipe is arranged so that one part is at the first, high temperature location, and another part of the heat pipe is at the second, low temperature location. The application of heat to the first part of the heat pipe causes the working fluid to vaporise, drawing latent heat of vaporisation from the first location into the fluid. The high temperature vapour then flows rapidly along the vapour channel to the cooler second part of the heat pipe, where it condenses on the pipe walls and the latent heat of vaporisation is released at the second location and dissipated. The condensed working fluid is then transported back to the first location by means of capillary action in the wick structure, gravity or both.
  • Heat pipes are found to be extremely effective in improving heat dissipation in confined environments such as aerospace applications. However, because of the significant cost involved in transporting components in certain aerospace applications, such as placing satellites in orbit, there is significant pressure to reduce the weight of components.
  • Heat pipes formed from aluminium alloys, with ammonia used as the working fluid, are known.
  • US 2004/0134643 discloses an attempt to reduce the weight of a heat pipe, in which a light weight heat pipe vessel is formed from magnesium, lined with a protective layer of oxide or nitride, depending on the choice of working fluid. For example, a stable nitride is used as the protective layer if ammonia is used as the working fluid, and a stable oxide is used as the protective layer if water is used as the working fluid.
  • This arrangement provides the advantage of enabling the weight to be reduced significantly, since magnesium has a density of 1738 kg/m3, i.e. about half the density of aluminium, but has similar thermal and mechanical properties. However, this arrangement suffers from the drawback that corrosion of magnesium often occurs when it comes into contact with certain types of working fluid. It is believed that the following corrosion reactions of magnesium in an aqueous environment occur:

  • Mg→Mg2++2e;

  • 2H1O+2e→H2+2OH;

  • Mg2++2OH→Mg(OH)2.
  • As a result, the overall corrosion reaction can be expressed as:

  • Mg+2H2O→Mg(OH)2+H2.
  • In the case of magnesium alloys, the corrosion process is more complex, since in an electrolytic environment, the presence of other metals in magnesium promotes galvanic attack and can increase the corrosion rate significantly. The introduction of metal impurities into the magnesium base metal can occur by means of many different processes, and it is very difficult to remove all of the impurities from the melt when producing pure magnesium. It has been found that the corrosion rate increases significantly when the tolerance limit of a specific impurity is exceeded. In some cases, some impurities are introduced intentionally to the magnesium melt during the alloying process to improve mechanical properties such as such strength of the alloy. However, even with high purity magnesium and or properly controlled magnesium alloys, impurities can still be unintentionally introduced to the final product during subsequent machining as a result of improper tool selection. Furthermore, the production of hydrogen gas during the corrosion process produces the disadvantage that because the hydrogen gas is non-condensable, it has a detrimental effect on heat pipe performance if formed inside the heat pipe.
  • In view of this, the protective layer must be made very robust in order to avoid any fractures through which the working fluid can leak into contact with the magnesium. This significantly increases the complexity, and therefore the cost of manufacture, of the heat pipe, and some customers may nonetheless be reluctant to use the heat pipe in aerospace applications because of the potentially serious consequences of contact between the magnesium and the working fluid.
  • Preferred embodiments of the present invention seek to overcome one or more of the above disadvantages of the prior art.
  • According to the present invention, there is provided a heat exchange apparatus comprising a container adapted to have at least one working fluid sealed therein, wherein at least one said working fluid is adapted to evaporate as a result of heating of at least one first part of the container and to condense as a result of cooling of at least one second part of the container, the container comprising at least one working fluid contacting portion, formed from at least one material containing at least one alloy including magnesium, 1% to 2.5% by weight manganese, and up to 2.5% by weight zinc, and defining at least one vapour channel adapted to allow at least one said working fluid to move in vapour state from at least one said first part towards at least one said second part, such that working fluid in liquid state is caused to move from at least one said second part towards at least one said first part.
  • The present invention is based on the surprising discovery that certain magnesium alloys are compatible with certain working fluids, for example ethanol, acetone, ammonia, propylene and ethane. This provides the advantage that no protective coating separating the magnesium from the working fluid is necessary, as a result of which the reliability of the heat exchange apparatus is improved, while its manufacture is simplified. This in turn significantly decreases the cost of manufacture of the heat exchange apparatus.
  • At least one said working fluid contacting portion may comprise wick means adapted to transport at least one said working fluid in liquid state from at least one said second part towards at least one said first part.
  • At least one said alloy may further include up to 0.2% by weight one or more metal impurities.
  • At least one said alloy may include up to 0.01% by weight iron.
  • At least one said alloy may include up to 0.005% by weight nickel and/or copper.
  • At least one said alloy may include 1.8% to 2.2% by weight zinc and 0.75% to 1.25% by weight manganese.
  • At least one said working fluid may include at least one alcohol and/or at least one ketone and/or ammonia and/or propylene and/or ethane.
  • At least one said working fluid may comprise ethanol and/or acetone.
  • At least one said working fluid may comprise ammonia.
  • The apparatus may comprise at least one heat pipe.
  • A preferred embodiment of the invention will now be described, by way of example only and not in any limitative sense, with reference to the accompanying drawing, which shows a schematic partially cut away perspective view of a heat pipe embodying the present invention.
  • Referring to FIG. 1, a heat pipe 2 comprises a sealed body 4 formed from a magnesium alloy such as ZM21 (i.e. approximately 2% by weight zinc, 1% by weight manganese and approximately 97% by weight magnesium) defining a grooved wick structure 6 surrounding a vapour transport channel 8 connecting an evaporator portion 10 of the heat pipe 2 to a condenser portion 12 of the heat pipe 2. The condenser portion 12 is surrounded by cooling fins 14 for effective heat dissipation. The body 4 is evacuated and a working fluid comprising ethanol, acetone, ethanol/acetone mixture or ammonia is sealed inside the body 4 such that the working fluid is at reduced pressure and wets the wick structure 6.
  • The body 4 is formed by first extruding a tube with a grooved structure which will subsequently form the wick structure 6. The grooves formed at each end of the tube are then machined away at each end to a depth of approximately 12 mm. The extruded tube is then spun, and then the end is formed over using a number of small incremental movements. Once both ends are completely formed over, the tube should then be hermetically sealed, and a small hole is created at one end and this is used to introduce the working fluid. The hole is then pinned or closed and the tube heated, and the pin is subsequently momentarily removed to expel the non condensable gases and then replaced and welded in place.
  • It has been found that the alloy ZM21 is compatible with certain working fluids such as acetone, ethanol, acetone/ethanol mixture or ammonia, as a result of which corrosion is avoided and no protective layer is required between the wick structure 6 and the working fluid. This therefore significantly improves the ease of manufacture and reliability of the heat pipe 2. In the ZM21 alloy used to form the body 4 of the heat pipe 2, metal impurities such as iron, nickel, copper or cobalt are often present, up to a total amount of approximately 0.2 weight % of the total alloy. In particular, iron is often present at less than 0.01 weight %, and nickel and copper present at no more than 0.005 weight %.
  • The presence of manganese improves the stress corrosion resistance of the alloy and further enhances the anticorrosion and welding properties of the alloy. Furthermore, manganese reacts with iron ions and generates Fe2Mn during the magnesium alloy formation process, which can be removed as slag and minimise contamination by iron. If excessive manganese is introduced into the magnesium alloy, the plasticity of the alloy is reduced. For example, if the manganese increases from 0.4 weight % to 2.5 weight %, the elongation ratio of the alloy decreases from 5% to 3%.
  • The presence of zinc makes the magnesium alloy electrochemically less reactive, thereby minimising the corrosion rate. However, the presence of more than 2.5 weight % of zinc can have a detrimental effect on the anti-corrosion behaviour of the magnesium alloy. The presence of the zinc assists in overcoming the harmful corrosive effect of iron and nickel impurities that may be present in the magnesium alloy.
  • The following alloys are found to be compatible with the working fluids ethanol, acetone, ethanol/acetone mixture, and ammonia, and the ZM21 alloy can be extruded from unscalped billets at speeds up to four times faster than for comparable magnesium alloys.
  • Main element Zn Mn Mg
    Standard ZM21[5, 2.00 wt % 1.00 wt % rest
    18, 19]
    ZM21 alloy 1 [20] 2.10 wt % 0.90 wt % rest
    ZM21 alloy 2 [17] 2.10 wt % 1.11 wt % rest
    ZM21 alloy 3 [21] 2.20 wt % 0.80 wt % rest
    ZM21 alloy 3 [22] 2.10 wt % 0.75 wt % rest
  • The operation of the heat pipe of FIG. 1 will now be described. The evaporator portion 10 of the heat pipe 2 is located in a region where heat is generated but is difficult to dissipate, such as adjacent to electronics in an aerospace application. The condenser portion 12 is located in a region spaced from the evaporator portion 10 and is surrounded by cooling fins 14 such that heat can be significantly more effectively dissipated in the vicinity of the condenser portion 12 than at the evaporator portion 10. The application of heat to the evaporator portion 10 causes evaporation of the working fluid which draws significant amounts of heat from the evaporator portion 10 in the form of the latent heat of evaporation of the working fluid. The working fluid then travels along the vapour transport channel 8 to the condenser portion 12 where it condenses, and the latent heat of evaporation is released and dissipated by the cooling fins 14. The wick structure 6 is wet by the working fluid condensing at the condenser portion 12, and then transports the working fluid back to the evaporator portion 10 as a result of capillary action, gravity or both. As a result, the process continues as long as the temperature difference between the evaporator portion 10 and condenser portion 12 is maintained.
  • EXAMPLE
  • Tests of various working fluids with the ZM21 alloy were carried out. Thermal tests started from room temperature (20° C.) to the 8K superheat temperature of each working fluid. The thermal test was carried out under a pressure of 5bar for ammonia and at atmospheric pressure for the other working fluids. The following conclusions were drawn after more than 100 hours of thermal testing.
  • 1. All of the working fluids gave good thermal performance.
    2. Water and methanol are not compatible with ZM21.
    3. Acetone, ethanol, acetone/ethanol mixture and ammonia are compatible with ZM21.
    4. Using acetone and ethanol as working fluids, an operating temperature range from −40° C. to 140° C. is provided.
    5. Using ammonia as a working fluid, the operating temperature ranges from −60° C. to 120° C.
  • Compatibility tests carried out over 24 months indicate the following:
  • 1. Copper and iron contaminate the ZM21 surface significantly.
    2. At room temperature, there is no corrosion on the ZM21 surface if small samples are placed in pure acetone, pure ethanol and an acetone/ethanol mixture.
    3. Water/ZM21, methanol/ZM21 compatibility life tests fail. In the case of the water/ZM21 tests, Mg(OH)2 was generated along the ZM21 surface and gaseous hydrogen was also generated. In the case of pure methanol, a vigorously exothermic reaction occurred in the test jar, and the ZM21 surface became black.
  • It will be appreciated by persons skilled in the art that the above embodiment has been described by way of example only, and not in any limitative sense, and that various alterations and modifications are possible without departure from the scope of the invention as defined by the appended claims. For example, instead of, or in addition to, cooling the condenser portion of the heat pipe by means of cooling fins, radiator panels or cold plates may be used. In addition, instead of sealing the body of the heat pipe by machining, welding and/or brazing can also be used.

Claims (21)

1.-9. (canceled)
10. A heat pipe comprising a container adapted to have at least one working fluid sealed therein such that at least one said working fluid is adapted to evaporate as a result of heating of at least one first part of the container and to condense as a result of cooling of at least one second part of the container, the container comprising at least one working fluid contacting portion, formed from at least one material containing at least one alloy including magnesium, 1% to 2.5% by weight manganese, and up to 2.5% by weight zinc, and defining at least one vapor channel adapted to allow at least one said working fluid to move in vapor state from at least one said first part towards at least one said second part, such that working fluid in liquid state is caused to move from at least one said second part towards at least one said first part.
11. The heat pipe of claim 10, wherein at least one said alloy further includes up to 0.2% by weight one or more metal impurities.
12. The heat pipe of claim 11, wherein at least one said alloy includes up to 0.01% by weight iron.
13. The heat pipe of claim 11, wherein at least one said alloy includes up to 0.005% by weight nickel and/or copper.
14. The heat pipe of claim 10, wherein at least one said alloy includes 1.8% to 2.2% by weight zinc and 1% to 1.25% by weight manganese.
15. The heat pipe of claim 10, further comprising at least one working fluid sealed therein.
16. The heat pipe of claim 15, wherein the at least one said working fluid includes at least one of an alcohol, a ketone, ammonia, propylene, or ethane.
17. The heat pipe of claim 16, wherein the at least one said working fluid comprises one of ethanol or acetone.
18. The heat pipe of claim 16, wherein the at least one said working fluid comprises ammonia.
19. The heat pipe of claim 10, wherein at least one said working fluid contacting portion comprises a wick adapted to transport at least one said working fluid in liquid state from at least one said second part towards at least one said first part.
20. A heat pipe, comprising:
a container comprising an alloy, the alloy comprising
1% to 2.5% by weight manganese, up to 2.5% by weight zinc, and balance magnesium,
the container having a working fluid sealed therein, the working fluid being adapted to evaporate as a result of heating of an evaporator portion of the container and to condense as a result of cooling of a condenser portion of the container,
the container defining at least one vapor channel adapted to allow the working fluid to move in a vapor state from the evaporator portion of the container towards the condenser portion of the container, such that working fluid in a liquid state is caused to move from the condenser portion of the container towards the evaporator portion of the container.
21. The heat pipe of claim 20, wherein the working fluid includes at least one of an alcohol, a ketone, ammonia, propylene, or ethane.
22. The heat pipe of claim 21, wherein the working fluid comprises one of ethanol or acetone.
23. The heat pipe of claim 21, wherein the working fluid comprises ammonia.
24. The heat pipe of claim 20, wherein the container comprises a wick adapted to cause the working fluid in a liquid state to move from the condenser portion of the container towards the evaporator portion of the container.
25. The heat pipe of claim 20, wherein the alloy further comprises up to 0.2% by weight metal impurities.
26. The heat pipe of claim 25, wherein the metal impurities comprise up to 0.01% by weight iron.
27. The heat pipe of claim 25, wherein the metal impurities comprise up to 0.005% by weight of nickel or copper.
28. The heat pipe of claim 20, wherein the alloy comprises 1.8% to 2.2% by weight zinc and 1% to 1.25% by weight manganese.
29. The heat pipe of claim 20, wherein the alloy comprises 2% by weight zinc and 1% by weight manganese.
US13/702,659 2010-06-08 2011-06-06 Heat exchange apparatus Abandoned US20130081788A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP10165306.1 2010-06-08
EP20100165306 EP2395309A1 (en) 2010-06-08 2010-06-08 Heat pipe
PCT/EP2011/059314 WO2011154366A1 (en) 2010-06-08 2011-06-06 Heat exchange apparatus

Publications (1)

Publication Number Publication Date
US20130081788A1 true US20130081788A1 (en) 2013-04-04

Family

ID=43063990

Family Applications (1)

Application Number Title Priority Date Filing Date
US13/702,659 Abandoned US20130081788A1 (en) 2010-06-08 2011-06-06 Heat exchange apparatus

Country Status (3)

Country Link
US (1) US20130081788A1 (en)
EP (1) EP2395309A1 (en)
WO (1) WO2011154366A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9763359B2 (en) 2015-05-29 2017-09-12 Oracle International Corporation Heat pipe with near-azeotropic binary fluid
US20260002472A1 (en) * 2024-06-27 2026-01-01 General Electric Company Gas turbine engine with heat exchanger

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105841539A (en) * 2015-01-15 2016-08-10 王青佐 Pipe material of heat radiation conduit
US11796257B2 (en) 2018-02-14 2023-10-24 Tusas—Turk Havacilik Ve Uzay Sanayii Anonim Sirketi Ammonia filling system

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4082575A (en) * 1976-04-21 1978-04-04 Thermacore, Inc. Production of liquid compatible metals
US4470451A (en) * 1981-03-16 1984-09-11 Grumman Aerospace Corporation Dual axial channel heat pipe
US6418017B1 (en) * 2000-03-30 2002-07-09 Hewlett-Packard Company Heat dissipating chassis member
US20040035558A1 (en) * 2002-06-14 2004-02-26 Todd John J. Heat dissipation tower for circuit devices
US7069978B2 (en) * 2001-01-03 2006-07-04 Thermal Corp. Chemically compatible, lightweight heat pipe

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2223852A (en) * 1939-03-13 1940-12-03 American Magnesium Metals Corp Magnesium base alloys
GB1378281A (en) * 1973-03-14 1974-12-27 Tikhova N M Blokhina V A Antip Magnesium-based alloy
US6911231B2 (en) * 1996-10-25 2005-06-28 New Qu Energy Limited Method for producing a heat transfer medium and device
JP4204681B2 (en) * 1998-11-20 2009-01-07 住友軽金属工業株式会社 Heat pipe fixing structure
US6896039B2 (en) * 1999-05-12 2005-05-24 Thermal Corp. Integrated circuit heat pipe heat spreader with through mounting holes
JP3597186B2 (en) * 2002-03-04 2004-12-02 住友電工スチールワイヤー株式会社 Magnesium-based alloy tube and method of manufacturing the same

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4082575A (en) * 1976-04-21 1978-04-04 Thermacore, Inc. Production of liquid compatible metals
US4470451A (en) * 1981-03-16 1984-09-11 Grumman Aerospace Corporation Dual axial channel heat pipe
US6418017B1 (en) * 2000-03-30 2002-07-09 Hewlett-Packard Company Heat dissipating chassis member
US7069978B2 (en) * 2001-01-03 2006-07-04 Thermal Corp. Chemically compatible, lightweight heat pipe
US20040035558A1 (en) * 2002-06-14 2004-02-26 Todd John J. Heat dissipation tower for circuit devices

Non-Patent Citations (4)

* Cited by examiner, † Cited by third party
Title
Catalog sheet for acetone by SASOL, "SASOL-Acetone", version 5a *
Montana et al., ZM-21 Magnesium Alloy Corrosion Properties and Crygenic to Elevated Temperature Mechanical Properties, March 14, 1972, NASA, NASA Technical Memorandum, NASA TM X-64645 *
Publication entitled "Electroless Nickel Plating on Magnesium Alloy" by A.K Sharma, Published March 1998 *
Publication entitled "EXPERIMENTS AND MOLECULAR DYNAMICS SIMULATION OF DROPLETS BEHAVIOUR AND PHASE CHANGE IN MAGNESIUM HEAT PIPE", Yang et al., 05/2009 *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9763359B2 (en) 2015-05-29 2017-09-12 Oracle International Corporation Heat pipe with near-azeotropic binary fluid
US10015910B2 (en) 2015-05-29 2018-07-03 Oracle International Corporation Heat pop with near-azeotropic binary fluid
US20260002472A1 (en) * 2024-06-27 2026-01-01 General Electric Company Gas turbine engine with heat exchanger

Also Published As

Publication number Publication date
EP2395309A1 (en) 2011-12-14
WO2011154366A1 (en) 2011-12-15

Similar Documents

Publication Publication Date Title
US7743502B2 (en) Chemically compatible, lightweight heat pipe
US20130081788A1 (en) Heat exchange apparatus
US8267575B2 (en) Temperature measuring device
TWI688662B (en) Nickel based alloy with high melting range suitable for brazing super austenitic steel
US20050099775A1 (en) Pumped liquid cooling for computer systems using liquid metal coolant
EP0626459B1 (en) Corrosion resistant copper alloy tube and fin-tube heat exchanger
US4372377A (en) Heat pipes containing alkali metal working fluid
JP2012532990A (en) Copper alloy for heat exchange tubes
US20070284087A1 (en) Waste heat recovery device
CN209605636U (en) Heat pipe and radiator with the heat pipe
JP2012061483A (en) Flux-less brazing method of aluminum material
CN115052706B (en) Brazing sheet, brazing method and manufacturing method of heat exchanger
JP4878317B2 (en) Copper tube made of copper or copper alloy
KR20110059799A (en) Boiling cooling system
WO2019039445A1 (en) Heat pipe and heat pipe production method
JP2006045667A (en) Heat exchanger tube made of aluminum and its production method
JP2013512341A (en) Copper alloy and heat exchange tube
JP2011080121A (en) Extruded tube for fin tube type heat exchanger for air conditioner and refrigerant piping for heat exchange cycle
US20230069333A1 (en) Vapor chamber
US20230375278A1 (en) Heat pipe
JP2020028895A (en) Heat exchanger manufacturing method
JP2004218083A (en) Aluminum pipe and its manufacturing method
CA2403081A1 (en) Oxygen-blowing lance in vacuum refining apparatus
TWI642891B (en) Heat pipe and radiator
US12516402B2 (en) Brazing foil, object and method for brazing

Legal Events

Date Code Title Description
AS Assignment

Owner name: THERMAL CORP., DELAWARE

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:YANG, XIAO;REEL/FRAME:029559/0267

Effective date: 20121206

AS Assignment

Owner name: PINE STREET CAPITAL PARTNERS II, L.P., NEW YORK

Free format text: SECURITY INTEREST;ASSIGNOR:THERMAL CORP.;REEL/FRAME:035134/0363

Effective date: 20141113

AS Assignment

Owner name: ANTARES CAPITAL LP, AS AGENT, ILLINOIS

Free format text: SECURITY INTEREST;ASSIGNOR:THERMAL CORP.;REEL/FRAME:040355/0672

Effective date: 20161013

AS Assignment

Owner name: THERMAL CORP., NEW HAMPSHIRE

Free format text: RELEASE OF SECURITY INTEREST RECORDED AT REEL/FRAME 035134/0363;ASSIGNOR:PINE STREET CAPITAL PARTNERS II, L.P.;REEL/FRAME:040425/0584

Effective date: 20161013

AS Assignment

Owner name: ANTARES CAPITAL LP, AS AGENT, ILLINOIS

Free format text: FIRST LIEN INTELLECTUAL PROPERTY SECURITY AGREEMENT;ASSIGNORS:LTI HOLDINGS, INC.;AAVID NIAGARA, LLC;AAVID THERMACORE, INC.;AND OTHERS;REEL/FRAME:042477/0565

Effective date: 20170516

Owner name: ANTARES CAPITAL LP, AS AGENT, ILLINOIS

Free format text: SECOND LIEN INTELLECTUAL PROPERTY SECURITY AGREEMENT;ASSIGNORS:LTI HOLDINGS, INC.;AAVID NIAGARA, LLC;AAVID THERMACORE, INC.;AND OTHERS;REEL/FRAME:042477/0643

Effective date: 20170516

AS Assignment

Owner name: THERMAL CORP., NEW HAMPSHIRE

Free format text: RELEASE OF SECURITY INTEREST RECORDED AT REEL/FRAME 40355/0672;ASSIGNOR:ANTARES CAPITAL LP, AS SUCCESSOR TO GENERAL ELECTRIC CAPITAL CORPORATION, AS AGENT;REEL/FRAME:042554/0151

Effective date: 20170516

AS Assignment

Owner name: ROYAL BANK OF CANADA, CANADA

Free format text: FIRST LIEN SECURITY INTEREST;ASSIGNORS:LTI FLEXIBLE PRODUCTS, INC.;LIFETIME INDUSTRIES, INC.;AAVID THERMALLOY, LLC;AND OTHERS;REEL/FRAME:047026/0666

Effective date: 20180906

AS Assignment

Owner name: ROYAL BANK OF CANADA, CANADA

Free format text: SECOND LIEN SECURITY INTEREST;ASSIGNORS:LTI FLEXIBLE PRODUCTS, INC.;LIFETIME INDUSTRIES, INC.;AAVID THERMALLOY, LLC;AND OTHERS;REEL/FRAME:047028/0743

Effective date: 20180906

AS Assignment

Owner name: AAVID THERMAL CORP., NEW HAMPSHIRE

Free format text: RELEASE OF FIRST LIEN SECURITY INTEREST IN PATENTS PREVIOUSLY RECORDED AT REEL/FRAME (042477/0565);ASSIGNOR:ANTARES CAPITAL LP, AS ADMINISTRATIVE AND COLLATERAL AGENT;REEL/FRAME:047052/0001

Effective date: 20180906

Owner name: AAVID NIAGARA, LLC, NEW HAMPSHIRE

Free format text: RELEASE OF FIRST LIEN SECURITY INTEREST IN PATENTS PREVIOUSLY RECORDED AT REEL/FRAME (042477/0565);ASSIGNOR:ANTARES CAPITAL LP, AS ADMINISTRATIVE AND COLLATERAL AGENT;REEL/FRAME:047052/0001

Effective date: 20180906

Owner name: NUVENTIX, INC., NEW HAMPSHIRE

Free format text: RELEASE OF FIRST LIEN SECURITY INTEREST IN PATENTS PREVIOUSLY RECORDED AT REEL/FRAME (042477/0565);ASSIGNOR:ANTARES CAPITAL LP, AS ADMINISTRATIVE AND COLLATERAL AGENT;REEL/FRAME:047052/0001

Effective date: 20180906

Owner name: LIFETIME INDUSTRIES, INC., CALIFORNIA

Free format text: RELEASE OF FIRST LIEN SECURITY INTEREST IN PATENTS PREVIOUSLY RECORDED AT REEL/FRAME (042477/0565);ASSIGNOR:ANTARES CAPITAL LP, AS ADMINISTRATIVE AND COLLATERAL AGENT;REEL/FRAME:047052/0001

Effective date: 20180906

Owner name: AAVID THERMACORE, INC., NEW HAMPSHIRE

Free format text: RELEASE OF FIRST LIEN SECURITY INTEREST IN PATENTS PREVIOUSLY RECORDED AT REEL/FRAME (042477/0565);ASSIGNOR:ANTARES CAPITAL LP, AS ADMINISTRATIVE AND COLLATERAL AGENT;REEL/FRAME:047052/0001

Effective date: 20180906

Owner name: AAVID THERMALLOY, LLC,, NEW HAMPSHIRE

Free format text: RELEASE OF FIRST LIEN SECURITY INTEREST IN PATENTS PREVIOUSLY RECORDED AT REEL/FRAME (042477/0565);ASSIGNOR:ANTARES CAPITAL LP, AS ADMINISTRATIVE AND COLLATERAL AGENT;REEL/FRAME:047052/0001

Effective date: 20180906

Owner name: LTI FLEXIBLE PRODUCTS, INC., CALIFORNIA

Free format text: RELEASE OF FIRST LIEN SECURITY INTEREST IN PATENTS PREVIOUSLY RECORDED AT REEL/FRAME (042477/0565);ASSIGNOR:ANTARES CAPITAL LP, AS ADMINISTRATIVE AND COLLATERAL AGENT;REEL/FRAME:047052/0001

Effective date: 20180906

Owner name: LTI HOLDINGS, INC., CALIFORNIA

Free format text: RELEASE OF FIRST LIEN SECURITY INTEREST IN PATENTS PREVIOUSLY RECORDED AT REEL/FRAME (042477/0565);ASSIGNOR:ANTARES CAPITAL LP, AS ADMINISTRATIVE AND COLLATERAL AGENT;REEL/FRAME:047052/0001

Effective date: 20180906

Owner name: LTI HOLDINGS, INC., CALIFORNIA

Free format text: RELEASE OF SECOND LIEN SECURITY INTEREST IN PATENTS PREVIOUSLY RECORDED AT REEL/FRAME (042477/0643);ASSIGNOR:ANTARES CAPITAL LP, AS ADMINISTRATIVE AND COLLATERAL AGENT;REEL/FRAME:047223/0380

Effective date: 20180906

Owner name: LIFETIME INDUSTRIES, INC., CALIFORNIA

Free format text: RELEASE OF SECOND LIEN SECURITY INTEREST IN PATENTS PREVIOUSLY RECORDED AT REEL/FRAME (042477/0643);ASSIGNOR:ANTARES CAPITAL LP, AS ADMINISTRATIVE AND COLLATERAL AGENT;REEL/FRAME:047223/0380

Effective date: 20180906

Owner name: AAVID THERMAL CORP., NEW HAMPSHIRE

Free format text: RELEASE OF SECOND LIEN SECURITY INTEREST IN PATENTS PREVIOUSLY RECORDED AT REEL/FRAME (042477/0643);ASSIGNOR:ANTARES CAPITAL LP, AS ADMINISTRATIVE AND COLLATERAL AGENT;REEL/FRAME:047223/0380

Effective date: 20180906

Owner name: NUVENTIX, INC., NEW HAMPSHIRE

Free format text: RELEASE OF SECOND LIEN SECURITY INTEREST IN PATENTS PREVIOUSLY RECORDED AT REEL/FRAME (042477/0643);ASSIGNOR:ANTARES CAPITAL LP, AS ADMINISTRATIVE AND COLLATERAL AGENT;REEL/FRAME:047223/0380

Effective date: 20180906

Owner name: LTI FLEXIBLE PRODUCTS, INC., CALIFORNIA

Free format text: RELEASE OF SECOND LIEN SECURITY INTEREST IN PATENTS PREVIOUSLY RECORDED AT REEL/FRAME (042477/0643);ASSIGNOR:ANTARES CAPITAL LP, AS ADMINISTRATIVE AND COLLATERAL AGENT;REEL/FRAME:047223/0380

Effective date: 20180906

Owner name: AAVID THERMACORE, INC., NEW HAMPSHIRE

Free format text: RELEASE OF SECOND LIEN SECURITY INTEREST IN PATENTS PREVIOUSLY RECORDED AT REEL/FRAME (042477/0643);ASSIGNOR:ANTARES CAPITAL LP, AS ADMINISTRATIVE AND COLLATERAL AGENT;REEL/FRAME:047223/0380

Effective date: 20180906

Owner name: AAVID THERMALLOY, LLC, NEW HAMPSHIRE

Free format text: RELEASE OF SECOND LIEN SECURITY INTEREST IN PATENTS PREVIOUSLY RECORDED AT REEL/FRAME (042477/0643);ASSIGNOR:ANTARES CAPITAL LP, AS ADMINISTRATIVE AND COLLATERAL AGENT;REEL/FRAME:047223/0380

Effective date: 20180906

Owner name: AAVID NIAGARA, LLC, NEW HAMPSHIRE

Free format text: RELEASE OF SECOND LIEN SECURITY INTEREST IN PATENTS PREVIOUSLY RECORDED AT REEL/FRAME (042477/0643);ASSIGNOR:ANTARES CAPITAL LP, AS ADMINISTRATIVE AND COLLATERAL AGENT;REEL/FRAME:047223/0380

Effective date: 20180906

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION

AS Assignment

Owner name: CSI MEDICAL, INC., TENNESSEE

Free format text: RELEASE (REEL047028/FRAME0743);ASSIGNOR:ROYAL BANK OF CANADA;REEL/FRAME:068195/0243

Effective date: 20240729

Owner name: THERMAL CORP. (NOW KNOWN AS AAVID THERMAL CORP., NEW HAMPSHIRE

Free format text: RELEASE (REEL047028/FRAME0743);ASSIGNOR:ROYAL BANK OF CANADA;REEL/FRAME:068195/0243

Effective date: 20240729

Owner name: NUVENTIX, INC., NEW HAMPSHIRE

Free format text: RELEASE (REEL047028/FRAME0743);ASSIGNOR:ROYAL BANK OF CANADA;REEL/FRAME:068195/0243

Effective date: 20240729

Owner name: AAVID THERMALLOY, LLC (NOW KNOWN AS BOYD LACONIA, LLC, NEW HAMPSHIRE

Free format text: RELEASE (REEL047028/FRAME0743);ASSIGNOR:ROYAL BANK OF CANADA;REEL/FRAME:068195/0243

Effective date: 20240729

Owner name: LIFETIME INDUSTRIES, INC., CALIFORNIA

Free format text: RELEASE (REEL047028/FRAME0743);ASSIGNOR:ROYAL BANK OF CANADA;REEL/FRAME:068195/0243

Effective date: 20240729

Owner name: LTI FLEXIBLE PRODUCTS, INC., CALIFORNIA

Free format text: RELEASE (REEL047028/FRAME0743);ASSIGNOR:ROYAL BANK OF CANADA;REEL/FRAME:068195/0243

Effective date: 20240729