Patent application number | Description | Published |
20080229780 | System and Method for Separating Components of a Fluid Coolant for Cooling a Structure - According to one embodiment of the invention, a cooling system for a heat-generating structure includes a heating device, a cooling loop, and a separation structure. The heating device heats a flow of fluid coolant including a mixture of water and antifreeze. The cooling loop includes a director structure which directs the flow of the fluid coolant substantially in the form of a liquid to the heating device. The heating device vaporizes a substantial portion of the water into vapor while leaving a substantial portion of the antifreeze as liquid. The separation structure receives, from the heating device, the flow of fluid coolant with the substantial portion of the water as vapor and the substantial portion of the antifreeze as liquid. The separation structure separates one of the substantial portion of the water as vapor or the substantial portion of the antifreeze as liquid from the cooling loop while allowing the other of the substantial portion of the water as vapor or the substantial portion of the antifreeze as liquid to remain in the cooling loop. | 09-25-2008 |
20090008063 | System and Method for Passive Cooling Using a Non-Metallic Wick - According to an embodiment of the invention, a cooling system for a heat-generating device comprises a base plate, a fluid transfer chamber, a non-metallic wicking material, and a coolant. The base plate is in thermal communication with a heat generating structure and is operable to communicate thermal energy from the heat-generating device. The non-metallic wicking material and the coolant are disposed within the fluid transfer chamber. The non-metallic wicking material wicks a portion of the coolant towards a portion of the base plate communicating the thermal energy. The portion of the coolant absorb at least a portion of the thermal energy communicated from the heat-generating device. The coolant comprising at least an alcohol and at least one additional fluid. | 01-08-2009 |
20090020266 | System and Method of Boiling Heat Transfer Using Self-Induced Coolant Transport and Impingements - According to one embodiment of the invention, a cooling system for a heat-generating structure comprises a chamber and structure disposed within the chamber. The chamber has an inlet and an outlet. The inlet receives fluid coolant into the chamber substantially in the form of a liquid. The outlet dispenses the fluid coolant out of the chamber at least partially in the form of a vapor. The structure disposed within the chamber receive thermal energy from the heat generating structure and transfers at least a portion of the thermal energy to the fluid coolant. The thermal energy from the heat-generating structure causes at least a portion of the fluid coolant substantially in the form of a liquid to boil and effuse vapor upon contact with a portion of the structure. The effusion of vapor creates a self-induced flow in the chamber. The self-induced flow distributes non-vaporized fluid coolant substantially in the form of a liquid to other portions of the structure. | 01-22-2009 |
20090071630 | Cooling System for High Power Vacuum Tubes - According to one embodiment, a two-phase cooling system includes a condensing heat exchanger fluidly coupled to an evaporator assembly and a pressure controller. The condensing heat exchanger condenses a coolant from a vapor phase to a liquid phase by removing heat from the coolant. The evaporator assembly is thermally coupled to a vacuum tube and operable to receive liquid coolant from the condensing heat exchanger, cool the vacuum tube by evaporating the coolant from the liquid phase to the vapor phase, and transporting the evaporated coolant to the condensing heat exchanger. The pressure controller maintains the pressure of the coolant in the evaporator assembly at a sub-ambient pressure to lower the boiling point of the coolant for reducing the operating temperature of the vacuum tube. | 03-19-2009 |
20090101311 | System and Method for Cooling Using Two Separate Coolants - According to one embodiment, a cooling system for a heat-generating structure includes a first cooling loop that directs a flow of a first fluid coolant from a heat-generating structure to a first heat exchanger. The system also includes a second cooling loop that directs a flow of a second fluid coolant from the first heat exchanger to a second heat exchanger. The first heat exchanger receives thermal energy from the first fluid coolant and transfers at least a portion of the thermal energy to the second fluid coolant. The first fluid coolant has a specific heat and a mass flow rate, and the second fluid coolant has a specific heat and a mass flow rate. A product of the specific heat and the mass flow rate of the first fluid coolant is greater than a product of the specific heat and the mass flow rate of the second fluid coolant. | 04-23-2009 |
20090107663 | System and Method for Cooling Structures Having Both an Active State and an Inactive State - According to one embodiment, a cooling system for heat-generating structures comprises a cooling loop and a heat exchanger. The cooling loop directs a flow of a fluid coolant to both an active heat-generating structure and an inactive heat-generating structure. The fluid coolant receiving thermal energy from the active heat-generating structure and transfers thermal energy to the inactive heat-generating structure when a temperature of the fluid coolant is greater than an ambient temperature of an environment surrounding the heat-generating structures. The active heat-generating structure is operable to switch to an inactive state and the inactive heat-generating structure is operable to switch to an active state. The heat exchanger is in thermal communication with the first and second heat-generating structures and is operable to receive the fluid coolant at a first temperature and dispense of the fluid coolant out of the heat exchanger at a second temperature. | 04-30-2009 |
20090242170 | Cooling Fins for a Heat Pipe - According to one embodiment, a cooling apparatus has a number of cooling fins that are coupled to a heat pipe. The heat pipe has a hollow cavity that is at least partially filled with a refrigerant. Each of the cooling fins has a hollow cavity that is fluidly coupled to the hollow cavity of heat pipe such that the refrigerant may flow between the hollow cavity of the heat pipe and hollow cavities of the cooling fins. | 10-01-2009 |
20090244829 | Heat Removal System for Computer Rooms - According to one embodiment, a heat removal system for a computer room includes a heat pipe having two ends. One of the ends is thermally coupled to one or more of a number of components forming a portion of a computing system. The other end is thermally coupled to a heat dissipation mechanism. The heat pipe is operable to move heat from the components of the computing system to the heat dissipation mechanism. | 10-01-2009 |
20090244830 | Systems and Methods for Cooling a Computing Component in a Computing Rack - According to one embodiment, a system for cooling computing components includes a computing rack housing a plurality of computing components of a computing system. A heat absorbing plate is disposed in and removable from the computing rack. The heat absorbing plate is thermally coupled to an outer surface of a computing component and comprises a plurality of walls defining a cavity containing a two-phase coolant. The cavity has a continuous volume allowing the two-phase coolant to absorb heat from the computing component and to transfer the heat to a heat transfer mechanism. The computing rack has a sidewall that is thermally coupled to the heat absorbing plate and comprises the heat transfer mechanism, which is operable to receive the heat transferred from the heat absorbing plate. | 10-01-2009 |
20100089461 | Removing Non-Condensable Gas from a Subambient Cooling System - In certain embodiments, removing non-condensable gas from a cooling system includes trapping contents of a discharge tube of a heat exchanger, where the heat exchanger is in thermal communication with an ambient environment at an ambient temperature. The contents of the discharge tube comprises a vapor portion of a cooling fluid, a liquid portion of the cooling fluid, and a non-condensable gas. The cooling fluid is at a subambient pressure, and the ambient temperature is lower than a boiling point of the cooling fluid. A first additional portion of the cooling fluid is inlet into the discharge tube to increase a pressure within the discharge tube. The vapor portion of the cooling fluid within the discharge tube is allowed to condense. A second additional portion of the cooling fluid is inlet to purge the non-condensable gas from the discharge tube. | 04-15-2010 |
20100206523 | INTERNAL COOLING SYSTEM FOR A RADOME - According to one embodiment, a radome includes two dielectric layers separated by an internal layer. The internal layer is configured with an internal cooling system including a fluid channel that receives a fluid through an inlet port, conducts heat from the radome to the fluid, and exhausts the heated fluid through an outlet port. | 08-19-2010 |
20110157828 | Method And Apparatus for Cooling Electronics with a Coolant at a Subambient Pressure - According to one embodiment of the invention, a method is provided for cooling heat-generating structure disposed in an environment having an ambient pressure. The heat-generating structure includes electronics. The method includes providing a coolant, reducing a pressure of the coolant to a subambient pressure at which the coolant has a boiling temperature less than a temperature of the heat-generating structure, and bringing the heat-generating structure and the coolant at the subambient pressure into contact with one another, so that the coolant boils and vaporizes to thereby absorb heat from the heat-generating structure. In a more particular embodiment the coolant is either pure water or pure methanol with an electrical resistivity level of greater than one million Ohms-cm. Further, in another particular embodiment the method includes filtering the coolant to maintain its purity above a particular level. | 06-30-2011 |
20120227949 | AERODYNAMIC HEAT EXCHANGE STRUCTURE - The present invention relates to heat exchangers, and more particularly to a heat exchange structure configured to operate in an air stream. In one embodiment, a heat exchange structure configured to operate in an air stream includes coolant flow portions, each of the coolant flow portions having at least one substantially closed surface directed into the air stream; and air flow portions disposed between adjacent coolant flow portions for receiving air from the air stream, the air flow portions having air passages directed into the air stream; the substantially closed surface of the coolant flow portions having an aerodynamic shape. | 09-13-2012 |
20120227950 | FREE AIR STREAM HEAT EXCHANGER DESIGN - The present invention relates to heat exchangers, and more particularly to a heat exchange apparatus configured to operate in a free air stream. In an embodiment, a heat exchange apparatus configured to operate in a free air stream includes a heat exchange structure having a shape configured to conform to a body of a vehicle when in a stowed condition; and a deployment mechanism for moving the heat exchange structure to a deployed condition external to the vehicle. The heat exchange structure has a curved surface that is concave into the air stream when the heat exchange structure is in the deployed condition. | 09-13-2012 |
20140037423 | RAM AIR TURBINE OVERSPEED PROTECTION - A power generation system includes a ram air turbine that is connected to a generator. The power generation system may be located in a pod, for example a pod for mounting on an aircraft. The ram air turbine receives air that passes through an air path through the pod, going in through an air inlet, through the turbine to turn the turbine, and out through an air outlet. The system includes a deployable flow obstruction, such as one or more airbags, that are deployable to suddenly obstruct the flow through the air path. The obstruction may be used to cut off flow (or greatly reduce flow), when overspeed of the ram air turbine is detected. The obstruction deploys (for example, airbags deploy in an air inlet of the system) to prevent continuation of the overspeed operation of the turbine, which may damage parts of the system. | 02-06-2014 |
20140216088 | AIRCRAFT THERMAL MANAGEMENT SYSTEM FOR COOLING USING EXPENDABLE COOLANTS - A system for cooling an aircraft includes a fuel tank, a fuel delivery system, a cooling system, and a heat exchanger. The fuel tank is configured to hold cooled fuel for the aircraft. The fuel delivery system is configured to provide at least a portion of the fuel from the fuel tank to an engine of the aircraft. The cooling system is configured to absorb heat generated by components on the aircraft. The heat exchanger is thermally connected to the fuel delivery system and the cooling system. The heat exchanger is configured to transfer at least a portion of the heat from the components on the aircraft to the cooled fuel. The system may further include a two or three phase expendable liquid system. The expendable liquid system is configured to transfer heat to a frozen or liquid coolant to vaporize and expend the coolant from the aircraft. | 08-07-2014 |