Patent classifications
F28F23/00
HEAT EXCHANGER MODULE AND METHODS OF USING THEREOF
The invention provides in one embodiment a heat exchanger module (1) comprising a) a flexible support (100); b) at least one tubular member (200) having its main axis substantially parallel with the plane of the flexible support (100); c) a conductive flexible matrix (300) embedding the at least one tubular member (200); and d) a flexible case (400) enwrapping the flexible support (100), the at least one tubular member (200) and the conductive flexible matrix (300). A coating for a built environment comprising a plurality of heat exchanger modules (1) can be implemented, as well as a system further including pumping means (600). The invention also foresees a method for providing heat exchange processes between the heat exchanger module (1), the coating or the system of the invention and a built environment.
Heat storage material for the high-temperature range and method for the production thereof
The present invention relates to a material and process for producing water- and oxygen-free halogen salts of an alkali metal or alkaline earth metal, or of a transition metal, or of a metal of groups 13 or 14 of the Periodic Table, in which at least one halogen salt is heated with a heating rate of from 0.2 K/min to 30 K/min, especially from 1.0 K/min to 10 K/min, proceeding from room temperature.
Evaporative cooling system and device
An evaporative cooling system includes an indirect cooling coil containing a cooling fluid to be circulated and a blower assembly configured to generate an inlet air stream through the indirect cooling coil. The cooling fluid in the indirect cooling coil is a slurry of water and phase change material.
Evaporative cooling system and device
An evaporative cooling system includes an indirect cooling coil containing a cooling fluid to be circulated and a blower assembly configured to generate an inlet air stream through the indirect cooling coil. The cooling fluid in the indirect cooling coil is a slurry of water and phase change material.
AUXILIARY ENGINE ELECTRIC CAR HEATING SYSTEM
The invention relates to an auxiliary engine system (AES) for heating an electric car comprising a heating system and a rechargeable power source powering an electric motor. The AES comprises an internal combustion engine (ICE) producing heat to heat the electric car. The AES can heat people transported in the electric car and/or the rechargeable power source. The ICE can be coupled with an electric energy generator. The ICE can be air and/or liquid cooled which systems can heat the electric car. The ICE can be fueled by defined types of fuel. The ICE can be a two-stroke engine, a four-stroke engine, a turbine. The rechargeable power source can be coupled with a defined electrocomponent. The AES can be provided in a modular system. A heating method for an electric car is proposed.
AUXILIARY ENGINE ELECTRIC CAR HEATING SYSTEM
The invention relates to an auxiliary engine system (AES) for heating an electric car comprising a heating system and a rechargeable power source powering an electric motor. The AES comprises an internal combustion engine (ICE) producing heat to heat the electric car. The AES can heat people transported in the electric car and/or the rechargeable power source. The ICE can be coupled with an electric energy generator. The ICE can be air and/or liquid cooled which systems can heat the electric car. The ICE can be fueled by defined types of fuel. The ICE can be a two-stroke engine, a four-stroke engine, a turbine. The rechargeable power source can be coupled with a defined electrocomponent. The AES can be provided in a modular system. A heating method for an electric car is proposed.
Anhydrous heat transfer medium and application thereof
An anhydrous heat transfer medium, comprising any one or a combination of at least two of cis-1-chloro-3,3,3-trifluoropropene, cis-1,1,1,4,4,4-hexafluorobutene or perfluorobutane methyl ether. The heat transfer medium does not require an external device to perform work on the heat transfer medium during a heat transfer process, and is anhydrous, non-combustible, non-conductive and environmentally friendly.
Anhydrous heat transfer medium and application thereof
An anhydrous heat transfer medium, comprising any one or a combination of at least two of cis-1-chloro-3,3,3-trifluoropropene, cis-1,1,1,4,4,4-hexafluorobutene or perfluorobutane methyl ether. The heat transfer medium does not require an external device to perform work on the heat transfer medium during a heat transfer process, and is anhydrous, non-combustible, non-conductive and environmentally friendly.
THERMAL MANAGEMENT SYSTEM
A gas turbine engine includes a turbomachine and a thermal management system. The thermal management system includes a heat source heat exchanger configured to collect heat from the turbomachine during operation; a heat sink heat exchanger; and a thermal transport bus having a heat exchange fluid configured to flow therethrough at a pressure within an operational pressure range. The thermal management system defines an operational temperature range for the heat exchange fluid, the operational temperature range having a lower temperature limit less than about zero degrees Fahrenheit at a pressure within the operational pressure range and an upper temperature limit of at least about 1000 degrees Fahrenheit at a pressure within the operational pressure range.
THERMAL MANAGEMENT SYSTEM
A gas turbine engine includes a turbomachine and a thermal management system. The thermal management system includes a heat source heat exchanger configured to collect heat from the turbomachine during operation; a heat sink heat exchanger; and a thermal transport bus having a heat exchange fluid configured to flow therethrough at a pressure within an operational pressure range. The thermal management system defines an operational temperature range for the heat exchange fluid, the operational temperature range having a lower temperature limit less than about zero degrees Fahrenheit at a pressure within the operational pressure range and an upper temperature limit of at least about 1000 degrees Fahrenheit at a pressure within the operational pressure range.