Method for cooling air and devices

摘要

A method of constructing self-powered air-conditioner comprises a convergent divergent nozzle where powered fan pushes air into said nozzle. While the pushed air accelerates toward the nozzle throat it becomes colder as air internal energy transformed into kinetic energy. An axial turbine installed within the nozzle throat extracts energy from the air in the nozzle and drives an electrical generator that provides electricity to the fan electric motor. Alternatively the turbine and fan are installed on common shaft, which could be the electric generator shaft. The cold air within the nozzle throat cools the nozzle throat skin, which serves as air-conditioner core. The cold nozzle skin is wrapped with coiled pipes in which liquid flows, becomes colder and this cold liquid flows away to heat exchanger where air is flowing through it and becomes colder. This cold air is then flows into spaces needed to be air-conditioned.

主权项

1. A device for producing useful power by converting the internal energy of air that enters said device and flows through it into useful power that is greater than the kinetic energy per second of the airflow entering said device, said device comprising:
a) a nozzle comprising:
i) a nozzle inlet;ii) a nozzle throat; andiii) a nozzle exit; b) a fan or compressor powered by a source of energy to generate airflow into said nozzle; c) a rotor comprised of a hub to which a plurality of blades are attached designed to produce power out of airflow kinetic energy; d) a rotor shaft that rotates with said hub attached to said rotor hub, said rotor shaft adapted to transfer said rotor output power to a mechanism that generates said useful power; e) a heat exchanger installed at the nozzle throat, or near this throat, wherein fluid that flows in this heat exchanger provides heat to the air flowing within said nozzle; f) a heat exchanger installed in a space such that fluid that flows in this heat exchanger collects heat from the space and that heat is transferred to said nozzle throat heat exchanger; wherein:
said rotor is installed inside said nozzle near said nozzle throat;airflow entering said nozzle inlet flows in the direction of said nozzle exit, impacts on said rotor blades, continues to flow towards said nozzle exit, and exits said nozzle;the cross-sectional area of said nozzle inlet is larger than the cross-sectional area of said nozzle throat, thereby causing the speed of said airflow to increase and its temperature to decrease as it flows towards said throat, so that the kinetic energy of the air in said airflow at said nozzle throat is larger than the kinetic energy of the air in said airflow at said nozzle inlet by essentially the difference between the internal energy thermal part (Cp:T) of the air in said airflow at said nozzle inlet and the internal energy thermal part (Cp:T) of the air in said airflow at said nozzle throat; andwhen said airflow impacts upon said rotor blades, part of said kinetic energy of said airflow is transferred to said rotor blades in the form of aerodynamic force pushing against said blades causing said rotor and said rotor shaft to rotate, thereby transforming part of said kinetic energy of said airflow to work done on said rotor per unit time, which said rotor shaft transfers to said mechanism that generates said useful power;said rotor device being characterized by the number of blades and the aerodynamic cross sections of said blades that are defined by airfoil, blade inlet angles and blade exit angles, whose parameters are chosen such as to generate an amount of power which is greater than the kinetic energy per second of the airflow in said nozzle inlet;and said nozzle and said rotor are designed such that the local speed of the airflow is accelerated to at least a speed of Mach number equal to 0.2;
wherein fluid that flows in this nozzle throat heat exchanger provides heat to the air flowing within said nozzle; andwherein said fluid inside nozzle throat heat exchanger flows into the heat exchanger in the space and collects heat from the space, thus increasing the amount of power generated by the turbine.