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Aerodynamic separation nozzle

a technology of aerodynamic separation and nozzle, which is applied in the direction of steam engine plants, refrigeration machines, lighting and heating apparatus, etc., can solve the problems of differential drag force, inapplicability, and high production cost of these tiny nozzles, and achieves improved mach velocity, increased centrifugal effect, and improved pressure diffusion and consequently gas velocity performan

Inactive Publication Date: 2013-07-11
TENOROC
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

The patent describes a nozzle design that improves the performance of a separation process by cooling the body of the nozzle. This reduces shock effects and increases the velocity of the process gas within the nozzle, enhancing the separation effects. The cooled nozzle can also be combined with pre-conditioned or cooled process gas to further improve performance. This design can be used in various thermodynamic cycles, eliminating the need for certain devices such as evaporators and condensers, and preventing deleterious effects on turbines. The patent also provides examples of improved routing for such cycles.

Problems solved by technology

Production of these tiny nozzles by manufacturing is technically demanding, and the overall process typically includes stages having multiple vessels containing hundreds of separation elements, gas distribution manifolds, gas coolers to remove the heat of compression, and centrifugal compressors to pressurize the flow.
Second, the lighter balance gas exerts a differential drag force on the heavier and lighter isotopes.
As a result of these requirements and design constraints, the Becker process nozzle has a number of significant limitations that have reduced its applicability to general purpose gas separation including:1. The small size of the curvature wall requires that the nozzle and skimmer components are also minute in size, requiring the components be made of foil material and bonded to assemble even one nozzle.
Due to the small degree of separation caused by a single probe, the method has not progressed to any commercial degree.

Method used

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third embodiment

[0206]In a third embodiment, the process gas also includes a substantially liquid constituent that passes the skimmer 112 into the deflection diffuser 104 and remains liquid as it passes through the deflection diffuser 104 and passes external to the separation nozzle. In this manner a portion of the heavier species of the process gas that are separated by the separation nozzle are recovered in liquid form suitable for use as part of a refrigerant system.

[0207]The CFD results depicted in FIGS. 7d and 8b with respect to an embodiment of a type-2 nozzle 200 detail the effect of a pre-conditioned, or in this embodiment a cooled process gas entering a cooled type-2 nozzle 200. FIG. 8b is a depiction of CFD results of the static temperature of a process gas going through an embodiment of a Type-2 nozzle 200 having the inlet gas pressure of 29 psig and an inlet gas temperature of 434° R. It can be seen at point 827 where T=434°, that the gas enters the inlet gas reservoir 106 and continues...

first embodiment

[0272]a multi-stage, single source, separation loop assembly whereby raw feed gas is introduced at only a single stage 2400, also described as a source separation loop 2500, is depicted in FIG. 22. In the schematic of the source separation loop 2500, the elements of the stage 2400 are simplified into a schematic compressor 2502 and a the stage nozzle module 2190. The schematic compressor 2502 generally in the case of the stage 2400 embodiment described in FIG. 21, comprises the following elements: (a) compressor vessel2420; (b) compressor 2410; (c) pulse vessel 2404; (d) the valves interconnected each of the aforementioned elements (e.g., the nozzle valve 2402); and, (e) sensors (e.g., the temperature sensor 2432). Effectively, the schematic compressor 2502 represents all elements of the stage 2400 external to the stage nozzle module 2190 or the outlet manifold of the stage nozzle module 2190. Each stage 2400 present in the source separation loop 2500 is labeled from the stage 2400 ...

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Abstract

Multiple designs and methods for aerodynamic separation nozzles and systems for integrating multiple aerodynamic separation nozzles into a single system are disclosed herein. These aerodynamic separation nozzles utilize a combination of aerodynamic forces and separation nozzle structure to induce large centrifugal forces on the fluids that in combination with the structure of the nozzle are used to separate heavier constituents of the fluid from lighter constituents, and more particularly to separate a first or liquid phase from gaseous phases. In some embodiments a number of separation nozzles are combined into a single system suitable for dynamic processing of a process gas. In other embodiments the separation nozzles are temperature controlled to condition the incoming gas to a temperature in order to encourage a phase change in certain constituents of the gas to occur within the nozzle to further enhance separation.

Description

CROSS-REFERENCE TO RELATED APPLICATIONS[0001]This application claims the benefit of U.S. Provisional Application 61 / 563,301, filed Nov. 23, 2011; U.S. Provisional Application 61 / 583,853, filed Jan. 6, 2012; and U.S. Provisional Application 61 / 590,580, filed Jan. 25, 2012. Each patent application identified above is incorporated here by reference in its entirety to provide continuity of disclosure.TECHNICAL FIELD[0002]The subject matter described herein relates to devices, systems, and methods related to the separation and concentration or depletion of various constituents of a flow or gas, including gas species, particles, phase separation within the same specie of fluid, the separation of compressible fluids from non compressible fluids, and so forth.BACKGROUND[0003]Aerodynamic separation of gas constituents is useful for a number of industrial and commercial applications. An aerodynamic separation nozzle, or, as used herein, a separation nozzle, uses aerodynamic effects and forces...

Claims

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Application Information

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Patent Type & Authority Applications(United States)
IPC IPC(8): F25B43/00
CPCF01K25/08F25B43/00F25B2400/23
Inventor BLOOM, MICHAEL R.
Owner TENOROC
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