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Injection system and method for injecting cylindrical array of discrete liquid jets

A jet system, liquid jet technology, applied in the direction of using plasma, fluid flow, plasma, etc., can solve the problems of not being able to apply the pulse fusion propulsion system, time-consuming, etc.

Active Publication Date: 2018-08-14
THE BOEING CO
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Building new z-pinch reactions using metal wires is a time-consuming process
Furthermore, z-pinch reactions using metal wires cannot be applied to pulsed fusion propulsion systems, which require the repeated introduction of new columns of conductive material between the anode and cathode, and the application of current pulses to each new column.

Method used

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  • Injection system and method for injecting cylindrical array of discrete liquid jets
  • Injection system and method for injecting cylindrical array of discrete liquid jets
  • Injection system and method for injecting cylindrical array of discrete liquid jets

Examples

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Embodiment Construction

[0026] Referring now to the drawings, in which the illustrations are for purposes of illustrating the preferred embodiment and various embodiments of the present disclosure, figure 1 Illustrated in is an example of an injection system 150 for injecting a cylindrical array of liquid jets 286 into an injection zone 252 as disclosed herein. The injection system 150 includes a reservoir 152 for holding a liquid 158 such as molten metal. The reservoir may include a piston 168 for applying pressure to the liquid 158 . Additionally, the spray system 150 includes a motor 242 for rotating a gate control plate 216 located at the end 164 of the reservoir. Injection system 150 may include planetary gears 226 for maintaining gate control plate 216 centered on central axis 222 during rotation. The gate plate includes a circular array of gate plate holes 218 and is rotated by a motor 242 under the command of a controller 248 to selectively allow fluid 158 from a reservoir 152 to pass throu...

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PUM

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Abstract

An injection system includes a reservoir for containing liquid, and a gating plate having a circular array of gating plate apertures. The injection system additionally includes a faceplate positionedadjacent to the gating plate and having a circular array of faceplate orifices. The injection system also has a motor to rotate the gating plate, and a controller to control the motor for rotating thegating plate into an aligned clocking orientation in which the gating plate apertures and the faceplate orifices are aligned to initiate the formation of a cylindrical array of liquid jets, and rotate the gating plate into a non-aligned clocking orientation terminate formation of the liquid jets after a predetermined discrete quantity of the liquid is injected.

Description

technical field [0001] The present disclosure relates generally to liquid ejectors, and more particularly, to an ejector system and method for repeatably ejecting liquid in discrete quantities to repeatably form a cylindrical array of liquid jets capable of conducting electrical current. Background technique [0002] Fusion propulsion holds the potential for interplanetary space travel on human-practical timescales. One way of fusion propulsion is the z-pinch plasma approach, in which high-amplitude current pulses are passed through a column of conductive material extending between the anode and cathode of a z-pinch device. Over a relatively short period of time (for example, 10 -6 seconds), the current heats the material into a high-temperature plasma and generates a magnetic flux that interacts with the current, resulting in the Lorentz force that compresses the plasma radially to a very high density. The hot plasma can expand in the nozzle and be expelled to generate pr...

Claims

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Application Information

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IPC IPC(8): B64G1/40F03H1/00B05B5/057B05B5/16
CPCB05B5/057B05B5/16B64G1/40B64G1/405F03H1/0006F15D1/08H05H1/06H05H1/54F03H1/0081F03H1/0012Y02E30/10B64G1/408
Inventor J·S·安德森E·R·吉什
Owner THE BOEING CO
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