System for throttling and compensation for variable feedstock properties

Apparatus is shown for adjusting the feed rate of pulverized feed material into a pressurized container. The apparatus also has utility for compensating for variations in the permeability of the feed material. A rotor that includes sprues with provision for controlling the pressure distribution along the sprues is located within the pressurized container. The rotor hub is connected to a drive means and a material supply means which extend through the wall of the container. A line for controlling pressure along the sprues by gas injection is connected to a chamber between sections of the sprue for controlling gas pressure at that point. The gas pressure control line is connected to a pressurized gas source and a control system external to the rotor. 10 figs.

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Publication Details

Journal
OSTI OAI (U.S. Department of Energy Office of Scientific and Technical Information)
Published
2024-11-11
Primary Topic
Rocket and propulsion systems research
Type
article
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article

System for throttling and compensation for variable feedstock properties

John W Meyer
OSTI OAI (U.S. Department of Energy Office of Scientific and Technical Information)
Rocket and propulsion systems research
article

System for throttling and compensation for variable feedstock properties

John W Meyer
article en

Abstract

Apparatus is shown for adjusting the feed rate of pulverized feed material into a pressurized container. The apparatus also has utility for compensating for variations in the permeability of the feed material. A rotor that includes sprues with provision for controlling the pressure distribution along the sprues is located within the pressurized container. The rotor hub is connected to a drive means and a material supply means which extend through the wall of the container. A line for controlling pressure along the sprues by gas injection is connected to a chamber between sections of the sprue for controlling gas pressure at that point. The gas pressure control line is connected to a pressurized gas source and a control system external to the rotor. 10 figs.

OSTI OAI (U.S. Department of Energy Office of Scientific and Technical Information)
Palo Alto Institute (US)
Rocket and propulsion systems research
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