Additively manufactured components for electric propulsion thrusters
AssigneeBoard of Trustees of the University of Alabama, for and on behalf of the University of Alabama in Huntsville
InventorsKunning Gabriel Xu, Sydney D. Miller
Life of this patent
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Abstract
A Hall effect thruster is provided having one or more components fabricated using additive manufacturing techniques. Additive manufacturing can be used to fabricate the magnetic flux guide and the discharge channel of the thruster. In addition, the propellant distributor for the thruster can be incorporated into the base of the discharge channel. The magnetic flux guide can be fabricated with a filament impregnated with a magnetic material and the discharge channel can be fabricated with a filament impregnated with a ceramic material. Permanent magnets can be positioned in the magnetic flux guide at locations that surround the discharge channel.
Claims7
A method for manufacturing a Hall effect thruster, the method comprising:
- developing a model of a magnetic flux guide of a Hall effect thruster;
- selecting a filament to be used to fabricate the magnetic flux guide, wherein the selecting includes selecting a magnetic material impregnated filament for the magnetic flux guide;
- identifying a desired shape of a magnetic field generated by the magnetic flux guide;
- printing, with an additive manufacturing system, the magnetic flux guide with the selected filament;
- and
- causing the printing to incorporate a functional grading into the magnetic flux guide by changing a density of the selected filament used in the printing such that the shape of the magnetic field generated by the magnetic flux guide is tailored to the desired shape.
A method for manufacturing a Hall effect thruster, the method comprising:
- developing a model of a component of a Hall effect thruster, wherein the component of the Hall effect thruster includes one of a magnetic flux guide or a discharge channel;
- selecting a filament to be used to fabricate the component of the Hall effect thruster, wherein selecting a filament includes selecting a magnetic material impregnated filament for the magnetic flux guide or selecting a ceramic impregnated filament for the discharge channel;
- adjusting at least one setting of an additive manufacturing system based on the selected filament for the component of the Hall effect thruster, wherein adjusting at least one setting includes adjusting a print speed of the additive manufacturing system based on the selected filament;
- and
- printing, with the additive manufacturing system, the component according to the adjusted at least one setting of the additive manufacturing system with the selected filament,
- wherein the magnetic material impregnated filament is an iron impregnated filament and the ceramic impregnated filament is a zirconium oxide impregnated filament or a zirconium silicate impregnated filament.
A method for manufacturing a Hall effect thruster, the method comprising:
- developing a model of a component of a Hall effect thruster, wherein the component of the Hall effect thruster includes one of a magnetic flux guide or a discharge channel;
- selecting a filament to be used to fabricate the component of the Hall effect thruster, wherein selecting a filament includes selecting a magnetic material impregnated filament for the magnetic flux guide or selecting a ceramic impregnated filament for the discharge channel:
- adjusting at least one setting of an additive manufacturing system based on the selected filament for the component of the Hall effect thruster, wherein adjusting at least one setting includes adjusting a print speed of the additive manufacturing system based on the selected filament;
- and
- printing, with the additive manufacturing system, the component according to the adjusted at least one setting of the additive manufacturing system with the selected filament,
- wherein the magnetic material impregnated filament has about 25% magnetic material to about 85% magnetic material, wherein the ceramic impregnated filament has about 25% ceramic to about 85% ceramic, wherein the magnetic material impregnated filament has about 80% iron, and wherein the ceramic impregnated filament has about 55% zirconium silicate.
Dependencies are inferred from the claim text.