Electrically-actuated valve and regulator for electrospray thrusters

Patent metadata

Field	Value
Publication number	US-11739714-B2
Application number	US-202117506411-A
Country	US
Kind code	B2
Filing date	Oct 20, 2021
Priority date	Dec 21, 2020
Publication date	Aug 29, 2023
Grant date	Aug 29, 2023

Abstract

Electrical propulsion systems and related methods are generally described. In some embodiments, an electrical propulsion system may include an electrically-actuated valve to selectively permit flow of propellant from a reservoir tank to a thruster. The valve may physically isolate the propellant from the thruster when inactivated, exhibiting a non-wetting surface which may inhibit propellant from passing through the valve towards the thrusters. In some embodiments, a valve may be activated through application of a voltage potential to the valve relative to the propellant, which may change the wettability of the valve, permitting propellant to wet and subsequently pass through the valve. The voltage potential may be adjusted to vary the wettability of the valve, resulting in the valve effectively regulating propellant flow rate. The valve may include a conductive layer, a dielectric or insulating layer, and a non-wetting layer to enhance the non-wetting behavior of the valve.

First claim

The invention claimed is:

1. A propulsion system comprising:
a reservoir tank configured to hold a propellant;
at least one thruster;
at least one valve positioned along a flow path between the reservoir tank and the at least one thruster, the at least one valve comprising:
one or more through holes extending from a first surface of the at least one valve to a second surface of the at least one valve, and
one or more channels fluidly connected to the one or more through holes; and

a first power source electrically connected to the propellant and the at least one valve,
wherein in a first operating mode the first power source is configured to apply a first voltage potential to the at least one valve relative to the propellant to inhibit propellant flow through at least a portion of the at least one valve, and wherein in a second mode of operation the first power source is configured to apply a second voltage potential to the at least one valve relative to the propellant to permit propellant flow through at least a portion of the at least one valve.

2. The propulsion system of claim 1 , wherein the one or more channels comprise a plurality of channels, and wherein the one or more through holes comprise a plurality of through holes.

3. The propulsion system of claim 1 , wherein the at least one valve comprises:
a conductive substrate comprising the one or more through holes and the one or more channels;
at least one dielectric layer disposed at least partially on the conductive substrate; and
at least one non-wetting layer disposed at least partially on the at least one dielectric layer,
wherein the propellant exhibits a larger contact angle on the at least one non-wetting layer than on the at least one dielectric layer and/or the conductive substrate.

4. The propulsion system of claim 1 , wherein the at least one valve comprises:
a conductive substrate comprising the one or more through holes and the one or more channels; and
at least one dielectric layer disposed at least partially on the conductive substrate,
wherein the propellant exhibits a non-wetting contact angle on the at least one dielectric layer.

5. The propulsion system of claim 1 , wherein the at least one valve comprises:
a substrate comprising the one or more through holes and the one or more channels;
at least one conductive layer disposed on one or more surfaces of each of the one or more through holes and/or one or more channels;
at least one dielectric layer disposed at least partially on the at least one conductive layer; and
at least one non-wetting layer disposed at least partially on the at least one dielectric layer,
wherein the propellant exhibits a larger contact angle on the at least one non-wetting layer than on the at least one dielectric layer and/or the at least one conductive layer.

6. The propulsion system of claim 1 , further comprising a second power source electrically connected to the propellant and the at least one thruster.

7. The propulsion system of claim 6 , further comprising one or more controllers configured to control the second power source to adjust a magnitude of the second voltage potential.

8. The propulsion system of claim 1 , further comprising a shunt resistor, wherein the first power source is connected to the at least one valve through the shunt resistor.

9. The propulsion system of claim 1 , further comprising a switch configured to selectively connect the first power source to the at least one valve.

10. A valve comprising:
a substrate;
one or more through holes extending from a first surface of the substrate to a second surface of the substrate;
one or more channels partially extending into the second surface of the substrate and fluidly connected to the one or more through holes; and
one or more layers disposed on at least a portion of the substrate including the one or more channels and/or the one or more through holes,
wherein the one or more layers are configured to electrically isolate the one or more through holes and the one or more channels from the substrate, and wherein the one or more layers are configured to provide a non-wetting surface on the one or more through holes and the one or more channels.

11. The valve of claim 10 , wherein the one or more layers comprise:
at least one dielectric layer; and
at least one non-wetting layer disposed at least partially on the at least one dielectric layer,
wherein a conductive liquid exhibits a larger contact angle on the at least one non-wetting layer than on the at least one dielectric layer.

12. The valve of claim 10 , wherein the substrate is formed of an electrically conductive and/or semiconducting material.

13. The valve of claim 10 , wherein the one or more layers comprise at least one layer configured to both electrically isolate the one or more through holes and the one or more channels from the substrate and provide the non-wetting surface on the one or more through holes and the one or more channels.

14. The valve of claim 10 , wherein the one or more channels comprise a plurality of channels, and wherein the one or more through holes comprise a plurality of through holes.

15. The valve of claim 10 , further comprising a power source electrically connected to the substrate and a conductive liquid disposed on the one or more layers.

16. The valve of claim 15 , wherein in a first operating mode the power source is configured to apply a first voltage potential to the substrate relative to the conductive liquid to inhibit the conductive liquid from flowing through at least a portion of the valve, and
wherein in a second mode of operation the power source is configured to apply a second voltage potential to the valve relative to the conductive liquid to permit the conductive liquid to flow through at least a portion of the valve.

17. The valve of claim 11 , wherein the conductive liquid is at least one selected from the group of an ionic liquid and a room temperature molten salt.

18. A method of operating a propulsion system, comprising:
applying a voltage potential to at least one valve relative to a propellant;
wetting one or more through holes extending from a first surface of the at least one valve to a second surface of the at least one valve in response to the applied voltage potential; and
wetting one or more channels in fluid communication with the one or more through holes,
wherein wetting the one or more through holes and wetting the one or more channels places the propellant in fluid communication with a thruster.

Assignees

• Massachusetts Inst Technology

Inventors

• Lozano Paulo C
• Freeman Dakota
• Macarthur Jonathan

Classifications

• F02K9/58 Primary

  Propellant feed valves · CPC title

• F16K13/00

  Other constructional types of cut-off apparatus (means for plugging pipes or hoses F16L55/10); Arrangements for cutting-off · CPC title

• F16K31/02

  electric {(F16K31/004 takes precedence)}; magnetic · CPC title

• F03H1/0012 Primary

  Means for supplying the propellant · CPC title

• F03H1/005

  using field emission, e.g. Field Emission Electric Propulsion [FEEP] · CPC title