IP Library › Granted Patent US 12,531,226
Granted Patent B2
US 12,531,226 · App. 18/070,174 · Granted Jan 20, 2026

Apparatus for electrospray emission

Inventors: Louis Perna (Boston, MA); Christy Petruczok (Boston, MA); Alexander Bost (Boston, MA)
Assignee: Accion Systems, Inc.
H01J49/167B05B5/0255B05B5/0533H01J49/168
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Quick Facts
Patent No.
US 12,531,226
App. No.
18/070,174
Granted
Jan 20, 2026
Kind
B2
Abstract

An electrospray apparatus including a plurality of emitters, disposed on a substrate, wherein the plurality of emitters can have a narrow parameter distribution.

Claims (14)

1 . A satellite thruster chip apparatus comprising:

a first and a second emitter array, each comprising a plurality of substantially identical porous emitters, wherein each porous emitter of the plurality of substantially identical porous emitters has a concave lateral surface, wherein each porous emitter of the plurality of substantially identical porous emitters consists of silica, has a radius of curvature between about 4 and 6 μm, and comprises a substantially smooth surface; and

a power supply configured to apply a first voltage to working material within the first emitter array and to contemporaneously apply a second voltage to working material within the second emitter array.

2 . The satellite thruster chip apparatus of claim 1 , wherein each emitter comprises an apex comprising a first radius of curvature along a first reference axis and a second radius of curvature along a second reference axis.

3 . The satellite thruster chip apparatus of claim 1 , wherein a pore size of each emitter of the first emitter array is between about 60 and 250 nm.

4 . The satellite thruster chip apparatus of claim 1 , wherein a height of each emitter of the first emitter array is between about 200 and 750 μm.

5 . The satellite thruster chip apparatus of claim 1 , wherein the plurality of emitters of the first emitter array are arranged in a hexagonal grid, wherein an apex to apex separation distance between emitters arranged in the hexagonal grid is between about 40 and 500 μm.

6 . The satellite thruster chip apparatus of claim 1 , wherein the working material comprises an ionic liquid; wherein the working material wets the emitters.

7 . The satellite thruster chip apparatus of claim 1 , wherein a variance of a pore size of the emitters of each emitter array is at most 30% of a mean pore size of the respective emitter array.

8 . The satellite thruster chip apparatus of claim 1 , wherein a variance of a radius of curvature of an apex of the emitters of each emitter array is at most 30% of a mean radius of curvature of the respective emitter array.

9 . The satellite thruster chip apparatus of claim 1 , wherein each emitter array comprises at least 0.5 emitters per square millimeter.

10 . The satellite thruster chip apparatus of claim 1 , wherein each emitter array comprises a dielectric material.

11 . The satellite thruster chip apparatus of claim 1 , wherein the first voltage and second voltage comprise the same magnitude and opposite polarity.

12 . The satellite thruster chip apparatus of claim 2 , wherein the first radius of curvature of the apex and the second radius of curvature of the apex are not the same.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 28, 2022
From: PERNA, LOUIS; PETRUCZOK, CHRISTY; BOST, ALEXANDER
To: ACCION SYSTEMS, INC.
Reel/Frame 061894/0403 →
Continuity (4)
Division 16879540 · May 20, 2020
Provisional Application 62882294 · Aug 2, 2019
Provisional Application 62850907 · May 21, 2019
Related Publication 20230112566A1 · Apr 13, 2023
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