Discharge chamber of an ion drive, ion drive having a discharge chamber, and a diaphragm for being affixed in a discharge chamber of an ion drive

Patent metadata

Field	Value
Publication number	US-10184459-B2
Application number	US-201715486114-A
Country	US
Kind code	B2
Filing date	Apr 12, 2017
Priority date	Apr 12, 2016
Publication date	Jan 22, 2019
Grant date	Jan 22, 2019

Abstract

A discharge chamber of an ion drive, an ion drive having a discharge chamber, and a diaphragm for being affixed in a discharge chamber of an ion drive. The discharge chamber comprises a diaphragm, wherein the diaphragm of the discharge chamber comprises a magnet and is disposed and/or affixed in the discharge chamber.

First claim

The invention claimed is:

1. A discharge chamber of an ion drive, the discharge chamber comprising:
an ionization region;
a diaphragm having a diaphragm hole which is vacant and located at a center of said diaphragm for ions from said ionization region to pass therethrough, and wherein said diaphragm is disposed in the discharge chamber so as to increase an ionization efficient in said ionization region
said diaphragm further comprising a magnet affixed to said diaphragm and disposed in the discharge chamber, wherein the magnet is configured for constricting a magnetic field in a direction perpendicular to a common axis of rotation of at least two of the ion drive, the discharge chamber, and the diaphragm, and
wherein the common axis of rotation is defined by an essential exit direction of a thrust generating ion beam.

2. The discharge chamber according to claim 1 , wherein the diaphragm is magnetic, or wherein the magnet comprises a magnet array that is affixed on the diaphragm, or both.

3. The discharge chamber according to claim 1 , wherein the diaphragm is circular and the magnet comprises at least one circular magnet ring.

4. The discharge chamber according to claim 1 , wherein the outer dimension of the diaphragm is coordinated with the discharge chamber and the inner dimension of the diaphragm does not go below a predetermined threshold value.

5. The discharge chamber according to claim 3 , wherein one of the at least one circular magnet rings is disposed along the diaphragm hole.

6. An ion drive having a discharge chamber according to claim 1 .

7. The discharge chamber according to claim 1 , wherein the inner dimension of the diaphragm is a radius or a diameter of the diaphragm hole.

8. The discharge chamber according to claim 1 , wherein the outer dimension of the diaphragm is a radius or a diameter of the diaphragm.

9. The discharge chamber according to claim 1 , wherein the outer dimension is a cross section of the diaphragm.

Assignees

• Airbus Ds Gmbh

Inventors

• Hey Franz Georg
• Kornfeld Guenter
• Johann Ulrich

Classifications

• F03H1/0006 Primary

  Details applicable to different types of plasma thrusters (arrangements specially adapted for fitting plasma engines in or to cosmonautic vehicles B64G1/413) · CPC title

• B64G1/405

  Operations & Transport · mapped topic

• F03H1/0037 Primary

  Electrostatic ion thrusters · CPC title

• H05H1/54

  Plasma accelerators · CPC title

• B64G1/413

  Ion or plasma engines · CPC title