Gas inlet for an ion thruster

Patent metadata

Field	Value
Publication number	US-2017316909-A1
Application number	US-201715581710-A
Country	US
Kind code	A1
Filing date	Apr 28, 2017
Priority date	Apr 29, 2016
Publication date	Nov 2, 2017
Grant date	—

Abstract

A gas inlet suitable in particular for use in an ion thruster includes a housing which is made of a gas-tight ceramics material, and an insert which is arranged in the housing and is made of a porous ceramics material. The geometry and pore structure of the insert are such that the insert forms a desired flow resistance for a gas stream flowing through the insert.

First claim

1 . A gas inlet for use in an ion thruster, comprising:
a housing made of a gas-tight ceramics material; and an insert which is arranged in the housing and made of a porous ceramics material, wherein a geometry and pore structure of the insert are configured such that the insert forms a desired flow resistance for a gas stream flowing through the insert.

2 . The gas inlet as claimed in claim 1 ,
wherein the geometry and pore structure of the insert are configured such that, at a given breakdown voltage, a product of a gas pressure of the gas stream flowing through the insert and an electrode gap lies within a predetermined range.

3 . The gas inlet as claimed in claim 2 ,
wherein, at a given breakdown voltage, the product of the gas pressure of the gas stream flowing through the insert and the electrode gap is either less than a lower threshold value or greater than an upper threshold value.

4 . The gas inlet as claimed in claim 3 ,
wherein a range of the product of the gas pressure of the gas stream flowing through the insert and the electrode gap that lies, at a given breakdown voltage, between the lower threshold value and the upper threshold value is a range that is suitable for permitting ignition of a fuel gas fed to the ion thruster by the gas inlet.

5 . The gas inlet as claimed in claim 1 ,
wherein the housing is made of an aluminum oxide material and/or wherein the insert is made of an aluminum oxide material.

6 . The gas inlet as claimed in claim 1 ,
wherein the insert is seated in the housing without a gap and/or without additional material.

7 . The gas inlet as claimed in claim 1 ,
which further comprises: a housing cover which is provided with a gas inlet opening for feeding a fuel gas from a fuel line into the gas inlet; and/or at least one gas outlet opening for removing a fuel gas from the gas inlet, wherein the at least one gas outlet opening is preferably formed in a lateral surface of the housing and/or wherein the at least one gas outlet opening is arranged in the region of an edge of the housing opposite the housing cover.

8 . A method for producing a gas inlet which is suitable in particular for use in an ion thruster, comprising:
producing a housing green body; producing an insert body; inserting the insert body into the housing green body; and jointly baking the housing green body and the insert body, wherein the baking cycle is so chosen that the housing green body sinters to form a housing made of a gas-tight ceramics material, and that an insert arranged in the housing and made of a porous ceramics material is produced from the insert body, the geometry and pore structure of which insert, after baking, is such that the insert forms a desired flow resistance for a gas stream flowing through the insert.

9 . The method as claimed in claim 8 ,
wherein the insert body is an insert green body which, when the housing green body and the insert body are jointly baked, sinters to form the insert arranged in the housing and made of a porous ceramics material, wherein the housing green body and/or the insert body in a form of an insert green body is/are produced by cold isostatic pressing.

10 . The method as claimed in claim 8 ,
wherein the insert body is a pre-baked porous insert body whose pore structure remains substantially identical when the housing green body and the insert body are jointly baked.

11 . The method as claimed in claim 8 ,
wherein the housing green body and/or the insert body is/are machined prior to baking, and/or wherein the housing green body and the insert body are baked at a temperature of approximately 1700° C.

12 . The method as claimed in claim 8 ,
wherein the housing is produced from an aluminum oxide material and/or wherein the insert is produced from an aluminum oxide material.

13 . The method as claimed in claim 8 ,
wherein the insert is seated in the housing without a gap and/or without additional material as a result of the joint baking of the housing green body and of the insert body.

14 . The method as claimed in claim 8 ,
wherein a housing cover which is provided with at least one gas inlet opening for feeding a fuel gas from a fuel line into the gas inlet is further fitted, in particular soldered, to the housing with the insert arranged therein.

15 . An ion thruster having a gas inlet for use in an ion thruster, the gas inlet comprising:
a housing made of a gas-tight ceramics material; and an insert which is arranged in the housing and made of a porous ceramics material, wherein a geometry and pore structure of the insert are configured such that the insert forms a desired flow resistance for a gas stream flowing through the insert.

Assignees

• Airbus Ds Gmbh

Inventors

• Pfeiffer Bernd
• Teuchner Reiner

Classifications

• H01J9/34

  Joining base to vessel · CPC title

• F03H1/0037

  Electrostatic ion thrusters · CPC title

• H01J27/022 Primary

  Details · CPC title

• F03H1/0012 Primary

  Means for supplying the propellant · CPC title

• C04B2237/84

  Joining of a first substrate with a second substrate at least partially inside the first substrate, where the bonding area is at the inside of the first substrate, e.g. one tube inside another tube · CPC title