IP Library Granted Patent US 8,129,913
Granted Patent B2
US 8,129,913 · App. 12/693,705 · Granted Mar 6, 2012

Closed electron drift thruster

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Quick Facts
Patent No.
US 8,129,913
App. No.
12/693,705
Granted
Mar 6, 2012
Kind
B2
Abstract

In a closed electron drift thruster, a magnetic circuit for creating a magnetic field in a main annular channel comprises at least one axial magnetic core surrounded by a first coil and an inner upstream pole piece forming a body of revolution, together with a plurality of outer magnetic cores surrounded by outer coils. The magnetic circuit further comprises an essentially radial outer first pole piece defining a concave inner peripheral surface and an essentially radial second pole piece defining a convex outer peripheral surface. The concave inner peripheral surface and the convex outer peripheral surface present respective adjusted profiles that are distinct from circular cylindrical surfaces so as to form between them a gap of varying width presenting zones of maximum value in register with the outer coils and zones of minimum value in between the outer coils so as to create a uniform radial magnetic field.

Claims (20)

1. A closed electron drift thruster comprising:

a main annular ionization and acceleration channel about an axis of the thruster;

at least one hollow cathode;

an annular anode concentric about the main annular channel;

a pipe and a manifold for feeding the anode with ionizable gas; and

a magnetic circuit for creating a magnetic field in said main annular channel;

said magnetic circuit comprising:

at least one axial magnetic core surrounded by a first coil and by an inner upstream pole piece forming a body of revolution; and

a plurality of outer magnetic cores surrounded by outer coils;

wherein said magnetic circuit further comprises an essentially radial outer first pole piece defining:

a concave inner peripheral surface; and

an essentially radial inner second pole piece defining a convex outer peripheral surface; and

wherein said concave inner peripheral surface and said convex outer peripheral surface present respective adjusted profiles that are distinct from circular cylindrical surfaces so as to form between them a gap of varying width presenting zones of maximum value in register with the outer coils, and zones of minimum value in between said outer coils, so as to create a uniform radial magnetic field.

2. A thruster according to claim 1 , wherein said inner upstream pole piece forming a body of revolution is essentially conical and defines a profiled peripheral margin at its free end that is closer to said cathode.

3. A thruster according to claim 2 , wherein said magnetic circuit further comprises an essentially conical outer upstream pole piece that defines a profiled peripheral margin at its free end closer to said cathode, and wherein said profiled peripheral margin of said essentially conical inner upstream pole piece forming a body of revolution and said profiled peripheral margin of said essentially conical outer upstream pole piece present respective adjusted profiles with portions set back along the axis of the thruster in register with the outer coils in such a manner as to keep the profile of the magnetic field constant in azimuth.

4. A thruster according to claim 1 , wherein said inner upstream pole piece forming a body of revolution comprises an essentially cylindrical inner magnetic shield defining a profiled peripheral margin at its free end close to said cathode.

5. A thruster according to claim 4 , wherein said magnetic circuit further comprises an essentially cylindrical outer magnetic shield that defines a profiled peripheral margin at its free end closer to said cathode, and wherein said profiled peripheral margin of said inner magnetic shield and said profiled peripheral margin of said outer magnetic shield present respective adjusted profiles with proportions set back along the axis of the thruster in register with the outer coils so as to keep the magnetic field profile constant in azimuth.

6. A thruster according to claim 1 , having four outer coils surrounding four outer magnetic cores.

7. A thruster according to claim 1 , having three outer coils surrounding three outer magnetic cores.

8. A thruster according to claim 1 , having two outer coils surrounding two outer magnetic cores.

Assignments (4)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 2, 2023
From: SAFRAN AIRCRAFT ENGINES
To: SAFRAN SPACECRAFT PROPULSION
Reel/Frame 065434/0105 →
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 17, 2010
From: DUCHEMIN, OLIVIER; VALENTIAN, DOMINIQUE
To: SNECMA
Reel/Frame 023947/0655 →