IP Library Granted Patent US 9,625,515
Granted Patent B2
US 9,625,515 · App. 14/300,214 · Granted Apr 18, 2017

Predicting the end of service life for a vacuum electron device

Inventors: John B. Overstreet (Los Gatos, CA); Michael J. Cascone (Sunnyvale, CA); John A. Lazar (Menlo Park, CA); Louis R. Falce (Surprise, AZ)
Assignee: COMMUNICATIONS & POWER INDUSTRIES LLC
G01R31/25
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Quick Facts
Patent No.
US 9,625,515
App. No.
14/300,214
Granted
Apr 18, 2017
Kind
B2
Abstract

The subject matter described herein generally relates to apparatus, systems, methods and associated computer instructions for predicting the end of service life of a space charge limited vacuum electron device. The device produces an electron beam current and has a cathode and a filament powered by an adjustable voltage power supply providing a voltage between a first low voltage and a second higher voltage to heat the cathode to an electron emitting temperature. The process includes periodically, while the device is in operation, adjusting the voltage provided by the power supply while monitoring the beam current, determining a knee-point in the voltage where the beam current begins to decrease as the voltage is decreased, and calculating, based on the determined knee-point and a predetermined voltage vs service life remaining relationship, the amount of service life left in the device.

Claims (46)

1. A method for predicting the end of service life of a space charge limited vacuum electron device producing an electron beam current and having a cathode and a filament powered by an adjustable voltage power supply providing a voltage between a first low voltage and a second high voltage to heat the cathode to an electron emitting temperature, the method comprising:

adjusting the voltage provided by the power supply while monitoring the beam current of the space charged limited vacuum electron device periodically, while the space charged limited vacuum electron device is in operation;

determining a knee-point in the voltage where the beam current of the space charged limited vacuum electron device begins to decrease as the voltage is decreased; and

calculating the amount of service life left in the space charged limited vacuum electron device based on the determined knee-point and a predetermined relationship between a filament voltage of the space charged limited vacuum electron device and the service life remaining for the space charged limited vacuum electron device.

2. The method of claim 1 , wherein the vacuum electron device is a travelling wave tube.

3. The method of claim 1 , wherein the vacuum electron device is a triode.

4. The method of claim 1 , wherein the vacuum electron device is a tetrode.

5. The method of claim 1 , wherein the cathode comprises barium.

6. The method of claim 1 , wherein the cathode comprises thoriated tungsten.

7. The method of claim 1 , wherein the cathode is a tungsten dispenser cathode.

8. The method of claim 1 , further comprising displaying the calculated amount of service life left in the device.

9. The method of claim 8 , wherein the displaying comprises displaying an estimated date of end of service life.

10. An apparatus for predicting the end of service life of a space charge limited vacuum electron device producing an electron beam current and having a cathode and a filament powered by an adjustable voltage power supply providing a voltage between a first low voltage and a second high voltage to heat the cathode to an electron emitting temperature, the apparatus comprising:

means for adjusting the voltage provided by the power supply while monitoring the beam current of the space charged limited vacuum electron device periodically, while the space charged limited vacuum electron device is in operation;

means for determining a knee-point in the voltage where the beam current of the space charged limited vacuum electron device begins to decrease as the voltage is decreased; and

means for calculating an amount of service life left in the space charged limited vacuum electron device based on the determined knee-point and a predetermined relationship between a filament voltage of the space charged limited vacuum electron device and the service life remaining for the space charged limited vacuum electron device.

11. The apparatus of claim 10 , wherein the vacuum electron device is a travelling wave tube.

12. The apparatus of claim 10 , wherein the vacuum electron device is a triode.

13. The apparatus of claim 10 , wherein the vacuum electron device is a tetrode.

14. The apparatus of claim 10 , wherein the cathode comprises barium.

15. The apparatus of claim 10 , wherein the cathode comprises thoriated tungsten.

16. The apparatus of claim 10 , wherein the cathode is a tungsten dispenser cathode.

17. The apparatus of claim 10 , further comprising means for displaying the calculated amount of service life left in the device.

18. The apparatus of claim 17 , wherein the means for displaying comprises means for displaying an estimated date of end of service life.

19. A system for predicting the end of service life of a space charge limited vacuum electron device producing an electron beam current and having a cathode and a filament powered by an adjustable voltage power supply providing a voltage between a first low voltage and a second high voltage to heat the cathode to an electron emitting temperature, the system comprising:

a circuit configured to measure the voltage;

a circuit configured to measure the beam current;

a circuit configured to adjust the voltage provided by the power supply while monitoring the beam current of the space charged limited vacuum electron device periodically, while the space charged limited vacuum electron device is in operation;

a processor configured to determine a knee-point in the voltage where the beam current of the space charged limited vacuum electron device begins to decrease as the voltage is decreased;

the processor further configured to calculate an amount of service life left in the space charged limited vacuum electron device based on the determined knee-point and a predetermined relationship between a filament voltage of the space charged limited vacuum electron device and the service life remaining for the space charged limited vacuum electron device; and

an output device for outputting a message indicative of the calculated remaining service life.

20. The system of claim 19 , wherein the vacuum electron device is a travelling wave tube.

21. The system of claim 19 , wherein the vacuum electron device is a triode.

22. The system of claim 19 , wherein the vacuum electron device is a tetrode.

23. The system of claim 19 , wherein the cathode comprises barium.

24. The system of claim 19 , wherein the cathode comprises thoriated tungsten.

25. The system of claim 19 , wherein the cathode is a tungsten dispenser cathode.

26. The system of claim 19 , wherein the output device is configured to output the calculated remaining service life as an estimated date of end of service life.

27. A computer program product for predicting the end of service life of a space charge limited vacuum electron device producing an electron beam current and having a cathode and a filament powered by an adjustable voltage power supply providing a voltage between a first low voltage and a second high voltage to heat the cathode to an electron emitting temperature, the computer program product comprising:

a computer readable storage medium having computer readable code embodied therewith, the computer readable code comprising:

computer readable program code configured to cause a circuit to measure the voltage;

computer readable program code configured to cause a circuit to measure the beam current;

computer readable program code configured to cause a circuit to adjust the voltage provided by the power supply while monitoring the beam current of the space charged limited vacuum electron device periodically, while the space charged limited vacuum electron device is in operation;

computer readable code configured to determine a knee-point in the voltage where the beam current of the space charged limited vacuum electron device begins to decrease as the voltage is decreased;

computer readable code configured to calculate an amount of service life left in the space charged limited vacuum electron device based on the determined knee-point and a predetermined relationship between a filament voltage of the space charged limited vacuum electron device and the service life remaining for the space charged limited vacuum electron device; and

computer readable code configured to cause an output device to output a message indicative of the calculated remaining service life.

Assignments (12)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 18, 2025
From: COMMUNICATIONS & POWER INDUSTRIES LLC; CPI INTERNATIONAL, INC.
To: COMMUNICATIONS & POWER INDUSTRIES INTERNATIONAL INC.
Reel/Frame 072051/0554 →
RELEASE OF SECURITY INTEREST Recorded Jun 10, 2024
From: ALTER DOMUS (US) LLC
To: COMMUNICATIONS & POWER INDUSTRIES LLC; CPI SATCOM & ANTENNA TECHNOLOGIES INC.; CPI RADANT TECHNOLOGIES DIVISION INC.; CPI ESSCO INC.
Reel/Frame 067678/0059 →
RELEASE OF FIRST LIEN SECURITY INTEREST (REEL 043349 / FRAME 0881) Recorded Oct 10, 2022
From: UBS AG, STAMFORD BRANCH
To: COMMUNICATIONS & POWER INDUSTRIES LLC; CPI RADANT TECHNOLOGIES DIVISION INC.; ASC SIGNAL CORPORATION; CPI MALIBU DIVISION
Reel/Frame 061639/0044 →
RELEASE OF SECOND LIEN SECURITY INTEREST (REEL 043349 / FRAME 0916) Recorded Oct 10, 2022
From: UBS AG, STAMFORD BRANCH
To: COMMUNICATIONS & POWER INDUSTRIES LLC; CPI RADANT TECHNOLOGIES DIVISION INC.; ASC SIGNAL CORPORATION; CPI MALIBU DIVISION
Reel/Frame 061639/0054 →
SECURITY AGREEMENT Recorded Oct 7, 2022
From: COMMUNICATIONS & POWER INDUSTRIES LLC; CPI SATCOM & ANTENNA TECHNOLOGIES, INC.; CPI RADANT TECHNOLOGIES DIVISION INC.; CPI ESSCO INC.
To: ALTER DOMUS (US) LLC, AS COLLATERAL AGENT
Reel/Frame 061623/0543 →
RELEASE OF SECURITY INTEREST Recorded Jul 26, 2017
From: UBS AG, STAMFORD BRANCH
To: COMMUNICATIONS & POWER INDUSTRIES LLC; ASC SIGNAL CORPORATION; CPI MALIBU DIVISION; CPI RADIANT TECHNOLOGIES DIVISION INC.
Reel/Frame 043349/0649 →
FIRST LIEN PATENT SECURITY AGREEMENT Recorded Jul 26, 2017
From: COMMUNICATIONS & POWER INDUSTRIES LLC; CPI RADIANT TECHNOLOGIES DIVISION INC.; ASC SIGNAL CORPORATION; CPI MALIBU DIVISION
To: UBS AG, STAMFORD BRANCH
Reel/Frame 043349/0881 →
SECOND LIEN PATENT SECURITY AGREEMENT Recorded Jul 26, 2017
From: COMMUNICATIONS & POWER INDUSTRIES LLC; CPI RADIANT TECHNOLOGIES DIVISION INC.; ASC SIGNAL CORPORATION; CPI MALIBU DIVISION
To: UBS AG, STAMFORD BRANCH
Reel/Frame 043349/0916 →
RELEASE OF SECURITY INTEREST Recorded Jul 26, 2017
From: UBS AG, STAMFORD BRANCH
To: COMMUNICATIONS & POWER INDUSTRIES LLC; CPI MALIBU DIVISION; CPI LOCUS MICROWAVE, INC.; CPI RADIANT TECHNOLOGIES DIVISION INC.; ASC SIGNAL CORPORATION
Reel/Frame 043358/0573 →
SECOND LIEN SECURITY AGREEMENT Recorded Mar 21, 2017
From: COMMUNICATIONS & POWER INDUSTRIES LLC; CPI MALIBU DIVISION; CPI LOCUS MICROWAVE, INC.; CPI RADANT TECHNOLOGIES DIVISION, INC.; ASC SIGNAL CORPORATION
To: UBS AG, STAMFORD BRANCH, AS COLLATERAL AGENT
Reel/Frame 042050/0862 →
SECURITY INTEREST Recorded Aug 24, 2015
From: COMMUNICATIONS & POWER INDUSTRIES LLC
To: UBS AG, STAMFORD BRANCH, AS COLLATERAL AGENT
Reel/Frame 036401/0537 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 3, 2014
From: OVERSTREET, JOHN B.; CASCONE, MICHAEL J.; LAZAR, JOHN A.; FALCE, LOUIS R.
To: COMMUNICATIONS & POWER INDUSTRIES LLC
Reel/Frame 033660/0698 →
Continuity (1)
Related Publication 20150355264A1 · Dec 10, 2015