Multifunction circuit continuity and sensor tester

• US 6,653,846 B2
• Filed: 09/14/2001
• Issued: 11/25/2003
• Est. Priority Date: 09/14/2001
• Status: Expired due to Fees

• Current Assignee: Eaton Corp. (Wisconsin) (Eaton Corporation PLC.)
• Original Assignee: Eaton Corp. (Wisconsin) (Eaton Corporation PLC.)
• Inventors: James, Rolland T.
• Primary Examiner(s): Deb, Anjan K.
• Application Number:
  US09/952,345
• Publication Number:
  US 20030052697A1
• Time in Patent Office: 802 Days
• Field of Search: 324/555, 324/698, 324/511, 324/503, 324/556, 340/635, 340/652, 340/945
• US Class Current: 324/555
• CPC Class Codes: G01R 31/005 Testing of electric installations on transport means
• CPC Class Codes: G01R 31/54 Testing for continuity

Abstract

A primary, normally open, DC monitoring circuit with a circuit continuity test device is disclosed which will also test one or more additional sensors connected to the circuit. The sensing of lack of continuity or of a fault condition detected by an additional sensor governs the status of a single indicator, generally a warning light.

Claims

1. A multifunction direct current monitoring circuit having a single conductor and ground for an aircraft, which indicates an adverse condition detected by at least one or more sensors connected to the circuit, by a single indicator located in the aircraft cockpit:

a) a first sensor connected to the conductor and ground;

b) a continuity testing circuit having a conducting and non-conducting state connected electrically in parallel with the first sensor;

c) at least one additional sensor; and

d) means responsive to the at least one additional sensor for causing the continuity testing circuit to remain in a conducting or a non-conducting state depending on the status of the additional sensor.

2. The circuit of claim 1 in which the first sensor comprises a chip detector.

3. The circuit of claim 2 in which the continuity testing circuit comprises:

a) a self-powered a stable oscillator; and

b) a timer

wherein the oscillator and timer are activated by application of power to the conductor, the oscillator permitting current to flow between the conductor and ground until the timer output, upon reaching a predetermined setting, deactivates the oscillator.

4. The circuit of claim 3 in which the at least one additional sensor comprises an oil level sensor.

5. The circuit of claim 4 in which the responsive means comprises interface logic connecting the at least one additional sensor to the continuity testing circuit.

6. The circuit of claim 2 in which the at least one additional sensor comprises an oil level sensor.

7. The circuit of claim 6 in which the responsive means comprises interface logic connecting the at least one additional sensor to the continuity testing circuit.

8. The circuit of claim 1 in which the continuity testing circuit comprises:

a) a self-powered astable oscillator; and

b) a timer

wherein the oscillator and timer are activated by application of power to the conductor, the oscillator permitting current to flow between the conductor and ground until the timer output, upon reaching a predetermined setting, deactivates the oscillator.

9. The circuit of claim 1 in which the at least one additional sensor comprises an oil level sensor.

10. The circuit of claim 1 in which the responsive means comprises interface logic.

11. A method of indicating in an aircraft using a direct current monitoring circuit having a single conductor, ground, and indicator an adverse condition detected by at least one or more sensors connected to the circuit comprising:

a) connecting a first sensor to the conductor and ground;

b) connecting a continuity testing circuit having a conducting and a non-conducting state electrically in parallel to the first sensor;

c) providing at least one additional sensor; and

d) modifying the conducting or non-conducting status of the continuity testing circuit in accordance with the status of the at least one additional sensor.

12. The method of claim 11 in which the first sensor comprises a chip detector.

13. The method of claim 12 in which the continuity testing circuit comprises:

a) a self-powered a stable oscillator; and

b) a timer

wherein the oscillator and timer are activated by application of power to the conductor, the oscillator permitting current to flow between the conductor and ground until the timer output, upon reaching a predetermined setting, deactivates the oscillator.

14. The method of claim 13 in which the at least one additional sensor comprises an oil level sensor.

15. The method of claim 14 in which the conducting or non-conducting status of the continuity testing circuit is modified in accordance with the status of the at least one additional sensor by interface logic means connecting the at least one additional sensor to the continuity testing circuit.

16. The method of claim 12 in which the at least one additional sensor comprises an oil level sensor.

17. The method of claim 16 in which the conducting or non-conducting status of the continuity testing circuit is modified in accordance with the status of the at least one additional sensor by interface logic means connecting the at least one additional sensor to the continuity testing circuit.

18. The method of claim 11 in which the continuity testing circuit comprises:

a) a self-powered a stable oscillator; and

b) a timer

wherein the oscillator and timer are activated by application of power to the conductor, the oscillator permitting current to flow between the conductor and ground until the timer output, upon reaching a predetermined setting, deactivates the oscillator.

19. The method of claim 11 in which the at least one additional sensor comprises an oil level sensor.

20. The method of claim 11 in which the conducting or non-conducting status of the continuity testing circuit is modified in accordance with the status of the at least one additional sensor by interface logic means connecting the at least one additional sensor to the continuity testing circuit.

21. A multifunction direct current monitoring circuit comprising:

a) an electrically operated panel indicator;

b) first sensor means for activating the panel indicator to indicate the presence of metallic chips in a lubricating fluid;

c) means for checking the continuity of electrical conductors leading from the panel indicator to the sensor means for activating the panel indicator to indicate the presence of metallic chips;

d) second sensor means for detecting the presence of lubricating fluid at said first sensor means for activating the panel indicator to indicate the presence of metallic chips; and

e) means for causing the means for checking the continuity of electrical conductors to remain in a conducting or a non-conducting state depending on the status of the second sensor means for detecting the presence of lubricating fluid.