Automated lamp monitoring system for comparing light intensities with a preselected valve

• US 5,446,277 A
• Filed: 12/27/1993
• Issued: 08/29/1995
• Est. Priority Date: 12/27/1993
• Status: Expired due to Term

• Current Assignee: Devore Aviation Corporation
• Original Assignee: Devore Aviation Corporation
• Inventors: Rutter, Robert E.
• Primary Examiner(s): Nelms, David C.
• Assistant Examiner(s): NICHOLS, STEVEN
• Application Number:
  US08/173,087
• Time in Patent Office: 610 Days
• Field of Search: 250/227.31, 250/205, 250/214 R, 356/213, 356/215, 356/224, 315/149, 315/150, 315/151
• US Class Current: 250/214.00R
• CPC Class Codes: A01N 2300/00 Combinations or mixtures of active ingredients covered by classes A01N27/00 - A01N65/48 with other active or formulation relevant ingredients, e.g. specific carrier materials or surfactants, covered by classes A01N25/00 - A01N65/48
• CPC Class Codes: A01N 25/10 Macromolecular compounds
• CPC Class Codes: A01N 25/26 in coated particulate form
• CPC Class Codes: A01N 43/70 Diamino—1,3,5—triazines with only one oxygen, sulfur or halogen atom or only one cyano, thiocyano (—SCN), cyanato (—OCN) or azido (—N3) group directly attached to a ring carbon atom
• CPC Class Codes: A01N 57/12 containing acyclic or cycloaliphatic radicals
• CPC Class Codes: G01J 1/42 using electric radiation detectors optical or mechanical part G01J1/04; by comparison with a reference light or electric value G01J1/10
• CPC Class Codes: G01J 2001/4247 for testing lamps or other light sources

Abstract

Flash tube and lamp monitoring systems. The flash tube intensity monitoring system includes: a human eye spectral response photodiode for producing analog signals, each of which is directly proportional to the intensity of each flash from the flash tube; electronics for converting each of the analog signals to a digital time function proportional to the intensity of the corresponding flash; and electronics, including a microprocessor, for monitoring each of the digital time functions, for flagging those time functions which are below a preselected minimum, and for sending a fault signal when a preselected number of consecutive time functions are below the pre-selected minimum. The monitoring system and flash tube are, preferably, incorporated into single unit for easy installation in the fuselage of an aircraft. The lamp monitoring system includes: a light pickup; a photodiode for producing an analog signal which is directly proportional to the intensity of the lamp being monitored; a line transceiver; an A/D converter; and a microcontroller. The microcontroller, which has a unique identification code, sends a command to the A/D converter only upon receipt of the matching poll command.

Claims

1. A flash tube intensity monitoring system, said system comprising:

a. a human eye spectral response photodiode for producing analog signals, each of said analog signals being directly proportional to the intensity of each flash from said flash tube;

b. means for converting each of said analog signals to a digital time function proportional to said intensity of the corresponding one of said flash; and

c. means for monitoring each of said digital time functions, for flagging those of said time functions which are below a preselected minimum and for sending a fault signal when a preselected number of consecutive time functions are below said pre-selected minimum.

2. The monitoring system as set forth in claim 1, further including means, interposed between said flash tube and said photodiode, for at least partially blocking infrared radiation from reaching said photodiode.

3. The monitoring system as set forth in claim 2, wherein said means for blocking is a light pipe which filters infrared radiation.

4. The monitoring system as set forth in claim 1, wherein said means for converting said analog signals includes analog integration on circuit.

5. The monitoring system as set forth in claim 4, wherein said analog integration circuit includes a resistor, a capacitor and an operational amplifier.

6. The monitoring system as set forth in claim 1, wherein said means for converting includes means to compensate for variations in said flash intensity from said flash tube as seen by said photodiode.

7. The monitoring system as set forth in claim 1, wherein said means for monitoring includes a microcontroller.

8. An automated anticollision light monitoring unit for aircraft, said unit comprising:

a. a housing;

b. a flash tube supported by said housing;

c. a human eye spectral response photodiode disposed relative to said housing, said diode producing an electronic signal, said signal being proportional to the intensity of the corresponding flash from said flash tube;

d. means for converting said electronic signal to a digital time function proportional to said intensity of said corresponding flash; and

e. means for monitoring said digital function and for generating a fault signal when said digital function is below a preselected value for a preselected period of time, said converting means interconnecting said monitoring means and said photodiode.

9. The unit as set forth in claim 8, further including means for shielding said photodiode from the heat generated by said flash tube.

10. The unit as set forth in claim 9, further including means, interposed between said flash tube and said photodiode for at least partially blocking infrared radiation from reaching said photodiode.

11. A monitoring system for a lamp such as used in an airport approach array, said lamp having a power line, said system comprising:

a. a light pickup positionable relative to said lamp to pick up a portion of the light emitted by said lamp;

b. a human eye spectral response photodiode for producing an electronic signal which is proportional to the intensity of visible light emitted by said lamp;

c. a line transceiver for sending and receiving digital data and instructions over said lamp power line;

d. means for converting said electronic signal to a digital function proportional to the intensity of said lamp, said converting means connected to said photodiode and said line transceiver; and

e. a microcontroller connected to said line transceiver and said converting means, said microcontroller including a unique identification code and adapted to receive a poll command over said power line, whereby when said microcontroller receives a poll command which matches said unique identification code, said microcontroller sends a command to said converting means and said converting means converts said electronic signal to said digital function.

12. The monitoring system as set forth in claim 11, further including means for amplifying and conditioning said electronic signal from said photodiode so as to fit the input range of said converting means.

13. The monitoring system as set forth in claim 12, wherein said converting means is an A/D chip.

14. The monitoring system as set forth in claim 11, further including an optical pickup bezel for collecting visible light from said lamp for transmission to said photodiode.

15. The monitoring system as set forth in claim 14, wherein said bezel contacts at least a portion of the perimeter of said lamp without degrading or interfering with said lamp'"'"'s projected beam path.

16. The monitoring system as set forth in claim 14, further including optical coupling means for coupling said bezel to said photodiode.

17. The monitoring system as set forth in claim 16, wherein said optical coupling means separates said photodiode, said line transceiver, said converting means, and said microcontroller from the intense heat generated by said lamp.

18. The monitoring system as set forth in claim 17, wherein said optical coupling means is a fiber optic cable.