Combustible vapor detection system

• US 4,517,161 A
• Filed: 09/29/1982
• Issued: 05/14/1985
• Est. Priority Date: 09/29/1982
• Status: Expired due to Fees

• Current Assignee: Grumman Aerospace Corporation (Northrop Grumman Corporation)
• Original Assignee: Grumman Aerospace Corporation (Northrop Grumman Corporation)
• Inventors: Keitel, Murray, Charland, Edmund G. Jr., Wiley, Joseph N., Weiss, Harvey, Gravina, Anthony N.
• Primary Examiner(s): Richman, Barry S.
• Assistant Examiner(s): NOT, DEFINED
• Application Number:
  US06/426,608
• Time in Patent Office: 958 Days
• Field of Search: 422/95, 422/98, 422/88, 422/90, 422/94, 422/96, 422/97, 340/634, 324/71.5, 73/23, 73/27 R
• US Class Current: 422/95
• CPC Class Codes: G01N 27/122 Circuits particularly adapted therefor, e.g. linearising circuits
• CPC Class Codes: G01N 33/0031 comprising two or more sensors, e.g. a sensor array electrochemical electrode arrays G01N27/27
• CPC Class Codes: G08B 17/117 by using a detection device for specific gases, e.g. combustion products, produced by the fire G08B17/103, G08B17/11 take precedence
• CPC Class Codes: G08B 29/14 checking the detection circuits

Abstract

A system for sensing and annunciating the presence at any one of a plurality of locations of accumulations of potentially hazardous gaseous and vapor mixtures prior to their reaching a lower explosive limit thereof. The system has particular applicability to aircraft, and has a number of advantageous features such as adjustable annunciator set points which are settable between relatively wide lower explosive level limits, compensation in the sensor circuitry for temperature variations, built in diagnostic and test features, and a circuit design wherein multiple sensors at multiple locations are operable independently of each other.

Claims

1. A combustible vapor detection system for an aircraft for detecting and annunciating the pressure and location of combustible vapors at a plurality of locations on the aircraft, comprising:

a. a plurality of combustible vapor detectors, each adapted to be placed at a location to be monitored on an aircraft at which combustible vapors may be present, each combustible vapor detector having a resistance which varies in dependence upon the concentration of a combustible vapor to be detected, such that it produces an electrical output signal which varies in dependence upon the concentration of the combustible vapor, each vapor detector comprising a semiconductor gas detecting element wherein adsorption of select types of gases on its surface decreases its resistance, and having a greater element for thermally activating surface reactions on the semi-conductor element, and each vapor detector having a temperature compensation circuit, including a thermistor, for providing thermally stable operation for the vapor detector;

b. a central control means, which receives the plurality of electrical output signals, comprising;

(1) means for comparing each electrical signal with a separate threshold value for each vapor detector, such that individual characteristics of each vapor detector are considered in setting its threshold value, and the threshold value for each vapor detector being set at a level corresponding to a fraction of the concentration of combustible vapors in air which will just support combustion;

(2) means for generating an annunciation signal when at least one of the electrical output signals surpasses its threshold value;

(3) and a plurality of annunciator indicators, one corresponding to each combustible vapor detector, for signaling the occurrence of each annunciation signal to an operator; and

(4) a separate electrical channel for each vapor detector, each separate electrical channel comprising a dedicated circuit board for that channel, each electrical channel including separate first and second power supplies, the first power supply being for the vapor detecting element and the second power supply being for the heater element, and each electrical channel including a separate signal processing circuit for comparing the electrical signal from the vapor detector for that channel with a threshold value for that channel, each said dedicated circuit board comprising annunicator lights thereon for indicating proper operation of the components of that electrical channel, said annunciator lights including five LEDs, first and second LEDs for indicating operation of the first and second power supplies, a third LEd for indicating operation of the semi-conductor vapor detecting element, a fourth LED for indicating operation of the temperature compensation circuit, and a fifth LED for indicating operation of the heater element; and

c. diagnostic means for testing the combustible vapor detectors for operation, and for indicating a malfunction thereof to the operator.

2. A system as claimed in claim 1, wherein said diagnostic means are designed to enable all five LEDs on each circuit board, and further enable each annunciator indicator during an operational test in which all of the tested components are operating.

3. A system as claimed in claim 1, said central control means including a control and display unit, and said annunciator indicators comprising annunciator lights on said control and display unit.

4. A system as claimed in claim 3, said diagnostic means including a diagnostic testing switch on said control and display unit for actuating testing of the system.

5. A system as claimed in claim 1, further comprising:

a. a housing for each combustible vapor detector element, and defining an input port therefor;

b. a first fine mesh screen provided over said input port; and

c. a second fine mesh screen spaced from said first fine mesh screen and also extending over said input port, to virtually ensure provision of effective explosion suppression and flame arresting functions.

6. A combustible vapor detecting system as claimed in claim 5, said combustible vapor detecting element comprising a semiconductor gas detecting element wherein adsorption of combustible vapors on its surface decreases its resistance, and a heater element for thermally activating surface reactions on the semiconductor element, whereby the first and second spaced fine mesh screens provide isolation of the heater element to provide effective explosion suppression and flame arresting functions.

7. A combustible vapor detecting system as claimed in claim 6, said first and second fine mesh screens defining respectively smaller and larger convex surfaces which are positioned, spaced from each other, over said input port and said detector element.

8. A combustible vapor detecting system as claimed in claim 1, further comprising:

a. a mounting bracket for said detecting element;

b. a plurality of resilient vibration attenuators positioned between said bracket and said detecting element for providing vibration and shock isolation and attenuation for the detecting element.

9. A combustible vapor detecting system as claimed in claim 8, said detecting element being secured to said mounting bracket by a plurality of screws, and said plurality of attenuators being mounted on the screw shafts between said mounting bracket and said detecting element, said screws being selectively tightenable to tune the vibration attenuation by said resilient attenuators to minimize transmission to the detecting element of vibration frequencies which are particularly detrimental to its operation.

10. A combustible vapor detecting system as claimed in claim 9, each resilient vibration attenuator comprising a rubber grommet.