Resistance monitors

• US 5,382,912 A
• Filed: 08/19/1993
• Issued: 01/17/1995
• Est. Priority Date: 10/10/1991
• Status: Expired due to Term

• Current Assignee: QED Intellectual Property Services Limited
• Original Assignee: Smiths Industries Public Limited Company
• Inventors: Blain, David I.
• Primary Examiner(s): Regan, Maura K.
• Application Number:
  US08/108,939
• Time in Patent Office: 516 Days
• Field of Search: 324/715, 324/713, 324/502, 307/10.1, 340/436, 340/438, 73/118.1, 280/734, 280/735, 180/271
• US Class Current: 324/713
• CPC Class Codes: G01R 27/14 Measuring resistance by measuring current or voltage obtained from a reference source G01R27/16, G01R27/20, G01R27/22 take precedence
• CPC Class Codes: G01R 31/008 on air- or spacecraft, railway rolling stock or sea-going vessels
• CPC Class Codes: G01R 31/2829 Testing of circuits in sensor or actuator systems testing of apparatus for measuring electric or magnetic variables G01R35/00; testing of indicating or recording apparatus G01D; in airbag systems B60R21/0173; checking gas analysers G01N33/007; monitoring or fail-safe circuits for electromagnets H01F7/1844
• CPC Class Codes: G01R 31/50 Testing of electric apparatus, lines, cables or components for short-circuits, continuity, leakage current or incorrect line connections testing of sparking plugs H01T13/58
• CPC Class Codes: G01R 31/54 Testing for continuity

Abstract

An aircraft fire extinguisher system includes a fire extinguisher bottle and an attached explosive squib which has one side connected to ground and its other side connected alternately to two constant current sources in opposite senses. A differential amplifier subtracts the voltages in two sample-and-hold circuits caused by the opposite currents to eliminate the effect of the voltage at the point where the squib is grounded. A utilization circuit, coupled to the output of the differential amplifier, is used to indicate the presence of a fault in the squib or in associated circuitry.

Claims

1. A fire extinguisher system for an aircraft comprising:

a fire extinguisher bottle located in an aircraft;

a resistive explosive squib attached to said fire extinguisher bottle;

means connecting one side of said squib to ground;

a firing circuit;

a firing cable connecting the other side of said squib to said firing circuit; and

a test circuit connected to said other side of said squib via said firing cable for testing said squib and associated circuitry in the fire extinguisher system, said test circuit comprising a first current source connected via a first switch to said firing cable for supplying a first current to said squib via said firing cable in a first direction relative to ground, said first current being insufficient to cause firing of the squib, a second current source connected via a second switch to said firing cable for supplying a second current via said firing cable to said squib in a second direction relative to ground opposite from said first direction, said second current being substantially equal in magnitude to said first current and being insufficient to cause firing of the squib, said first and second switches being so arranged that only one of said switches may be closed at any given time to connect one of said current sources to said squib via said firing cable, first and second sample-and-hold circuits having inputs that are connected respectively via third and fourth switches to a junction between said first and second switches, said first and third switches being ganged together as a switch pair for simultaneous opening and closing, said second and fourth switches being ganged together as a switch pair for simultaneous opening and closing, means for alternately closing one and thereafter the other of said ganged switch pairs, a differential amplifier having a pair of inputs that are connected respectively to outputs of said first and second sample-and-hold circuits, and utilization means connected to an output of said differential amplifier for indicating the presence of a fault in said squib, in said firing cable, or in said ground connection.

2. The fire extinguisher system of claim 1 wherein each of said first and second current sources is a constant current source.

3. The fire extinguisher system of claim 1 wherein said utilization means comprises a visual display.

4. The fire extinguisher system of claim 1 wherein said utilization means comprises an audible alarm.

5. The fire extinguisher system of claim 1 wherein said utilization means is operative to calculate the resistance of said squib and determine whether said resistance is within predetermined limits.