×

TEMPERATURE INDICATOR FOR AIRCRAFT BRAKES AND THE LIKE

  • US 3,582,926 A
  • Filed: 04/08/1968
  • Issued: 06/01/1971
  • Est. Priority Date: 04/08/1968
  • Status: Expired due to Term
First Claim
Patent Images

1. A temperature indicating system adapted to indicate increase in temperature above first and second temperature levels sensed at a plurality of spaced apart temperatures sensor locations, said system comprising:

  • power supply means;

    a plurality of temperature sensor means including junction thermocouple means arranged to sense temperature at a respective one of said spaced apart locations and each having a sensing junction and a reference junction which reference junctions are located at a common station remote from the respective sensing junctions and subject to the same temperature conditions;

    operational amplifier means connected to said power supply means and to each of said thermocouple means and having respective feedback circuit means including temperature-sensitive resistive means effective to compensate for changes in ambient temperature at said common station for said reference junctions of said thermocouple means; and

    first and second potential-sensitive circuit means connected to the output of said amplifier means and to said power supply means and each comprising a respective indicator means and each rendered active incident to sensing of a respective one of said first and second temperatures at said thermocouple means thereby to provide respective indications of attainment of said first and second temperature levels at said thermocouple means.

View all claims
  • 0 Assignments
Timeline View
Assignment View
    ×
    ×