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Programmable jet engine test station

  • US 4,821,217 A
  • Filed: 01/12/1987
  • Issued: 04/11/1989
  • Est. Priority Date: 01/12/1987
  • Status: Expired due to Term
First Claim
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1. For use in connection with a jet aircraft engine having certain electrical and pneumatic systems including oil and fuel pressure transducers, engine igniters, and EEC computer, air bleed valves, air-operated starter and thermo/anti-ice valves, and certain solenoids, a test station for automatically performing on-ground tests of such electrical and pneumatic systems when said engine is in a static, nonrunning condition, such station comprising:

  • a programmable data acquisition computer;

    input means, controllable by said computer, and operable to provide a certain test stimulus to any one of said electrical and pneumatic systems;

    output means, operatively connected to said computer, for sensing response of said any one of said systems to said test stimulus, in a manner so that computer may generate test data indicative of such response; and

    wherein said computer includes programming means operable by a test station user for permitting said user to select said certain test stimulus and to cause said computer to control said input means in accordance with said selected stimulus, and further, said programming means being operable by said user to control generation of test data by said computer, such data indicating system response to said test stimulus.

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