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Fiber optic aircraft load relief control system

  • US 4,692,610 A
  • Filed: 01/30/1986
  • Issued: 09/08/1987
  • Est. Priority Date: 01/30/1986
  • Status: Expired due to Fees
First Claim
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1. A fiber optic load measuring system comprising:

  • (a) an optical pulse generator;

    (b) an optical bus connected to said optical pulse generator;

    (c) a plurality of optical pulse routing switches serially disposed along the length of said optical bus;

    (d) a plurality of optical attenuators, each of said optical attenuators being disposed along a dedicated surface where an applield load is to be measured, each of said optical attenuators further being connected to a dedicated optical pulse routing switch and being operative to vary the attenuation of the optical pulse in response to the applied load as said optical pulse is reflected by said optical attenuators;

    (e) said optical pulse routing switches being operative to selectively direct said optical pulses to individual optical attenuators such that each of said optical attenuators is separately pulsed;

    (f) an optical pulse receiver connected to said optical bus and operative to receive optical pulses reflected from said optical attenuators; and

    (g) a signal processor connected to said optical receiver and operative to process the signal received by said optical pulse receiver to determine the load along each of said surfaces.

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