Method and an instrument for determining the limiting parameter of a turboshaft engine

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United States of America Patent

PATENT NO 8121773
APP PUB NO 20080125931A1
SERIAL NO

11808168

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Abstract

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The present invention relates to a method and to an instrument for determining the limiting margin of a surveillance parameter of a turboshaft engine. During a preliminary stage, a secondary processor means (11) determines a preliminary comfort margin. Thereafter, during a main stage, it estimates a useful comfort margin from the preliminary comfort margin, and then an apparent difference between the current value and the limit value of the surveillance parameter, and finally the limiting margin by subtracting the useful comfort margin from the apparent difference.

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Patent Owner(s)

  • AIRBUS HELICOPTERS

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Gaulmin, François-Xavier Salon de Provence, FR 3 9
Iraudo, Lionel Marseilles, FR 10 86

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