Determination of gross thrust-related parameters

G - Physics – 01 – M

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354/24

G01M 15/00 (2006.01) G01L 5/13 (2006.01)

Patent

CA 1160345

ABSTRACT OF THE DISCLOSURE It is known to obtain a correction factor by determining theoretical gross thrust by measuring engine pressures and by measuring actual gross thrust and using a comparison between theoretical and measured gross thrust to develop a correction factor. However the correction factor is variable in accordance with certain engine pressures and requires the use of elaborate altitude test cell facilities to define it for a practical working range. This invention measures engine pressures in a static sea level facility, derives a correction factor to be applied to one of the measured pressures for use in a determination of gross thrust useful under all operating conditions.

150685

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