The difference in dynamic pressure in the propeller slipstreams as measured by sensors is divided by the freestream dynamic pressure generating a quantity proportional to the differential thrust coefficient. This quantity is used to command an electric trim motor to change the position of trim tab thereby retrimming the airplane to the new asymmetric power condition. The change in position of the trim tab produced by the electric trim motor is summed with the pilot's input to produce the actual trim tab position.
Airplane Automatic Control Force Trimming Device for Asymmetric Engine Failures
1985
14 pages
Report
Keine Angabe
Englisch
French airplane engine failures analyzed to find causes
Engineering Index Backfile | 1927
Engineering Index Backfile | 1929
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