PROCEDURE FOR REDUCING LOADS BY GUSTS IN AN AIRPLANE.

摘要

PROCEDURE TO REDUCE THE CHARGES FOR GUSTS THAT COME IN AN AIRPLANE, USING ADJUSTMENT ELEMENTS THAT CONTRACT THE LOADS FOR GUSTS THAT ARE PRODUCED THROUGH AN ADJUSTMENT, IN PARTICULAR OF TIMON OF ADDRESS, ALERONS IN THE INTERIOR PART OF THE WINGS WHERE THE LOAD BY TOTAL GUSTS IS THE RESULT OF THE SUM OF THE 1G BASE LOAD AND THE ADDITIONAL LOAD DUE TO THE GUSTS THAT ARE PRODUCED, REGULATING THE ADJUSTMENT ELEMENTS BASED ON THE FLIGHT HEIGHT, THE FLIGHT SPEED AND THE FLIGHT WEIGHT. IN ORDER TO AVOID THE HIGH ADJUSTMENT SPEEDS NEED UNTIL THE ADJUSTMENT ELEMENTS ARE CARRIED OUT UNDER THE RISING ADJUSTMENT ELEMENTS UNTIL REACHING THE HEIGHT OF CRUISE CROSSING OF THE AIRPLANE OR THE AIRCRAFT THE LANDING OF THE AIRPLANE, AS SUCH AS A MODIFICATION OF THE DISTRIBUTION OF THE ASCENSIONAL FORCE OF THE WINGS IS PRODUCED, AND THE LOAD IS REDUCED BY RESULTING GUSTS THROUGH THE REDUCTION OF THE BASIC LOAD 1G.