Patent ID: 11897597
Assignee: THE BOEING COMPANY
Field: Transport (Mechanical engineering)
Classification: CPC B  G  Y | IPC B  G

Claim 10:
11. A method to bias a pressure shape corresponding to an aircraft, the method comprising:
determining, by executing instructions with at least one processor, a movement parameter, the movement parameter corresponding to at least one of a Mach number of the aircraft, an airspeed of the aircraft, or a vertical acceleration of the aircraft;
calculating, by executing instructions with the at least one processor, a load of a flap based on the movement parameter,
comparing, by executing instructions with the at least one processor, the calculated load to a load threshold; and
determining, by executing instructions with the at least one processor, an adjustment of a position of a spoiler of the aircraft based on the comparison to move a pressure transition away from the flap.