Abstract: An aircraft includes a fuselage and a wing extending from each lateral side of the fuselage. A nacelle is pivotably se cured to each wing. The nacelle has a rotor located thereat, with the rotor having a rotor tip path plane defined by rotation of the rotor about a rotor axis of rotation. When the rotor tip path plane is changed relative to the wing, the nacelle pivots relative to the wing about a nacelle hinge axis to reduce flapping required by the rotor. A method of operating an aircraft includes changing a rotor tip path plane orientation relative to a wing of the aircraft. The rotor disposed at a nacelle, with the nacelle pivotably secured to the wing. The nacelle is pivoted relative to the wing to reduce an overall tip path plane change requirement of the rotor.
Abstract: Embodiments are directed to receiving, by a control station, an input including a command for re-location of a vehicle from a first location to a second location, the input identifying the second location, determining, by the control station, at least one of a distance, a direction, an altitude, and a latitude and longitude for the vehicle to travel from the first location to the second location, and transmitting, by the control station, the command and the at least one of a distance, a direction, an altitude, and a latitude and longitude to the vehicle.
Type:
Application
Filed:
August 2, 2012
Publication date:
August 21, 2014
Applicant:
SIKORKSY AIRCRAFT CORPORATION
Inventors:
Thomas Zygmant, Jesse J. Lesperance, Ira E. Zoock