Rotary aircraft and method of use

A rotary aircraft, comprising:

• a streamlined body extending from a front end to a back end, the streamlined body having a center axis extending the longitudinal length of the body;
• a forward wing rigidly attached to and extending from a front section near the front end, the forward wing having a first section and a second section rigidly attached to the body and extending in directions opposing each other, the forward wing being positioned below a dimensional plane that extends along the center axis of the body;
• an aft wing rigidly attached to and extending from a back section near the back end, the aft wing having a third section and a fourth section rigidly attached to the body and extending in directions opposing each other, the aft wing being positioned above the dimensional plane that extends along the center axis of the body;
• a first rotor assembly secured to the first section and configured to create lift and thrust during flight;
• a second rotor assembly secured to the second section and configured to create lift and thrust during flight;
• a third rotor assembly secured to the third section and configured to create lift and thrust during flight;
• and
• a fourth rotor assembly secured to the fourth section and configured to create lift and thrust during flight;
• wherein the forward wing has a different thickness than a thickness of the aft wing.

A method to create vertical lift and forward flight of an aircraft, comprising:

• providing an aircraft having:
• a streamlined body extending from a front end to a back end;
• a forward wing rigidly attached to and extending from a front section near the front end, the forward wing having a first section and a second section rigidly attached to the body and extending in directions opposing each other;
• an aft wing rigidly attached to and extending from a back section near the back end, the aft wing having a third section and a fourth section rigidly attached to the body and extending in directions opposing each other;
• a first rotor assembly secured to the first section and configured to create lift and thrust during flight;
• a second rotor assembly secured to the second section and configured to create lift and thrust during flight;
• a third rotor assembly secured to the third section and configured to create lift and thrust during flight;
• a fourth rotor assembly secured to the fourth section and configured to create lift and thrust during flight;
• and
• a center rotor assembly moveably attached to the body and configured to create lift and thrust during flight;
• the center wing is positioned at a location between the forward wing and the aft wing;
• simultaneously create lift and thrust during flight with the first rotor assembly, the second rotor assembly, the third rotor assembly, and the center rotor assembly simultaneously create lift and thrust during flight.