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Aircraft vertical stabilizer having a lift propeller and the method of using the same

  • US 10,322,814 B1
  • Filed: 09/01/2018
  • Issued: 06/18/2019
  • Est. Priority Date: 09/01/2018
  • Status: Active Grant
First Claim
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1. An aircraft comprising:

  • a left fixed wing;

    a right fixed wing;

    a fuselage coupled to the left and the right fixed wings;

    a left vertical stabilizer coupled to the fuselage, wherein the left vertical stabilizer has a left top distal end;

    a right vertical stabilizer coupled to the fuselage, wherein the right vertical stabilizer has a right top distal end;

    a left tail propeller disposed on the left top distal end of the left vertical stabilizer, said left tail propeller having a horizontal plane of rotation;

    a left motor to drive the left tail propeller; and

    wherein the left motor has a rotary axis and the rotary axis is substantially parallel to a longitudinal axis of the aircraft.

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