US Patent Application 18249730. MOTOR UNIT AND AIRCRAFT simplified abstract

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MOTOR UNIT AND AIRCRAFT

Organization Name

Panasonic Intellectual Property Management Co., Ltd.

Inventor(s)

DAISUKE Sato of Osaka (JP)

MOTOR UNIT AND AIRCRAFT - A simplified explanation of the abstract

This abstract first appeared for US patent application 18249730 titled 'MOTOR UNIT AND AIRCRAFT

Simplified Explanation

The abstract describes a motor unit that uses a magnetic force to rotate. It consists of a first rotary wing with two rotors, a second rotary wing, and a blade that can move between two rotational positions.

  • The motor unit operates by generating a magnetic force in a stator.
  • The first rotary wing includes a first rotor and a second rotor that rotate due to the rotational force of the first rotor.
  • The second rotary wing rotates due to the rotational force of the second rotor.
  • The blade of the second rotary wing is connected in a way that allows it to move between two rotational positions.
  • In the first rotational position, the blade extends in a direction that intersects the second axial center from the rotator.
  • In the second rotational position, the tip end of the blade is positioned in a direction opposite to the first direction relative to the tip end of the blade in the first rotational position.


Original Abstract Submitted

A motor unit rotates by a magnetic force generated in a stator. A first rotary wing includes a first rotor and a second rotor that rotate by a rotational force of the first rotor. A second rotary wing rotates by a rotational force of the second rotor. A blade of the second rotary wing is coupled rotationally movably to the rotator at the first rotational position and the second rotational position. When the blade is at the first rotational position, the blade protrudes in the direction intersecting the second axial center from the rotator. When the blade is at the second rotational position, a tip end of the blade is positioned in a second direction opposite to the first direction relative to the tip end of the blade positioned at the first rotational position.

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