18415805. THRUST GENERATOR FOR ROTORCRAFT simplified abstract (Honda Motor Co., Ltd.)

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THRUST GENERATOR FOR ROTORCRAFT

Organization Name

Honda Motor Co., Ltd.

Inventor(s)

Ryuzaburo Kobayashi of Saitama (JP)

THRUST GENERATOR FOR ROTORCRAFT - A simplified explanation of the abstract

This abstract first appeared for US patent application 18415805 titled 'THRUST GENERATOR FOR ROTORCRAFT

Simplified Explanation:

The patent application describes a thrust generator for a rotorcraft, consisting of a support part, a rotor shaft, rotating blades, and a detachable drive unit connected to the rotor shaft.

  • The support part is detachably mounted to a base in the rotorcraft.
  • The rotor shaft is rotatably supported by the support part.
  • Multiple rotating blades are attached to the rotor shaft.
  • The drive unit is detachably mounted to the support part or the base, with its output shaft detachably connected to the rotor shaft.

Key Features and Innovation:

  • Detachable support part and drive unit for easy maintenance and replacement.
  • Rotating blades for generating thrust efficiently.
  • Versatile design for use in various rotorcraft applications.

Potential Applications:

The thrust generator can be used in helicopters, drones, and other rotorcraft for propulsion and lift generation.

Problems Solved:

  • Simplifies maintenance and repair processes.
  • Enhances thrust generation efficiency.
  • Increases versatility in rotorcraft design.

Benefits:

  • Improved performance and reliability.
  • Cost-effective maintenance.
  • Enhanced adaptability for different rotorcraft configurations.

Commercial Applications:

Potential commercial applications include the aerospace industry, defense sector, and unmanned aerial vehicle (UAV) market.

Questions about Rotorcraft Thrust Generators:

1. How does the detachable drive unit improve maintenance processes for rotorcraft thrust generators? 2. What are the key advantages of using rotating blades in a rotorcraft thrust generator?


Original Abstract Submitted

A thrust generator for a rotorcraft includes: a support part detachably mounted to a base provided in the rotorcraft; a rotor shaft rotatably supported by the support part; multiple rotating blades joined to the rotor shaft; and a drive unit detachably mounted to the support part or the base, wherein an output shaft of the drive unit is detachably connected to the rotor shaft.

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