Honda motor co., ltd. (20240300663). THRUST GENERATOR FOR ROTORCRAFT simplified abstract
Contents
THRUST GENERATOR FOR ROTORCRAFT
Organization Name
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 20240300663 titled 'THRUST GENERATOR FOR ROTORCRAFT
The abstract describes a patent application for a thrust generator for a rotorcraft, which includes a support part detachably mounted to a base 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, with an output shaft of the drive unit detachably connected to the rotor shaft.
- Support part detachably mounted to a base in the rotorcraft
- Rotor shaft rotatably supported by the support part
- Multiple rotating blades joined to the rotor shaft
- Drive unit detachably mounted to the support part or the base
- Output shaft of the drive unit detachably connected to the rotor shaft
Potential Applications: - This technology can be used in various types of rotorcraft, such as helicopters and drones. - It can improve the efficiency and performance of rotorcraft by providing a reliable thrust generation system.
Problems Solved: - Provides a detachable thrust generator system for rotorcraft, allowing for easy maintenance and replacement. - Enhances the overall stability and maneuverability of the rotorcraft.
Benefits: - Improved thrust generation system for rotorcraft. - Easy maintenance and replacement of components. - Enhanced stability and performance of the rotorcraft.
Commercial Applications: Thrust generators for rotorcraft can have commercial applications in the aviation industry, military applications, search and rescue operations, and aerial photography.
Questions about the technology: 1. How does the detachable thrust generator system improve the maintenance of rotorcraft? 2. What are the potential cost-saving benefits of using this technology in rotorcraft design?
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.
