Honda motor co., ltd. (20240300642). 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 20240300642 titled 'THRUST GENERATOR FOR ROTORCRAFT
Simplified Explanation:
The patent application describes a thrust generator for a rotorcraft, consisting of a support part conductively mounted to a conductive base in the rotorcraft, a rotor shaft supported by the support part, rotating blades attached to the rotor shaft, and a drive unit connected to the support part through electrically insulating parts.
- The thrust generator includes a support part mounted to a conductive base in the rotorcraft.
- A rotor shaft is conductively supported by the support part.
- Multiple rotating blades are connected to the rotor shaft.
- A drive unit is mounted to the support part using electrically insulating parts.
- The output shaft of the drive unit is linked to the rotor shaft through another electrically insulating part.
Potential Applications: This technology can be used in various rotorcraft applications, such as helicopters, drones, and other vertical take-off and landing (VTOL) aircraft.
Problems Solved: The thrust generator provides a reliable and efficient means of generating thrust in rotorcraft, improving overall performance and stability.
Benefits: - Enhanced thrust generation - Improved rotorcraft performance - Increased stability during flight
Commercial Applications: Title: Innovative Thrust Generator for Rotorcraft This technology can be utilized in the aerospace industry for the development of advanced rotorcraft with improved thrust capabilities, leading to safer and more efficient air transportation solutions.
Prior Art: Readers can explore prior patents related to thrust generators for rotorcraft, conductive mounting systems, and electrically insulated drive units to gain a deeper understanding of the technological advancements in this field.
Frequently Updated Research: Researchers are continually exploring new materials and designs to enhance the efficiency and performance of thrust generators for rotorcraft, leading to potential breakthroughs in the aerospace industry.
Questions about Thrust Generators for Rotorcraft: 1. What are the key components of a thrust generator for a rotorcraft? - The key components include a support part, rotor shaft, rotating blades, and a drive unit. 2. How does the conductive mounting system contribute to the overall performance of the thrust generator? - The conductive mounting system ensures efficient power transfer and stability in the rotorcraft.
Original Abstract Submitted
a thrust generator for a rotorcraft includes: a support part conductively mounted to a conductive base provided in the rotorcraft; a rotor shaft rotatably and conductively supported by the support part; multiple rotating blades joined to the rotor shaft; and a drive unit mounted to the support part via a first electrically insulating part, wherein an output shaft of the drive unit is connected to the rotor shaft via a second electrically insulating part.
