18360288. VERTICAL TAKE-OFF AND LANDING AIRCRAFT simplified abstract (HONDA MOTOR CO., LTD.)
Contents
VERTICAL TAKE-OFF AND LANDING AIRCRAFT
Organization Name
Inventor(s)
Bon Aizawa of Wako-shi, Saitama (JP)
Toshinori Tsukamoto of Wako-shi, Saitama (JP)
Masashi Kato of Wako-shi, Saitama (JP)
Kenta Uchida of Wako-shi, Saitama (JP)
Kaisaku Yoshimura of Wako-shi, Saitama (JP)
VERTICAL TAKE-OFF AND LANDING AIRCRAFT - A simplified explanation of the abstract
This abstract first appeared for US patent application 18360288 titled 'VERTICAL TAKE-OFF AND LANDING AIRCRAFT
Simplified Explanation: The patent application describes a vertical take-off and landing aircraft with multiple VTOL rotors grouped together. A controller stops the rotation of these rotors in a sequential group-by-group manner after lift is generated by front and rear wings.
- Key Features and Innovation:
- Vertical take-off and landing aircraft design
- Multiple VTOL rotors divided into groups
- Controller for sequential rotor rotation stoppage
- Lift generated by front and rear wings
Potential Applications: This technology could be used in military drones, search and rescue operations, and urban air mobility vehicles.
Problems Solved: This technology addresses the challenge of efficiently controlling the vertical take-off and landing process in aircraft.
Benefits: The benefits of this technology include improved maneuverability, increased safety during take-off and landing, and enhanced control over the aircraft.
Commercial Applications: Potential commercial applications include the development of advanced drones for surveillance and delivery purposes, as well as the creation of innovative urban air mobility solutions for transportation.
Prior Art: Readers can explore prior art related to this technology by researching patents in the field of vertical take-off and landing aircraft design and control systems.
Frequently Updated Research: Stay informed about the latest advancements in vertical take-off and landing aircraft technology by following research publications and industry developments.
Questions about Vertical Take-off and Landing Aircraft: 1. What are the key challenges in designing vertical take-off and landing aircraft? 2. How does the sequential rotor rotation stoppage improve the performance of these aircraft?
Original Abstract Submitted
In a vertical take-off and landing aircraft, a plurality of VTOL rotors are divided into a plurality of groups, and each VTOL rotor is included in any one of the groups. After lift is generated by wings (a front wing and a rear wing), a controller sequentially stops rotation of the plurality of VTOL rotors on a group-by-group basis.
