View source for 18360288. VERTICAL TAKE-OFF AND LANDING AIRCRAFT simplified abstract (HONDA MOTOR CO., LTD.)

=VERTICAL TAKE-OFF AND LANDING AIRCRAFT=


==Organization Name==

[[:Category:HONDA MOTOR CO., LTD.|HONDA MOTOR CO., LTD.]]


[[Category:HONDA MOTOR CO., LTD.]]

==Inventor(s)==

[[:Category:Bon Aizawa of Wako-shi, Saitama (JP)|Bon Aizawa of Wako-shi, Saitama (JP)]][[Category:Bon Aizawa of Wako-shi, Saitama (JP)]]

[[:Category:Toshinori Tsukamoto of Wako-shi, Saitama (JP)|Toshinori Tsukamoto of Wako-shi, Saitama (JP)]][[Category:Toshinori Tsukamoto of Wako-shi, Saitama (JP)]]

[[:Category:Masashi Kato of Wako-shi, Saitama (JP)|Masashi Kato of Wako-shi, Saitama (JP)]][[Category:Masashi Kato of Wako-shi, Saitama (JP)]]

[[:Category:Kenta Uchida of Wako-shi, Saitama (JP)|Kenta Uchida of Wako-shi, Saitama (JP)]][[Category:Kenta Uchida of Wako-shi, Saitama (JP)]]

[[:Category:Kaisaku Yoshimura of Wako-shi, Saitama (JP)|Kaisaku Yoshimura of Wako-shi, Saitama (JP)]][[Category: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.



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