Honda motor co., ltd. (20240329662). CONTROL DEVICE, AIRCRAFT, AND CONTROL METHOD simplified abstract

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CONTROL DEVICE, AIRCRAFT, AND CONTROL METHOD

Organization Name

honda motor co., ltd.

Inventor(s)

Bon Aizawa of Wako-shi (JP)

CONTROL DEVICE, AIRCRAFT, AND CONTROL METHOD - A simplified explanation of the abstract

This abstract first appeared for US patent application 20240329662 titled 'CONTROL DEVICE, AIRCRAFT, AND CONTROL METHOD

Simplified Explanation: When one of multiple vtol rotors fails, a rotor controller increases the thrust of an adjacent rotor without causing vibration suppression control, shifting the burden to other rotors.

  • The patent application focuses on a rotor controller system for vtol rotors.
  • In the event of a rotor failure, the system increases thrust in an adjacent rotor without affecting vibration suppression control.
  • The technology ensures that other rotors bear the burden of the thrust variation caused by the failed rotor.
  • This innovation aims to improve the efficiency and safety of vtol rotor systems.
  • By redistributing thrust among rotors, the system enhances overall performance and stability.

Potential Applications:

  • This technology can be applied in unmanned aerial vehicles (UAVs) for improved reliability and performance.
  • It can also be utilized in manned aircraft for enhanced safety during emergency situations.
  • The system may find applications in military drones, commercial aircraft, and other vtol rotor-based vehicles.

Problems Solved:

  • Addresses the issue of rotor failure in vtol rotor systems.
  • Ensures continuous operation and stability in the event of a rotor malfunction.
  • Improves overall efficiency and safety of vtol rotor-based vehicles.

Benefits:

  • Enhanced reliability and safety in vtol rotor systems.
  • Improved performance and stability during rotor failures.
  • Optimal thrust distribution for increased efficiency.

Commercial Applications: Commercial Applications: Rotor Controller System for VTOL Rotors in UAVs, Manned Aircraft, Military Drones, and Commercial Aircraft

Questions about VTOL Rotor Controller System: 1. How does the rotor controller system redistribute thrust in the event of a rotor failure? 2. What are the potential applications of this technology in the aerospace industry?

Frequently Updated Research: Stay updated on advancements in vtol rotor technology and rotor controller systems for improved performance and safety.


Original Abstract Submitted

when any one of a plurality of first rotors (vtol rotors) fails, a rotor controller (a vtol rotor controller) executes thrust increase control for increasing the thrust generated by an adjacent first rotor that is the first rotor adjacent to the failed first rotor, without making the adjacent first rotor cause the thrust variation for vibration suppression control, and executes the vibration suppression control in a manner so that one or more second rotors (vtol rotors) bear the burden of the thrust variation that has been borne by the adjacent first rotor.