Patent · US Active

System and method for airspeed estimation utilizing propulsor data in electric vertical takeoff and landing aircraft

US11447244B1 · kind B1 · utility

4Cited by
14References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJun 29, 2021
Grant dateSep 20, 2022
Priority date
Expiry dateJun 29, 2041

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64D43/02
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A system for airspeed estimation utilizing propulsor data in electric vertical takeoff and landing (eVTOL) aircraft is provided. The system generally comprises at least a propulsor, at least one sensor and a flight controller. The at least a propulsor is mechanically coupled to a body of an eVTOL aircraft, wherein the at least a propulsor is configured to propel the eVTOL aircraft. The at least one sensor is configured to detect a torque of the at least a propulsor, and transmit the torque of the at least a propulsor. The flight controller is configured to receive the torque of the at least a propulsor and determine an airspeed of the eVTOL aircraft as a function of the torque of the at least a propulsor. A method for airspeed estimation utilizing propulsor data in electric vertical takeoff and landing (eVTOL) aircraft is also provided.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.