Patent · US Active

Rotorcraft and method of controlling rotorcraft

US11320840B2 · kind B2 · utility

0Cited by
2References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 17, 2019
Grant dateMay 3, 2022
Priority date
Expiry dateJul 26, 2040

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG01L1/22
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

According to one implementation, a rotorcraft includes rotors, a fuselage, at least three rods, at least one load sensor and a control device. The rotors obtain lift. The fuselage is coupled to the rotors. The at least three rods support the fuselage. The at least one load sensor detects loads applied on the at least three rods. The control device automatically controls the rotors so that measured values of the loads detected by the at least one load sensor are brought to targeted values of the loads.

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