Patent · US Active

Airfoil system

US12049299B2 · kind B2 · utility

0Cited by
7References
17Claims
0Family size

Inventors

Key dates

Filing dateMar 11, 2020
Grant dateJul 30, 2024
Priority date
Expiry dateJan 28, 2041

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/30
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A winged vertical take-off and landing aircraft with compound control surfaces comprising flaps and ailerons which can be operated simultaneously with each other offers improved aerodynamic performance and maneuverability. Configuration of the compound control surfaces may be varied to optimize performance in hovering (vertical) flight modes, cruising (horizontal) flight modes, and transitional flight modes.

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