Global Patent Index - EP 4087779 A1

EP 4087779 A1 20221116 - VTOL AIRCRAFT

Title (en)

VTOL AIRCRAFT

Title (de)

SENKRECHTSTART- UND -LANDEFLUGZEUG

Title (fr)

AÉRONEF VTOL

Publication

EP 4087779 A1 20221116 (EN)

Application

EP 21708467 A 20210201

Priority

  • US 202062968914 P 20200131
  • US 202062971958 P 20200208
  • US 2021016116 W 20210201

Abstract (en)

[origin: WO2021155385A1] Disclosed is a VTOL aircraft, and a method of operating the same. The VTOL aircraft employs a propulsion system comprising at least one propulsion unit, which can be rotated to generate lift during VTOL operations and thrust during cruise. A folding wing is employed to provide lift during cruise, and to meet external size constraints during storage and VTOL operations.

IPC 8 full level

B64C 27/26 (2006.01); B64C 3/56 (2006.01); B64C 27/08 (2006.01); B64C 29/00 (2006.01)

CPC (source: EP)

B64C 3/56 (2013.01); B64C 27/26 (2013.01); B64C 29/0033 (2013.01); B64C 29/0075 (2013.01); B64C 27/08 (2013.01); Y02T 50/10 (2013.01)

Designated contracting state (EPC)

AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

Designated extension state (EPC)

BA ME

Designated validation state (EPC)

KH MA MD TN

DOCDB simple family (publication)

WO 2021155385 A1 20210805; EP 4087779 A1 20221116

DOCDB simple family (application)

US 2021016116 W 20210201; EP 21708467 A 20210201