Abstract: A vertical take-off and landing (VTOL) aircraft is disclosed. The VTOL aircraft may include: a fuselage, a thrust rotor to produce a propulsion thrust, rotor booms, canard surfaces, wing surfaces, tail surfaces, and lift rotors to produce lifting thrust force.
Type:
Application
Filed:
November 17, 2021
Publication date:
August 18, 2022
Applicant:
BCG DIGITAL VENTURES GMBH
Inventors:
Robert W. PARKS, Francesco GIANNINI, Diana SIEGEL, Jan D. LIENHARD
Abstract: Disclosed herein is a vertical take-off and landing (VTOL) aircraft having three lifting surfaces and separate lift and cruise systems. The VTOL aircraft may include a fuselage having a roll axis, a thrust rotor to produce a propulsion thrust, first and second rotor booms, first and second canard surfaces, first and second wing surfaces, first and second tail surfaces, and a plurality of lift rotors to produce a lifting thrust force. The plurality of lift rotors includes a first plurality of lift rotors positioned on the first rotor boom and a second plurality of lift rotors positioned on the second rotor boom. The first and second rotor booms may be substantially parallel to the roll axis of the fuselage, where the fuselage is positioned between the first and second rotor booms. Each of the first and second rotor booms may be secured to the aircraft at three locations.
Type:
Grant
Filed:
January 23, 2020
Date of Patent:
December 28, 2021
Assignee:
BCG Digital Ventures GmbH
Inventors:
Robert W. Parks, Francesco Giannini, Diana Siegel, Jan D. Lienhard
Abstract: Disclosed herein is a vertical take-off and landing (VTOL) aircraft having three lifting surfaces and separate lift and cruise systems. The VTOL aircraft may include a fuselage having a roll axis, a thrust rotor to produce a propulsion thrust, first and second rotor booms, first and second canard surfaces, first and second wing surfaces, first and second tail surfaces, and a plurality of lift rotors to produce a lifting thrust force. The plurality of lift rotors includes a first plurality of lift rotors positioned on the first rotor boom and a second plurality of lift rotors positioned on the second rotor boom. The first and second rotor booms may be substantially parallel to the roll axis of the fuselage, where the fuselage is positioned between the first and second rotor booms. Each of the first and second rotor booms may be secured to the aircraft at three locations.
Type:
Application
Filed:
January 23, 2020
Publication date:
September 3, 2020
Applicant:
BCG Digital Ventures GmbH
Inventors:
Robert W. PARKS, Francesco GIANNINI, Diana SIEGEL, Jan D. LIENHARD
Abstract: Disclosed herein is a vertical take-off and landing (VTOL) aircraft having three lifting surfaces and separate lift and cruise systems. The VTOL aircraft may include a fuselage having a roll axis, a thrust rotor to produce a propulsion thrust, first and second rotor booms, first and second canard surfaces, first and second wing surfaces, first and second tail surfaces, and a plurality of lift rotors to produce a lifting thrust force. The plurality of lift rotors includes a first plurality of lift rotors positioned on the first rotor boom and a second plurality of lift rotors positioned on the second rotor boom. The first and second rotor booms may be substantially parallel to the roll axis of the fuselage, where the fuselage is positioned between the first and second rotor booms. Each of the first and second rotor booms may be secured to the aircraft at three locations.
Type:
Grant
Filed:
April 24, 2017
Date of Patent:
March 3, 2020
Assignee:
BCG Digital Ventures GmbH
Inventors:
Robert W. Parks, Francesco Giannini, Diana Siegel, Jan D. Lienhard