The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Oct. 08, 2019

Filed:

Jul. 27, 2016
Applicant:

Airbus Defence and Space Gmbh, Taufkirchen, DE;

Inventors:

Jürgen Steinwandel, Uhldingen-Mühlhofen, DE;

Ning Wang, München, DE;

Michael Judas, München, DE;

Jan Van Toor, München, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 35/08 (2006.01); B64D 27/24 (2006.01); B64C 39/02 (2006.01); B64C 29/00 (2006.01); B64D 27/02 (2006.01);
U.S. Cl.
CPC ...
B64D 35/08 (2013.01); B64C 29/0025 (2013.01); B64C 39/024 (2013.01); B64D 27/24 (2013.01); B64C 2201/042 (2013.01); B64C 2201/044 (2013.01); B64C 2201/088 (2013.01); B64C 2201/104 (2013.01); B64C 2201/108 (2013.01); B64C 2201/162 (2013.01); B64D 2027/026 (2013.01);
Abstract

A vertical take-off aircraft with a propulsion drive for generating a driving force being effective in a horizontal direction and with a lift drive for generating a lifting force being effective in a vertical direction includes a motor for providing mechanical energy for the propulsion drive and a first generator for providing electrical energy for the lift drive. Moreover, the aircraft includes an exhaust gas turbocharger for the motor with a first turbine being driven by an exhaust gas flow of the motor, wherein the first turbine is configured to provide mechanical energy for the propulsion drive.


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