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:
Jan. 03, 2023

Filed:

Oct. 13, 2021
Applicant:

Dr. Ing. H.c. F. Porsche Aktiengesellschaft, Stuttgart, DE;

Inventors:

Patrick Scholl, Bietigheim-Bissingen, DE;

Jens-Ole Thoebel, Hankensbuettel, DE;

Christian Wenzel, Untergruppenbach, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 11/10 (2006.01); B64C 3/32 (2006.01); B64C 11/00 (2006.01); B64C 27/24 (2006.01); B64C 29/00 (2006.01);
U.S. Cl.
CPC ...
B64C 11/001 (2013.01); B64C 27/24 (2013.01); B64C 29/0025 (2013.01);
Abstract

A ducted fan for an aircraft includes a rotor-side fan and a stator-side duct that surrounds the rotor-side fan. The stator-side duct includes an inner wall facing the rotor-side fan and an outer wall averted from the fan. The ducted fan further includes a fastening device configured to support mounting of the ducted fan on a structural component of the aircraft. The fastening device includes a pin and a guide body. The guide body is configured to receive and guide the pin, the pin is insertable proceeding from the inner wall into a recess of the guide body, a first end of the pin protrudes relative to the outer wall, and the pin is configured to be mounted, via the first end, on a bearing of the structural component of the aircraft.


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