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:
May. 06, 2025

Filed:

Sep. 21, 2023
Applicant:

Whisper Aero Inc., Crossville, TN (US);

Inventors:

Mark Douglass Moore, Crossville, TN (US);

Ian Andreas Villa, Crossville, TN (US);

Devon Jedamski, Crossville, TN (US);

Xiaofan Fei, Bellevue, WA (US);

Assignee:

Whisper Aero Inc., Crossville, TN (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/32 (2005.12); B64C 11/02 (2005.12); B64D 27/31 (2023.12); B64D 27/32 (2023.12); B64D 27/34 (2023.12); F01D 5/14 (2005.12); F01D 5/22 (2005.12); F01D 5/30 (2005.12); F01D 25/24 (2005.12); F04D 29/32 (2005.12); F04D 25/06 (2005.12); F04D 29/54 (2005.12); F04D 29/58 (2005.12);
U.S. Cl.
CPC ...
F01D 5/32 (2012.12); B64C 11/02 (2012.12); B64D 27/31 (2023.12); B64D 27/32 (2023.12); B64D 27/34 (2023.12); F01D 5/141 (2012.12); F01D 5/225 (2012.12); F01D 5/303 (2012.12); F01D 5/326 (2012.12); F01D 25/24 (2012.12); F04D 29/326 (2012.12); F04D 25/0606 (2012.12); F04D 29/542 (2012.12); F04D 29/5806 (2012.12); F05D 2220/323 (2012.12); F05D 2260/36 (2012.12); F05D 2260/96 (2012.12);
Abstract

A propulsor fan array having reduced noise emission is disclosed. The propulsor fan array includes a plurality of propulsor fans that collectively generate thrust. Each of the propulsor fans include a blade fan having a plurality of blades. The plurality of blades are tensioned at tips of the plurality of blade fans such that a pitch of the blades during thrust generation is substantially the same as a pitch of the blades at rest. By tensioning the tips of the blades, an angle of the blades is maintained during operation of the propulsor fan thereby reducing noise that may result from changes in the angle of the blades.


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