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:
Feb. 02, 2021

Filed:

May. 17, 2018
Applicant:

Textron Innovations Inc., Providence, RI (US);

Inventors:

Frank Bradley Stamps, Colleyville, TX (US);

Michael K. McNair, Weatherford, TX (US);

John Richard McCullough, Weatherford, TX (US);

Assignee:

Textron Innovations Inc., Providence, RI (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/08 (2006.01); B64C 29/00 (2006.01); B64D 27/02 (2006.01); B64C 27/00 (2006.01); B64D 27/10 (2006.01); B64D 27/24 (2006.01);
U.S. Cl.
CPC ...
B64C 27/006 (2013.01); B64C 27/08 (2013.01); B64D 27/10 (2013.01); B64D 27/24 (2013.01); B64C 29/0033 (2013.01); B64D 2027/026 (2013.01);
Abstract

A propulsion assembly for a rotorcraft includes a blade assembly, a drive shaft coupled to the blade assembly and an electric motor coupled to the drive shaft and operable to provide rotational energy to the drive shaft to rotate the blade assembly. The propulsion assembly includes a landing assistance turbine coupled to the drive shaft and operable to selectively provide rotational energy to the drive shaft during an underpowered descent to rotate the blade assembly and provide upward thrust, thereby reducing a descent rate of the rotorcraft prior to landing.


Find Patent Forward Citations

Loading…