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. 11, 2022

Filed:

Feb. 03, 2019
Applicant:

Bell Helicopter Textron Inc., Fort Worth, TX (US);

Inventors:

Aaron Alexander Acee, Flower Mound, TX (US);

Andrew Paul Haldeman, Fort Worth, TX (US);

Assignee:

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/12 (2006.01); B64D 33/08 (2006.01); B64C 27/20 (2006.01); F04D 29/58 (2006.01); B64C 27/82 (2006.01);
U.S. Cl.
CPC ...
B64C 27/12 (2013.01); B64C 27/20 (2013.01); B64D 33/08 (2013.01); F04D 29/5806 (2013.01); B64C 2027/8254 (2013.01);
Abstract

Systems and methods include providing an aircraft with a ducted rotor assembly. The ducted rotor assembly includes a housing having a duct, a rotor drive mechanism coupled to a rotor system, and a plurality of stators that both structurally support the rotor drive mechanism within the duct of the housing and carry a fluid through internal fluid passages in the plurality of stators to provide cooling to the rotor drive mechanism. Some of the stators carry fluid to the rotor drive mechanism, where the fluid absorbs heat from the rotor drive mechanism, and some of the stators carry fluid away from the rotor drive mechanism. The rotor system generates an airflow over the stators carrying fluid away from the rotor drive mechanism to effect transfer between the fluid and the airflow.


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