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:
Sep. 08, 2020

Filed:

Dec. 20, 2017
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventor:

Huguette De Wergifosse, Saint Augustin, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 11/32 (2006.01); B64C 11/44 (2006.01); F01D 7/00 (2006.01);
U.S. Cl.
CPC ...
B64C 11/325 (2013.01); B64C 11/44 (2013.01); F01D 7/00 (2013.01); F05D 2220/324 (2013.01); F05D 2220/325 (2013.01); F05D 2260/40311 (2013.01); F05D 2260/74 (2013.01); F05D 2260/79 (2013.01); F05D 2270/09 (2013.01); F05D 2270/62 (2013.01);
Abstract

A pitch actuation system for a turbine engine propeller includes an actuator with movable part configured to rotate the blades of the propeller relative to the blade pitch axes. The actuator includes a transmission screw that is rotatable and movable in translation along a longitudinal axis, and a nut that engages the screw to move in translation along the longitudinal axis to adjust the pitch of the propeller blades. The actuator further includes non-rotatable decoupler for decoupling the rotation between the propeller and the nut. A blade feathering device has at least one electric drive motor and is configured to translate a member along the longitudinal axis. A blade pitch control device includes at least one electric motor configured to drive a rotor about the longitudinal axis, wherein that rotation rotates the screw and transmits translation of the member.


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