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. 17, 2023

Filed:

Jun. 22, 2021
Applicant:

Piasecki Aircraft Corporation, Essington, PA (US);

Inventors:

Luigi U Ricci Moretti, Swarthmore, PA (US);

Frederick W. Piasecki, Haverford, PA (US);

George L. Firpi, Glenolden, PA (US);

Shane A. Lewis, West Chester, PA (US);

Assignee:

Piasecki Aircraft Corporation, Essington, PA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/82 (2006.01); B64C 13/12 (2006.01); B64C 27/22 (2006.01);
U.S. Cl.
CPC ...
B64C 27/22 (2013.01); B64C 27/82 (2013.01); B64C 13/12 (2013.01); B64C 2027/8209 (2013.01); B64C 2027/8218 (2013.01); B64C 2027/8272 (2013.01);
Abstract

A compound aircraft includes a convertible thruster that pivots between an anti-torque position, a forward thrust position, and intermediate positions. A pilot has two inceptors to control thruster rotor pitch in the anti-torque and forward thrust positions. A mixer mechanically blends the signals from the two inceptors during transition between the anti-torque and forward thrust positions. A transfer rod coaxial with the pivot axis of the convertible thruster conveys convertible thruster pitch commands from the pilot to a pitch control actuator. The pitch control actuator may be located partially within the rotor of an electric motor that rotates the convertible thruster rotor. The electric motor and pitch control actuator are unitary. Both the electric motor and pitch control actuator pivot with the convertible thruster. The pitch actuator output shaft is coaxial to and disposed within a hollow electric motor output shaft.


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