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.
Patent No.:
Date of Patent:
Jan. 14, 2020
Filed:
May. 23, 2017
Applicant:
Bell Helicopter Textron Inc., Fort Worth, TX (US);
Inventors:
Richard E. Rauber, Euless, TX (US);
Mithat Yuce, Lantana, TX (US);
Thomas C. Parham, Jr., Colleyville, TX (US);
Thomas J. Newman, Midlothian, TX (US);
Mark A. Wiinikka, Hurst, TX (US);
Assignee:
Other;
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/54 (2006.01); B64C 27/51 (2006.01); F16C 11/06 (2006.01); B64C 27/635 (2006.01); B64C 27/59 (2006.01); B64C 27/58 (2006.01); F16C 11/04 (2006.01); F16C 23/02 (2006.01);
U.S. Cl.
CPC ...
B64C 27/54 (2013.01); B64C 27/51 (2013.01); F16C 11/0695 (2013.01); B64C 27/58 (2013.01); B64C 27/59 (2013.01); B64C 27/635 (2013.01); F16C 11/045 (2013.01); F16C 11/0614 (2013.01); F16C 23/02 (2013.01); F16C 2326/43 (2013.01);
Abstract
An aircraft includes a rotor blade and a rotor hub system. The rotor hub system includes a lead-lag damper having a rod end and being operably associated with the rotor blade; a blade adapter having a first arm and an opposing second arm; a pin carried by the blade adapter and configured to secure in position via the first arm and the second arm; and an actuator secured to the pin and configured to adjust the position of the lead-lag rod end relative to the first arm and the second arm.