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:
Oct. 23, 2018

Filed:

Mar. 10, 2016
Applicant:

Goodrich Aerospace Services Private Limited, Bangalore, Karnataka, IN;

Inventors:

Santyar Srivatsa, Karnataka, IN;

Guru Prasad Mahapatra, Karnataka, IN;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B60S 1/22 (2006.01); B60S 1/16 (2006.01); B60S 1/08 (2006.01); B08B 1/00 (2006.01); B60S 1/24 (2006.01); B60S 1/26 (2006.01); B64C 1/14 (2006.01);
U.S. Cl.
CPC ...
B60S 1/0896 (2013.01); B08B 1/001 (2013.01); B60S 1/163 (2013.01); B60S 1/166 (2013.01); B60S 1/22 (2013.01); B60S 1/245 (2013.01); B60S 1/26 (2013.01); B64C 1/14 (2013.01); Y10T 74/18056 (2015.01);
Abstract

A windshield wiper system for an aircraft is provided and includes a motor, an output shaft, a wrap spring and crank rocker mechanism (WSCRM) to which the motor and the output shaft are coupled and a controller. By way of the WSCRM, first directional rotation input to the WSCRM from the motor via a two-stage gear reduction is converted such that the output shaft drives wiper blade oscillation through a first sweep angle and second directional rotation input to the WSCRM from the motor is converted such that the output shaft drives wiper blade oscillation through a second sweep angle. The controller is configured to control the motor such that the first directional rotation is continuously or non-continuously input during first or second flight conditions, respectively, and the second directional rotation is continuously input during third flight conditions.


Find Patent Forward Citations

Loading…