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:
May. 14, 2019

Filed:

Feb. 16, 2016
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Mark Gregory Wotzak, Chestnut Hill, MA (US);

Daniel Waslo, Marblehead, MA (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 27/10 (2006.01); F02C 3/04 (2006.01); F02C 3/107 (2006.01); F02C 6/20 (2006.01); F02C 7/36 (2006.01); F16H 1/28 (2006.01); F16H 57/10 (2006.01);
U.S. Cl.
CPC ...
F02C 3/107 (2013.01); B64D 27/10 (2013.01); F02C 3/04 (2013.01); F02C 6/20 (2013.01); F02C 6/206 (2013.01); F02C 7/36 (2013.01); F16H 57/10 (2013.01); F05D 2220/323 (2013.01); F05D 2240/60 (2013.01); F05D 2260/40311 (2013.01); F05D 2260/902 (2013.01); F16H 1/28 (2013.01);
Abstract

An in-line propeller gearbox of a turboprop gas turbine engine includes an epicyclic gearing arrangement that has a sun gear, a ring gear and at least one planet gear disposed between and meshing with both the sun gear and the ring gear. The propeller gearbox includes a disk brake that can be operated to slow down or stop altogether the rotation of the propeller. The disk brake has an axially extending shaft having at one end a disk and at the opposite end a gear having teeth that engage with one of the gears in the epicyclic gearing arrangement. The disk brake includes a hydraulic caliper or an electric caliper that can be actuated to slow down rotation of the disk to an eventual full stop and to hold the disk at full stop to thereby stop rotation of the propeller.


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