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. 17, 2019

Filed:

Mar. 22, 2016
Applicant:

Safran Transmission Systems, Colombes, FR;

Inventors:

Lionel Bauduin, Houilles, FR;

Maxence Guillemont, Colombes, FR;

Julien Viel, Argenteuil, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16H 1/22 (2006.01); F02C 7/32 (2006.01); F16H 37/06 (2006.01);
U.S. Cl.
CPC ...
F16H 1/222 (2013.01); F02C 7/32 (2013.01); F16H 37/065 (2013.01); F05D 2250/313 (2013.01); F05D 2250/314 (2013.01); F05D 2260/4031 (2013.01); Y02T 50/671 (2013.01);
Abstract

A gearbox for an aircraft turbine engine includes a drive shaft, a secondary drive shaft coupled to the drive shaft with a reduction mechanism, and output shafts, each of which is coupled to the drive shaft or to the secondary drive shaft with a set of ring and pinion gears, wherein the reduction mechanism includes an intermediate shaft, a first end coupled to the drive shaft with a first stage of gears and the second end coupled to the secondary drive shaft with a second stage of gears, and wherein the intermediate shaft is rotatably mounted in the gearbox about the main axis thereof which is oriented substantially perpendicular to the main axis of the drive shaft.


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