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:
Apr. 05, 2022

Filed:

Jul. 30, 2018
Applicant:

Safran Aero Boosters SA, Herstal, BE;

Inventors:

Mathieu Chenoux, Arlon, BE;

Nicolas Fellin, Marchin, BE;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B33Y 80/00 (2015.01); B33Y 10/00 (2015.01); F01D 25/20 (2006.01); B22F 5/10 (2006.01); F02C 7/06 (2006.01);
U.S. Cl.
CPC ...
F01D 25/20 (2013.01); B22F 5/106 (2013.01); B33Y 10/00 (2014.12); B33Y 80/00 (2014.12); F02C 7/06 (2013.01); F05D 2220/323 (2013.01); F05D 2230/22 (2013.01); F05D 2230/72 (2013.01); F05D 2260/60 (2013.01); F05D 2260/98 (2013.01);
Abstract

An aircraft bypass turbojet engine lubrication unit includes from three to five superposed pumps, a body housing the pumps and an internal passage in the body for communicating with each of the pumps. The material of the body exhibits a stack of layers in a direction of stacking, the pumps being housed in the said stack of layers. The passage exhibits an end in the direction of stacking of the layers and an internal profile, for example triangular, with two straight lines which form the said end and which are inclined with respect to the stacked layers. The lubrication unit may be manufactured by additive manufacturing in layers.


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