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:
Nov. 30, 2021

Filed:

Feb. 06, 2018
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Antoine Jean-Philippe Beaujard, Moissy-Cramayel, FR;

Serge Benyamin, Moissy-Cramayel, FR;

Tewfik Boudebiza, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/16 (2006.01); F02C 7/06 (2006.01); F02K 3/02 (2006.01);
U.S. Cl.
CPC ...
F01D 25/162 (2013.01); F02C 7/06 (2013.01); F02K 3/025 (2013.01); F05D 2220/323 (2013.01); F05D 2220/3217 (2013.01); F05D 2240/54 (2013.01); F05D 2250/36 (2013.01);
Abstract

A turbojet includes an inlet casing, a low pressure compressor, a high pressure spool, a low pressure turbine, and an exhaust casing. The inlet casing and the low pressure compressor define an air inlet channel that divides downstream into a primary flow channel and a secondary flow channel. A low pressure shaft is supported by a first roller bearing, borne by the inlet casing, a second bearing borne by the intermediate casing, a third bearing borne by the exhaust casing, and an additional ball bearing borne by the intermediate casing and arranged between the first bearing and the second bearing. Such a configuration of bearings makes it possible to withstand an increased level of load and to be compatible with an increase in the rate of dilution.


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