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.
Patent No.:
Date of Patent:
Dec. 08, 2020
Filed:
Jul. 06, 2018
Applicant:
Safran Aircraft Engines, Paris, FR;
Inventors:
Philippe Gerard Chanez, Moissy-Cramayel, FR;
Claude Sensiau, Moissy-Cramayel, FR;
Assignee:
Safran Aircraft Engines, Paris, FR;
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 3/06 (2006.01); F02C 7/045 (2006.01); F02C 3/107 (2006.01); F02C 7/36 (2006.01); F02C 7/04 (2006.01);
U.S. Cl.
CPC ...
F02K 3/06 (2013.01); F02C 3/107 (2013.01); F02C 7/04 (2013.01); F02C 7/36 (2013.01); F05D 2220/323 (2013.01); F05D 2240/14 (2013.01); F05D 2260/40311 (2013.01); F05D 2260/606 (2013.01);
Abstract
A double flow turbojet includes a fan including a disk centered on an axis of the fan which is provided with fan blades on its periphery, the blades having a leading edge, and an air inlet sleeve extending upstream of the fan and configured to delimit a gas flow designed to enter into the fan the air inlet sleeve having a collecting surface, the turbojet having an aspect ratio included in the interval where L/D is the form factor of the air inlet sleeve.