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:
Mar. 07, 2023

Filed:

Aug. 26, 2021
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Benjamin Mohankumar, Cambridge, GB;

Mark J. Wilson, Kirby-in-Ashfield, GB;

Cesare A. Hall, Cambridge, GB;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); B64D 27/10 (2006.01); B64D 27/24 (2006.01); B64D 33/02 (2006.01); F02K 3/075 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
F01D 5/141 (2013.01); B64D 27/10 (2013.01); B64D 27/24 (2013.01); F05D 2220/323 (2013.01); F05D 2240/30 (2013.01);
Abstract

An aircraft engine comprising a fan, the fan having a diameter D and including a plurality of fan blades, the fan blades having a sweep metric S, each fan blade having a leading edge, and a forward-most portion on the leading edge of each fan blade being in a first reference plane. The aircraft engine further comprises a nacelle, comprising an intake portion forward of the fan, a forward edge on the intake portion being in a second reference plane, wherein the intake portion has a length L measured along an axis of the aircraft engine between the first reference plane and the second reference plane, the aircraft engine having a cruise design point condition M, wherein Mis between 0.4 and 0.93, and L/D is between 0.2 and 0.45.


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