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:
Oct. 10, 2023

Filed:

Sep. 23, 2021
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

Wesley K. Lord, South Glastonbury, CT (US);

Robert E. Malecki, Storrs, CT (US);

Yuan J. Qiu, Glastonbury, CT (US);

Becky E. Rose, Colchester, CT (US);

Jonathan Gilson, West Hartford, CT (US);

Assignee:

RTX CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 25/24 (2006.01); F02K 3/06 (2006.01); F01D 5/14 (2006.01); F02C 7/04 (2006.01); F01D 5/02 (2006.01); F01D 15/12 (2006.01); F01D 17/10 (2006.01);
U.S. Cl.
CPC ...
F01D 25/24 (2013.01); F01D 5/02 (2013.01); F01D 5/141 (2013.01); F01D 15/12 (2013.01); F01D 17/105 (2013.01); F02C 7/04 (2013.01); F02K 3/06 (2013.01); F05D 2220/32 (2013.01); F05D 2250/00 (2013.01); F05D 2260/40311 (2013.01); F05D 2260/96 (2013.01); Y02T 50/60 (2013.01);
Abstract

A gas turbine engine assembly may include, among other things, a fan section including a fan, the fan including a plurality of fan blades, a diameter of the fan having a dimension D, each fan blade having a leading edge, and a forward most portion on the leading edges of the fan blades in a first reference plane, a geared architecture, a turbine section including a high pressure turbine and a low pressure turbine, the low pressure turbine driving the fan through the geared architecture, a nacelle surrounding the fan, the nacelle including an inlet portion forward of the fan, a forward edge on the inlet portion in a second reference plane, and a length of the inlet portion having a dimension L between the first reference plane and the second reference plane. A dimensional relationship of L/D may be between 0.30 and 0.40.


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