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:
May. 25, 2021

Filed:

Feb. 02, 2018
Applicant:

United 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, W. Hartford, CT (US);

Assignee:

RAYTHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 3/068 (2006.01); F01D 25/24 (2006.01); F02C 7/04 (2006.01);
U.S. Cl.
CPC ...
F02K 3/068 (2013.01); F01D 25/24 (2013.01); F02C 7/04 (2013.01); F05D 2220/36 (2013.01); F05D 2240/303 (2013.01); F05D 2260/40311 (2013.01); F05D 2260/96 (2013.01); Y02T 50/60 (2013.01);
Abstract

According to an example embodiment, a gas turbine engine assembly includes, 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 that is based on a dimension of the fan blades, 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 turbine section including a high pressure turbine and a low pressure turbine, the low pressure turbine driving the fan, a 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 measured along an engine axis between the first reference plane and the second reference plane. A dimensional relationship of L/D is no more than 0.45.


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