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:
Feb. 19, 2019

Filed:

Apr. 05, 2016
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventor:

David A. Welch, Quaker Hill, CT (US);

Assignee:

United Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/30 (2006.01); F02K 3/06 (2006.01); F02C 7/04 (2006.01); F04D 29/32 (2006.01); F04D 29/64 (2006.01); F01D 5/32 (2006.01);
U.S. Cl.
CPC ...
F02K 3/06 (2013.01); F01D 5/3007 (2013.01); F02C 7/04 (2013.01); F04D 29/322 (2013.01); F04D 29/644 (2013.01); F01D 5/3023 (2013.01); F01D 5/3053 (2013.01); F01D 5/323 (2013.01); F01D 5/326 (2013.01); F05D 2220/36 (2013.01); F05D 2230/70 (2013.01);
Abstract

A gas turbine engine includes a fan forward of a primary flowpath inlet. The fan includes multiple fan blades distributed radially about, and connected to, a hub. A fan nacelle is positioned radially outward of the fan and includes an inner diameter. The inner diameter is sloped relative to an engine axis such that a forward portion of the fan nacelle has a smaller inner diameter than an aft portion of the fan nacelle. A fan blade spacer is disposed between a radially inward facing surface of at least one fan blade and a radially outward facing surface of the hub. The fan blade spacer has a radial thickness at least equal to a slope drop of the fan nacelle.


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