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. 21, 2019

Filed:

May. 25, 2016
Applicant:

Honeywell International Inc., Morris Plains, NJ (US);

Inventors:

Nick Nolcheff, Chandler, AZ (US);

Michael LaMar Trego, Mesa, AZ (US);

John Repp, Gilbert, AZ (US);

James Kroeger, Tempe, AZ (US);

Assignee:

HONEYWELL INTERNATIONAL INC., Morris Plains, NJ (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/16 (2006.01); F01D 5/34 (2006.01); F02C 3/08 (2006.01); F04D 17/02 (2006.01); F04D 19/00 (2006.01); F04D 19/02 (2006.01); F04D 29/32 (2006.01); F04D 29/38 (2006.01); F04D 29/66 (2006.01);
U.S. Cl.
CPC ...
F04D 29/668 (2013.01); F01D 5/16 (2013.01); F01D 5/34 (2013.01); F02C 3/08 (2013.01); F04D 17/025 (2013.01); F04D 19/002 (2013.01); F04D 19/02 (2013.01); F04D 29/321 (2013.01); F04D 29/325 (2013.01); F04D 29/328 (2013.01); F04D 29/38 (2013.01); F04D 29/666 (2013.01); F05D 2220/30 (2013.01); F05D 2220/36 (2013.01); F05D 2260/96 (2013.01); Y02T 50/671 (2013.01); Y02T 50/673 (2013.01);
Abstract

A blisk fan is provided for a turbine engine propulsion system. The blisk fan includes a hub configured to rotate about a rotational axis at a maximum rotational speed, and a plurality of blades extending radially outward from the hub to define a fan leading edge tip diameter. Each of the blades has a first vibratory mode at a natural frequency, which is greater than a first fan order and less than a second fan order at the maximum rotational speed. The compression system preferably has a balance factor of the compression system between 1.9 and 3.2.


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