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. 07, 2019

Filed:

Jul. 07, 2016
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Ninad Joshi, Brampton, CA;

Gaetan Girard, Outremont, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/82 (2006.01); F02K 1/42 (2006.01); F01D 25/30 (2006.01); F02K 3/04 (2006.01);
U.S. Cl.
CPC ...
F02K 1/827 (2013.01); F01D 25/30 (2013.01); F02K 3/04 (2013.01); F05D 2250/63 (2013.01); F05D 2260/96 (2013.01); F05D 2300/516 (2013.01); Y02T 50/671 (2013.01);
Abstract

A nacelle exhaust nozzle having a deployable noise-reducing component is described. The noise-reducing component includes an annular perforated sleeve coinciding with the inner nacelle loft line and circumscribing a mixed exhaust gas flow exiting the nacelle. The annular perforated sleeve is radially spaced apart from of a displaceable wall of an inflatable envelope that is displaceable between a deployed position, wherein noise-reduction is active, and a retracted position, wherein noise-reduction is inactive. When the inflatable envelope is pressurized, portions of the displaceable wall project through openings in the perforated sleeve and into the exhaust gas flow to form a rough surface at the loft line which causes a reduction in noise level. The portions of the displaceable wall that project through the openings in the perforated sleeve when the inflatable enveloped is pressurized include a plurality of dimples formed on the inner wall and forming the rough surface.


Find Patent Forward Citations

Joshi, Ninad. (2019). Gas turbine exhaust having reduced jet noise (U.S. Patent No. 10280871). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10280871

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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