logo

For the Inventor, By the Inventor

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.

Patent No.:

US 10385777 B1

PDFFull Text
Date of Patent:
Aug. 20, 2019

Filed:

Jun. 25, 2013

Bifurcated inlet scoop for gas turbine engine

Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Hsianmin Jen, Woodbridge, CT (US);

Sergey Losyev, Waterbury, CT (US);

Assignee:

UNITED TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:

Cantor Colburn LLP

Primary Examiner:

Ninh H Nguyen

Assistant Examiner:

Wayne A Lambert

Int. Cl.
CPC ...
F02C 7/04 (2006.01); F01D 9/02 (2006.01); F01D 9/06 (2006.01); F02C 6/08 (2006.01); F02C 7/14 (2006.01); B64D 13/06 (2006.01);
U.S. Cl.
CPC ...
F02C 7/04 (2013.01); F01D 9/02 (2013.01); F01D 9/065 (2013.01); F02C 6/08 (2013.01); F02C 7/14 (2013.01); B64D 2013/0603 (2013.01); F05D 2220/36 (2013.01); F05D 2250/51 (2013.01); Y02T 50/675 (2013.01);
Abstract

A bifurcated inlet scoop frame for a gas turbine engine and method of using such frame for a gas turbine engine are disclosed. The bifurcated inlet scoop frame having a nose, a first side panel, and a second side panel. The first side panel and the nose defining a first inlet port. The second side panel and the nose defining a second inlet port. The method including the steps of providing a bifurcated inlet scoop frame, splitting the fan air flow, and receiving fan air through the bifurcated inlet scoop frame.

Find Patent Forward Citations

Quick Actions:

Jen, Hsianmin. (2019). Bifurcated inlet scoop for gas turbine engine (U.S. Patent No. 10385777). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10385777

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

Loading…