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:
Jun. 04, 2019

Filed:

Jan. 15, 2016
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Naimishkumar B. Harpal, Everett, WA (US);

Chen Chuck, Mercer Island, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/72 (2006.01); F02K 1/70 (2006.01); B64D 29/02 (2006.01); B64D 29/04 (2006.01); B64D 33/04 (2006.01); F02K 1/62 (2006.01);
U.S. Cl.
CPC ...
F02K 1/72 (2013.01); B64D 29/02 (2013.01); B64D 29/04 (2013.01); B64D 33/04 (2013.01); F02K 1/625 (2013.01); F02K 1/70 (2013.01); F05D 2240/129 (2013.01);
Abstract

Systems and methods are provided for a formed thrust reverser cascade. The formed thrust reverser cascade may be coupled to an aircraft propulsor and may include a first portion disposed at a first angle to a portion of the aircraft propulsor and a second portion disposed at a second angle to the first portion. The formed thrust reverser cascade may be circumferentially disposed around a core engine of the aircraft propulsor. The formed thrust reverser cascades may be retrofitted to aircraft propulsors using linear thrust reverser cascade and may increase airflow through the formed thrust reverser cascade due to a greater throat area as compared to the linear thrust reverser cascade. Alternatively, the formed thrust reverser cascades may allow for shorter cascades while retaining the same performance, thus resulting in shorter nacelles.


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