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:
Mar. 18, 2025

Filed:

Dec. 26, 2023
Applicants:

Beijing Aeronautical Science & Technology Research Inst., Commercial Aircraft Corporation of China, Beijing, CN;

Commercial Aircraft Corporation of China, Ltd., Shanghai, CN;

Inventor:

Zheng Cui, Beijing, CN;

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/52 (2006.01); B64C 7/02 (2006.01); F02K 1/40 (2006.01); B64C 7/00 (2006.01);
U.S. Cl.
CPC ...
B64C 7/02 (2013.01); F02K 1/40 (2013.01); F02K 1/52 (2013.01); B64C 7/00 (2013.01); F05D 2220/36 (2013.01);
Abstract

A fan duct nozzle of an aviation turbofan engine. A notch is formed in a rear edge of an engine nacelle on an outer side of an engine pylon, and a flow guide curved surface matching the notch in shape is arranged on a profile of the fan duct nozzle. The notch is unilaterally formed in the outer side of the engine pylon, and a transition section between the notch and the rear edge of the engine nacelle includes two transition rounded corners. The present disclosure adopts a unilateral notch-shaped nozzle in the external duct of the turbofan engine, uses high-speed flowing of venting by an engine fan to provide flowing protection for an airfoil, improves a lift coefficient, and reduces negative impact on the airfoil exerted by the engine nacelle at a high incidence, thus lowering resistance, lowering a weight of the nacelle, and improving a lift-drag ratio.


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