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:
Oct. 22, 2024

Filed:

Aug. 26, 2020
Applicant:

Nanjing University of Aeronautics and Astronautics, Jiangsu, CN;

Inventors:

Yue Zhang, Jiangsu, CN;

Huijun Tan, Jiangsu, CN;

Chao Wang, Jiangsu, CN;

Chao Li, Jiangsu, CN;

Liang Chen, Jiangsu, CN;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 33/02 (2006.01); F02C 7/042 (2006.01); F02C 7/057 (2006.01);
U.S. Cl.
CPC ...
F02C 7/042 (2013.01); B64D 33/02 (2013.01); F02C 7/057 (2013.01); B64D 2033/026 (2013.01); Y10T 137/0536 (2015.04);
Abstract

The present invention discloses an internal-parallel inlet with mode conversion combined with variable geometry adjustment, which comprises a high-speed channel, a low-speed channel, a mode conversion component, a variable geometry component and a motor actuating component. When the inlet is in a low-speed mode, the variable geometry component adjusts the throat area and the internal contraction ratio of the inlet. When the flight Mach number is in a range of the mode conversion Mach number, the mode conversion component and the variable geometry component work simultaneously. When the inlet is in a high-speed mode, the mode conversion component is combined with the variable geometry component to adjust the throat area and the internal contraction ratio of the inlet. The present invention also provides a method for controlling the inlet.


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