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:
Sep. 23, 2025

Filed:

Dec. 23, 2023
Applicants:

Purdue Research Foundation, West Lafayette, IN (US);

University of Notre Dame Du Lac, South Bend, IN (US);

Inventors:

Mark Edward Noftz, Villa Park, IL (US);

Joseph Stephen Jewell, West Lafayette, IN (US);

Andrew James Shuck, Indianapolis, IN (US);

Jonathan Poggie, West Lafayette, IN (US);

Andrew Nixon Bustard, South Bend, IN (US);

Thomas James Juliano, Granger, IN (US);

Assignees:

Purdue Research Foundation, West Lafayette, IN (US);

University of Notre Dame Du Lac, South Bend, IN (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F02K 7/10 (2006.01);
U.S. Cl.
CPC ...
F02K 7/10 (2013.01);
Abstract

Systems and methods capable for use in the development of high-speed, shape-transitioning, inward-turning inlets for air-breathing hypersonic vehicles, and inlets formed thereby. The systems and methods preferably provide for designing high-speed inlets for air-breathing hypersonic vehicles, wherein unique solutions are defined in each osculating plane of the inlet. Such systems and methods optionally provide an optimization process for tuning the post throat-shock Mach number of the inlet, and/or designs a shock-capture surface using a parallel-streamlines methodology, and/or a double cowl-lip geometry to allow flow to spill overboard.


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