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:
Feb. 24, 2026

Filed:

Oct. 02, 2024
Applicant:

Venus Aerospace Corp., Houston, TX (US);

Inventors:

William Thomas Ross, Houston, TX (US);

Sibylle Frederike Walter, Houston, TX (US);

Assignee:

Venus Aerospace Corp., Houston, TX (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F02K 7/18 (2006.01); F02C 6/08 (2006.01); F02C 9/18 (2006.01); F02C 9/52 (2006.01); F02K 7/12 (2006.01); F02K 7/16 (2006.01); F02K 7/20 (2006.01); F02K 9/66 (2006.01); F02K 9/78 (2006.01);
U.S. Cl.
CPC ...
F02K 7/18 (2013.01); F02C 6/08 (2013.01); F02C 9/18 (2013.01); F02C 9/52 (2013.01); F02K 7/12 (2013.01); F02K 7/16 (2013.01); F02K 7/20 (2013.01); F02K 9/66 (2013.01); F02K 9/78 (2013.01); F05D 2220/10 (2013.01);
Abstract

A rocket-based combined cycle propulsion system comprising an air inlet and a centerbody extending along a center axis. The centerbody at least partially defines the air inlet. The system further includes a first propulsion system (e.g., a rotating detonation rocket engine, RDRE) and a second propulsion system (e.g., a scramjet) coupled with the first propulsion system. The system further includes an air bleed assembly including an inlet aperture formed in the centerbody, an outlet aperture positioned in the first propulsion system, and a duct fluidly connecting the inlet aperture and the outlet aperture.


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