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. 06, 2020

Filed:

Jul. 31, 2017
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

John R. Hull, Sammamish, WA (US);

James A. Grossnickle, Bellevue, WA (US);

Dejan Nikic, Seattle, WA (US);

Kevin G. Bowcutt, Aliso Viejo, CA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 7/00 (2006.01); F02K 7/14 (2006.01); B64D 27/16 (2006.01); F23R 3/28 (2006.01); F23R 3/02 (2006.01); F23R 7/00 (2006.01); F23D 11/32 (2006.01); F23K 5/08 (2006.01);
U.S. Cl.
CPC ...
F02K 7/14 (2013.01); B64D 27/16 (2013.01); F23D 11/32 (2013.01); F23K 5/08 (2013.01); F23R 3/02 (2013.01); F23R 3/28 (2013.01); F23R 7/00 (2013.01); F05D 2220/80 (2013.01); F05D 2240/128 (2013.01); F05D 2240/35 (2013.01); F05D 2260/99 (2013.01); F23K 2300/101 (2020.05);
Abstract

A scramjet includes a converging inlet, a combustor configured to introduce a fuel stream into an air stream in a combustion chamber and to combust the fuel air mixture stream to create an exhaust stream, and a diverging exit nozzle configured to accelerate the exhaust stream. The combustor includes a fuel injection system including at least one arcjet. A method of creating thrust for an aircraft includes compressing a supersonic incoming air stream in a converging inlet, injecting a fuel stream into the air stream in a combustion chamber to create a fuel air mixture stream, igniting the fuel air mixture stream to create an exhaust stream, and exhausting the exhaust stream from a diverging exit nozzle. The injecting the fuel stream into the air stream includes injecting the fuel stream at a fuel speed sufficient to create shear between the fuel stream and the air stream.


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