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:
Dec. 26, 2023

Filed:

Apr. 15, 2021
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

Christopher Britton Greene, Hebron, CT (US);

James M. Donohue, Glastonbury, CT (US);

Peter AT Cocks, South Glastonbury, CT (US);

Assignee:

RTX Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F23R 7/00 (2006.01); F02C 7/224 (2006.01); F23R 3/44 (2006.01); F23R 3/32 (2006.01); F23R 3/56 (2006.01); F02C 7/264 (2006.01); F02C 3/24 (2006.01); F02K 7/02 (2006.01); F02C 5/00 (2006.01);
U.S. Cl.
CPC ...
F02C 7/224 (2013.01); F02C 3/24 (2013.01); F02C 7/264 (2013.01); F23R 3/32 (2013.01); F23R 3/44 (2013.01); F23R 3/56 (2013.01); F23R 7/00 (2013.01); F02C 5/00 (2013.01); F02K 7/02 (2013.01); F05D 2240/36 (2013.01); F05D 2250/141 (2013.01); F05D 2260/232 (2013.01); F05D 2260/99 (2013.01); F23R 2900/03043 (2013.01);
Abstract

A method for operating a rotating detonation engine, having a radially outer wall extending along an axis; a radially inner wall extending along the axis, wherein the radially inner wall is positioned within the radially outer wall to define an annular detonation chamber having an inlet and an outlet, wherein the method includes flowing liquid phase fuel along at least one wall of the radially inner wall and the radially outer wall in a direction from the outlet toward the inlet to cool the at least one wall and heat the liquid fuel to provide a heated liquid fuel; flowing the heated liquid fuel to a mixer at the inlet to reduce pressure of the heated liquid fuel, flash vaporize the heated liquid fuel and mix flash vaporized fuel with oxidant to produce a vaporized fuel-oxidant mixture; and detonating the mixture in the annular detonation chamber.


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