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:
Mar. 07, 2023

Filed:

Dec. 01, 2021
Applicant:

Korea Aerospace Research Institute, Daejeon, KR;

Inventors:

Keum Oh Lee, Daejeon, KR;

Byoung Jik Lim, Daejeon, KR;

Jun Sung Lee, Daejeon, KR;

Kee Joo Lee, Daejeon, KR;

Jae Sung Park, Daejeon, KR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 9/64 (2006.01); F02K 9/97 (2006.01); F02K 9/44 (2006.01);
U.S. Cl.
CPC ...
F02K 9/64 (2013.01); F02K 9/44 (2013.01); F02K 9/97 (2013.01);
Abstract

A combustor of a liquid rocket engine includes a nozzle unit including a regenerative cooling channel, in which the nozzle unit includes a fuel manifold outer shell, a combustor inner shell, and a combustor outer shell having a downward channel inlet, and the combustor includes a fuel inlet connected to a nozzle neck of the nozzle unit, a fuel manifold formed between the fuel manifold outer shell and the combustor outer shell, and in which fuel introduced from the fuel inlet flows, a downward channel connected in communication with the fuel manifold through the downward channel inlet, and extending in a downward direction from an upper portion of the combustor, a diverting manifold provided at a distal end of the nozzle unit and connected in communication with the downward channel, and an upward channel connected in communication with the diverting manifold and extending in an upward direction of the combustor.


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