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:
Jan. 07, 2020

Filed:

Apr. 08, 2016
Applicant:

Rocket Lab Usa, Inc., Los Angeles, CA (US);

Inventors:

Peter Joseph Beck, Auckland, NZ;

Lachlan Jesse Matchett, Auckland, NZ;

Peter William Edward Barlow, Napier, NZ;

Assignee:

Rocket Lab USA, Inc., Los Angeles, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 9/52 (2006.01); F02K 9/97 (2006.01); B33Y 10/00 (2015.01); B33Y 80/00 (2015.01); F02K 9/64 (2006.01); F28F 13/18 (2006.01); F28F 13/14 (2006.01);
U.S. Cl.
CPC ...
F02K 9/52 (2013.01); B33Y 10/00 (2014.12); B33Y 80/00 (2014.12); F02K 9/972 (2013.01); F02K 9/64 (2013.01); F05D 2230/31 (2013.01); F28F 13/14 (2013.01); F28F 13/185 (2013.01);
Abstract

Disclosed herein are various technologies pertinent to rocket engines, including injector, thrust chamber, and electrical turbopump devices that may be combined to provide a highly efficient rocket engine and methods of manufacturing such devices, such as additive manufacturing. The use of additive manufacturing techniques allows for injectors and thrust chambers with complex geometries that provide for more efficient engine operation, including, for example, thrust chambers with varying surface roughness within cooling passages thereof and injectors with multiple annular plenums.


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