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:
May. 11, 2021

Filed:

Jul. 20, 2017
Applicant:

Aerojet Rocketdyne, Inc., Sacramento, CA (US);

Inventor:

Khin Phui, Sacramento, CA (US);

Assignee:

Aerojet Rocketdyne, Inc., Canoga Park, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 9/48 (2006.01); F04D 7/00 (2006.01); F04D 29/54 (2006.01); B64G 1/40 (2006.01); F04D 3/00 (2006.01);
U.S. Cl.
CPC ...
F02K 9/48 (2013.01); B64G 1/401 (2013.01); F04D 7/00 (2013.01); F04D 29/548 (2013.01); F04D 3/00 (2013.01); F05D 2260/60 (2013.01);
Abstract

A liquid propellant rocket engine includes a main turbo-pump and a boost turbo-pump. The main turbo-pump has a main pump with an outlet that is fluidly coupled with a supply line. The boost turbo-pump includes a housing, a rotor, a boost pump, and a turbine. The boost pump includes a first portion of the housing and a first portion the rotor. The turbine includes a second portion of the housing and a second portion of the rotor. The turbine has turbine blades attached to the second portion of the rotor and an inlet fluidly coupled with the supply line. The turbine has a plurality of circumferentially disposed feed lines defined by the second portion of the housing and not the first portion of the housing. The feed lines are fluidly coupled between the inlet and the turbine blades. The feed lines have an acute angle turn.


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