Liquid rocket engine with hybrid electric motor driven pump

US9964073B1 · US · B1

Patent metadata
FieldValue
Publication numberUS-9964073-B1
Application numberUS-201414548598-A
CountryUS
Kind codeB1
Filing dateNov 20, 2014
Priority dateNov 6, 2014
Publication dateMay 8, 2018
Grant dateMay 8, 2018

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A nuclear thermal rocket with a superconducting electric motor driven boost pump submerged within a tank of liquid hydrogen, where the boost pump is driven by both an electric motor and a turbine. The boost pump can be submerged in liquid hydrogen so that the electric motor operates as a superconducting motor. Also, a turbopump for a rocket engine can include both a turbine and an electric motor to drive the liquid oxidizer and liquid fuel pumps of the turbopump.

First claim

Opening claim text (preview).

We claim the following: 1. A boost pump for a liquid rocket engine, the boost pump comprises: a blade to pressurize a cryogenic liquid; an electric motor to drive the blade of the boost pump; a turbine connected to a rotor of the blade to drive the blade of the boost pump; an electric motor controller to control operation of the electric motor of the boost pump; and the electric motor is reversed to be a generator and generator power is discharged to a resistive load bank. 2. The boost pump of claim 1 and further comprising: the motor controller can demand more or less power to either slow or speed up the boost pump in order to suppress cavitation. 3. A liquid rocket engine comprising: a combustion chamber to produce a hot gas from combining a liquid fuel with a liquid oxidizer; a turbopump with a gas turbine driving both a liquid fuel pump and a liquid oxidizer pump; a boost pump having an outlet connected to an inlet of the liquid oxidizer pump to provide pressurized liquid oxidizer to the liquid oxidizer pump to prevent cavitation; an electric motor/generator connected to the boost pump to drive the boost pump or be driven by the boost pump and produce electrical power; a battery to receive electrical power from the electric motor/generator to charge the battery; a resistor/load bank to dissipate electrical power produced by the electric motor/generator; a heat exchanger around the combustion chamber to pass liquid fuel; and, the liquid fuel that is passed through the heat exchanger is also passed through the resistor/load bank to cool the resistor/load bank.

Assignees

Inventors

Classifications

  • the pump and drive motor are both submerged · CPC title

  • F02K9/46Primary

    using pumps · CPC title

  • Pumps adapted for handling specific fluids, e.g. by selection of specific materials for pumps or pump parts (F04D11/005, F04D29/22 take precedence) · CPC title

  • the pump being fluid driven · CPC title

  • the pump being electrically driven · CPC title

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What does patent US9964073B1 cover?
A nuclear thermal rocket with a superconducting electric motor driven boost pump submerged within a tank of liquid hydrogen, where the boost pump is driven by both an electric motor and a turbine. The boost pump can be submerged in liquid hydrogen so that the electric motor operates as a superconducting motor. Also, a turbopump for a rocket engine can include both a turbine and an electric moto…
Who is the assignee on this patent?
Pinera Alejandro, Miller Timothy J, Florida Turbine Tech Inc
What technology area does this patent fall under?
Primary CPC classification F02K9/46. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue May 08 2018 00:00:00 GMT+0000 (Coordinated Universal Time) (B1). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).