METHOD AND A CIRCUIT FOR REGULATING A ROCKET ENGINE

Number of patents in Portfolio can not be more than 2000

United States of America Patent

APP PUB NO 20170101963A1
SERIAL NO

15288521

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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The invention relates to the field of rocket engines, and in particular to a method and a circuit for regulating a rocket engine (1) comprising at least one combustion chamber (3) and a first liquid propellant feed circuit (10) with a first pump (12) for pumping a first liquid propellant and a first turbine (14) for actuating the first pump (12), a first feed valve (15), and a regulator device for regulating the first turbine (14). In the regulation method and circuit, an opening command (DVCH) for opening the first feed valve (15) is calculated from an external command (Cext) in application of an open loop control relationship; a command for the regulator device of the first turbine (14) is calculated on the basis of said external command (Cext) and at least one feedback value, in application of a closed loop control relationship; and the first feed valve (15) and the regulator device of the first turbine (14) are controlled in application of the respective commands.

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Patent Owner(s)

Patent OwnerAddress
ARIANEGROUP SAS78130 LES MUREAUX

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
HAYOUN, David Montreal, CA 10 19
KLEIN, Manuel Vernon, FR 4 2
LE, GONIDEC Serge Vernon, FR 27 101
REICHSTADT, Sebastien Asnieres Sur Seine, FR 4 4

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