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:
Sep. 11, 2018

Filed:

Nov. 04, 2013
Applicant:

Snecma, Paris, FR;

Inventors:

Jean Michel Sannino, Saint-marcel, FR;

François Lassoudiere, Vernon, FR;

David Hayoun, Paris, FR;

Assignee:

Arianegroup SAS, Paris, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 9/48 (2006.01); F02K 9/50 (2006.01); F02K 9/97 (2006.01); F02K 9/64 (2006.01);
U.S. Cl.
CPC ...
F02K 9/48 (2013.01); F02K 9/50 (2013.01); F02K 9/64 (2013.01); F02K 9/972 (2013.01);
Abstract

The invention relates to a feed device for feeding a thrust chamber () of a rocket engine () with first and second propellants. According to the invention, a first feed circuit () of the thrust chamber () comprises a turbopump () having at least one pump () for pumping the first propellant from a first tank (), and a turbine () mechanically coupled to said pump (). The first feed circuit connects an outlet of the pump to an inlet of the turbine via a heat exchanger () configured to heat the first propellant with heat generated by the thrust chamber, in order to actuate the turbine. According to the invention, a second feed circuit () is configured to feed the thrust chamber with second propellant from a second tank () that is configured to be pressurized. The invention also provides a method of feeding a rocket engine thrust chamber with first and second propellants.


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