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:
Oct. 22, 2019

Filed:

Oct. 18, 2016
Applicant:

Airbus Safran Launchers Sas, Issy-les-Moulineaux, FR;

Inventors:

Alban Du Tertre, Vernon, FR;

Didier Guichard, Menilles, FR;

Cedric Pierre Michel Thomas, Palaiseau, FR;

Assignee:

ARIANEGROUP SAS, Paris, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 9/52 (2006.01); F02K 9/64 (2006.01); F02K 9/97 (2006.01); B29C 70/34 (2006.01); B29C 70/48 (2006.01); B29L 31/30 (2006.01); B29K 101/10 (2006.01); B29K 307/04 (2006.01);
U.S. Cl.
CPC ...
F02K 9/64 (2013.01); B29C 70/345 (2013.01); B29C 70/48 (2013.01); F02K 9/52 (2013.01); F02K 9/972 (2013.01); B29K 2101/10 (2013.01); B29K 2307/04 (2013.01); B29L 2031/3097 (2013.01); F05D 2220/80 (2013.01); F05D 2230/30 (2013.01); F05D 2240/35 (2013.01); F05D 2300/603 (2013.01);
Abstract

A propulsion chamber for a liquid propellant rocket engine is provided. The propulsion chamber includes an inside wall made of metal, an outside covering made of organic matrix composite material, and a cooling circuit arranged between the outside covering and the inside wall. The propulsion chamber further includes at least a first axial endpiece secured to the metal inside wall and presenting at least one radial protrusion received in a concave recess in an inside face of the outside covering. The concave recess is situated axially between first and second belts of reinforcing fibers oriented substantially circumferentially in the outside covering in such a manner as to take up forces associated with inside pressure and thrust.


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