Loading patent…
AssigneeArianegroup SAS
InventorChris Udo Maeding
Estimating the term…
A combustion chamber section (110) for a combustion chamber (100) for a rocket engine (10) is described, the combustion chambersection (110) comprising a combustion chamber body (120) enclosing a combustion chamber volume and having coolant channels (130) disposed therein, and at least one baffle (140) integrally formed with the combustion chamber body (120) and projecting from the combustion chamber body (120) into the interior of the combustion chamber. The at least one baffle (140) comprises at least one coolant channel (133-135) fluidly connected to at least one of the coolant channels (130) in the combustion chamber body (120). Furthermore, an additive layer manufacturing method for manufacturing such a combustion chamber section is described.
A combustion chamber section for a combustion chamber for a rocket engine, the combustion chamber section comprising:
(canceled)
(canceled)
A method of manufacturing a combustion chamber section including a combustion chamber body which encloses a combustion chamber volume and in which coolant channels are arranged, a baffle formed integrally with the combustion chamber body and projecting from the combustion chamber body into the interior of the combustion chamber, the baffle includes at least one coolant channel fluidly connected to at least one of the coolant channels in the combustion chamber body, the method comprising:
Dependencies are inferred from the claim text.