Thrust chamber liner and fabrication method therefor

A thrust chamber liner includes a metallic combustion chamber having an annular protrusion extending radially away from an exterior surface of the combustion chamber adjacent to its injector opening. A metallic nozzle is coupled to the combustion chamber at its throat opening. A composite material e...

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Bibliographische Detailangaben
Hauptverfasser:	Mireles, Omar R, Brandsmeier, William C. C, Medina, Cory R, Greene, Sandra Elam, Protz, Christopher Stephen, Jackson, Justin R, Gradl, Paul R
Format:	Patent
Sprache:	eng
Schlagworte:	ADDITIVE MANUFACTURING TECHNOLOGY ADDITIVE MANUFACTURING, i.e. MANUFACTURING OFTHREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVEAGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING,STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING ALLOYS BLASTING CASTING CHEMISTRY COMBUSTION ENGINES FERROUS OR NON-FERROUS ALLOYS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MAKING METALLIC POWDER MANUFACTURE OF ARTICLES FROM METALLIC POWDER MECHANICAL ENGINEERING METALLURGY PERFORMING OPERATIONS POWDER METALLURGY TRANSPORTING TREATMENT OF ALLOYS OR NON-FERROUS METALS WEAPONS WORKING METALLIC POWDER
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Beschreibung
Zusammenfassung:	A thrust chamber liner includes a metallic combustion chamber having an annular protrusion extending radially away from an exterior surface of the combustion chamber adjacent to its injector opening. A metallic nozzle is coupled to the combustion chamber at its throat opening. A composite material encases the exterior surface of the combustion chamber, but is only bonded to the annular protrusion.