Seal-Free Multi-Metallic Thrust Chamber Liner

A thrust chamber liner includes a main combustion chamber (MCC) with MCC coolant channels extending axially there along. Each MCC coolant channel has a port at an outside surface of the MCC. A nozzle is integrated with the MCC. The nozzle has nozzle coolant channels extending axially there along. A...

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Bibliographische Detailangaben
Hauptverfasser:	Brandsmeier, William C. C, Medina, Cory R, Protz, Christopher Stephen, Greene, Sandra Elam, Gradl, Paul R
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LAYERED PRODUCTS LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	A thrust chamber liner includes a main combustion chamber (MCC) with MCC coolant channels extending axially there along. Each MCC coolant channel has a port at an outside surface of the MCC. A nozzle is integrated with the MCC. The nozzle has nozzle coolant channels extending axially there along. A coolant-supply manifold, integrated with one of the MCC and the MCC and nozzle, is in fluid communication with each port in the MCC coolant channels.