CERAMIC MATRIX COMPOSITE NOZZLE MOUNTED WITH A STRUT

A nozzle assembly 130 is provided which is, in part, formed of a low coefficient of thermal expansion material. The assembly 130 includes a nozzle fairing 150 formed of the low coefficient of thermal expansion material and includes a metallic strut 170 extending radially through the nozzle fairing 1...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	RADWANSKI, Michael Todd, GLYNN, Christopher Charles, FREDERICK, Robert Alan, TUERTSCHER, Michael Ray, HUIZENGA, Benjamin Scott, PHELPS, Greg Scott, SENILE, Darrell Glenn
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	A nozzle assembly 130 is provided which is, in part, formed of a low coefficient of thermal expansion material. The assembly 130 includes a nozzle fairing 150 formed of the low coefficient of thermal expansion material and includes a metallic strut 170 extending radially through the nozzle fairing 150. Load is transferred from the nozzle fairing 150 to a static structure in either of two ways: first, the strut 170 may receive the load directly and/or second, load may be transferred from the nozzle fairing 150 to at least one of the inner and outer support rings 140, 160. Further, the nozzle fairing 150 and strut 170 may allow for internal airflow for cooling.