Air turbine starter with nozzle retention mechanism

An air turbine starter has a housing defining an interior having a primary inlet and a primary outlet to define a primary airflow path from the primary inlet to the primary outlet. A nozzle is located in the interior and has circumferentially spaced apart vanes. A shroud is also located in the inter...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	DRANSCHAK, DAVID, ALAN, CHHABRA PARMEET SINGH, KORAM RAMANA REDDY, RICHTER MARK LESLIE, YAMAS, DAVID, RAJU, KERLEY STEVEN RYAN
Format:	Patent
Sprache:	chi ; eng
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:	An air turbine starter has a housing defining an interior having a primary inlet and a primary outlet to define a primary airflow path from the primary inlet to the primary outlet. A nozzle is located in the interior and has circumferentially spaced apart vanes. A shroud is also located in the interior and circumscribes at least a portion of the vanes. The retention mechanism restricts axial movement of the nozzle. 一种空气涡轮启动器，其具有壳体，该壳体限定具有主进口和主出口的内部，以限定从主进口到主出口的主气流路径。喷嘴位于内部中并且具有周向间隔开的轮叶。护罩也位于内部中并与轮叶的至少一部分外接。保持机构约束喷嘴的轴向移动。