AIR TURBINE STARTER WITH NOZZLE RETENTION MECHANISM

An air turbine starter (10) having a housing (78) defining an interior (28) with a primary inlet (32) and a primary outlet (34) to define a primary air flow path (36) from the primary inlet (32) to the primary outlet (34). A nozzle (42) is located within the interior (28) and has circumferentially s...

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Bibliographische Detailangaben
Hauptverfasser:	KOLLAM, Ramana Reddy, DRANSCHAK, David, YAMARTHI, David Raju, KERLEY, Steven, RICKERT, Mark, CHHABRA, Parmeet Singh
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 GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	An air turbine starter (10) having a housing (78) defining an interior (28) with a primary inlet (32) and a primary outlet (34) to define a primary air flow path (36) from the primary inlet (32) to the primary outlet (34). A nozzle (42) is located within the interior (28) and has circumferentially spaced vanes (50). A shroud (44) is also located within the interior (28) and circumscribes at least a portion of the vanes (50). A retention mechanism (44) constrains the axial movement of nozzle (42).