Rotating inlet cowl for turbine engine i.e. jet engine, of aircraft, has front end taking shape of rod, where rod comprises axis parallely merged with rotation axis and made of inconel alloy

The cowl (30) has a front end taking shape of a rod (44), where length of the rod ranges between 50 and 150 mm and average diameter of the rod is lower than 15 mm. The rod comprises an axis (46) parallely merged with a rotation axis (34), where the rod, a nose cone (32) and a back ferrule (36) are a...

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Bibliographische Detailangaben
Hauptverfasser:	LORO GAEL, GIGNOUX HERVE, WINTENBERGER SYLVIE, DELAPIERRE MICKAEL
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE WEAPONS
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Beschreibung
Zusammenfassung:	The cowl (30) has a front end taking shape of a rod (44), where length of the rod ranges between 50 and 150 mm and average diameter of the rod is lower than 15 mm. The rod comprises an axis (46) parallely merged with a rotation axis (34), where the rod, a nose cone (32) and a back ferrule (36) are arranged from front to rear of the cowl. The rod is made of inconel alloy. La présente invention se rapporte à un capot d'entrée tournant (30) pour turbomachine, dont l'extrémité avant prend la forme d'une tige (44), excentrée ou non vis-à-vis de l'axe de rotation de ce capot (30).