DISPOSITIF D'EQUILIBRAGE MOTEUR POUR CAPOT D'ENTREE DE TURBOMACHINE

The device has a ferrule (300) that includes a main body (301) having an overall annular form. A balancing disk (307) is placed in the main body. The balancing disk is arranged with a set of drillings (310), where each drilling is ready to receive a balancing screw that is placed axially. Another ba...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	ROGUES, FREDERIC, KIENER-CALVET, BENJAMIN, BOIS, STEPHANE
Format:	Patent
Sprache:	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 ENGINE PLANTS IN GENERAL 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 INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES 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 device has a ferrule (300) that includes a main body (301) having an overall annular form. A balancing disk (307) is placed in the main body. The balancing disk is arranged with a set of drillings (310), where each drilling is ready to receive a balancing screw that is placed axially. Another balancing screw is arranged in the device, where the balancing screws are provided in an identical manner. A runner extends radially towards the interior of the balancing disk. The number of drillings is provided higher than 36. An independent claim is also included for an inlet cowl.