Rigid bar for electrically connecting a machine in an aircraft turbine engine

Disclosed is an electrically conductive rigid bar (80) for electrically connecting an electric machine (70) of an aircraft turbine engine, characterised in that it comprises: -an elongate body (80a) made from electrically conductive material having a polygonal cross-section greater than or equal to...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	Guillotel, Loic Paul Yves, Delbosc, Philippe, Millier, Vincent Francois Georges
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING CONVERSION OR DISTRIBUTION OF ELECTRIC POWER DYNAMO-ELECTRIC MACHINES ELECTRICITY ENGINE PLANTS IN GENERAL GENERATION HEATING 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:	Disclosed is an electrically conductive rigid bar (80) for electrically connecting an electric machine (70) of an aircraft turbine engine, characterised in that it comprises: -an elongate body (80a) made from electrically conductive material having a polygonal cross-section greater than or equal to 50 mm2, and- an electrical insulation sheath (80b) that surrounds the body, at least one of the longitudinal ends (84a) of the body not being covered by the sheath and comprising a through-hole (86) in which a bolt (88) for fastening and electrically connecting this end is mounted.