TURBINE ENGINE COMPRISING IMPROVED HARNESS SUPPORT MEANS

TURBINE ENGINE COMPRISING IMPROVED HARNESS SUPPORT MEANS

The invention relates to an aircraft turbine engine (10) with main axis A, comprising: an arm (18) that is radial with respect to the main axis A, extending through an air flow duct (14); a support wall (22) belonging to the radial arm (18) and which has two openings (24); a plurality of electric ha...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: MATHIAS, Cyrille François Antoine, TAN, Khy, THEBAUD, Edouard, HOBALLAH, Samy Alexandre, GASPAR, Patrice
Format: Patent
Sprache:eng ; fre
Schlagworte:
BLASTING
ENGINE PLANTS IN GENERAL
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:The invention relates to an aircraft turbine engine (10) with main axis A, comprising: an arm (18) that is radial with respect to the main axis A, extending through an air flow duct (14); a support wall (22) belonging to the radial arm (18) and which has two openings (24); a plurality of electric harnesses (16) extending partially through the radial arm (18) and for which a section (26) of each harness (16) is secured to the support wall (22) of the arm (18); characterised in that it comprises two mounting blocks (20) each of which mounting block (20) is associated with a group of sections (26) of harness (16). L'invention concerne une turbomachine (10) d'aéronef d'axe principal A comportant : un bras radial (18) par rapport à l'axe principal A s'étendant au travers d'une veine (14) d'écoulement d'air; une paroi de support (22) appartenant au bras radial (18) et qui comporte deux ouvertures (24); une pluralité de harnais (16) électriques s'étendant en partie au travers du bras radial (18) et dont un tronçon (26) de chaque harnais (16) est fixé à ladite paroi de support (22) du bras (18); caractérisée en ce qu'elle comporte deux blocs de montage (20) dont chaque bloc de montage (20) est associé à un groupe de tronçons (26) de harnais (16).