Aerodynamic arm for aircraft turbine engine casing

The invention relates to an aerodynamic arm (100) for an aircraft turbine engine casing, characterized in that it comprises: a tubular outer shell (110) having a generally elongate shape extending substantially along an axis (A-A), the shell (110) comprising axial ends (112) for connecting to a turb...

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Bibliographische Detailangaben
1. Verfasser:	MISSOUT MARC
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	The invention relates to an aerodynamic arm (100) for an aircraft turbine engine casing, characterized in that it comprises: a tubular outer shell (110) having a generally elongate shape extending substantially along an axis (A-A), the shell (110) comprising axial ends (112) for connecting to a turbine engine casing; an electrically conductive core (120) extending inside the shell (110) and having ends for electrically connecting to each of the ends (112) of the shell (110); and an insulating material (130) configured to occupy a space provided between the core (120) and the shell (110). 本发明涉及一种用于飞行器涡轮发动机壳体的空气动力学臂(100)，其特征在于，该空气动力学臂包括：外部管状壳层(110)，该外部管状壳层具有基本上沿着轴线(A-A)延伸的大体细长的形状，壳层(110)包括用于连接到涡轮发动机壳体的轴向端部(112)；导电芯(120)，该导电芯在壳层(110)的内部延伸，并具有用于电连接到壳层(110)的端部(112)中的每个端部的端部；和绝缘材料(130)，该绝缘材料被构造成占据设置在芯(120)与壳层(110)之间的空间。