TURBOMACHINE ASSIST

Abstract

The invention relates to a protective cover (9) for the external surface of an aircraft turbomachine computer (8), said external surface of said computer (8) comprising a lower face (80) intended to be mounted on a housing of said turbomachine, and an upper face (81) opposite said lower face (80), said upper face (81) and lower face (80) being connected by a lateral perimeter comprising two opposing longitudinal faces (82) connected by two opposing transverse faces (83, 84), one of the longitudinal faces (82) being connected to one of the transverse faces (83, 84) by a corner recess forming an angle, the corner recess having a first corner face (85, 85') and a second corner face (86, 86'), the computer (8) being intended to be positioned in the vicinity of a bolted connection (7) provided opposite the first corner face (85, 85'). Figure 2.

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