Coupling device for connecting the two half-shells of an aircraft engine nacelle, and nacelle equipped with such a device
A technology for engine nacelles and connecting devices, which is applied to aircraft power units, aircraft power unit components, and detachable inspection panels for power units, etc., which can solve the problems of increased weight and complexity by strengthening, and achieve the goal of reducing weight and complexity Effect
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[0032] now refer to figure 1 , figure 1 The right-hand half-shell 1 of the nacelle is shown, which in this case should be positioned at the rear of the nacelle and form part of a thrust reversal arrangement (it should be understood that the invention is also applicable in the case of a simple nacelle, i.e. nacelles without thrust reversers).
[0033] Reference signs AV and AR denote respectively the front and the rear of the half-shell 1 with respect to the flow direction of the air that should flow inside the half-shell 1 .
[0034] In this particular case, the half-shell 1 comprises an inner half-structure 3 delimiting a half-cavity C intended to house a jet engine (not shown).
[0035] The half-shell 1 also comprises an outer structure 5 which, together with the inner structure 3, defines a half-flow path V through which the flow of cold air flowing between the front and the rear of the half-shell 1 will travel.
[0036] In its upper part, that is to say in its part that...
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