Air inflow lip for turbojet nacelle
A technology of turbojet and engine, which is applied to the combustion of the intake port of the power plant, engine function, jet propulsion device, etc., and can solve the problems of difficult pipeline integration and difficult sealing
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[0062] In the description and claims, the terms "upstream" and "downstream" are to be understood with respect to the circulation of the air flow inside the propulsion unit formed by the nacelle and the turbojet, that is to say with reference to figure 1 from left to right.
[0063] Likewise, the terms "inner" and "outer" will be used without limitation with reference to the radial distance relative to the longitudinal axis of the nacelle, the term "inner" defining the area radially closer to the longitudinal axis of the nacelle, the same as the term " External" on the contrary.
[0064] Furthermore, in the description and claims, the terms longitudinal, vertical and transverse will be used without limitation with reference to the trihedron L, V, T shown in the drawings for the purpose of clarifying the description and claims.
[0065] Furthermore, the same or similar reference numerals denote the same or similar components or component groups throughout the drawings.
[0066...
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