Bypass turbojet engine nacelle
A technology of turbojet and nacelle, applied in the direction of jet power plant, arrangement/installation of power plant, aircraft parts, etc.
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[0065] figure 1 and figure 2 A nacelle 1 for a bypass turbojet 2 is shown.
[0066] The nacelle 1 constitutes a tubular casing for bypassing the turbojet engine 2 and for guiding it through the air flow generated by the blades of the fan 3 , that is to say the hot air flow through the combustion chamber 4 of the turbojet engine 2 and out of the turbojet engine 2 of cold air.
[0067] The nacelle 1 has a structure comprising a front part forming an air intake structure 5 , a central part 6 surrounding a fan 3 of the turbojet engine 2 , and a rear part 7 surrounding the turbojet engine 2 . The air intake structure 5 has an inner surface 5a designed to guide the intake air and an outer rectifying surface 5b. The central part 6 comprises on the one hand an inner casing 6a enclosing the fan 3 of the turbojet engine 2 and on the other hand an outer fairing 6b of the casing extending the outer surface 5b of the air intake structure 5 .
[0068] The housing 6a is connected to the...
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