FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, namely, to turbojet aircraft nacelle. Proposed nacelle comprises air intake to direct airflow towards turbojet blower and central structural element 5 that includes housing 9 embracing said blower and jointed to air intake. Noise absorbing appliance 13 is arranged on a part of said air intake to envelope said housing. Note here that clearance 14 is allowed for between said appliance and housing.
EFFECT: reduced vibration of nacelle.
11 cl, 9 dwg
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Authors
Dates
2011-11-10—Published
2007-02-27—Filed