DETACHABLE AIR INTAKE FOR TURBOJET NACELLE Russian patent published in 2012 - IPC F02C7/04 B64D29/08 

FIELD: engines and pumps.

SUBSTANCE: turbojet nacelle comprises air intake directing airflow to turbojet blower and central compartment enveloping central compartment with air intake jointed thereto and aerodynamically conjugated therewith. Central compartment has jacket to cover blower and moving cowl to allow access inside nacelle. Air intake has inner panel secured by jacket to central compartment to make therewith a stationary structure and lengthwise outer panel plugged in to said stationary structure and including air intake edge. Outer panel may displace from working position into servicing position. In working position, outer panel is aerodynamically conjugated with central compartment outer assembly while air intake edge is aerodynamically conjugated with air intake inner panel. In servicing position, outer panel is shifted from central compartment assembly while air intake edge is shifted from air intake inner panel.

EFFECT: ease of servicing, access into nacelle every compartment.

20 cl, 31 dwg