INNER COWL STRUCTURE FOR AIRCRAFT TURBINE ENGINE

摘要

PROBLEM TO BE SOLVED: To provide an inner cowl structure having advantages of low cost design and a simple structure.SOLUTION: An inner cowl structure for circumscribing at least a portion of a jet engine extending from an aircraft includes an apron disposed directly on the engine 10 independently of the pylon to cover an upper portion of the jet engine, and an inner body configured to circumscribe a portion of the jet engine not circumscribed by the apron.