发明名称 INTEGRAL ENGINE INTAKE-PORT ACOUSTIC BARREL
摘要 PURPOSE: To reduce the stress concentration at a splice by providing a one-piece engine inlet acoustic barrel comprising an inner surface sheet, a core structure, and a solid face sheet outwardly from the barrel side, and extending the splice from a forward end to a rear end. CONSTITUTION: A one-piece engine inlet acoustic barrel is provided with an integrated engine-mountable flange 20 in which an engine frame is mounted on a rear end, a fireproof wall ring frame fitting flange 21, an L. E. to a forward end and a ring frame fitting flange 22. It comprises a perforated surface sheet 25, a honeycomb core 25 and a solid surface sheet 23. The surface sheets 23, 25 are formed of graphite/epoxy, and the core structure 24 is formed to be of honeycomb type so that at a narrow single fore-to-aft splice, or no splice at all, is present in a finished product. The splice may be integrated. The acoustic modal content remains unaffected, thus, preserving a high degree of liner effectiveness, increasing the total active acoustic area of the barrel while decreasing its weight, and increasing its durability.
申请公布号 JPH06280614(A) 申请公布日期 1994.10.04
申请号 JP19930305514 申请日期 1993.12.06
申请人 GRUMMAN AEROSPACE CORP 发明人 ROBAATO ERON ANDAASON;CHIYAARUZU EE PARENTE
分类号 F02C7/00;F02C7/04;F02C7/045;F02K1/82;(IPC1-7):F02C7/045 主分类号 F02C7/00
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