专利名称:Apparatus and method for reducing noise
emissions from a gas turbine engine inlet
发明人:Dougherty, Robert P.申请号:EP97202179.4申请日:19970711公开号:EP08237A1公开日:19980211
专利附图:
摘要:Noise attenuating linings for a turbofan engine inlet are installed around theupper crown area (94,92) and/or around the lower lip (112-116). The acoustical lining atthe upper crown area (90-91) attenuates those fan noise emissions which are normally
reflected from the crown area downward toward the ground. The acoustical lining at thelower inlet lip (111-106) attenuates those fan noise emissions which travel along the innersurface of the lip and are diffracted around the lower lip downward toward the ground.
申请人:THE BOEING COMPANY
地址:P.O. Box 3707, M.S. 13-08 Seattle, Washington 98124-2207 US
国籍:US
代理机构:Land, Addick Adrianus Gosling
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