发明名称 EXHAUST GAS INFRARED RADIATION SUPPRESSOR FOR A GAS TURBINE ENGINE
摘要 An IR suppressor produces a thin "ribbon" exhaust plume using a tapered exhaust manifold (3) which has a plurality of discrete exhaust nozzles (6) that are longitudinally aligned with the exhaust manifold (3). Optionally, the nozzles (6) extend within but are spaced apart from mixing ducts (15) which are open to the ambient air at both ends. The mixing ducts (15)mix ambient air with the exhaust plume. For use in a helicopter the IR suppressor is rotatable so that the exhaust can be directed substantially parallel to the helicopter blades when the blades are not turning to protect them from exhaust heat.
申请公布号 IL94322(A) 申请公布日期 1993.07.08
申请号 IL19900094322 申请日期 1990.05.08
申请人 UNITED TECHNOLOGIES CORPORATION 发明人
分类号 F41H11/02;B64D7/00;B64D33/04;F02C7/00;F02K1/82 主分类号 F41H11/02
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