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EXHAUST GAS INFRARED RADIATION SUPPRESSOR FOR A GAS TURBINE ENGINE

机译:燃气轮机发动机的排气红外辐射抑制器

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.
机译:IR抑制器使用锥形排气歧管(3)产生细的“丝带”排气羽流,锥形排气歧管(3)具有与排气歧管(3)纵向对齐的多个离散排气喷嘴(6)。可选地,喷嘴(6)在混合管道(15)内延伸但与混合管道(15)隔开,该混合管道的两端均向周围空气敞开。混合管道(15)将环境空气与排气羽流混合。为了在直升飞机上使用,IR抑制器是可旋转的,因此当叶片不转动以保护其免受废热时,废气可被定向为基本上平行于直升飞机叶片。

著录项

  • 公开/公告号IL94322A

    专利类型

  • 公开/公告日1993-07-08

    原文格式PDF

  • 申请/专利权人 UNITED TECHNOLOGIES CORPORATION;

    申请/专利号IL19900094322

  • 发明设计人

    申请日1990-05-08

  • 分类号B64D33/04;F02K1/82;F01N7/08;

  • 国家 IL

  • 入库时间 2022-08-22 05:11:21

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