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INFRARED SUPPRESSOR OF HELICOPTER

机译:直升机红外抑制器

摘要

The present invention is the exhaust gas nozzle for guiding the gas discharged from the engine of the helicopter into the infrared suppression apparatus and the air suction pipe for introducing the outside air to cool the gas discharged from the exhaust gas nozzle and sucked through the air suction pipe An air induction pipe for guiding the outside air backward and a diffuser for mixing the gas and the outside air to be discharged in a specific direction, and a pairing for preventing the exhaust gas nozzle and the diffuser from being exposed to the outside. Helicopter infrared suppressor characterized in that, according to the invention there is an effect that can effectively suppress the infrared signal emitted from the helicopter while minimizing the size and weight of the infrared suppressor.
机译:本发明是用于将从直升机的发动机排出的气体引导到红外线抑制装置中的废气喷嘴和用于引入外部空气以冷却从废气喷嘴排出并通过吸气口吸入的气体的吸气管。管空气引导管,用于将外部空气向后引导;扩散器,其用于在特定方向上混合要被排放的气体和外部空气;以及一对,用于防止排气喷嘴和扩散器暴露于外部。直升机红外抑制器,其特征在于,根据本发明,具有在最小化红外抑制器的尺寸和重量的同时可以有效地抑制从直升机发射的红外信号的效果。

著录项

  • 公开/公告号KR101211289B1

    专利类型

  • 公开/公告日2012-12-11

    原文格式PDF

  • 申请/专利权人

    申请/专利号KR20100115508

  • 发明设计人 신필권;김형욱;정상원;황유상;

    申请日2010-11-19

  • 分类号B64D33/04;F02K1/82;F02K1/38;

  • 国家 KR

  • 入库时间 2022-08-21 16:28:03

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