HELICOPTER ENGINE AIR INTAKE WITH IMPROVED BYPASS FLOW

• 1. 一种直升机用发动机进气装置及直升机 [P] . 中国专利： CN207195037U . 2018.04.06
• 2. 一种直升机用发动机进气装置及直升机 [P] . 中国专利： CN107120193A . 2017-09-01
• 3. HELICOPTER ENGINE AIR INTAKE WITH IMPROVED BYPASS FLOW [P] . 欧洲知识产权局专利： EP2879955A1 . 2015-06-10

  机译： 改善了旁路流量的直升机发动机进气

• 4. HELICOPTER ENGINE AIR INTAKE WITH IMPROVED BYPASS FLOW [P] . IN616DEN2015A . 2015-08-21

  机译： 改善了旁路流量的直升机发动机进气

• 5. Helicopter engine air intake with improved bypass flow [P] . IN2015DN00616A . 2015-08-21

  机译： 直升机发动机进气口，旁通流量提高

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• 2. 基于阿牛巴流量计测试固冲发动机进气流量 [C] . 李前虎 . 中国宇航学会固体火箭推进24届年会 . 2007
• 3. 直升机外流干扰下涡轴发动机进气道的流动特性研究 [A] . 曾平君 . 2012