SUPERSONIC JET ENGINE INLET FLUERIC BYPASS CONTROL

• 1. 用于控制热力发动机系统的加压装置的入口处的工作流体的压力的系统和方法 [P] . 中国专利： CN110959066A . 2020-04-03
• 2. 包括入口流体控制和可移除容纳凸缘的模内覆盖层流体的选择控制 [P] . 中国专利： CN1292884C . 2007.01.03
• 3. Supersonic airplane with low fuel consumption, utilizes low bypass ratio jet engines in conjunction with high bypass ratio engines [P] . 法国专利： FR2784960A1 . 2000-04-28

  机译： 低油耗的超音速飞机，结合了低旁通比喷气发动机和高旁通比发动机

• 4. Half rotationally symmetrical supersonic air inlet for reaction jet engines, especially for ram jet rocket engines powered by solid fuel [P] . 德国专利： DE3142464C1 . 1983-07-07

  机译： 半旋转对称超音速进气口，用于反应喷气发动机，尤其是由固体燃料驱动的冲压喷气火箭发动机

• 5. Half rotationally symmetrical supersonic air inlet for reaction jet engines, especially for ram jet rocket engines powered by solid fuel [P] . 德国专利： DE3142463C1 . 1983-07-07

  机译： 半旋转对称超音速进气口，用于反应喷气发动机，尤其是由固体燃料驱动的冲压喷气火箭发动机

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• 6. Effect of Inlet and Outlet Flow Conditions on Natural Gas Parameters in Supersonic Separation Process [O] . Yan Yang, Chuang Wen, Shuli Wang, 2010
• 7. Review of variable leading-edge patents for aircraft wings and engine inlets and their relevance for variable pitot inlets in future supersonic transport [O] . S. Kazula, K. Höschler 2021
• 8. Coupled supersonic inlet-engine control using overboard bypass doors and engine speed to control normal shock position [R] . Cole, G. L., Neiner, G. H., Wallhagen, R. E. 1970

• 1. A Supersonic Plasma Jet Source for Controlled and Efficient Thin Film Deposition [J] . Ilaria Biganzoli ,Francesco Fumagalli ,Fabio Di Fonzo . 现代物理（英文） . 2012,第10期
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• 4. 四大家鱼应对不同旁路入口的特征行为研究 [A] . 望磊 . 2020