By means of sound inlet diffuser for a an airbreathing aircraft engine, in particular in the ramjet engine

• 1. 涡轮喷气发动机叶片、尤其是导向叶片,以及接纳此种叶片的涡轮喷气发动机 [P] . 中国专利： CN103080476A . 2013-05-01
• 2. 配备有推力反向器的飞机涡轮喷气发动机机舱，包括用于避免飞机机翼活动缝翼的切口 [P] . 中国专利： CN106574573B . 2018.08.07
• 3. Inlet diffusers for jet engines, jet engines, jet aircraft, and methods for diffusing incoming air of jet engines [P] . 美国专利： US10718264B2 . 2020.07.21
• 4. INLET DIFFUSERS FOR JET ENGINES, JET ENGINES, JET AIRCRAFT, AND METHODS FOR DIFFUSING INCOMING AIR OF JET ENGINES [P] . 美国专利： US2019284996A1 . 2019-09-19

  机译： 喷气发动机，喷气发动机，喷气飞机的进气扩散器，以及扩散喷气发动机空气的方法

• 5. Ramjet engine having inlet cone diffuser automatically adjustable as to length and cone angle [P] . 美国专利： US2638738A . 1953-05-19

  机译： 具有进气锥扩散器的Ramjet发动机，其长度和锥角可自动调节

• 1. A Generative Adversarial Nets Method for Monitoring Data Generation on Aircraft Engines [J] . FU Qiang, WANG Huawei 南京航空航天大学学报（英文版） . 2019,第004期
• 2. Ensemble Recurrent Neural Network-Based Residual Useful Life Prognostics of Aircraft Engines [J] . Jun Wu, Kui Hu, Yiwei Cheng, 结构耐久性与健康监测(英文) . 2019,第003期
• 3. NUMERICAL MODELING OF TURBULENT EVAPORATING GAS-DROPLET TWO-PHASE FLOWS IN AN AFTERBURNER DIFFUSOR OF TURBO-FAN JET ENGINES [J] . 中国航空学报：英文版 . 1990,第004期
• 4. DEVELOPMENT AND TESTING OF THE NAVSEA / ALLIANT TECHSYSTEMS TACTICAL AIRBREATHING PROPULSION, INTEGRAL-ROCKET/RAMJET-ENGINE TEST FACILITY [C] . Gariel D. Randolph, Kenneth W. Beck, Lawrence S. Zajdel, International Symposium on Air Breathing Engines . 2003
• 5. Thrust chamber dynamics and propulsive performance of airbreathing pulse detonation engines. [D] . Ma, Fuhua. 2003
• 6. Non-volatile particle emissions from aircraft turbine engines at ground-idle induce oxidative stress in bronchial cells [O] . Hulda R. Jonsdottir, Mathilde Delaval, Zaira Leni, 2019
• 7. A study of ramjet engine (Part 3) Air inlet performance as the engine component. [O] . Katsumi FUNAKI 1985

• 1. Numerical Analysis and Verification of the Gas Jet from Aircraft Engines Impacting a Jet Blast Deflector [J] . Fu-Dong Gao ,De-Xin Wang ,Hai-Dong Wang . 中国机械工程学报 . 2018,第005期
• 2. Measuring Sound Pressure Levels during Thermoacoustic Instabilities in Large Engines: Case Study [J] . Alice Elizabeth González ,José Cataldo Ottieri ,Pablo Gianoli Kovar . 现代物理（英文） . 2017,第10期
• 3. 富氧对冲压喷气发动机推力影响的模拟试验方案 [C] . 陈正举 . 第二届发动机试验与测试学术交流会 . 1995
• 4. 非均匀进口对超燃冲压发动机尾喷管性能影响的研究 [A] . 全志斌 . 2012