Device for heating, flames and utilization of the damping becomes rueckstosses to the propulsion increase of aircraft

• 1. 障碍物检测装置、利用了障碍物检测装置的自动制动装置、障碍物检测方法以及利用了障碍物检测方法的自动制动方法 [P] . 中国专利： CN111937002A . 2020-11-13
• 2. 路面检测装置、利用了路面检测装置的图像显示装置、利用了路面检测装置的障碍物检测装置、路面检测方法、利用了路面检测方法的图像显示方法以及利用了路面检测方法的障碍物检测方法 [P] . 中国专利： CN111971682A . 2020-11-20
• 3. Device for heating, flames and utilization of the damping becomes rueckstosses to the propulsion increase of aircraft [P] . 德国专利： DE749544C . 1944-11-24

  机译： 加热，燃烧和利用阻尼的装置成为飞机推进力增长的障碍

• 4. Device for the utilization of the rueckstosses of the exhaust gases of internal combustion engines for flames damping and heating in the case of aircraft [P] . 德国专利： DE749457C . 1944-11-23

  机译： 在飞机上利用用于消减和加热火焰的内燃机排气管的装置

• 5. device for utilization of the gases from the rueckstosses brennkraftmaschinen flammendaempfung and heating for aircraft [P] . 德国专利： DE000000749457A . 1944-11-23

  机译： 利用来自吕肯啤酒公司的气体燃烧和燃烧飞机的气体的装置

• 1. GENERALIZED THERMODYNAMIC ASSESSMENT OF CONCEPTS FOR INCREASING THE EFFICIENCY OF CIVIL AIRCRAFT PROPULSION SYSTEMS [C] . Florian Schmidt, Stephan Staudacher ASME turbo expo: turbine technical conference and exposition . 2015
• 2. THE EXPERIMENTAL DETERMINATION OF THE LOCAL AND AVERAGE HEAT TRANSFER CHARACTERISTICS AND AVERAGE FRICTION COEFFICIENTS FOR TURBULENT FLOW OF AIR AND ARGON WITH VARIABLE PROPERTIES IN SMOOTH TUBES WITH THE BOUNDARY CONDITIONS OF CONSTANT WALL TEMPERATURE HEATING AND INCREASING HEAT FLUX HEATING. [D] . PRIDEAUX, JEAN PAUL. 1966
• 3. Measurements of Aerodynamic Interference of a Hybrid Aircraft with Multirotor Propulsion [O] . Zbigniew Czyż, Mirosław Wendeker 2020
• 4. Overheating, flame, smoke, and freight movement detection algorithms based on charge-coupled device camera for aircraft cargo hold surveillance [O] . Sentenac, T, Le Maoult, Y, Orteu, Jean-José, 2004
• 5. Influence of Tuned Dampers on Flexure-Aileron Flutter Part I Theoretical Investigation on the Influence of Tuned Damping Devices on Flexure-Aileron Flutter Part II Some Further Calculations on the Influence of Tuned Damping Devices on Flexure-Aileron Flutter Part III Experiments on the Effect of Tuned Damping Devices on Flexure-Aileron Flutter [R] . R. A. FRAZER, W. P. JONES, C. SCRUTON 1952

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