An automatic engine driven pump (EDP) depressurization system for an aircraft is disclosed. The aircraft includes at least two EDPs driven by a main engine for converting mechanical power provided by the main engine into hydraulic power for distribution by a hydraulic system. The EDP ...
This vehicle was driven by two 1194 kW (1600 hp) radial piston engines, buried in the wing, on either side of the cockpit. This aircraft, the design and construction of which appears to have taken place between 1943 and 1946, was never test flown [1,2]. The XF5U-1 is illustrated in...
Aircraft engines emit principally carbon dioxide (CO2) and water (H2O) with minor contributions from nitrogen oxides (NOx), sulfur oxides (SOx), unburned hydrocarbons (HC), and soot. From: Encyclopedia of Atmospheric Sciences, 2003 About this pageSet alert ...
The pump-jet must be driven by a separate engine such as a Diesel or gas turbine. 【参考译文】水喷射推进器,或称为泵喷射推进器,是一种利用水流喷射的海洋推进系统。其机械结构可能包括带有喷嘴的导管螺旋桨,或者离心压缩机和喷嘴。泵喷射推进器必须由单独的发动机驱动,如柴油机或燃气轮机。这种推进方式...
The structure of engine driven pump in aircraft hydraulic system is complex, its fault forms are diverse, and the fault transmission path is complex and multi factor coupling. In view of the above problems, based on the in-depth analysis... B Han,W Niu,T Yan - 《Journal of Physics Confe...
High-Temperature Heat Pump for Aircraft Engine Oil Cooling Oil heat management must be reviewed globally as an integrated function as a consequence of the development of the next generation of aeroengines because o... S Maalouf,A Isikveren,P Dumoulin,... - 《Journal of Thermophysics & Heat ...
Motor mit kontinuierlicher VerbrennungThe continuous combustion engine has a compressor (10), a combustion chamber and a working part (14). The compressor and the working part provided by a cogwheel pair in the form of an Eaton pump, having an outer cogwheel (16) and an inner cogwheel ...
By the flushing method, the flushing efficiency on the aircraft engine plunger pump rotor bushing is improved, the flushing time is greatly shortened, and the production efficiency is improved by over 6 times.吴廷朗
to bypass airflow that propels the aircraft. The fuel-to-air ratio in modern combustors is approximately 1:9, hence large quantities of ambient air are processed in aircraft engines.Jet fuelis composed predominately of high-weight (C12–C15) alkanes, with substantially smaller quantities of alk...
The Fan Driven by High Pressure Tip Turbine A new concept turbofan engine based on the idea of the "Separated Core Ultrahigh Bypass Engine" for small light aircraft and VTOL airplanes are presented. ... S Iwase,Y Saito,Y Matsuda - 《Journal of the Gas Turbine Society of Japan》 被引量:...