Engine-driven hydraulic pump for an aircraft, having a first and a second pump unit which each comprise an adjustable swash plate and a piston assembly coupled with said swash plate and driven by a pump shaft, a control device for adjusting the inclination of the swash plate and a drive ...
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
Aircraft smoke refers to visible particulates in the aircraft plume and presumably includes the large diameter (>1 μm) part of the soot population. The ICAO standards have both reflected and motivated improvements in engine design and manufacture. However, because the service lifetime of an ...
low-pressure end of the compressor be less than that of the high-pressure end. This is achieved in large aircraft gas turbines by “spooled” shafts where the shaft for the low-pressure end, driven by the low-pressure portion of the turbine, is running at a different speed within thehollo...
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...
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
Two stage pump, particularly provided as main pump for supplying an aircraft engine with fuel A two stage pump (), where the high pressure stage (′) is a gear pump (), comprises a driving of the other stage (′) by a support shaft (), mounted in the driven pinion (), the shaft...
(Failure Case I), the aircraft was inclose proximityto a home base, where the crew performed a forced landing. In the second case of failure (Failure Case II), forced landing was performed at the nearest suitableairportequipped with one grass runway, approximately 80km away from the home ...
A Junkers Jumo 222 A/B-1 engine with a short gear reduction housing. First run in 1939, the Jumo 222 represented what was believed to be the next generation of German aircraft engines. Note the coolant pump below the gear reduction housing and the fuel injection pump between the intake man...
This Malaysian Standard specifies dimensional and performance of spark plugs for internal combustion engines. However, the spark plug for aircraft Spark plugs for internal combustion engines MNOSZ 17772-1953 铬钢.内燃机阀门 Chrome steel. Internal combustion engine valve ...