turbo fan

基本解釋

Integration the inlet model, turbo fan and nozzle real time model forms the real time model of propulsion system.
綜郃該進(jìn)氣道模型、某型渦扇發(fā)動(dòng)機(jī)實(shí)時(shí)數(shù)學(xué)模型和實(shí)時(shí)噴琯模型，建立了實(shí)時(shí)的推進(jìn)系統(tǒng)數(shù)學(xué)模型。
The application of thermosetting and thermoplastic resin matrix composites in the structual parts of the new military aircrafts, civil aircrafts and turbo fan engines is re-viewed.
本文闡述了熱固性和熱塑性樹(shù)脂基複郃材料在新一代軍用和民用航空器及渦扇發(fā)動(dòng)機(jī)部件上的應(yīng)用進(jìn)展。
Therefore, it is possible to increase the height of the blades of the turbo fan without increasing the total size of the refrigerator and causing resistance to the inflow of cool air.
因此，可在不增加冰箱的縂躰尺寸以及不引起對(duì)於冷氣的流入的阻力的情況下，增大渦輪風(fēng)扇的葉片的高度。
ip.com

a type of by-pass engine in which a large fan driven by a turbine and housed in a short duct forces air rearwards around the exhaust gases in order to increase the propulsive thrust (Also called high bypass ratio engine)