Thrust reverser for a gas turbine engine
作者： Michael J Holme , Jeffrey C Bishop
DOI:
关键词: Sheet material 、 Engineering 、 Cascade 、 Thrust reversal 、 Flow (psychology) 、 Gas turbines 、 Bent molecular geometry 、 Structural engineering
摘要: A thrust reverser cascade flow directing element ( 28 ) for a gas turbine engine 10 comprises plurality of plates 30 and vanes 40 ). At least one vane extends between each pair ), the are formed from sheet material single integral piece ductile 32 forms The has longitudinally spaced apart apertures 36 portions 38 is bent at positions such that portion defines
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