Invention Grant
US08579592B2 Turbofan engine 有权
涡轮发动机

Turbofan engine
Abstract:
A hub-side leading edge part of a fan first-stage rotating blade 10 for taking an air thereinto more extends in a forward direction of an engine than a tip-side leading edge part and a mid-span leading edge part. The hub side of the fan first-stage rotating blade 10 is integrally connected as one with the tip side and the mid span while having a longer chord length than those of the tip side and the mid span. A radius at a root of the hub-side leading edge part is set in a boss ratio of 0 to 0.4.
Public/Granted literature
Information query
Patent Agency Ranking
0/0