TURBOFAN

To provide a turbofan capable of suppressing twisting due to relative rotation of blade members constituting a blade.SOLUTION: A negative pressure side blade member 41 functioning as a first blade member forming one surface of a blade 27 is provided with a protrusion part 46 having a non-circular cr...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: DOI YASUYUKI, OKABE KIYOSHI
Format: Patent
Sprache:eng ; jpn
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
Zusammenfassung:To provide a turbofan capable of suppressing twisting due to relative rotation of blade members constituting a blade.SOLUTION: A negative pressure side blade member 41 functioning as a first blade member forming one surface of a blade 27 is provided with a protrusion part 46 having a non-circular cross section, which protrudes toward a positive pressure side blade member 51 functioning as a second blade member forming the other surface. Also, the positive pressure side blade member 51 is provided with an insertion part 56 into which the protrusion part 46 is inserted and the portion of the non-circular cross section is fitted so as not to be relatively rotatable.SELECTED DRAWING: Figure 4 【課題】羽根を構成する羽根部材同士の相対回転を伴うねじれを抑制可能なターボファンを提供すること。【解決手段】羽根27の一方の面を形成する第1の羽根部材として機能する負圧側羽根部材41には、他方の面を形成する第2の羽根部材として機能する正圧側羽根部材51に向けて突出すると共に非円形断面の突出部46が設けられる。また、正圧側羽根部材51には、突出部46が挿入されて前記非円形断面の箇所が相対回転不能に嵌まる挿入部56が設けられる。【選択図】図4