The wall of a turbo machine having a cascade of blades comprises a first platform facing a first channel between the blades in the cascade of blades, and a second platform facing a second channel between adjoining cascade of blades on the upstream side and the downstream side and having a circumferential outline having a distribution of radial position. With such an arrangement, loss due to disturbance of flow through the gap of axially adjoining walls can be reduced.
申请公布号
WO2008120748(A1)
申请公布日期
2008.10.09
申请号
WO2008JP56181
申请日期
2008.03.28
申请人
IHI CORPORATION;THE SOCIETY OF JAPANESE AEROSPACE COMPANIES;MITSUHASHI, KATSUNORI;TAKAHASHI, AKIRA;HAMAZAKI, HIROSHI;YAMAWAKI, RURIKO