|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||416/223B; 416/243; 416/DIG.2|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 4 인용 특허 : 20|
A turbine rotor for an Air Cycle Machine includes a hub with a multiple turbine blades which extend therefrom, each of the multiple of turbine blades defined by a set of coordinates.
1. A turbine rotor for an Air Cycle Machine comprising: a hub with a multiple turbine blades which extend therefrom, each of said multiple of turbine blades defined by a set of X-coordinates, Y-coordinates and Z-coordinates in any of Table B-1 and B-2 scaled by a desired factor or Table S-1 and S-2 scaled by a desired factor, said X-coordinate is the tangential direction, said Y-coordinate is the axial direction, and said Z-coordinate is the radial direction. 2. The turbine rotor as recited in claim 1, wherein said multiple turbine blades have a tip cont...