|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F04D-029/54 F02C-006/12 F01D-025/28 F02C-009/18|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 3 인용 특허 : 19|
A turbine nozzle for an air cycle machine includes a disk section with a multiple turbine vanes which each extend for a vane height H, a throat width W defined between each of the multiple of turbine vanes, wherein a ratio W/H is 0.745-0.769.
1. A turbine nozzle for an air cycle machine comprising: a disk section with a multiple of turbine vanes which extend for a vane height H relative said disk section, a throat width W defined between each of said multiple of turbine vanes, where a ratio W/H is 0.745-0.769, wherein each of said multiple of turbine vanes have an airfoil profile section defined by a set of points in Table T-1 scaled by a desired factor, said set of points include paired chord and thickness dimensions. 2. The turbine nozzle as recited in claim 1, wherein said paired chord and...