An example airfoil array includes an airfoil array configured to rotate within a turbomachine at a different rotational speed than a fan within the turbomachine. The airfoil array includes a first airfoil (58) that is circumferentially spaced a distance (98) from an adjacent second airfoil (58a). A ratio of the distance (98) to an axial chord length (82) of the first airfoil (58) is less than 1.3. An uncovered turning angle of the first airfoil (58) is greater than 15 degrees.
申请公布号
EP2441919(A1)
申请公布日期
2012.04.18
申请号
EP20110181843
申请日期
2011.09.19
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
ESTES, MATTHEW B.;JUREK, RENEE J.;MAGGE, SHANKAR S.;HUEBNER, NORBERT