发明名称 CENTRIFUGAL FAN
摘要 Each of blades of a centrifugal fan includes a primary wing section that has a trailing edge which is parallel to a central axis of rotation, a leading edge end section which is parallel to the central axis of rotation, and a thickness gradually growing thinner toward the trailing edge and the leading edge end section; and an auxiliary wing section that extends from the leading edge end section of the primary wing section toward the interior of the centrifugal fan. The auxiliary wing section has a length from the leading edge end section of the primary wing section to the leading edge of the auxiliary wing section that is greater at a side of a support section than at an intake side when viewed in a direction of the central axis of rotation, and a constant thickness across the entire area of the auxiliary wing section.
申请公布号 US2016290353(A1) 申请公布日期 2016.10.06
申请号 US201415033340 申请日期 2014.12.10
申请人 KEIHIN CORPORATION 发明人 KASAHARA Masamichi;ISHIZAKI Masaaki
分类号 F04D29/28;F04D29/30 主分类号 F04D29/28
代理机构 代理人
主权项 1. A centrifugal fan in which a rotation shaft is attached to a mounting section to rotate in a predetermined direction so that air taken in from a front of a support section is blown out radially, the centrifugal fan comprising: the support section having a circular shape viewed from the front; a plurality of blades arranged in an annular shape along an outer circumference of the support section; and the mounting section provided at a center of the support section, wherein each of the blades includes: a primary wing section that has a trailing edge which is parallel to a central axis of rotation of the rotation shaft, a leading edge end section which is parallel to the central axis of rotation, and a thickness gradually growing thinner toward the trailing edge and the leading edge end section; and an auxiliary wing section that extends from the leading edge end section of the primary wing section toward the interior of the centrifugal fan, and wherein the auxiliary wing section has a length from the leading edge end section of the primary wing section to a leading edge of the auxiliary wing section that is greater at a side of the support section than at an intake side when viewed in a direction of the central axis of rotation, and wherein the auxiliary wing section has a constant thickness across the entire area of the auxiliary wing section.
地址 Shinjuku-ku, Tokyo JP