Flow guiding device and fan assembly with flow guiding device

    公开(公告)号:US11976668B2

    公开(公告)日:2024-05-07

    申请号:US16742957

    申请日:2020-01-15

    IPC分类号: F04D29/42 F04D19/00 F04D29/54

    摘要: A flow guiding device for use on a fan assembly with a motor-operated radial impeller rotating about an axis of rotation. The guiding device has an outer housing and an inner diffuser. A flow duct is formed between the outer housing and inner diffuser. The flow duct extends along an axial flow direction. The outer housing forms a receiving space for the integral holding of the radial impeller. The impeller borders, in the axial direction, on the inner diffuser. The impeller, during operation, takes in a flow axially and blows it out radially into the flow duct. The flow duct is adapted to deflect the flow from a radial direction into an axial direction.

    BLOWER AND AIR CONDITIONER HAVING THE SAME
    3.
    发明申请

    公开(公告)号:US20180180060A1

    公开(公告)日:2018-06-28

    申请号:US15738394

    申请日:2015-07-10

    发明人: Seiji SATO

    摘要: An air conditioner comprises a compressor to compress a refrigerant, a heat exchanger to move heat of the refrigerant, and a blower to blow air. The blower comprises a fan rotatable about a rotation axis, and a plurality of stationary blades installed to be a radial shape about the rotation axis in a direction in which the airflow generated by the rotation of the fan is discharged, and are curved in a direction opposite to the rotation direction of the fan from an inner circumferential portion to an outer circumferential portion. The stationary blades comprise an inlet edge, and an outlet edge, and an inlet angle formed by the inlet edge and the rotation axis and a chord angle formed by a chord connecting the inlet edge and the outlet edge and the rotation axis are larger at the inner and outer circumferential portions than at a radial center portion.

    Tip treatment bars in a gas turbine engine

    公开(公告)号:US09957976B2

    公开(公告)日:2018-05-01

    申请号:US14494103

    申请日:2014-09-23

    申请人: ROLLS-ROYCE PLC

    发明人: Peter Allford

    摘要: There is presented a casing arrangement for a gas turbine engine. The casing arrangement includes a plurality of tip treatment bars extending between a pair of spaced-apart annular supports, with each tip treatment bar being elongate and supported at each end by a respective support such that each end of the bar is received within an opening formed in the respective support. At least the ends of each tip treatment bar are tapered in transverse cross-section so as to have a wedge-shaped profile, and the openings in the supports have a complementary tapered shape for receipt and retention of the bar ends therein.

    Axial flow fan motor
    8.
    发明授权

    公开(公告)号:US09664196B2

    公开(公告)日:2017-05-30

    申请号:US14454527

    申请日:2014-08-07

    申请人: MINEBEA CO., LTD.

    IPC分类号: F04D29/54 F04D25/06

    摘要: An axial flow fan motor 100 comprises: a casing outer frame 61; an impeller 10; a rotor shaft 20 as a rotation axis at a center of the impeller 10; a bearing housing 30 in an inside of a rotor housing 11; and a base portion hub 62 in an air blowout opening side 2, wherein, in a cross-sectional view along the rotation axis, the base portion hub 62 has an outer peripheral portion 65 at least partially inclined to the rotation axis side by an angle θ1 toward the air blowout opening side 2 with regard to a straight line parallel to the rotation axis, and the casing outer frame 61 has an inner peripheral portion 67 at least partially inclined to the rotation axis side by an angle θ2 toward the air blowout opening side 2 with regard to a straight line parallel to the rotation axis.