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    • 35. 发明申请
    • IMPELLER HAVING PRIMARY BLADES AND SECONDARY BLADES
    • US20200370562A1
    • 2020-11-26
    • US16761530
    • 2017-12-15
    • AERONET INC.
    • Seungbae LEE
    • F04D29/30
    • Provided is an impeller including a first portion including a first hub and a plurality of primary blades each extending while being spaced an equal distance from each other along an outer circumference of the first hub and a second portion including a second hub coupled to a lower side of the first hub by using a projection-groove coupling manner and a plurality of secondary blades each extending while being spaced apart from each other along an outer circumference of the second hub. Here, when a projection angle between a leading edge (L.E.) and a trailing edge (T.E.) of each of the primary blades is Φ1, and a projection angle between a leading edge (L.E.) and a trailing edge (T.E.) of each of the secondary blades is θ1, the projection angle Φ1 and θ1 includes an upstream angle Φ1u and θ1u and a downstream angle Φ1d and θ1d, at which the primary blade and the secondary blade overlap each other, and an angle Φ1m and θ1m at which the primary blade and the secondary blade do not overlap each other, and the projection angle θ1 is less than the projection angle Φ1 to satisfy an equation 0