Impeller and centrifugal compressor including the same
Abstract
Provided is an impeller of a centrifugal compressor including: a hub fixed to a rotation shaft; and a plurality of blades extending outward from a center portion of the hub on one surface of the hub, wherein a length of the blade is greater than a straight length between an inlet end of the blade and an outlet end thereof. Assuming that an outlet angle formed along a longitudinal direction of the blade at the outlet end of the blade is β and an inclination angle of the blade from the one surface of the hub at the outlet end of the blade is γ, the following equation is satisfied: 1<sin(β−20°)+cos(γ−40°)<1.5.
Claims
exact text as granted — not AI-modified1 . An impeller of a centrifugal compressor comprising:
a hub fixed to a rotation shaft; and a plurality of blades extending outward from a center portion of the hub on one surface of the hub, wherein a length of the blade is greater than a straight length between an inlet end of the blade and an outlet end thereof, and assuming that an outlet angle formed along a longitudinal direction of the blade at the outlet end of the blade is β and an inclination angle of the blade from the one surface of the hub at the outlet end of the blade is γ, the following equation is satisfied:
1<sin(β−20°)+cos(γ−40°)<1.5.
2 . The impeller according to claim 1 , wherein the outlet angle is in a range of 20° to 70°.
3 . The impeller according to claim 1 , wherein the inclination angle is in a range of 40° to 90°.
4 . A centrifugal compressor comprising:
an impeller which is fixed to a rotation shaft to be rotated at high speed; and a diffuser which converts kinetic energy of a compressible medium that is increased by the impeller into pressure energy, wherein the impeller comprises: a hub fixed to the rotation shaft; and a plurality of blades extending outward from a center portion of the hub on one surface of the hub, a length of the blade is greater than a straight length between an inlet end of the blade and an outlet end thereof, and assuming that an outlet angle formed along a longitudinal direction of the blade at the outlet end of the blade is β and an inclination angle of the blade from the one surface of the hub at the outlet end of the blade is γ, the following equation is satisfied:
1<sin(β−20°)+cos(γ−40°)<1.5.
5 . The centrifugal compressor according to claim 4 , wherein the outlet angle is in a range of 20° to 70°.
6 . The centrifugal compressor according to claim 4 , wherein the inclination angle is in a range of 40° to 90°.Join the waitlist — get patent alerts
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