US2017260998A1PendingUtilityA1
Centrifugal impeller and centrifugal compressor
Est. expirySep 18, 2034(~8.2 yrs left)· nominal 20-yr term from priority
F04D 29/30F04D 29/284F04D 29/4206F05D 2240/303F05D 2250/70F04D 29/681F05D 2240/304
39
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Claims
Abstract
The impeller provides that when an angle made by a projection line 33 that is obtained by projecting a camber line 32 of the blade 22 onto a predetermined meridional cross section and the camber line 32 is defined as an inclination angle γθ and an inclination in a direction opposite to a rotating direction of the rotary shaft is defined to be positive, the blade 22 is formed in such a manner that the inclination angle γθ of a leading edge 22 A is zero or positive on the hub 20 side and gradually increasing toward the shroud 21 and the inclination angle is gradually decreasing from the leading edge toward a trailing edge in a flow direction of the fluid.
Claims
exact text as granted — not AI-modified1 . A centrifugal impeller comprising: a hub; a shroud; and a plurality of blades disposed between the hub and the shroud, the centrifugal impeller blowing out fluid in a radial direction by rotation of a rotary shaft fixed to the hub, wherein
when an angle made by a projection line that is obtained by projecting a camber line of the blade onto a predetermined meridional cross section and the camber line is defined as an inclination angle and an inclination in a direction opposite to a rotating direction of the rotary shaft is defined to be positive, the blade is formed in such a manner that the inclination angle of a leading edge is zero or positive on a hub side and gradually increasing toward the shroud and the inclination angle is gradually decreasing from the leading edge toward a trailing edge in a flow direction, and the inclination angle of the trailing edge in the blade is zero or positive on the hub side and gradually increasing toward the shroud.
2 . (canceled)
3 . The centrifugal impeller according to claim 1 , wherein the inclination angle of the trailing edge in the blade is zero or positive over a region from the hub side to the shroud side.
4 . The centrifugal impeller according to claim 1 , wherein the leading edge of the blade, when projected onto the meridional cross section, has a linear shape from the hub side to the shroud side or a shape protruded toward an upstream side of the flow direction between the hub side and the shroud side.
5 . A centrifugal compressor comprising the centrifugal impeller according to claim 1 .
6 . The centrifugal impeller according to claim 3 , wherein the leading edge of the blade, when projected onto the meridional cross section, has a linear shape from the hub side to the shroud side or a shape protruded toward an upstream side of the flow direction between the hub side and the shroud side.
7 . A centrifugal compressor comprising the centrifugal impeller according to claim 3 .
8 . A centrifugal compressor comprising the centrifugal impeller according to claim 4 .Cited by (0)
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