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公开(公告)号:US20220025891A1
公开(公告)日:2022-01-27
申请号:US17380531
申请日:2021-07-20
Applicant: Eaton Intelligent Power Limited
Inventor: Sneha Abhyankar , Gurmeet Singh , Santosh Kr Sharma , Swetha Prakash , Amresh Kumar , Ragini Jain , Steven Andrew Dimino , David Glenn Loucks
Abstract: A control system includes: a controller configured to: access an estimated torque and estimated speed of a motor mechanically coupled to an impeller of a centrifugal machine; access at least one set of pre-determined performance data values associated with a known speed of the impeller, where each set of pre-determined performance data values includes: a plurality of flowrate values and a plurality of performance metric values; determine an operating point of the centrifugal machine based on the estimated torque, the estimated speed, and the at least one set of pre-determined performance data values; compare the determined operating point to a best efficiency point (BEP) associated with the centrifugal machine; and determine whether to change the speed of the motor based on the comparison.
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公开(公告)号:US11131307B2
公开(公告)日:2021-09-28
申请号:US15753295
申请日:2016-08-16
Applicant: EATON INTELLIGENT POWER LIMITED
Inventor: Kartikeya K Mahalatkar , Pavan Chandras , Matthew G Swartzlander , Rajeshekhar G Bagalakoti , Daniel Ouwenga , Sneha Abhyankar
Abstract: A supercharger rotor comprising a plurality of lobes around a center axis, each lobe of the plurality of lobes comprising a rotor profile. The rotor profile comprises a tip, a convex addendum comprised of at least two interpolated and stitched spline curves, an undercut region, and a root base.
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公开(公告)号:US20180245590A1
公开(公告)日:2018-08-30
申请号:US15753295
申请日:2016-08-16
Applicant: EATON INTELLIGENT POWER LIMITED
Inventor: Kartikeya K Mahalatkar , Pavan Chandras , Matthew G Swartzlander , Rajeshekhar G Bagalakoti , Daniel Ouwenga , Sneha Abhyankar
CPC classification number: F04C18/16 , F01C21/02 , F04C2/16 , F04C18/084 , F04C2250/20
Abstract: A supercharger rotor comprising a plurality of lobes around a center axis, each lobe of the plurality of lobes comprising a rotor profile. The rotor profile comprises a tip, a convex addendum comprised of at least two interpolated and stitched spline curves, an undercut region, and a root base.
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