公开(公告)号：US10914239B2

公开(公告)日：2021-02-09

申请号：US15694528

申请日：2017-09-01

Applicant: SuperTurbo Technologies, Inc.

Inventor： Jared William Brown ,  Christopher David Benson ,  Sterling Holman

IPC: F02C7/36 ,  F02B67/10 ,  F02B37/10 ,  F02B41/10 ,  F02B39/04 ,  F02B39/12 ,  F02C6/12

Abstract: Disclosed is a high-speed section disconnect for a driven turbocharger with a traction drive. The turbo shaft is attached to a turbine and compressor, and interfaces with a high-speed traction drive. A mechanical coupling connects the traction drive to a transmission, which is connected to the engine so that power can flow to or from the turbo shaft, but the mechanical coupling can be selectively disconnected so that the high-speed section of the driven turbocharger can also be decoupled from the engine during certain operating conditions to reduce mechanical losses in the system.

公开(公告)号：US10443485B2

公开(公告)日：2019-10-15

申请号：US15597729

申请日：2017-05-17

Applicant: SUPERTURBO TECHNOLOGIES, INC.

Inventor： Ryan Sherrill ,  Sterling Holman ,  Jared William Brown

IPC: F02B37/10 ,  F16H47/08 ,  F16H47/06 ,  F16H47/04 ,  F16H13/06

Abstract: Disclosed are embodiments of thrust absorbing planetary traction drives that utilize roller-shaft traction interfaces that are slanted to absorb thrust created on a turbo shaft by a turbine or compressor. Slanted traction surfaces on the sun portion of the turbo shaft are slanted inwardly so that the turbo shaft remains centered in the planetary traction drive. Either double roller planets or single roller planets can be used to absorb thrust in the axial direction of the turbo shaft. Various curved and slanted surfaces can be utilized to create traction interfaces that hold and stabilize the turbo shaft both axially and radially.

公开(公告)号：US20180128184A1

公开(公告)日：2018-05-10

申请号：US15694528

申请日：2017-09-01

Applicant: SuperTurbo Technologies, Inc.

Inventor： Jared William Brown ,  Christopher David Benson ,  Sterling Holman

IPC: F02C7/36 ,  F02C6/12

CPC classification number: F02C7/36 ,  F02B37/10 ,  F02B39/04 ,  F02B39/12 ,  F02B41/10 ,  F02B67/10 ,  F02C6/12 ,  F05D2220/40 ,  F05D2260/4023 ,  F05D2260/4031 ,  F05D2260/406 ,  Y02T10/144 ,  Y02T10/163

Abstract: Disclosed is a high-speed section disconnect for a driven turbocharger with a traction drive. The turbo shaft is attached to a turbine and compressor, and interfaces with a high-speed traction drive. A mechanical coupling connects the traction drive to a transmission, which is connected to the engine so that power can flow to or from the turbo shaft, but the mechanical coupling can be selectively disconnected so that the high-speed section of the driven turbocharger can also be decoupled from the engine during certain operating conditions to reduce mechanical losses in the system.

公开(公告)号：US20170248069A1

公开(公告)日：2017-08-31

申请号：US15597729

申请日：2017-05-17

Applicant: SUPERTURBO TECHNOLOGIES, INC.

Inventor： Ryan Sherrill ,  Sterling Holman ,  Jared William Brown

IPC: F02B37/10 ,  F16H47/08

CPC classification number: F02B37/105 ,  F16H13/06 ,  F16H47/04 ,  F16H47/065 ,  F16H47/08 ,  Y02T10/144

Abstract: Disclosed are embodiments of thrust absorbing planetary traction drives that utilize roller-shaft traction interfaces that are slanted to absorb thrust created on a turbo shaft by a turbine or compressor. Slanted traction surfaces on the sun portion of the turbo shaft are slanted inwardly so that the turbo shaft remains centered in the planetary traction drive. Either double roller planets or single roller planets can be used to absorb thrust in the axial direction of the turbo shaft. Various curved and slanted surfaces can be utilized to create traction interfaces that hold and stabilize the turbo shaft both axially and radially.