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公开(公告)号:US20210363891A1
公开(公告)日:2021-11-25
申请号:US17055485
申请日:2019-05-15
申请人: Cummins Ltd.
发明人: Matthew William Edwards , Karl Conlon , Simon David Moore , Christopher Parry , Andrew Sullivan , Paul Ghosh , Mark R. Holden , George E. Sandford , Nandakishore Arcot Madhusudan , Stephen David Hughes , Christopher J Shaw
IPC分类号: F01D9/04
摘要: A turbine for a turbo-machine is proposed in which, at a gas inlet for a turbine wheel, vanes extend from a nozzle ring though slots in a shroud. The nozzle ring and shroud are relatively rotatable about a rotational axis of the turbine by at least 0.1 degrees. In use, the nozzle ring and shroud are relatively rotated to bring one side of the vane into close contact with one surface of the slot, to inhibit leakage of gas between the vane and the slot surface. For this purpose the respective surfaces of the nozzle and slot can be configured to closely conform to each other. If there is differential thermal expansion of the shroud and nozzle ring, the nozzle ring and shroud can relatively rotate, to withdraw the vane from the edge of the slot to relieve the pressure between them.
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公开(公告)号:US20200370473A1
公开(公告)日:2020-11-26
申请号:US16756959
申请日:2018-10-17
申请人: Cummins Ltd.
摘要: There is provided a turbine comprising: a turbine housing; a turbine wheel; an inlet upstream of the turbine wheel, the inlet defining a first inlet portion and a second inlet portion; an outlet downstream of the turbine wheel, the outlet defining a first outlet portion and a second outlet portion; and a wastegate arrangement configured to selectively vent exhaust gas from the first inlet portion to the first outlet portion via a first bypass passage, and further configured to selectively vent exhaust gas from the second inlet portion to the second outlet portion via a second bypass passage; wherein the first outlet portion and the second outlet portion are separated by a baffle of the turbine housing.
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公开(公告)号:US12037916B2
公开(公告)日:2024-07-16
申请号:US18019006
申请日:2021-07-30
申请人: Cummins Ltd.
CPC分类号: F01D25/246 , F01D9/02 , F01D17/16 , F05D2220/40 , F05D2230/642
摘要: There is provided an assembly for a turbocharger, the assembly comprising a turbine housing and a nozzle ring, wherein one of the turbine housing and the nozzle ring comprises a tongue and the other of the turbine housing and the nozzle ring comprises a corresponding slot, the tongue and slot being configured to engage and prevent relative rotation of the turbine housing and the nozzle ring. Also provided is a method of manufacturing a turbine housing, assembly for use in a turbocharger, or a turbocharger.
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公开(公告)号:US11697997B2
公开(公告)日:2023-07-11
申请号:US17728855
申请日:2022-04-25
申请人: Cummins Ltd.
发明人: Matthew William Edwards , Karl Conlon , Simon David Moore , Christopher Parry , Andrew Sullivan , Paul Ghosh , Mark R. Holden , George E. Sandford , Nandakishore Arcot Madhusudan , Stephen David Hughes , Christopher J. Shaw
CPC分类号: F01D9/04 , F01D17/143 , F01D17/167 , F02B37/22 , F05D2220/40 , F05D2240/128
摘要: A turbine for a turbo-machine is proposed in which, at a gas inlet for a turbine wheel, vanes extend from a nozzle ring though slots in a shroud. The nozzle ring and shroud are relatively rotatable about a rotational axis of the turbine by at least 0.1 degrees. In use, the nozzle ring and shroud are relatively rotated to bring one side of the vane into close contact with one surface of the slot, to inhibit leakage of gas between the vane and the slot surface. For this purpose the respective surfaces of the nozzle and slot can be configured to closely conform to each other. If there is differential thermal expansion of the shroud and nozzle ring, the nozzle ring and shroud can relatively rotate, to withdraw the vane from the edge of the slot to relieve the pressure between them.
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公开(公告)号:US20220251960A1
公开(公告)日:2022-08-11
申请号:US17728855
申请日:2022-04-25
申请人: Cummins Ltd.
发明人: Matthew William Edwards , Karl Conlon , Simon David Moore , Christopher Parry , Andrew Sullivan , Paul Ghosh , Mark R. Holden , George E. Sandford , Nandakishore Arcot Madhusudan , Stephen David Hughes , Chistopher J. Shaw
IPC分类号: F01D9/04
摘要: A turbine for a turbo-machine is proposed in which, at a gas inlet for a turbine wheel, vanes extend from a nozzle ring though slots in a shroud. The nozzle ring and shroud are relatively rotatable about a rotational axis of the turbine by at least 0.1 degrees. In use, the nozzle ring and shroud are relatively rotated to bring one side of the vane into close contact with one surface of the slot, to inhibit leakage of gas between the vane and the slot surface. For this purpose the respective surfaces of the nozzle and slot can be configured to closely conform to each other. If there is differential thermal expansion of the shroud and nozzle ring, the nozzle ring and shroud can relatively rotate, to withdraw the vane from the edge of the slot to relieve the pressure between them.
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公开(公告)号:US11280259B2
公开(公告)日:2022-03-22
申请号:US16756959
申请日:2018-10-17
申请人: Cummins Ltd.
摘要: There is provided a turbine comprising: a turbine housing; a turbine wheel; an inlet upstream of the turbine wheel, the inlet defining a first inlet portion and a second inlet portion; an outlet downstream of the turbine wheel, the outlet defining a first outlet portion and a second outlet portion; and a wastegate arrangement configured to selectively vent exhaust gas from the first inlet portion to the first outlet portion via a first bypass passage, and further configured to selectively vent exhaust gas from the second inlet portion to the second outlet portion via a second bypass passage; wherein the first outlet portion and the second outlet portion are separated by a baffle of the turbine housing.
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公开(公告)号:US11578645B2
公开(公告)日:2023-02-14
申请号:US17684175
申请日:2022-03-01
申请人: Cummins Ltd
发明人: Robin Daniels , Thomas Morton , Thomas Roberts , Christopher Parry , Richard Goodyear , Mark R. Holden , Donald E. Willey
摘要: A valve system comprising a valve chamber at a junction of an inlet port, an outlet port and a bypass port, the inlet port configured for fluid communication with exhaust gas, the outlet port configured for fluid communication with an inlet of a turbine, and the bypass port configured for fluid communication with an exhaust aftertreatment device; a rotary valve comprising a valve rotor which rotates about a valve axis within the valve chamber between a first position to permit gas flow through the bypass port and a second position to block gas flow. At least one of the valve rotor and the valve chamber comprises a protrusion and the other comprises a recess, wherein, in the first position, the protrusion and recess are spaced from one another, and, in the second position the recess receives the protrusion such that gas flow between the protrusion and recess is substantially prevented.
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公开(公告)号:US11536192B2
公开(公告)日:2022-12-27
申请号:US16639869
申请日:2018-08-22
申请人: Cummins Ltd
发明人: Robin Daniels , Gareth Williamson , Ross Deacon , Laith Al-Kazaz , Thomas Morton , Christopher Parry , Richard Goodyear , Mark R. Holden , Jon-Luke Keating , Waqas Ali , John Bywater , Thomas Roberts
IPC分类号: F02B37/18 , F16K5/18 , F16K11/085
摘要: A rotary turbine bypass valve comprises a valve chamber positioned at a junction of an inlet port, an outlet port and a bypass port, the inlet port configured for fluid communication with a flow of exhaust gas from an engine, the outlet port configured for fluid communication with an inlet of a turbine, and the bypass port configured for fluid communication with an exhaust aftertreatment device; and a valve rotor supported for rotation, about a valve axis, within the valve chamber. The valve rotor is rotatable about the valve axis between a first position in which the valve rotor permits gas flow through the bypass port and a second position in which the valve rotor blocks gas flow through the bypass port. The valve rotor is eccentric such that it includes a seal portion which is a portion of the valve rotor within the valve chamber which is furthest radially spaced from the valve axis; and as the valve rotor moves from the first position to the second position the seal portion moves towards the bypass port such that the radial separation between the valve rotor and the bypass port decreases to a minimum when the valve rotor is in the second position in which the seal portion is adjacent the bypass port.
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公开(公告)号:USD931338S1
公开(公告)日:2021-09-21
申请号:US29715980
申请日:2019-12-05
申请人: Cummins Ltd
设计人: Iain M. Taylor , Sagar A. Hore , Mark R. Holden
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公开(公告)号:USD930707S1
公开(公告)日:2021-09-14
申请号:US29715978
申请日:2019-12-05
申请人: Cummins Ltd
设计人: Tain M. Taylor , Sagar A. Hore , Mark R. Holden
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