US2012159947A1PendingUtilityA1
Method and apparatus for controlling turbine efficiency
Est. expiryFeb 19, 2029(~2.6 yrs left)· nominal 20-yr term from priority
F02B 37/12F02D 41/0007Y02T10/40F02M 26/05F02D 41/0077F02B 37/24Y02T10/12F02M 26/02F02D 23/00F02M 26/10
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Claims
Abstract
A method of controlling turbine efficiency in a turbo unit provided on an internal combustion engine includes providing a flow of gas in an area upstream a turbine at a direction different to the flow of exhaust gases in the same area, regulating the flow by a valve, and controlling the valve from a control unit having at least boost pressure and/or EGR flow as input parameters.
Claims
exact text as granted — not AI-modified1 . A method of controlling turbine efficiency in a turbo unit for an internal combustion engine, comprising:
providing a flow of gas in an area upstream a turbine rotor at a direction different to the flow of exhaust gases in the same area, regulating the flow by a valve, controlling the valve from a control unit having at least boost pressure and/or EGR flow as input parameters.
2 . The method according to claim 1 , further comprising providing in the area a plurality of outlets for the flow of gas.
3 . The method according to claim 2 , further comprising providing an on-off valve in each of the outlets.
4 . The method according to claim 2 , further comprising providing a variable valve in each of the outlets.
5 . The method according to claim 1 , further comprising providing the valve outside a turbo unit housing.
6 . The method according to claim 1 , further comprising integrating the valve in a turbo unit housing.
7 . The method according to claim 1 , further comprising:
providing the flow of gases from a volute of the turbo unit.
8 . The method according to claim 1 , further comprising:
providing the flow of gases from an exhaust gas manifold.
9 . The method according to claim 1 , further comprising:
providing the flow of gases from an outlet downstream of a compressor of the turbo unit or from an external compressor tank.
10 . The method according to claim 1 , further comprising:
providing the turbo unit with adjustable vanes, and providing the flow of gas in a vane less space at least partially downstream the vanes and upstream the turbine.
11 . A system for controlling turbine efficiency in a turbo unit for an internal combustion engine comprising
at least one outlet arranged in a turbine scroll outlet for providing a flow of gas in a direction different to the direction of exhaust gases in the turbine scroll outlet; a valve arranged between a source for providing a flow of gas and the outlet in the turbine scroll outlet for regulating the flow of the gas; and a control unit for controlling the valve where the control unit has at least boost pressure and/or EGR flow as input parameters.
12 . The system according to claim 11 , wherein one valve is provided upstream each outlet and where the valve may be of on-off type or continuously variable.
13 . The system according to claim 11 , wherein at least one of the valves is provided outside a housing of the turbo unit
14 . The system according to claim 11 , wherein at least one of the valves is integrated in a housing of the turbo unit.
15 . The system according to claim 11 , wherein the source for providing ‘a flow of gas is one of the group of: exhaust gases from the internal combustion engine, boost pressure from the compressor of the turbo unit, air pressure tank.
16 . The system according to claim 11 , wherein the turbo unit comprises adjustable vanes and where the at least one outlet for providing the flow of gas into the turbine scroll outlet is provided in a vane less space at least partially downstream the vanes and upstream the turbine.
17 . A vehicle comprising a system according to claim 11 .Cited by (0)
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