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US 2014/0196696 A1Published application
Supercharged internal combustion engine with twin-flow turbine and method for operating an internal combustion engine of said type
AssigneeFord Global Technologies, LLC
InventorsVanco Smiljanovski, Helmut Matthias Kindl, Uwe Spaeder, Rob Stalman
Life of this patent
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Abstract
A supercharged internal combustion engine may include a twin-flow turbine with variable vane geometry. One example method to operate the device permits optimized operation of the internal combustion engine at low exhaust gas flow rates.
Claims18
A supercharged internal combustion engine having at least one cylinder head with at least two cylinders, comprising:
- each cylinder has at least one outlet opening for discharging the exhaust gases out of the cylinder via an exhaust-gas discharge system, and each outlet opening is adjoined by an exhaust line;
- at least two cylinders are configured in such a way as to form two groups with in each case at least one cylinder;
- the exhaust lines of the cylinders of each cylinder group merge in each case to form an overall exhaust line such that an exhaust manifold is formed, and
- the two overall exhaust lines are connected to a two-channel turbine, which comprises a rotor which is mounted on a rotatable shaft in a turbine housing, such that in each case one overall exhaust line is connected to one of the two inlet openings of the two-channel turbine, wherein each inlet opening is adjoined by an one channel of the two-channel turbine and the two channels are separated from one another as far as the rotor by means of a wall, such that the exhaust-gas streams of the two channels are conducted separate from one another to the rotor;
- and
- wherein a first group of adjustable guide blades is provided at the rotor-side end of the first channel, and a second group of adjustable guide blades is provided at the rotor-side end of the second channel.
3 more elements
A method for operating a supercharged engine including a twin flow turbine, comprising:
- adjusting a first group of adjustable guide blades provided at a rotor-side end of a first channel based on operating conditions;
- and
- adjusting a second group of adjustable guide blades provided at a rotor-side end of a second channel based on operating conditions.
Dependencies are inferred from the claim text.