摘要:
A control device applied to an internal combustion engine (20) including a first supercharger (50) and a second supercharger (60) disposed in series includes: a supercharging-system controlling portion (11) for controlling a boost pressure; a cooling-system controlling portion (12) for controlling a flow rate of coolant circulating through an intercooler (71); and a valve defect detection portion (13) for detecting that a compressor bypass valve (32) is stuck in an opened state. When the valve defect detection portion (13) detects that the compressor bypass valve (32) is stuck in the opened state, the cooling-system controlling portion (12) increases a driving amount of an electric pump (72) so as to increase a flow rate of the coolant circulating through the intercooler (71).
摘要:
Restricting exhaust gas treatment devices from contacting a washing medium supplied by a washing system may reduce affecting the exhaust gas treatment devices. A washing system (50) may comprise a washing device (52) configured to supply a washing medium to a turbine ( T H ) during an ON mode of the washing system (50) and a fluid flow control system (38). The fluid flow control system (38) may be configured, during an OFF mode of the washing system (50), to direct exhaust gas through the at least one exhaust gas treatment device (41), and during the ON mode of the washing system (50), to restrict a mixture of exhaust gas and washing medium exiting the turbine ( T H ) from being directed through the at least one exhaust gas treatment device (41).
摘要:
A compound engine assembly (10) for use as an auxiliary power unit for an aircraft and including an engine core (12) with internal combustion engine(s), a compressor (18) having an outlet (18o) in fluid communication with an engine core inlet (12i), a bleed conduit (74) in fluid communication with the compressor outlet (12o) through a bleed air valve, and a turbine section (20) having an inlet (20i) in fluid communication with the engine core outlet (20o) and configured to compound power with the engine core (12). The turbine section (20) may include a first stage turbine (22) having an inlet (22o) in fluid communication with the engine core outlet (12o) and a second stage turbine (24) having an inlet (24i) in fluid communication the first stage turbine outlet (22o). A method of providing compressed air and electrical power to an aircraft is also discussed.
摘要:
A turbocharger (1) includes a turbine wheel (3) driven by exhaust gas, first and second compressor wheels (4, 5) coaxially coupled to the turbine wheel (3) via a shaft member (6), a compressor housing (8) accommodating the first and second compressor wheels (4, 5) and having defined therein a communication passage (17) through which air compressed by the first compressor wheel (4) flows to the second compressor wheel (5), and an electric motor (11) arranged in the communication passage (17) and using the shaft member (6) as a rotation shaft thereof.
摘要:
The present invention relates to a supercharging system for an internal combustion engine, comprising: a charging device (6, 6a) with a turbine (7, 7a) and a compressor (8, 8a), said compressor having a high speed shaft (30); a planetary gear (25) coupled to said high speed shaft (30) and an electric motor, or generator, (20) via a low speed drive shaft (31); a clutch unit (18a); and a power transmission (16) for connecting a crank shaft (4) of the combustion engine (1) to said drive shaft (31) via the clutch unit (18a), wherein a system control unit (23) is configured to control an in-cylinder mean temperature of said internal combustion engine by controlling the electric motor, or generator, (20) speed.
摘要:
An internal combustion engine system includes an internal combustion engine, an exhaust system, an exhaust gas recirculation circuit and a turbocharger including a first turbine interacting with a first compressor for charging air to the internal combustion engine. An exhaust gas recirculation passage is arranged to divert exhaust gases from the internal combustion engine upstream the first turbine and to debouch the exhaust gases downstream the first compressor. The internal combustion engine includes a bleed air channel which is located to divert compressed air at a location in or downstream from the first compressor and upstream of the internal combustion engine. A second turbine is arranged for receiving bleed air from the bleed air channel to recover energy from the bleed air channel. A vehicle including such an internal combustion engine system is also provided.
摘要:
An exhaust gas pressure regulator for a combustion engine includes a regulator housing and an inner diffuser assembly arranged inside the regulator housing so that an exhaust gas flow duct is formed between an inner surface of the regulator housing and an outer surface of the inner diffuser assembly. The inner diffuser assembly includes a front portion and a regulating piston that is moveable relative to the front portion and the regulator housing between an idle position in which the exhaust gas flow duct is open, and a pressurized position in which the regulating piston at least partly closes the exhaust gas flow duct. The inner diffuser assembly includes at least one throttled flow passage between the gas flow duct and an exhaust gas pressure chamber defined by the regulating piston and an interior surface of the front portion.
摘要:
An exhaust-flow-rate control valve 1 for controlling a flow rate of exhaust gas flowing through an exhaust flow passage includes: a valve rod 2; a valve body 3 having a flat plate shape and configured to rotate about the valve rod 2; and a valve housing 4 having a cylindrical shape and defining a part of the exhaust flow passage inside the valve housing. A valve seat surface 41 extending along a direction intersecting with an axial direction of the exhaust flow passage and being configured to make contact with an outer peripheral portion 31 of the valve body 3 in a fully-closed state in which an opening degree of the valve body 3 is zero degree, and a flow passage surface 42 extending along the axial direction of the exhaust flow passage and defining a passage region R through which the exhaust gas passes between the flow passage surface 42 and the outer peripheral portion 31 of the valve body 3 in a valve-open state in which the opening degree of the valve body 3 is greater than zero degree are formed on an inner peripheral surface of the valve housing 4. The passage region R of exhaust gas increases slowly while the valve body transitions from the fully-closed state to a predetermined valve-open state in which the separation distance between the valve body 3 and the end portion 42b of the flow passage surface 42 is shortest.
摘要:
A engine system (1) is provided with: a plurality of cylinder groups (10,20) which burn a gas mixture and discharge an exhaust gas; a plurality of high-pressure stage superchargers (11, 21) each having high-pressure stage turbines (13, 23) driven by the exhaust gas from the corresponding cylinder group and high-pressure stage compressors (14, 24) rotated by driving of the high-pressure stage turbines and configured to compress a gas supplied to the corresponding cylinder group; and a plurality of low-pressure stage superchargers (12,22) having a low-pressure stage turbine (15) driven by an exhaust gas discharged from the high-pressure stage turbine (13) of the high-pressure supercharger (11) which is any one of the plurality of high-pressure stage superchargers, and a low-pressure stage compressor (16) rotated by driving of the low-pressure stage turbine (15) and configured to compress a gas supplied to the high-pressure stage compressor (24) of the high-pressure stage supercharger (21) other than the one high-pressure stage supercharger (11).