ENERGY RECOVERY APPARATUS FOR A TURBOCHARGED COMPOUND ENGINE

Abstract: Energy recovery apparatus for a turbocharged compound engine (1) includes an exhaust turbine (4a) in an exhaust pipe of the engine, coupled to a first rotary machine (5). A second rotary machine (16) is mounted on a wheel axle (15) of a motor vehicle on which the engine is mounted. An exhaust turbine (6a) coupled to the exhaust port (4c) of the first-mentioned exhaust turbine drives a third rotary machine (7) to operate as a generator. The apparatus also includes a sensor (1a) for detecting the speed of rotation of the engine and a sensor (21) for detecting the load on the engine. The first to third rotary machines are controlled by signals from the sensors for effectively utilising the exhaust energy carried by the exhaust gas discharged by the engine.

Description: This invention relates to an energy recovery apparatus for a turbocharged compound engine, which apparatus is capable of recovering the exhaust energy of an internal combustion engine, and more particularly to an energy recovery apparatus for a turbocharged compound engine for recovering the exhaust energy by controlling an AC machine driven by the exhaust energy and an AC machine mounted on a wheel axle. There have been developed in recent years thermally-insulated engines having various components made of ceramics, including an outer wall of an exhaust manifold, a cylinder liner, an insulating plate for a cylinder head, and a piston, for example. In such thermally insulated engines, it is not necessary to cool the engine by radiating the heat generated inside the engine, but the energy of high-temperature exhaust gas discharged by the engine is recovered and fed back to the output shaft of the engine for increasing the output power from the engine. One known method of recovering the exhaust energy of an engine utilises a multistage gear speed reducer mechanism for reducing the speed of rotation of a turbine which is rotated by the exhaust gas and rotating the crankshaft to increase its output power. Japanese Laid-Open Patent Publication No. 59 (1984)-141713 discloses an exhaust energy recovering apparatus. In the disclosed apparatus, an exhaust turbine with an AC generator is rotated by the energy of exhaust gas discharged from an internal combustion engine, and an induction motor, operatively coupled to the output shaft of the engine, is driven by the output from the AC generator to recover the exhaust energy. The device also includes means for determining the magnitude of the load on the engine to control the amount of intake air, so that the temperature of the exhaust gas can be increased when the engine load is small. In the former method of recovering the exhaust energy, the transmission efficiency of the gear mechanism is low, and the gear mechanism is complex, resulting in increased cost. In the latter exhaust energy recovering apparatus, the electric power generated by the AC generator is applied to an induction motor to rotate the motor, thus driving the output shaft of the engine. No gear mechanism is required and the amount of intake air is controlled by the engine load for recovering the exhaust energy more efficiently. However, it is desired to control the amount of generated power according to the engine load, and to charge the battery with the generated power. It is an object of the present invention to provide an energy recovery apparatus for a turbocharged compound engine which employs no gear mechanism and which includes a first rotary machine operable as a generator for converting exhaust energy to electric energy to recover the energy, and a second rotary machine mounted on a wheel axle and operable as a motor driven by the recovered electric power according to the speed of rotation and load on an internal combustion engine, whereby exhaust energy can be recovered. According to one aspect of the invention, there is provided energy recovery apparatus in a turbocharged compound internal combustion engine including an exhaust turbine coupled to a first rotary machine disposed in an exhaust pipe of an internal combustion engine; characterised by means for detecting the speed of rotation of the engine; means for detecting the load on the engine; a second rotary machine disposed on a wheel axle driven by the engine; and means for controlling the operation of the first and second rotary machines according to the speed of rotation of the engine and the load on the engine. According to another aspect of the invention, there is provided energy recovery apparatus in a turbocharged compound engine including an exhaust turbine disposed in an exhaust pipe and coupled to an AC generator; characterised by means for detecting the speed of rotation of a wheel axle drivable by the engine; an AC motor mounted on the wheel axle; and means coupled to the AC generator for supplying electric power to the AC motor according to the speed of rotation of the wheel axle. Embodiments of the invention will now be described, by way of example, with reference to the accompanying drawings, in which Fig. 1 is a schematic block diagram of an energy recovery apparatus for a turbocharged compound engine according to a first embodiment of the present invention; Fig. 2 is a flowchart showing the operation sequence of the apparatus of Fig. l; Fig. 3 is a graph showing the relationship between the torque and the speed of rotation of an internal combustion engine; Fig. 4 is a schematic view of an exhaust energy recovery apparatus according to a second embodiment of the present invention; and Fig. 5 is a block schematic diagram showing a modification of the second embodiment. Referring to Fig. 1, an internal combustion engine 1 has combustion chambers, an exhaust pipe and other components which are of a thermally-insulated structure. An intake pipe 2a is connected to an intake manifold 2, and an exhaust pipe 3a is connected to an exhaust manifold 3. A turbocharger 4 is driven by the exhaust gas discharged from the exhaust pipe 3a and includes a turbine blade wheel 4a and a compressor blade wheel 4b between which there is disposed a first rotary machine 5 operable as a generator or a motor. A rotor 5a composed of a perma­ nent magnet having strong residual magnetism is disposed coaxially with the turbine blade wheel 4a. When the turbine blade wheel 4a is driven by the energy of the exhaust gas, the windings of a stator 5b positioned in confronting relation to the rotor 5a induce AC electric power which is transmitted from the first rotary machine 5 as a generator to a switching device 5d. As the turbine blade wheel 4a is driven, the compressor blade wheel 4b charges air through the intake pipe 2a and the intake manifold 2 into the internal combustion engine l. The boost pressure of the supercharged air is detected by a boost sensor 2b on the intake pipe 2a, and a detected signal BS from the boost sensor 2b is supplied to a controller l0. The exhaust gas G with residual energy, which has driven the turbine blade wheel 4a, is introduced through an exhaust port 4c into an exhaust turbine 6, in which the exhaust gas drives a turbine blade wheel 6a. The exhaust gas, from which almost all exhaust energy has been removed, is discharged from an exhaust port 6b. The pressure of the exhaust gas G is detected by a pressure sensor 4d mounted on the exhaust port 4c, and a detected signal GS from the pressure sensor 4d is supplied to the controller l0. A third rotary machine 7 operable as a generator has its rotatable shaft disposed coaxially with the turbine blade wheel 6a. A rotor 7a composed of a permanent magnet with strong residual magnetism is disposed on the shaft of the third rotary machine 7. When the rotor 7a is driven to rotate, the windings of a stator 7b confronting the rotor 57a induce AC electric power which is transmitted to a transformer 8. The voltage of the electric power generated by the third rotary machine 7 is detected by a voltage detector 7c, and a detected voltage E2 from the voltage detector 7c is applied to the controller l0. The output voltage from the first rotary machine 5 which is operated as the generator is detected by a voltage detector 5c, and the detected AC voltage El from the voltage detector 5c is applied to the controller l0. The transformer 8 converts the voltage of the AC electric power from the third rotary machine 7 to a prescribed voltage based on a control signal CS2 from the controller l0. The AC electric power from the transformer 8 is fed to a rectifier 9, which produces DC electric power that is supplied to an inverter ll. The AC electric power generated by the first rotary machine 5 as the generator and applied to the switching device 5d is supplied to a transformer l2 under the control of a control signal CH from the controller l0. The transformer l2 converts the applied voltage to a prescribed voltage based on a control signal CSl from the controller l0, and the electric power from the transformer l2 is fed to a rectifier l3 which applies the DC output to a battery l4 and the inverter ll. The supplied DC electric power is converted by the inverter ll to AC electric power having a frequency corresponding to a control signal ISl from the controller l0. The AC electric power from the inverter ll is supplied to a second rotary machine l6 disposed coaxially with a wheel axle l5 and operable as a motor or a generator to drive the axle l5 thereby to rotate a wheel l7. The speed of rotation of the wheel axle l5 is detected by a rotation sensor l8, and a detected signal WS from the rotation sensor l8 is applied to the controller l0. A rectifier l9 can be turned on or off by a signal DS from the controller l0. In response to the signal DS, the rectifier l9 converts the AC electric power generated by the secondary rotary machine l6 to DC electric power which is supplied to charge the battery l4. An inverter 20 is responsive to a control signal IS2 from the controller l0 for converting the DC power from the battery l4 to AC power of a prescribed frequency. The AC power from the inverter 20 is fed through the switching device 5d to the first rotary machine 5, so that the first rotary machine 5 will be operated as a motor for increasing the boost pressure if the boost pressure of the air charged into the internal combustion engine l is low. The load on the internal combustion engine l is detected by a load sensor 2l which detects a rack position of the internal combustion engine l. The gear position of gear transmission is detected by a gear sensor 22. The clutch position is detected by a clutch sensor 23. These sensors 2l, 22, 23 apply detected signals RS, GP, CL, respectively, to the controller l0. The speed of rotation of the internal combustion engine l is detected by a rotation sensor la, which supplies a rotation signal r.p.m. to the controller l0. An operation sequence of the energy recovery apparatus shown in Fig. l will be described below with reference to Figs. 2 and 3. If the engine speed detected by the rotation sensor la is below 800 r.p.m. in a step l in Fig. 2, the idling condition of the internal combustion engine l is detected by the controller l0 from the gear signal GP from the gear sensor 22 and the clutch signal CL from the clutch sensor 23 (steps 2 and 3). The controller l0 then switches the switching device 5d with the control signal CH to operate the first rotary machine 5 as a generator and convert the generated power to DC power through the transformer 2 and the rectifier l3 for charging the battery l4 (steps 4 and 5). If the engine rotation speed is higher than 800 r.p.m. in the step l, and the clutch signal CL is off indicating clutch disconnection or the gear signal GL is off indicating a neutral gear position, then control goes to the steps 4 and 5 to charge the battery l4. If the gear signal GP is on, indicating any other gear position than the neutral gear position in a step 7, then the controller l0 further checks the rotation of the internal combustion engine l with the rotation signal r.p.m. to determine whether the engine speed is lower than 2000 r.p.m. in a step 8. If the engine speed is lower than 2000 r.p.m., and the engine load L is not nil, but is a light load smaller than LDl (see Fig. 3) in steps 8, 9, and l0, then control proceeds to a step ll. The electric power generated by the first rotary machine 5 is supplied through the rectifier l3 to the inverter ll (steps ll and l2). The exhaust turbine 6 is rotated by the exhaust gas G which has driven the turbine blade wheel 4a, to operate the third rotary machine 7 as a generator, and the generated power is supplied to the transformer 8 which is controlled by the control signal CS2 to regulate the voltage to a prescribed voltage. The electric power from the transformer 8 is converted by the rectifier 9 to DC power that is applied to the inverter ll (steps l3 and l4). The pressure of the exhaust gas G is detected by the pressure sensor 4d, and based on the pressure signal GS and the voltage signal E2, the controller l0 applies the control signal CS to the transformer 8 so that the energy of the exhaust gas will be converted to electric energy to a predetermined extent. The electric power fed to the inverter ll in the steps l2 and l4 is controlled by the control signal ISl applied to the inverter ll upon application of the rotation signal WS from the rotation sensor l8 to the controller l0, so as to be converted to AC power of a certain frequency which is supplied to the second rotary machine l6 to operate the same as the motor (steps l5 and l6). The second rotary machine l6 now operates to provide power to assist in the rotation of the wheel l7 (step l7). If the engine load L is between LDl and LD2 (Fig. 3) in the step l0, then control goes from a step l8 to a step l9 in which the power generated by the first rotary machine 5 is cut off by the switching device 5d, and the exhaust energy is primarily utilized for rotating the compressor blade wheel 4b to increase the boost pressure and supply the same into the interal combustion engine l (steps l9 and 20). The power generated by the third rotary machine 7 as a generator is fed via the transformer 8 and the rectifier 9 to the inverter ll for operating the second rotary machine l6 as a motor to assist in the rotation of the wheel shaft l5 (steps 2l and 22). If the engine load L is larger than LD2 in the step l8, then the switching device 5d is controlled by the control signal CH to switch the first rotary machine 5 into the motor mode, and the DC power from the battery l4 is supplied to the inverter 20 and converted by the control signal IS2 to AC power of a prescribed frequency, which is supplied through the switching device 5d to drive the first rotary machine 5. The boost pressure is controlled so that the pressure detected by the boost sensor 2b on the intake pipe 2a will become a prescribed pressure (steps 23 and 24). The AC power generated by the third rotary machine 7 based on the energy of the exhaust gas G is supplied through the transformer 8, the rectifier 9, and the inverter ll to the second rotary machine l6 as a motor to assist in the rotation of the wheel axle l5 (steps 25 and 26). If the engine load L is nil and the engine braking is detected from the load signal RS, the clutch signal CL, and the gear signal GP in the step 9, then control goes to a step 27. The switching device 5d is controlled by the control signal CH from the controller l0 to supply the power generated by the first rotary machine 5 as a generator to the transformer l2, which supplies the power through the rectifier l3 to charge the battery l4 (steps 27 and 28). The electric power generated by the third rotary machine 7 is also fed through the transformer 8 and the rectifier 9 to the inverter ll, from which it is supplied to the windings of the second rotary machine l6 (steps 29 and 30). In response to the control signal DS from the controller l0, the rectifier l9 converts, together with the power from the step 28, the power generated by the second rotary machine l6 driven as a generator under the inertial force of the wheel l7, to DC power which is supplied to charge the battery l4 (steps 29 through 3l). An energy recovery apparatus according to a second embodiment of the present invention is shown in Fig. 4. An engine l0l includes a combustion chamber defined by a piston l0la and a cylinder liner l0lb, and an exhaust port l0lc, the combustion chamber and the exhaust port l0lc being of a thermally-insulated construction made of ceramics. An exhaust turbine l03 having an AC generator l04 is mounted on an exhaust manifold l02 coupled to the exhaust port l0lc. The exhaust turbine l03 has a rotatable shaft coupled directly to the rotatable shaft of an AC generator l04. When a turbine blade wheel l03a of the exhaust turbine l03 is rotated by the high-temperature exhaust gas discharged from the exhaust manifold l02, the AC generator l04 generates AC electric power of a high frequency. Fuel is injected by a fuel injection pump l05 into the engine l0l. A load sensor l06 is mounted on the fuel injection pump l05 for detecting the amount of fuel injected, to generate a load signal FS. A converter l07 in the form of a cycloconverter, for example, converts the AC power of high frequency from the AC generator to AC power of a lower frequency with high efficiency. The frequency conversion effected by the converter l07 is controlled by a rotation signal WS from a rotation sensor l08 which detects the speed of rotation of a wheel axle ll0 supporting a wheel lll and the load signal FS from the load sensor l06. A motor l09 has a rotatable shaft disposed coaxially with the wheel axle ll0. The motor l09 is supplied with the AC power from the converter l07 to drive the wheel lll. The frequency of the AC power supplied from the converter l07 to the motor l09 is controlled by the rotation signal WS and the load signal FS at all times, so that the motor l09 is driven in a power running mode. Therefore, the wheel lll is always assisted in its rotation by the motor l09 driven in the power running mode. Fig. 5 shows a third embodiment of the present invention which is a modification of the arrangement shown in Fig. 4. Denoted in Fig. 5 at ll2 is a rectifier and ll3 an inverter. The power generated by the AC generator l04 (Fig. 4) is supplied to the rectifier ll2, and DC power from the rectifier ll2 is supplied to the inverter ll3 which is controlled by the rotation signal WS from the rotation sensor l08 and the load signal FS from the load sensor l06. The DC power supplied to the inverter ll3 is converted thereby to AC power of a prescribed frequency to energize the motor l0. Operation of the second and third embodiments is as follows: In the arrangement of Fig. 4, the high-­ temperature exhaust gas discharged from the engine l0l of thermally-insulated structure is introduced through the exhaust manifold l02 into the exhaust turbine l03 to drive the AC generator l04 coupled to the turbine blade wheel l03a. The AC power generated by the AC generator l04 is supplied to the converter l07. The converter l07 is responsive to the load signal FS from the load sensor l06 and the rotation signal WS from the rotation sensor l08 for converting the AC power of higher frequency from the AC generator l04 to the AC power of lower frequency, which is supplied to energize the motor l09. Therefore, the motor l09 is energized in the power running mode to drive the wheel axle ll0 to assist in the rotation of the wheel lll irrespective of the speed of rotation of the wheel axle ll0. In Fig. 5, the exhaust energy is converted by the AC generator l04 to the electric energy which is utilized to energize the motor l09 in the power running mode at a rate corresponding to the speed of rotation of the wheel axle ll0 for driving the wheel lll, as with the arrangement of Fig. 4. With the rectifier ll2 and the inverter ll3 added to the electric energy transmission path, however, the loss caused by these additional components makes the overall efficiency of exhaust energy recovery lower than that of the system of Fig. 4.

Claims: 1. Energy recovery apparatus in a turbocharged compound internal combustion engine including an exhaust turbine (4a) coupled to a first rotary machine (5) disposed in an exhaust pipe (3) of an internal combustion engine (1); characterised by means (1a) for detecting the speed of rotation of the engine; means (21) for detecting the load on the engine; a second rotary machine (16) disposed on a wheel axle driven by the l0engine; and means (10) for controlling the operation of the first and second rotary machines according to the speed of rotation of the engine and the load on the engine. 2. Apparatus according to claim 1, characterised by a third rotary machine (7) coupled to an exhaust turbine (6a) disposed in an exhaust port (4c) of a turbocharger (4) and operable as a generator for converting exhaust energy from the engine (1) to electric energy for energy recovery. 3. Apparatus according to claim 1 or claim 2, characterised by means (13) for charging a battery (14) with electric power generated by the first rotary machine (5) when the internal combustion engine is idling. 4. Apparatus according to any preceding claim, characterised by means (11) for driving the second rotary machine, operating as a motor, with electric power generated by the first rotary machine when the internal combustion engine is under a small load. 5. Apparatus according to any preceding claim, characterised by means (20) for driving the first rotary machine (5) as a motor with electric power from a battery (14) to increase boost pressure; and means (11) for driving the second rotary machine (16) as a motor with electric power generated by the third rotary machine (7). 6. Apparatus according to any preceding claim, characterised by means (19) for charging a battery (14) with electric power generated by the second rotary machine (16) upon engine braking. 57. Energy recovery apparatus in a turbocharged compound engine (101) including an exhaust turbine (103a) disposed in an exhaust pipe (102) and coupled to an AC generator (104); characterised by means (108) for detecting the speed of rotation of a wheel axle (110) drivable by the engine; an AC motor (109) mounted on the wheel axle; and means (107) coupled to the AC generator for supplying electric power to the AC motor according to the speed of rotation of the wheel axle. 8. Apparatus according to claim 7; characterised by means including a converter (107) for converting electric power of a higher frequency generated by the AC generator (104) to electric power of a lower frequency. 9. Apparatus according to claim 7, characterised by means including a rectifier (112) and an inverter (113) for converting electric power of a higher frequency generated by the AC generator (104) to electric power of a lower frequency.

Inventors: KAWAMURA HIDEO, TAMAI, KATSUYUKI
Applicants: ISUZU MOTORS LIMITED
Application year: 1986
Main classification: F02B37
IPC codes: B60W10, F02B37, F02B41, B60K6, F02D41, F01N5