WO2024087601A1 - 一种混合动力电驱动系统以及混合动力车辆 - Google Patents

一种混合动力电驱动系统以及混合动力车辆 Download PDF

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Publication number
WO2024087601A1
WO2024087601A1 PCT/CN2023/095714 CN2023095714W WO2024087601A1 WO 2024087601 A1 WO2024087601 A1 WO 2024087601A1 CN 2023095714 W CN2023095714 W CN 2023095714W WO 2024087601 A1 WO2024087601 A1 WO 2024087601A1
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WO
WIPO (PCT)
Prior art keywords
gear
assembly
shaft
cavity
drive system
Prior art date
Application number
PCT/CN2023/095714
Other languages
English (en)
French (fr)
Inventor
陈亘
王丹
章帅韬
Original Assignee
东风汽车集团股份有限公司
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Application filed by 东风汽车集团股份有限公司 filed Critical 东风汽车集团股份有限公司
Publication of WO2024087601A1 publication Critical patent/WO2024087601A1/zh

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60KARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
    • B60K6/00Arrangement or mounting of plural diverse prime-movers for mutual or common propulsion, e.g. hybrid propulsion systems comprising electric motors and internal combustion engines ; Control systems therefor, i.e. systems controlling two or more prime movers, or controlling one of these prime movers and any of the transmission, drive or drive units Informative references: mechanical gearings with secondary electric drive F16H3/72; arrangements for handling mechanical energy structurally associated with the dynamo-electric machine H02K7/00; machines comprising structurally interrelated motor and generator parts H02K51/00; dynamo-electric machines not otherwise provided for in H02K see H02K99/00
    • B60K6/20Arrangement or mounting of plural diverse prime-movers for mutual or common propulsion, e.g. hybrid propulsion systems comprising electric motors and internal combustion engines ; Control systems therefor, i.e. systems controlling two or more prime movers, or controlling one of these prime movers and any of the transmission, drive or drive units Informative references: mechanical gearings with secondary electric drive F16H3/72; arrangements for handling mechanical energy structurally associated with the dynamo-electric machine H02K7/00; machines comprising structurally interrelated motor and generator parts H02K51/00; dynamo-electric machines not otherwise provided for in H02K see H02K99/00 the prime-movers consisting of electric motors and internal combustion engines, e.g. HEVs
    • B60K6/22Arrangement or mounting of plural diverse prime-movers for mutual or common propulsion, e.g. hybrid propulsion systems comprising electric motors and internal combustion engines ; Control systems therefor, i.e. systems controlling two or more prime movers, or controlling one of these prime movers and any of the transmission, drive or drive units Informative references: mechanical gearings with secondary electric drive F16H3/72; arrangements for handling mechanical energy structurally associated with the dynamo-electric machine H02K7/00; machines comprising structurally interrelated motor and generator parts H02K51/00; dynamo-electric machines not otherwise provided for in H02K see H02K99/00 the prime-movers consisting of electric motors and internal combustion engines, e.g. HEVs characterised by apparatus, components or means specially adapted for HEVs
    • B60K6/40Arrangement or mounting of plural diverse prime-movers for mutual or common propulsion, e.g. hybrid propulsion systems comprising electric motors and internal combustion engines ; Control systems therefor, i.e. systems controlling two or more prime movers, or controlling one of these prime movers and any of the transmission, drive or drive units Informative references: mechanical gearings with secondary electric drive F16H3/72; arrangements for handling mechanical energy structurally associated with the dynamo-electric machine H02K7/00; machines comprising structurally interrelated motor and generator parts H02K51/00; dynamo-electric machines not otherwise provided for in H02K see H02K99/00 the prime-movers consisting of electric motors and internal combustion engines, e.g. HEVs characterised by apparatus, components or means specially adapted for HEVs characterised by the assembly or relative disposition of components
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H57/00General details of gearing
    • F16H57/04Features relating to lubrication or cooling or heating
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H57/00General details of gearing
    • F16H57/08General details of gearing of gearings with members having orbital motion
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K7/00Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
    • H02K7/10Structural association with clutches, brakes, gears, pulleys or mechanical starters
    • H02K7/116Structural association with clutches, brakes, gears, pulleys or mechanical starters with gears
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K9/00Arrangements for cooling or ventilating
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/60Other road transportation technologies with climate change mitigation effect
    • Y02T10/62Hybrid vehicles

Definitions

  • the present disclosure belongs to the technical field of hybrid electric drive systems, and in particular relates to a hybrid electric drive system and a hybrid vehicle.
  • Hybrid vehicle drive technology is the core stage of the development of new energy vehicles. Improving fuel economy and reducing emissions are important issues facing hybrid technology.
  • the mainstream hybrid electric drive products on the market are still of assembled structure.
  • the motor, gearbox and motor controller are designed separately and then assembled.
  • the current hybrid electric drive product structure becomes bulky, with many pipelines and poor carrying capacity.
  • the present disclosure provides a hybrid electric drive system and a hybrid vehicle, which have high integration, small overall size and good carrying performance.
  • a hybrid electric drive system comprising: a housing assembly, provided with a shaft gear cavity, a motor cavity and an oil storage cavity, wherein the oil storage cavity is connected to the shaft gear cavity and/or the motor cavity; a motor assembly, provided in the motor cavity, comprising more than one motor; a speed change mechanism assembly, provided in the shaft gear cavity, for transmission connection with both the engine and the motor, and outputting power; a controller assembly, comprising a housing provided with a control cavity and a control component installed in the control cavity, the housing being connected to the housing assembly, the housing being provided with a cooling flow channel for cooling the control component, the control component being provided with a three-phase output copper busbar electrically connected to the three-phase input copper busbar of the motor; wherein; a lubrication power device is installed on the housing assembly; a lubrication oil circuit is provided in the housing assembly, the motor assembly and the speed change mechanism assembly, and the lubrication power device is connected to the oil storage cavity
  • a hybrid vehicle comprising: a vehicle body provided with a front engine compartment; an engine installed in the front engine compartment; the above-mentioned hybrid electric drive system is installed in the front engine compartment, and the speed change mechanism assembly is transmission-connected to the engine.
  • FIG1 is a perspective view of a hybrid electric drive system according to some embodiments of the present disclosure.
  • FIG2 is a schematic structural diagram of a hybrid electric drive system according to some embodiments of the present disclosure at a first viewing angle
  • FIG3 is a schematic diagram of the structure of the hybrid electric drive system of FIG1 with the end cover removed;
  • FIG4 is a schematic diagram of the structure of the hybrid electric drive system of FIG1 after the right housing is removed;
  • FIG5 is a schematic diagram of the structure of a controller assembly in the hybrid electric drive system of FIG1 ;
  • FIG6 is an exploded view of the controller assembly of FIG5 ;
  • FIG7 is a front view of the controller assembly of FIG5 ;
  • FIG8 is a cross-sectional view of the controller assembly of FIG7 taken along the section line A-A in FIG7 ;
  • FIG9 is a rear view of the controller assembly of FIG5 ;
  • FIG10 is an internal structure diagram of the controller assembly of FIG5 after the housing is removed;
  • FIG11 is a schematic structural diagram of an upper housing in the controller assembly of FIG5 ;
  • FIG12 is a top view of the upper housing of the controller assembly of FIG7 ;
  • FIG13 is a cross-sectional view of the upper housing of the controller assembly of FIG8 taken along the section line B-B in FIG12;
  • FIG14 is a schematic diagram of the structure of the water cooling plate in the controller assembly of FIG5 ;
  • FIG15 is a front view of the water cooling plate in the controller assembly of FIG10;
  • FIG16 is a top view of the water cooling plate in the controller assembly of FIG10 ;
  • FIG17 is a top view of the structure of the high-voltage transfer box in the controller assembly of FIG5 after the top cover of the box body is removed;
  • FIG18 is a schematic diagram of the internal structure of the high-voltage transfer box in the controller assembly of FIG13;
  • FIG19 is a wiring circuit diagram of the high voltage transfer box in the controller assembly of FIG5;
  • FIG20 is a schematic structural diagram of a hybrid power transmission mechanism assembly in the hybrid power electric drive system of FIG1 ;
  • FIG21 is a schematic structural diagram of the hybrid power transmission mechanism assembly of FIG20 at a first viewing angle
  • FIG22 is a schematic structural diagram of the hybrid power transmission mechanism assembly of FIG20 at a second viewing angle
  • FIG23 is a cross-sectional view of the engine input shaft assembly in the hybrid transmission mechanism assembly of FIG20;
  • FIG24 is a schematic structural diagram of the internal lubrication passage of the engine input shaft assembly of FIG23;
  • FIG25 is a schematic structural diagram of the inner ring gear shaft in the engine input shaft assembly of FIG23;
  • FIG26 is a cross-sectional view of the inner gear ring shaft of FIG25;
  • FIG27 is a schematic structural diagram of a shift mechanism assembly in the hybrid electric drive system of FIG1 ;
  • FIG28 is a schematic structural diagram of the installation area of the left housing in the hybrid electric drive system of FIG1 ;
  • FIG29 is a schematic structural diagram of the middle plate of the hybrid electric drive system of FIG1 ;
  • FIG30 is a diagram showing the installation structure of the cooling spray pipeline in the hybrid electric drive system of FIG1 ;
  • FIG31 is a schematic diagram of the structure of the oil collecting tank on the left housing in the hybrid electric drive system of FIG1 ;
  • FIG. 32 is a schematic diagram of the structure of a hybrid vehicle according to some embodiments of the present disclosure.
  • 300-housing assembly 301-motor cavity; 302-shaft gear cavity; 303-oil inlet channel; 304-oil collecting groove; 305-bearing mounting hole, 3041-notch; 310-right housing; 320-left housing, 321-middle plate, 3211-bearing hole, 3212-avoidance area, 322-installation area, 3221-drainage hole, 3222-pin hole, 3223-oil baffle plate, 3224-oil guide area, 3225-drainage hole; 323-convex rib; 324-baffle; 325-cooling spray pipeline; 330-end cover; 340-lubricating power unit; 350-plug cover for covering thermostat; 360-temperature sensor; 370-solenoid valve; 380-radiator; 390-vent plug.
  • 400-controller assembly 401-control chamber, 402-high pressure chamber.
  • 410-housing 411-upper housing, 4111-top plate, 4112-heat dissipation structure, 4113-accommodating portion, 4114-through hole, 4115-third through hole, 4116-installation port; 412-water cooling plate, 4121-base plate, 4122-cover, 4123-cooling groove, 4124-first through hole, 4125-capacitor installation position, 4126-sealing groove; 413-lower housing, 4131-second through hole, 4132-positioning pin; 414-operating window; 415-waterproof breathable valve; 416-cover plate; 417-inlet pipe; 418-outlet pipe; 419-sealing ring.
  • 420-control component 421-control board; 422-drive board; 423-IGBT; 424-three-phase output copper busbar; 425-high-voltage capacitor; 426-current sensor; 427-low-voltage connector, 428-connection cable.
  • 430-high-voltage transfer box 431-box body, 4311-box wall, 4312-top cover, 4313-assembly port; 432-high-voltage connection component, 4321-positive copper busbar, 4322-negative copper busbar, 4323-connection harness; 433-power connector; 434-high-voltage connector, 4341-first high-voltage connector, 4342-second high-voltage connector; 435-fuse; 436-mounting base, 4361-sinking area, 4362-baffle.
  • 500-shift mechanism assembly 510-shift motor; 520-shift reduction mechanism; 530-shift hub; 540-shift fork.
  • 600-hybrid power transmission mechanism assembly 610-engine input shaft assembly; 620-generator, 621-generator rotor, 622-second hollow cavity; 630-ICE intermediate shaft assembly, 631-ICE intermediate shaft, 632-first ICE intermediate gear, 633-second ICE intermediate gear; 640-differential shaft assembly; 650-EV intermediate shaft assembly, 651-EV intermediate shaft, 652-first EV intermediate gear, 653-second EV intermediate gear; 660-drive motor input shaft assembly, 661-input shaft, 662-transmission gear; 670-drive motor, 671-drive motor rotor.
  • 200-inner gear ring shaft 201-inner hole; 210-sleeve portion; 220-cover portion, 221-gear sleeve portion, 222-baffle portion, 223-inner spline; 230-first mounting position; 240-assembly position, 241-inner hole wall; 250-second mounting position; 260-limiting structure, 261-circlip groove, 262-end face, 263-convex edge, 264-hole shoulder; 270-oil guide hole; 280-oil guide groove.
  • 10-oil guide pipe 11-oil outlet hole, 12-oil outlet; 20-oil guide member; 30-bushing; 40-actuator, 41-gear hub, 42-coupling gear, S1-first actuator, S2-second actuator; 50-first gear, 51-gear ring, 52-connecting part; 60-second gear; 70-circlip; 80-sleeve.
  • Figure 1 is a stereoscopic diagram of a hybrid electric drive system according to some embodiments of the present disclosure
  • Figure 2 is a structural schematic diagram of a hybrid electric drive system at a first perspective according to some embodiments of the present disclosure
  • Figure 3 is a structural schematic diagram of the hybrid electric drive system of Figure 1 after the end cover is removed
  • Figure 4 is a structural schematic diagram of the hybrid electric drive system of Figure 1 after the right shell is removed.
  • a hybrid electric drive system 1000 is provided. As shown in FIGS. 1 to 4 , the hybrid electric drive system 1000 may include a housing assembly 300, a hybrid transmission mechanism assembly 600 and a controller assembly 400.
  • the hybrid transmission mechanism assembly 600 is installed inside the housing assembly 300
  • the controller assembly 400 is installed outside the housing assembly 300.
  • the housing assembly 300 is provided with a shaft gear cavity 302, a motor cavity 301 and an oil storage cavity.
  • the oil storage cavity is used to store lubricating oil required by the hybrid electric drive system 1000.
  • the oil storage cavity is connected to the shaft gear cavity 302 and/or the motor cavity 301.
  • the hybrid transmission mechanism assembly 600 is composed of a motor assembly and a transmission mechanism assembly.
  • the motor assembly may include more than one motor, that is, the hybrid electric drive system 1000 may It is a single-motor hybrid electric drive system or a multi-motor hybrid electric drive system.
  • the motor assembly is installed in the motor cavity 301, and the speed change mechanism assembly is installed in the shaft gear cavity 302.
  • the speed change mechanism assembly is connected to the engine and one or more motors in a transmission manner, and outputs power to the wheels.
  • the speed change mechanism assembly can adopt any structure disclosed in the prior art, such as the hybrid speed change mechanism of the Chinese invention application "A single-motor single-planetary gearbox, system and vehicle” with publication number CN111873780A, or the hybrid speed change mechanism of the Chinese invention application “Hybrid power transmission system, method of use and hybrid vehicle” with publication number CN111942138A, which is not limited by the present disclosure.
  • a lubrication power device 340 is installed outside the housing assembly 300, and the lubrication power device 340 may be an oil pump.
  • the housing assembly 300, the motor assembly, and the speed change mechanism assembly are all provided with a lubrication oil circuit, and the lubrication oil circuit may be a space obtained by removing part of the material of the housing or the shaft, or a space formed by a plurality of parts.
  • the lubrication power device 340 provides power for the circulation of the lubrication oil, so that the lubrication oil circulates between the lubrication oil circuit and the oil storage chamber.
  • the housing assembly 300 adopts a split structure.
  • the specific division method is not limited in the present disclosure.
  • the housing assembly 300 can be divided in a horizontal plane to form two upper and lower housings, or divided in a vertical plane to form three left, middle and right housings.
  • the housing assembly 300 includes a right housing 310, a left housing 320 and an end cover 330 connected in sequence.
  • the right housing 310 and the left housing 320 enclose a shaft gear cavity 302.
  • the left housing 320 and the end cover 330 enclose a motor cavity 301.
  • FIG. 28 is a structural schematic diagram of the installation area of the left housing in the hybrid electric drive system of FIG. 1.
  • the controller assembly 400 is installed on the left housing 320.
  • an installation area 322 is provided on the left housing 320, and the controller assembly 400 is installed in the installation area 322.
  • the installation area 322 is a groove structure integrally formed on the left housing 320, and the side wall of the installation area 322 can wrap the controller assembly 400 to a certain extent, thereby improving the installation stability of the controller assembly 400.
  • the side wall of the installation area 322 is provided with a drainage hole 3221, which is convenient for draining the water stored in the installation area 322 and improving the safety of electricity use.
  • a positioning structure is provided between the installation area 322 and the housing 410, and the positioning structure can adopt a positioning pin 4132 and a pin hole, or a step surface matching structure, which is not limited by the present disclosure.
  • a positioning pin 4132 is provided at the bottom of the housing 410, and a pin hole 3222 is provided in the installation area 322. When installing, the positioning pin 4132 is inserted into the pin hole 3222, which can ensure that the three-phase output copper busbar 424 is opposite to the three-phase input copper busbar of each motor, which is convenient for installing high-pressure bolts.
  • Figure 5 is a structural schematic diagram of the controller assembly in the hybrid electric drive system of Figure 1;
  • Figure 6 is an exploded view of the controller assembly of Figure 5;
  • Figure 7 is a front view of the controller assembly of Figure 5;
  • Figure 8 is a sectional view of the controller assembly of Figure 7 taken along the section line A-A in Figure 7;
  • Figure 9 is a rear view of the controller assembly of Figure 5.
  • the housing 410 is a split structure.
  • the specific division method is not limited in this disclosure.
  • the housing 410 can be divided in a horizontal plane to form two upper and lower shells, or divided in a vertical plane to form three left, middle and right shells.
  • the housing 410 of the present disclosure does not have a water-cooling plate that is relatively independent of the housing 410, but directly sets a cooling groove 4123 on the housing 410 for the circulation of coolant. It can also be understood that the present disclosure uses the water-cooling plate as a part of the housing 410.
  • the housing 410 includes an upper housing 411 and a water-cooling plate 412.
  • the upper housing 411 and the water-cooling plate 412 are combined to form a control chamber 401.
  • Bolt holes are provided on the upper housing 411 and the water-cooling plate 412.
  • the two are sealed by a sealing ring 419 and fixed by bolts.
  • a cooling groove 4123 is provided on the water-cooling plate 412, and the cooling groove 4123 is formed by the top surface of the water-cooling plate 412 being concave downward.
  • the number of cooling slots 4123 is the same as the number of motors.
  • the cooling slots 4123 are evenly distributed in the horizontal direction and connected in sequence.
  • the cooling slot 4123 may also be a through-length slot, and a sealing plate is welded or bonded to the slot to form an open cooling position having the same number as the motors.
  • FIG10 is an internal structure diagram of the controller assembly of FIG5 after the housing is removed.
  • the control assembly 420 includes an electrically connected control board 421, a drive board 422, an IGBT423, a three-phase output copper bus 424 and a high-voltage capacitor 425.
  • the control board 421, the drive board 422, the IGBT423 and the three-phase output copper bus 424 are electrically connected in sequence, and the high-voltage capacitor 425 is electrically connected to the IGBT423.
  • the drive board 422, the IGBT423 and the high-voltage capacitor 425 are all installed on the water-cooled plate 412.
  • the IGBT423 and the high-voltage capacitor 425 are arranged side by side in the horizontal direction.
  • the drive board 422 is located above the IGBT423 and is fixed to the water-cooled plate 412 by screws.
  • the IGBT423 covers the notch of the cooling groove 4123 to enclose the cooling groove 4123 to form a cooling channel.
  • Figure 14 is a structural schematic diagram of the water cooling plate in the controller assembly of Figure 5;
  • Figure 15 is a front view of the water cooling plate in the controller assembly of Figure 10;
  • Figure 16 is a top view of the water cooling plate in the controller assembly of Figure 10.
  • the water-cooled plate 412 may include a connected substrate 4121 and a cover 4122, wherein the substrate 4121 is roughly plate-shaped, and the substrate 4121 is provided with a cooling groove 4123 and a first through hole 4124 for the three-phase output copper bar 424 to pass through.
  • a flow channel is arranged inside the substrate 4121, and the flow channel is an open structure to form a cooling groove 4123.
  • the cover 4122 is sleeve-shaped as a whole, and has an inner cavity.
  • the inner cavity of the cover 4122 is connected to the control cavity 401 of the housing 410 through the first through hole 4124, so that after the three-phase output copper bar 424 is electrically connected to the IGBT 423 located in the control cavity 401, it can extend into the inner cavity of the cover 4122 through the first through hole 4124 to be electrically connected to the three-phase input copper bar of the motor extending into the inner cavity of the cover 4122.
  • the base plate 4121 and the cover shell 4122 can be integrally formed by injection molding or metal casting, or fixedly connected by welding, bonding, bolting, etc. In this embodiment, the base plate 4121 and the cover shell 4122 are both made of aluminum alloy and are directly cast.
  • the substrate 4121 is provided with a sealing groove 4126 at the outer periphery of the notch of the cooling groove 4123, and a sealing ring 419 is provided in the sealing groove 4126.
  • the IGBT 423 has a mounting edge extending horizontally outward, and the mounting edge presses the sealing ring 419. The sealing of the cooling channel is achieved, as shown in FIG8 .
  • FIG16 is a top view of the water cooling plate in the controller assembly of FIG10 .
  • the high-voltage capacitor 425 is installed beside the IGBT 423.
  • a capacitor mounting position 4125 is provided on the substrate 4121.
  • the capacitor mounting position 4125 may be a boss protruding from the surface of the substrate 4121, or a sink matching the high-voltage capacitor 425.
  • the capacitor mounting position 4125 is a sink.
  • a heat conductive member such as a heat conductive pad or a heat conductive adhesive, is provided in the capacitor mounting position 4125. The heat conductive member can quickly transfer the heat of the high-voltage capacitor 425 to the water cooling plate 412.
  • the housing 410 further includes a lower housing 413 for sealing the inner cavity of the cover 4122, the lower housing 413 is provided with a second through hole 4131 through which the three-phase input copper bar of the power supply machine passes, and a sealing ring 419 is provided between the lower housing 413 and the cover 4122 of the water-cooled plate 412, and then fixedly connected by bolts.
  • a positioning structure is provided on the lower housing 413 and/or the water-cooled plate 412, and the positioning structure can be a positioning pin or a pin hole, and a matching pin hole or positioning pin is provided in the installation area of the controller assembly 400, so as to realize the installation and positioning of the controller assembly 400.
  • a positioning pin 4132 is provided on the bottom surface of the lower housing 413, and the positioning pin 4132 is detachably connected or integrally formed with the lower housing 413.
  • An inlet pipe 417 and an outlet pipe 418 are installed at the end of the base plate 4121, which are connected to the cooling groove 4123. Since the hybrid electric drive system 1000 is connected to the engine by transmission, and the engine has an independent cooling system, the inlet pipe 417 and the outlet pipe 418 can be connected to the cooling system of the engine. In some embodiments, the inlet pipe 417 and the outlet pipe 418 are connected to the pipeline of the cooling system of the engine, and the cooling water circulation power is provided by the water pump of the cooling system of the engine, and the cooling water is cooled by the low-temperature radiator installed in the front engine compartment.
  • the control board 421 is connected to the top plate 4111 of the housing 410, specifically, the control board 421 is mounted on the upper housing 411, the inner surface of the upper housing 411 is provided with a plurality of columns with threaded holes, the control board 421 is mounted on the columns by screws, and the control board 421 is electrically connected to the driving board 422 via the connecting cable 428.
  • the control assembly 420 further includes a current sensor 426, which is electrically connected to the control board 421 and is disposed in the inner cavity of the housing 4122.
  • both the upper housing 411 and the water-cooling plate 412 are provided with an operation window 414, wherein the operation window 414 of the upper housing 411 is used for plugging and connecting the connection cable 428, and the operation window 414 of the water-cooling plate 412 is used for electrically connecting the three-phase output copper bus 424 with the three-phase input copper bus of the motor.
  • a cover plate 416 is provided on the operation window 414, and the cover plate 416 can be a metal cover plate 416 or a plastic cover plate 416, and the connection method of the cover plate 416 and the upper housing 411/water-cooling plate 412 can be a detachable method such as a screw connection, a threaded connection, or a snap connection.
  • a waterproof breathable valve 415 is installed in at least one operation window 414.
  • the waterproof breathable valve 415 can prevent water from entering the control chamber 401 and the inner cavity of the cover 4122, but the air flow can smoothly pass through the waterproof breathable valve 415 to adapt to the pressure change in the control chamber 401.
  • a cover plate 416 can also be installed on each operation window 414, and a waterproof breathable valve 415 can be installed on other parts of the upper shell 411 or the water-cooling plate 412, as shown in FIG. 9.
  • the number of drive boards 422, IGBTs 423 and three-phase output copper bars 424 is the same as the number of motors.
  • the control board 421 is an integrated PCB board, and the control chips of each motor are installed on the control board 421.
  • the control board 421 also needs to be cooled.
  • the cooling can be achieved by setting a cooling fan on the chip of the control board 421.
  • the specific structure can refer to the heat dissipation structure of the CPU of a desktop computer host.
  • the control board 421 is cooled by setting a heat dissipation structure on the top plate 4111 of the housing 410 (i.e., the upper plate of the upper housing 411).
  • FIG11 is a schematic diagram of the structure of the upper housing in the controller assembly of FIG5 .
  • the top plate 4111 is provided with a heat dissipation structure 4112, and the heat dissipation structure 4112 is opposite to the position of the chip of the control board 421.
  • the heat dissipation structure 4112 may adopt structures such as heat dissipation fins and heat dissipation needles, which are not limited by the present disclosure.
  • the outer surface of the top plate 4111 is provided with a groove, and a plurality of needle rod structures are spaced apart in the groove to form the heat dissipation structure 4112. If the upper housing 411 is a casting, the needle rod structure can be integrally cast.
  • a thermal pad (not shown in the figure) is provided in the shell 410, and the two sides of the thermal pad are respectively in contact with the chip and the heat dissipation structure 4112.
  • the thermal pad can be a thermal conductive adhesive coating or a gasket with good thermal conductivity. By setting the thermal pad, the chip is in full contact with the heat dissipation structure 4112.
  • the top plate 4111 of the housing 410 i.e., the upper plate of the upper shell 411
  • the receiving portion 4113 is protruded from the upper surface of the top plate 4111.
  • the size of the accommodating portion 4113 can be larger than the size of the capacitor or be compatible with the shape of the capacitor. At least one of the length and width of the accommodating portion 4113 matches the size of the capacitor to play a certain limiting role, so that the inner surface of the accommodating portion 4113 can directly constitute a limiting structure to prevent the capacitor from failing due to vibration.
  • the inner cavity of the accommodating portion 4113 is provided with a thermally conductive curing glue that wraps the capacitor, so that the capacitor is in full contact with the inner surface of the accommodating portion 4113, meeting the heat dissipation requirements of the capacitor, and the thermally conductive curing glue wrapping the capacitor can further stabilize the capacitor, ensuring that the capacitor is stably electrically connected to the control board 421.
  • the top plate 4111 is also provided with a low-voltage connector 427 electrically connected to the control board 421.
  • the low-voltage connector 427 is used to plug in a low-voltage wiring harness plug to meet the communication requirements between the controller assembly 400 and the vehicle ECU.
  • FIG12 is a top view of the upper housing of the controller assembly of FIG7 ; as shown in FIG12 , a through hole 4114 is provided on the top plate 4111 , and the low-voltage connector 427 is installed in the through hole 4114 and also protrudes out On the upper surface of the top plate 4111, the low-voltage connector 427 and the receiving portion 4113 are arranged side by side, and the height space generated by each other is utilized, so that the height of the structure protruding from the outer surface of the controller assembly 400 is not increased as a whole, and the normal use and installation of other structural parts are not affected.
  • the low-voltage connector 427, the receiving portion 4113 and the high-voltage adapter box 430 are arranged in sequence along the flow direction of the fluid in the cooling groove 4123, so as to make full use of the space on the upper surface of the top plate 4111.
  • the controller assembly 400 may also include a high-voltage adapter box 430, which can realize the electrical connection between the high-voltage DC power supply and the high-voltage equipment (high-voltage capacitor 425, DCDC, air-conditioning compressor, etc.), and realize the electrical conduction between the power connector 433 and the high-voltage connector 434 through the high-voltage connection component 432 inside the high-voltage adapter box 430.
  • the corresponding number of high-voltage connectors 434 can be set according to the number of high-voltage equipment in the vehicle, so that the high-voltage adapter box 430 acts as a multi-pass electrical connector.
  • FIG17 is a top view of the structure of the high-voltage transfer box in the controller assembly of FIG5 after the top cover of the box body is removed.
  • the high-voltage transfer box 430 may include a box body 431, and an electrically connected high-voltage connection assembly 432, a power connector 433, and at least one high-voltage connector 434.
  • the box body 431 is connected to the housing 410, and the box body 431 is provided with a high-voltage cavity 402 for accommodating the high-voltage connection assembly 432.
  • the box body 431 is provided with at least one assembly port 4313 for installing the power connector 433 and/or at least one high-voltage connector 434.
  • the high-voltage connector 434 is installed in the assembly port 4313, and the power connector 433 is installed on the housing 410 or the box body 431.
  • the high-voltage connector 434 is used to connect the connector of the high-voltage equipment in the vehicle, such as DCDC (voltage converter), air conditioning compressor, PDU (high-voltage distribution box), PTC (car heater), high-voltage cable, etc.
  • the number of high-voltage connectors 434 depends on actual needs.
  • the power connector 433 is used to connect the high-voltage DC power plug to obtain electrical energy from the power supply (power battery, fuel cell, etc.).
  • the positive and negative copper bars of the high-voltage DC power plug extend into the high-voltage cavity 402, and the body of the high-voltage DC power plug is fixed to the shell 410 or the box body 431 by screws to prevent the high-voltage DC power plug from loosening.
  • the high-voltage capacitor 425 draws electricity from the high-voltage DC power plug. Since the high-voltage capacitor 425 is installed in the control cavity 401, the control cavity 401 and the high-voltage cavity 402 should be set to be interconnected so that the copper bar of the high-voltage capacitor 425 extends into the high-voltage cavity 402 and is electrically connected to the high-voltage connector 434.
  • FIG13 is a cross-sectional view of the upper housing in the controller assembly of FIG8 taken along the section line B-B in FIG12.
  • the box body 431 of the high-voltage transfer box 430 is a bottomless structure, including a top cover 4312 and a box wall 4311, and the box wall 4311 is integrally formed with the upper housing 411, or fixedly connected and sealed by welding, bonding, etc.
  • the box wall 4311 is integrally formed with the upper housing 411, and the assembly port 4313 is provided on the box wall 4311.
  • the portion of the upper housing 411 located in the area surrounded by the box wall 4311 is provided with a third through hole 4115, and the third through hole 4115 connects the high-voltage chamber 402 with the control chamber 401, so that the copper busbar of the high-voltage capacitor 425 can be extended into the high-voltage chamber 402.
  • the installation position of the high-voltage capacitor 425 is lower than that of the high-voltage adapter box 430, in order to facilitate the connection of the copper busbar of the high-voltage capacitor 425, the installation port 4116 for installing the power connector 433 is set on the upper shell 411, and the overall height is lower than that of the assembly port 4313, as shown in Figure 11.
  • FIG15 is a front view of the water cooling plate in the controller assembly of FIG10.
  • two assembly ports 4313 are provided on the box wall 4311, and the number of corresponding high-voltage connectors 434 is two, namely, a first high-voltage connector 4341 for electrically connecting to the air-conditioning compressor and a second high-voltage connector 4342 for electrically connecting to the DCDC, as shown in FIG15.
  • the two assembly ports 4313 and the installation port 4116 are located on different sides to avoid mutual interference between the first high-voltage connector 4341, the second high-voltage connector 4342 and the power connector 433.
  • the axes of the first high-voltage connector 4341 and the power connector 433 are along the width direction and the length direction of the vehicle body respectively, and the axis of the second high-voltage connector 4342 is set at an angle relative to the length direction and the width direction of the vehicle body, that is, relative to the length direction and the width direction of the vehicle body, the high-voltage connector of the air-conditioning compressor connected to the second high-voltage connector 4342 is tilted to avoid interference with structural equipment such as the intake manifold of the engine compartment.
  • Fig. 18 is a schematic diagram of the internal structure of the high-voltage transfer box in the controller assembly of Fig. 13.
  • each high-voltage connector 434 is connected in parallel with the power connector 433.
  • the high-voltage connection assembly 432 includes a positive copper busbar 4321, a negative copper busbar 4322 and a plurality of connecting harnesses 4323; the positive copper busbar 4321 and the negative copper busbar 4322 are both electrically connected to the power connector 433 and the copper busbar of the high-voltage capacitor 425, that is, the positive copper busbar 4321 and the negative copper busbar 4322 serve as the positive access port and the negative access port of the high-voltage connection assembly 432, respectively, and are electrically connected to the positive and negative poles of the power connector 433, and the copper busbar of the high-voltage capacitor 425 is also electrically connected to the positive and negative poles of the power connector 433.
  • the positive copper busbar 4321/negative copper busbar 4322, the copper busbar of the high-voltage capacitor 425, and the positive/negative copper busbar 4322 of the power connector 433 are electrically conductive through a high-voltage bolt.
  • the first high-voltage connector 4341 and the second high-voltage connector 4342 are connected in parallel between the positive copper bar 4321 and the negative copper bar 4322 through a plurality of connecting harnesses 4323 .
  • the connecting harnesses 4323 can be copper bars or wires.
  • control component 420 also includes a fuse 435, which is electrically connected to the high-voltage connection component 432.
  • the fuse 435 can be specifically arranged on the connection branch of the first high-voltage connector 4341 or the second high-voltage connector 4342, and the present disclosure does not limit it.
  • the high-voltage transfer box 430 also includes a mounting base 436 disposed in the box body 431, and the mounting base 436 is fixedly connected to the box wall 4311 or the upper shell 411, and the positive copper busbar 4321, the negative copper busbar 4322 and the fuse 435 are all installed on the mounting base 436.
  • the connecting harness 4323 specifically adopts a wire, and the wire has a certain flexibility to facilitate the connection between the copper busbar and the connector.
  • the mounting base 436 has a sinking area 4361, and the sinking area 4361 is opposite to the position of the third through hole 4115, and the electrical connection between the positive copper bar 4321, the negative copper bar 4322, the power connector 433 and the copper bar of the high-voltage capacitor 425 is located in the sinking area 4361, so that the copper bar of the power connector 433 and/or the high-voltage capacitor 425 can be a straight copper bar, which can be directly purchased and does not need to be designed separately.
  • the positive copper bar 4321 and the negative copper bar 4322 are correspondingly designed as a bent structure, which is bent downward from the upper surface of the mounting base 436 and extends to the sinking area 4361.
  • FIG14 is a schematic diagram of the structure of the water-cooling plate in the controller assembly of FIG5. As shown in FIG14, a baffle 4362 is provided on the side wall of the sinking area 4361 to completely block the gap or reduce the gap to a level that the bolt cannot pass through, thereby avoiding the risk of the bolt accidentally falling.
  • FIG20 is a schematic diagram of the structure of a hybrid transmission mechanism assembly in the hybrid electric drive system of FIG1.
  • the transmission mechanism assembly includes an engine input shaft assembly 610, a differential shaft assembly 640 and at least one intermediate shaft assembly connected in a transmission manner, and the power of the transmission mechanism assembly is output to the wheels by the differential shaft assembly 640.
  • the height of the outer circumference of the differential shaft assembly 640 is the lowest, so the differential shaft assembly 640 can directly contact the lubricating oil in the oil storage chamber, so that the differential shaft assembly 640 stirs the oil when rotating, forming splash lubrication for the gears of the transmission mechanism assembly.
  • the housing assembly 300 does not have a separate oil pan, and the bottom space of the shaft gear chamber 302 is increased as an oil storage chamber, and the differential shaft assembly is at least partially located in the oil storage chamber to stir the oil and form oil splash in the shaft gear chamber 302.
  • the lubrication power device 340 can also be arranged in the oil storage cavity and directly immersed in the oil. In order to ensure the cleanliness of the oil, the lubrication power device 340 is connected and installed with a filter.
  • the engine input shaft assembly 610 is simultaneously transmission-connected with the engine and one of the motors.
  • the shaft of the engine input shaft assembly 610 is provided with a through first hollow cavity 111
  • the rotor of the motor connected to the engine input shaft assembly 610 is provided with a through second hollow cavity 622
  • the end cover 330 is provided with an oil inlet channel 303.
  • the first hollow cavity 111, the second hollow cavity 622 and the oil inlet channel 303 are sequentially connected, so that the lubricating oil flowing into the oil inlet channel 303 flows into the engine input shaft assembly 610 through the rotor of the motor to lubricate the various bearings in the engine input shaft assembly 610.
  • the hybrid transmission mechanism assembly 600 is a dual-motor hybrid transmission mechanism.
  • the hybrid transmission mechanism assembly 600 includes a transmission-connected engine input shaft assembly 610, a generator 620, an ICE intermediate shaft assembly 630, a differential shaft assembly 640, an EV intermediate shaft assembly 650, a drive motor input shaft assembly 660, and a drive motor 670.
  • the engine input shaft assembly 610 is transmission-connected to the engine, and the engine input shaft assembly 610 is provided with a planetary gear 100, an actuator, and a gear gear, so that gear shifting can be achieved. That is, the hybrid transmission mechanism assembly 600 of this embodiment can achieve hybrid power input of the engine + motor, as well as multi-gearing of the hybrid engine.
  • FIG. 21 is a schematic diagram of the structure of the hybrid transmission mechanism assembly of FIG. 20 at a first viewing angle
  • FIG. 22 is a schematic diagram of the structure of the hybrid transmission mechanism assembly of FIG. 20 at a second viewing angle.
  • the engine input shaft assembly 610 is coaxially arranged with the generator 620, that is, the rotor 621 of the generator 620 is directly connected to the input shaft (sun gear shaft 110, planetary carrier 120 or inner gear ring shaft 200) of the engine input shaft assembly 610 by transmission, for example, by key connection, gear connection, etc.
  • the drive motor input shaft assembly 660 is coaxially arranged with the drive motor 670, that is, the rotor 671 of the drive motor 670 is directly connected to the input shaft 661 of the drive motor input shaft assembly 660 by transmission, for example, by key connection, gear connection, etc., and a transmission gear 662 is integrally formed on the input shaft 661 of the drive motor input shaft assembly 660.
  • the generator 620 and the drive motor 670 are located on the same side.
  • FIG. 21 and FIG. 22 show the structure of the hybrid transmission mechanism assembly 600 when the generator 620 and the drive motor 670 are located on the left side of the engine input shaft assembly 610.
  • the motor assembly generator 620 and the drive motor 670
  • the shaft gear assembly engine input shaft assembly 610, ICE intermediate shaft assembly 630, differential shaft assembly 640, EV intermediate shaft assembly 650, drive motor input shaft assembly 660
  • the motor is usually cooled by oil injection, and the working voltage of the motor is relatively high
  • the bearings of the shaft gear assembly are usually actively lubricated
  • the voltage of the electronic components such as the shift motor and the sensor is relatively low.
  • the scheme of arranging the motor coaxially with the input shaft can reduce the one-way size of the hybrid transmission mechanism assembly 600.
  • the axis center position of the drive motor 670 is the highest, the overall height of the ICE intermediate shaft assembly 630 and the differential shaft assembly 640 is the lowest, the installation height of the engine input shaft assembly 610 is located between the drive motor 670 and the differential shaft assembly 640, and the projection of the engine input shaft assembly 610 on the vertical plane overlaps with the projection of the drive motor 670 and the differential shaft assembly 640 on the vertical plane. Therefore, the axis center of the engine input shaft assembly 610, the axis center of the drive motor 670 and the axis center of the differential shaft assembly 640 are distributed in a triangular shape, as shown in FIG20.
  • the triangular distribution structure can not only reduce the one-way size of the hybrid transmission mechanism assembly 600, but also has a stable structure.
  • the triangular distribution can provide installation space for the ICE intermediate shaft assembly 630 and the EV intermediate shaft assembly 650, and can further reduce the size of the hybrid transmission mechanism assembly 600 on a plane perpendicular to the axis of the engine input shaft.
  • the axis of the EV intermediate shaft assembly 650 is located in a triangular area surrounded by the axis of the engine input shaft assembly 610, the drive motor 670, and the differential shaft assembly 640.
  • the axis of the ICE intermediate shaft assembly 630 is located below the axis line connecting the engine input shaft assembly 610 and the differential shaft assembly 640, and the axis of the ICE intermediate shaft assembly 630 is at the lowest height.
  • FIG23 is a cross-sectional view of the engine input shaft assembly in the hybrid transmission mechanism assembly of FIG20.
  • the engine input shaft assembly 610 is used to connect the engine, and the gear change of the engine is also realized through the engine input shaft assembly 610.
  • the engine input shaft assembly 610 includes a planetary gear 100, at least one actuator, at least one support bearing, at least one gear gear and an inner ring shaft 200; the inner ring shaft 200 is sleeved outside the planetary gear 100, and the inner ring shaft 200 is transmission-connected with the inner ring 150 of the planetary gear 100, acting as a part of the planetary gear 100; at least one actuator, at least one support bearing, and at least one gear gear are all arranged on the inner ring shaft 200.
  • the transmission function of the planetary gear 100, the installation of the actuator, the installation of the gear gear and the necessary axial limiting function can be integrated at the same time, thereby greatly improving the integration of the hybrid transmission mechanism assembly 600, reducing the functional volume of the hybrid transmission mechanism assembly 600 in the axial direction, and making it have more flexible layout and mounting performance.
  • the shift mechanism acts on the actuator, and the actuator changes the torque transmission path so that gears of different diameters participate in the power transmission, thereby realizing the gear change.
  • the torque of the engine input shaft assembly 610 is transmitted to the EV intermediate shaft assembly 650 and the ICE intermediate shaft assembly 630 by the gear gear.
  • the EV intermediate shaft assembly 650 includes an EV intermediate shaft 651 and a first EV intermediate gear 652 and a second EV intermediate gear 653 mounted on the EV intermediate shaft 651.
  • the diameter of the first EV intermediate gear 652 is larger than that of the second EV intermediate gear 653.
  • the second EV intermediate gear 653 can be integrally formed with the EV intermediate shaft 651, and the first EV intermediate gear 652 is mounted on the EV intermediate shaft 651, and the two are connected by a key.
  • the EV intermediate shaft assembly 650 is transmission-connected to the engine input shaft assembly 610 and the drive motor input shaft assembly 660 through the first EV intermediate gear 652.
  • the first EV intermediate gear 652 is meshed with the first gear gear 50 and the transmission gear 662 of the drive motor input shaft assembly 660.
  • the EV intermediate shaft assembly 650 is transmission-connected to the differential shaft assembly 640 through the second EV intermediate gear 653.
  • the ICE intermediate shaft assembly 630 includes an ICE intermediate shaft 631 and a first ICE intermediate gear 632 and a second ICE intermediate gear 633 mounted on the ICE intermediate shaft 631.
  • the diameter of the first ICE intermediate gear 632 is larger than that of the second ICE intermediate gear 633. Since the second ICE intermediate gear 633 is smaller, the second ICE intermediate gear 633 and the ICE intermediate shaft 631 can be integrally formed, and the first ICE intermediate gear 632 is sleeved on the ICE intermediate shaft 631, and the two are connected by a key.
  • the ICE intermediate shaft assembly 630 is transmission-connected to the engine input shaft assembly 610 through the first ICE intermediate gear 632, specifically, the first ICE intermediate gear 632 is meshed with the second gear 60; the ICE intermediate shaft assembly 630 is transmission-connected to the differential shaft assembly 640 through the second ICE intermediate gear 633.
  • the engine input shaft assembly 610 is the most important shaft-tooth assembly in the hybrid transmission mechanism assembly 600, which realizes the functions of engine power input, energy recovery, and gear shifting.
  • the inner ring gear shaft 200 in the engine input shaft assembly 610 serves as a supporting skeleton to realize the installation and fixation of the planetary gear 100, at least one actuator, at least one support bearing, and at least one gear gear.
  • the engine input shaft assembly 610 is provided with only one planetary gear 100, as shown in FIG. 23, and the planetary gear 100 includes a sun gear shaft 110, a planet carrier 120, a sun gear 130, a planetary gear 140, and an inner ring gear 150.
  • the sun gear 130 is mounted on the sun gear shaft 110, or is integrally formed with the sun gear shaft 110.
  • the planetary gear 140 is mounted on the planetary gear shaft 123 of the planet carrier 120 through a planetary gear bearing 171, and the sun gear 130, the planetary gear 140, and the inner ring gear 150 are sequentially arranged from the inside to the outside and meshed in sequence, and the inner ring gear 150 is transmission-connected with the inner ring gear shaft 200.
  • the sun gear shaft 110 or the planetary carrier shaft 121 of the planetary gear row 100 is connected to the engine to realize the engine power input.
  • the sun gear shaft 110 or the planetary carrier shaft 121 of the planetary gear row 100 is connected to the generator 620 to realize the motor power input.
  • the inner ring shaft 200 is sleeved on the planetary carrier shaft 121 or the sun gear shaft 110 of the planetary gear row 100 for engine power input.
  • the planetary gear row 100 uses the sun gear shaft 110 for engine input, the inner ring shaft 200 and the planetary carrier shaft 121 are used as outputs, and the inner ring shaft 200 is correspondingly sleeved on the planetary carrier shaft 121, and the inner ring shaft 200 or the planetary carrier shaft 121 is provided with a connection structure for transmission connection with the generator 620.
  • the planetary gear row 100 uses the planetary carrier shaft 121 as input, the inner ring gear shaft 200 and the sun gear shaft 110 are used as outputs, and the inner ring gear shaft 200 is correspondingly sleeved on the sun gear shaft 110, and the sun gear shaft 110 or the inner ring gear shaft 200 is provided with a connection structure for transmission connection with the generator 620.
  • the planetary gear row 100 uses the planetary carrier shaft 121 to input engine power, and the inner ring gear shaft 200 and the sun gear shaft 110 output engine power.
  • the inner ring gear shaft 200 is sleeved on the sun gear shaft 110.
  • the inner gear ring shaft 200 includes a sleeve portion 210 and a cover portion 220.
  • the sleeve portion 210 is a sleeve structure that can be mounted on a shaft, such as the sun gear shaft 110 or the planetary carrier shaft 121 of the planetary gear 100.
  • the sleeve portion 210 has a relatively long axial dimension, and a plurality of first mounting positions 230 for mounting the actuator 40, or a plurality of assembly positions 240 for mounting the support bearing, or a plurality of second mounting positions 250 for mounting the gear position can be arranged axially thereon.
  • the cover portion 220 is in transmission connection with the inner gear ring 150 of the planetary gear 100, and participates in the operation of the planetary gear 100 as a part of the planetary gear 100. Both the inner hole profile and the outer profile of the cover portion 220 can be used as the assembly position 240 for mounting the support bearing or the second mounting position 250 for mounting the gear. Therefore, by setting the inner ring gear shaft 200, the transmission function of the planetary gear 100, the installation of the actuator 40, the installation of the gear gear and the necessary axial limiting function can be integrated at the same time, thereby greatly improving the integration of the engine input shaft assembly 610, reducing the functional volume of the engine input shaft assembly 610, and making the electric drive system equipped with the engine input shaft assembly 610 have more flexible layout and mounting performance.
  • the cover portion 220 of the inner gear ring shaft 200 and the inner gear ring 150 of the planetary gear row 100 can be specifically connected by integral molding, welding or keying.
  • the inner gear ring shaft 200, the planetary carrier shaft 121, and the sun gear shaft 110 need to rotate during operation, and there is a speed difference under certain working conditions, so it is necessary to install a bearing between the inner gear ring shaft 200 and the sun gear shaft 110 or the planetary carrier shaft 121, and the inner ring of the bearing is sleeved on the sun gear shaft 110 or the planetary carrier shaft 121, and the inner gear ring shaft 200 is sleeved on the outer ring of the bearing.
  • the inner gear ring shaft 200 is sleeved on the sun gear shaft 110 through two needle bearings 177b, as shown in Figure 23.
  • the inner gear ring shaft 200 may be an integral structure, that is, the sleeve portion 210 and the cover portion 220 are integrally formed by casting or machining.
  • the inner gear ring shaft 200 may also be a split structure, and the sleeve portion 210 and the cover portion 220 may be fixedly connected by welding, bonding, screwing, etc.
  • the inner gear ring shaft 200 is an integral structure formed by casting, and then the inner and outer surfaces are machined, and the material may be a metal material such as stainless steel and cast aluminum.
  • the cover portion 220 of the inner gear ring shaft 200 is covered on the main part of the planetary gear 100, and the sun gear 130, the planetary gear 140, and the inner gear ring 150 of the planetary gear 100 are all located in the inner hole of the cover portion 220.
  • the cover portion 220 includes a gear sleeve portion 221 and a baffle portion 222, and the inner ring of the baffle portion 222 is connected to the shaft sleeve portion 210, and the outer ring is connected to the gear sleeve portion 221.
  • the structure of the gear sleeve portion 221 is similar to that of the shaft sleeve portion 210, and both are shaft sleeve structures.
  • the gear sleeve portion 221 is transmission-connected to the inner gear ring 150 of the planetary gear 100.
  • the baffle portion 222 can be an annular flat plate, an annular spherical shell, or a three-dimensional structure composed of multiple connecting rods. The specific structural form of the baffle portion 222 is not limited in this disclosure.
  • the shaft sleeve portion 210, the baffle portion 222, and the gear sleeve portion 221 can be an integrated structure, or fixedly connected by welding, bonding, screwing, etc.
  • the gear sleeve portion 221 and the inner gear ring 150 may be an integral structure or key-connected to achieve power transmission, so that the entire inner gear ring shaft 200 can rotate together with the inner gear ring 150 of the planetary gear set 100 .
  • the gear sleeve 221 is connected to the inner gear ring 150 via a spline, and the inner profile of the gear sleeve 221 is configured
  • the inner spline 223, the inner profile of the inner gear ring 150 is a tooth meshing with the planetary gear 140, and the outer profile is an outer spline.
  • the inner gear ring 150 is axially inserted into the inner spline 223.
  • One side of the inner gear ring 150 is axially limited by the inner end face 262 of the baffle portion 222.
  • a retaining spring groove 261 is provided on the inner spline 223 of the gear sleeve portion 221.
  • the retaining spring 70 can axially limit the other side of the inner gear ring 150. This ensures that the gear sleeve portion 221 and the inner gear ring 150 will not move relative to each other in the axial direction.
  • the retaining spring 70 is a detachable structure and will not affect the installation and removal of the inner gear ring 150.
  • the multiple component installation positions on the inner ring gear shaft 200 mainly include a first installation position 230 for installing the actuator 40, an assembly position 240 for setting the support bearing, and a second installation position 250 for setting the gear.
  • the actuator 40 can be a synchronizer or a clutch, and the actuator 40 can be loosely mounted on the inner ring gear shaft 200, or fixedly connected or transmission connected to the inner ring gear shaft 200.
  • the support bearing is used to install the inner ring gear shaft 200 on the housing assembly 300.
  • the gear can be a gear gear or a transmission gear that only plays a transmission role.
  • the gear can be loosely mounted on the inner ring gear shaft 200, or fixedly connected or transmission connected to the inner ring gear shaft 200.
  • other component installation positions can be set on the inner ring gear shaft 200 according to specific circumstances, such as a component installation position for installing an oil retaining member, a component installation position for setting a sensor, etc.
  • the first installation position 230 is only arranged on the sleeve portion 210, mainly because the action of the actuator 40 requires a certain axial space, and the axial dimension of the sleeve portion 210 is larger than that of the cover portion 220, which can meet the axial space required for the action of the actuator 40; on the other hand, the sleeve portion 210 is sleeved on the sun gear shaft 110 or the planetary carrier shaft 121 of the planetary gear row 100, and the cover portion 220 is sleeved on the sun gear 130, the planetary gear 140, and the inner ring gear 150 of the planetary gear row 100.
  • the radial dimension of the sleeve portion 210 is smaller than that of the cover portion 220, which is convenient for arranging the actuator 40.
  • the function of the actuator 40 is to change the transmission ratio of the planetary gear row 100, such as engaging the inner gear ring 150 of the planetary gear row 100 with the sun gear shaft 110 for joint rotation, engaging the inner gear ring 150 with the planet carrier for joint rotation, engaging the planet carrier with the sun gear shaft 110 for joint rotation, locking the inner gear ring 150, locking the sun gear 130, locking the planet gear 140, etc.
  • the first mounting position 230 is a key connection structure, so that the actuator 40 is transmission-connected with the inner gear ring shaft 200.
  • the actuator 40 can change the movement of the inner gear ring 150, such as engaging the inner gear ring 150 with the sun gear shaft 110 or the planet carrier, or locking the inner gear ring 150.
  • the inner gear ring shaft 200 is provided with a plurality of limiting structures 260 for axial limiting, and the limiting structures 260 may be limiting bosses, limiting steps or grooves for installing retaining springs 70. If the limiting structure 260 is used to limit the bearing axially, a limiting boss, limiting step or structural end face limiting is usually selected; if the limiting structure 260 is used to limit the gear axially, and the gear is connected to the inner gear ring shaft 200 by transmission, such as a spline connection, then retaining springs 70 are usually selected for axial limiting.
  • the outer surface of the sleeve part 210 is designed as a stepped shaft, specifically, from the far planetary gear end to the near planetary gear end, the outer diameter of the sleeve part 210 increases, and each structural part is mounted on the sleeve part 210 one by one.
  • the stepped shaft itself can form a number of limiting steps for axial positioning.
  • the stepped shaft is also provided with a number of convex edges 263 for axially limiting the shaft sleeve 80, bearings, etc.
  • a limiting structure 260 for axially limiting the actuator 40 is provided on the first installation position 230 to prevent axial relative rotation between the actuator 40 and the inner gear ring shaft 200.
  • the actuator 40 and the inner gear ring shaft 200 are splined, that is, the key connection structure of the first installation position 230 adopts an external spline, and the inner ring of the gear hub 41 and/or the combined tooth 42 of the actuator 40 is provided with an internal spline.
  • the actuator 40 and the inner gear ring shaft 200 are limited by a retaining spring 70, and the corresponding limiting structure 260 is a retaining spring groove 261 provided on the external spline.
  • the retaining spring 70 is stuck in the retaining spring groove 261 after the gear hub 41 and/or the combined tooth 42 of the actuator 40 are installed in place.
  • first support bearing 175 and the second support bearing 176 two support bearings are provided, namely, the first support bearing 175 and the second support bearing 176.
  • the first support bearing 175 and the second support bearing 176 can adopt ball bearings, needle bearings, thrust bearings, etc., and the present embodiment adopts ball bearings.
  • the number of assembly positions 240 is correspondingly two, and both the gear sleeve portion 221 and the shaft sleeve portion 210 are provided with assembly positions 240. As shown in FIG.
  • the first support bearing 175 and the second support bearing 176 are respectively installed on the shaft sleeve portion 210 and the cover portion 220, the first support bearing 175 is arranged in the inner hole of the cover portion 220, and the second support bearing 176 is arranged between the first actuator S1 and the second actuator S2 through the shaft sleeve 80. Since the first support bearing 175 and the second support bearing 176 mainly play the role of supporting the inner gear ring shaft 200, they can both adopt ball bearings.
  • the first support bearing 175 is axially limited by the end surface 262 of the first mounting position 230, that is, the hole shoulder 264 formed by the first mounting position 230 and the supporting position of the cover part 220; the second support bearing 176 is axially limited by the boss provided on the sleeve 80.
  • the inner ring of the first support bearing 175 and the outer ring of the second support bearing 176 are respectively interference fit with the bearing mounting holes of the housing assembly 300.
  • the support bearing and the gear work in the form of rotation, and do not need to move axially, so they can be set on the cover part 220 and/or the sleeve part 210 according to actual needs.
  • the first support bearing 175 is installed on the assembly position 240 of the gear sleeve part 221, and the second support bearing 176 is installed on the assembly position 240 of the sleeve part 210.
  • FIG25 is a schematic structural diagram of the inner gear ring shaft in the engine input shaft assembly of FIG23;
  • FIG26 is a cross-sectional view of the inner gear ring shaft of FIG25.
  • the assembly position 240 of the cover part 220 is the inner hole wall 241 of the gear sleeve part 221
  • the assembly position 240 of the shaft sleeve part 210 is the bare rod section
  • the first support bearing 175 is interference fit with the inner hole wall 241
  • the second support bearing 176 is interference fit with the bare rod section.
  • a limiting structure 260 for axially limiting the first support bearing 175 is provided between the assembly position 240 of the gear sleeve part 221 and the installation position of the inner gear ring 150, and the limiting structure 260 at this place can adopt end face limiting (such as shaft shoulder limiting, boss limiting) or retaining spring limiting.
  • end face limiting such as shaft shoulder limiting, boss limiting
  • retaining spring limiting As shown in FIG. 7 , in some embodiments, a hole shoulder 264 is formed between the inner hole wall 241 of the gear sleeve portion 221 and the inner spline 223 , and the first support bearing 175 installed on the inner hole wall 241 is axially limited by the hole shoulder 264 .
  • a sleeve 80 is provided on the assembly position 240 of the sleeve portion 210, which can compensate for the diameter difference between the second support bearing 176 and the polished rod section on the one hand, and can be used for axial positioning of surrounding structural members on the other hand.
  • the sleeve 80 is press-fitted with the corresponding polished rod section by interference fit, and the second support bearing 176 is installed on the sleeve 80 by interference fit.
  • the surrounding structural members also play an axial positioning role for the sleeve 80. role.
  • the engine input shaft assembly 610 is configured to meet the engine fourth gear, specifically, the engine fourth gear is achieved through two actuators 40 and two gear gears, the two actuators 40 and the two gear gears are respectively recorded as: the first actuator S1, the second actuator S2, the first gear gear 50 and the second gear gear 60.
  • the first actuator S1 and the second actuator S2 are both synchronizers, the first gear gear 50 is a large gear ring, and the engine third gear and the engine fourth gear are achieved; the second gear gear 60 is a small gear ring, and the engine first gear and the engine second gear are achieved.
  • the inner gear ring shaft 200 is provided with two first mounting positions 230, two assembly positions 240, and two second mounting positions 250.
  • the two first mounting positions 230 are distributed at both ends of the sleeve portion 210. It should be noted that the first mounting position 230 can be used to install all components of the actuator 40, or only part of the components of the actuator 40, such as only installing the gear hub 41 of the synchronizer or the single-sided coupling gear 42.
  • the two assembly positions 240 and the two second mounting positions 250 are respectively provided on the sleeve portion 210 and the cover portion 220, as shown in FIG. 25.
  • the first actuator S1 and the second actuator S2 are distributed at both ends of the sleeve portion 210.
  • the first actuator S1 and the second actuator S2 can use synchronizers (single or double) or clutches as needed.
  • the first actuator S1/the second actuator S2 can be set to selectively connect the sun gear shaft 110 and the inner gear ring shaft 200, selectively connect the planet carrier shaft 121 and the inner gear ring shaft 200, selectively connect the inner gear ring shaft 200 and the first gear 50, or selectively connect the inner gear ring shaft 200 and the second gear 60 according to actual needs.
  • the first actuator S1 adopts a synchronizer, having a gear hub 41 and combining teeth 42 on both sides.
  • the gear hub 41 of the first actuator S1 is transmission-connected to the first mounting position 230; the combining teeth 42 on one side of the first actuator S1 are fixedly connected to the first gear gear 50; the combining teeth 42 on the other side of the first actuator S1 are fixedly connected to the second gear gear 60.
  • the first actuator S1 is used to optionally connect the inner ring shaft 200 to the first gear gear 50 or the second gear gear 60.
  • the second actuator S2 also uses a synchronizer, having a gear hub 41 and coupling teeth 42 on both sides.
  • the gear hub 41 of the second actuator S2 is transmission-connected to the sun gear shaft 110 of the planetary gear row 100, the coupling teeth 42 on one side of the second actuator S2 are transmission-connected to the shaft sleeve 210, and the coupling teeth 42 on the other side of the second actuator S2 are fixedly connected to the housing assembly 300.
  • the second actuator S2 is used to connect the sun gear shaft 110 to the inner gear ring shaft 200 or the housing assembly 300 to achieve different speed ratio outputs of the planetary gear row 100.
  • a thrust bearing is provided between the gear hub 41 of the second actuator S2 and the housing assembly 300, and the thrust bearing is sleeved on the sun gear shaft 110.
  • the first gear gear 50 and the second gear gear 60 are respectively installed at two second installation positions 250. Since the first gear gear 50 and the second gear gear 60 are both loosely sleeved on the inner gear ring shaft 200, the inner holes of the first gear gear 50 and the second gear gear 60 are both installed with bearings, such as ball bearings, as shown in FIG23. In other embodiments, if the gears are in transmission connection with the inner gear ring shaft 200, no bearings are required.
  • the gear sleeve portion 221 and the shaft sleeve portion 210 are both provided with second installation positions 250, that is, the first gear gear 50 is loosely sleeved on the gear sleeve portion 221 through a bearing, and the second gear gear 60 is loosely sleeved on the shaft sleeve portion 210 through a bearing.
  • the first gear 50 and the second gear 60 are both gear rings.
  • the first gear 50 is sleeved on the cover portion 220 through a needle bearing 177a
  • the second gear 60 is sleeved on the shaft sleeve portion 210 through a needle bearing 177c and is located between the first actuator S1 and the second support bearing 176.
  • Both the first gear 50 and the second gear 60 can rotate freely relative to the inner gear ring shaft 200.
  • the first gear 50 is a large gear ring, and the inner diameter of the first gear 50 is larger than that of the second gear 60.
  • the first gear gear 50 must not only meet the diameter requirement of being able to be sleeved on the cover part 220, but also meet the connection with the first actuator S1 installed on the sleeve part 210. Therefore, the first gear gear 50 is specifically configured to include a ring gear part 51 and a connecting part 52.
  • the ring gear part 51 is similar in structure to the sleeve part 221 of the inner gear ring shaft 200, both of which are sleeve structures.
  • the connecting part 52 is similar in structure to the baffle part 222 of the inner gear ring shaft 200, both of which are annular plate structures.
  • the ring gear part 51 and the connecting part 52 can be an integrally formed structure, or connected and fixed by welding or threaded fasteners.
  • the ring gear part 51 is sleeved on the cover part 220 through a needle bearing 177a, and the bearing is axially limited by a convex edge 263 provided on the outer surface of the cover part 220.
  • the connecting part 52 is fixedly connected to the coupling tooth 42 on one side of the first actuator S1.
  • the connecting part 52 and the coupling tooth 42 of the first actuator S1 can be integrally formed, welded, or transmission-connected.
  • the second gear 60 is fixedly connected to the coupling tooth 42 on the other side of the first actuator S1 , and the second gear 60 and the coupling tooth 42 of the first actuator S1 can be integrally formed, welded, or transmission-connected.
  • the second gear 60 is axially limited by the sleeve 80 of the second support bearing 176 .
  • a thrust bearing 178 is provided between the connecting portion 52 and the cover portion 220, specifically, a thrust bearing 178 is provided between the connecting portion 52 and the baffle portion 222. That is, the first gear position gear 50 is sleeved on the inner gear ring shaft 200 through the needle bearing 177a and the thrust bearing 178, and is axially limited by the thrust bearing 178 and the end face 262 outside the baffle portion 222.
  • the cover portion 220 of the inner gear ring shaft 200 is provided with an oil guide hole 270 that penetrates the wall thickness, so that the lubricating oil splashed in the planetary gear 100 can enter the gap between the first gear position gear 50 and the cover portion 220 through the oil guide hole 270 on the cover portion 220, and lubricate the needle bearing 177a and the thrust bearing 178 therein.
  • the hybrid electric drive system 1000 further includes a shift mechanism assembly 500, and the shift mechanism assembly 500 and the hybrid transmission mechanism assembly 600 are both installed in the housing assembly 300.
  • FIG. 27 is a schematic diagram of the structure of the shift mechanism assembly in the hybrid electric drive system of FIG. 1.
  • the shift mechanism assembly 500 includes a shift motor 510, a shift reduction mechanism 520, a shift hub 530 and a shift fork 540.
  • the shift motor 510, the shift reduction mechanism 520 and the shift hub 530 are sequentially connected in transmission, and one end of the shift fork 540 is slidably matched with the shift hub 530, and the other end acts on the actuator.
  • the shift reduction mechanism 520500 can adopt a planetary reduction mechanism or other reduction mechanism, and the specific structure is not limited in this disclosure.
  • Other structures of the shift mechanism assembly 500 that are not described in detail can refer to the relevant disclosures of the prior art, such as the Chinese invention application "A dual-clutch automatic transmission shift actuator" with publication number CN108131447A.
  • the left housing 320 is provided with an intermediate plate 321, and the intermediate plate 321 is a cover body, which is fixedly connected to the left housing 320 by threaded fasteners or welding.
  • the intermediate plate 321 is installed with a ball bearing 179 for supporting the rotor 621 of the generator 620.
  • FIG29 is a structural schematic diagram of the intermediate plate of the hybrid electric drive system of FIG1.
  • the coupling teeth 42 of the second actuator S2 are fixedly connected to the intermediate plate 321, and specifically, the coupling teeth 42 of the second actuator S2 can be directly processed on the intermediate plate 321.
  • the coupling teeth 42 of the second actuator S2 can also be welded or press-fitted on the intermediate plate 321.
  • the middle plate 321 is provided with a bearing hole 3211 for setting a bearing and an escape area 3212 for avoiding the shift fork 540 of the shift mechanism assembly 500.
  • the middle plate 321 can be provided with a bearing and a certain installation space can be formed between the middle plate 321 and the left housing 320.
  • the shift fork 540 installation position can be set between the middle plate 321 and the left housing 320, and the shift fork 540 can be installed in the shift fork 540 installation position through the escape area 3212 on the middle plate 321, making the installation of the shift fork 540 more convenient.
  • the middle plate 321 is provided with a bearing hole 3211 for setting the bearing of the rotor of the generator 620, increasing the number of bearing installation holes of the left housing 320 as a whole.
  • the rotor 621 of the generator 620 is supported on the middle plate 321 and the end cover 330 via two bearings, and the planet carrier shaft 121 of the planetary gear 100 is supported on the right housing 310 via the first planet carrier bearing 172 and the second planet carrier bearing 173 .
  • the sleeve portion 210 is provided with at least one oil guide hole 270 penetrating the sleeve wall of the sleeve portion 210.
  • the oil guide holes 270 are usually arranged in a plurality along the circumferential direction.
  • the plurality of oil guide holes 270 located in the same cross section are grouped together.
  • the sleeve portion 210 may be provided with a plurality of groups of oil guide holes 270 along its axial direction.
  • the outer surface of the sleeve portion 210 is provided with an oil guide groove 280 connected to the oil guide hole 270.
  • the oil guide groove 280 is connected to a group of oil guide holes 270.
  • the specific number of the oil guide grooves 280 is determined according to actual needs.
  • the oil guide groove 280 is an inwardly concave groove. By providing the oil guide groove 280, the lubricating oil flowing out of the oil guide hole 270 can be evenly distributed along the circumferential direction.
  • the oil guide groove 280 is a groove, the groove can also be used as a tool-retracting groove when machining the outer surface of the inner gear ring shaft 200.
  • the cover portion 220 may also be provided with an oil guide hole 270, which may be selectively provided on the gear sleeve portion 221 and/or the baffle portion 222 to facilitate the lubricating oil to enter and exit the inner hole of the cover portion 220.
  • the baffle portion 222 may be provided with a plurality of oil guide holes 270, which are arranged to be inclined outwardly along the splashing direction, so that the splashed lubricating oil is thrown out from the oil guide hole 270 when the planetary gear 100 rotates, and lubricating the external structural parts of the inner gear ring shaft 200.
  • the planetary gear 100 is the main component for power distribution.
  • the lubrication of the planetary gear 100 is an important condition for ensuring the normal operation of the engine input shaft assembly 610.
  • the main lubrication requirement of the planetary gear 100 is the planetary gear bearing 171.
  • the number of planetary gear bearings 171 is large and the distribution is wide.
  • the installation position of the planetary gear bearing 171 is located in the area surrounded by the planetary carrier 120 and between the planetary gear 140 and the planetary gear shaft 123, it is blocked by the planetary gear 140 and the planetary carrier 120, and it is difficult for lubricating oil to enter the installation position of the planetary gear bearing 171. Therefore, the planetary gear bearing 171 is prone to ablation, affecting the use of the entire planetary gear 100.
  • FIG24 is a schematic diagram of the structure of the internal lubrication channel of the engine input shaft assembly of FIG23.
  • the planetary gear 100 is provided with a lubrication channel 160
  • the sun gear shaft 110 of the planetary gear 100 is provided with a first hollow cavity 111 that penetrates along the axial direction, and the sun gear shaft 110 can be integrally formed with the sun gear 130 of the planetary gear 100, or key-connected.
  • the sun gear shaft 110 is integrally formed with the sun gear 130.
  • the planet carrier 120 of the planetary gear 100 is provided with an oil collecting cavity 124, and the first hollow cavity 111, the oil collecting cavity 124 and the lubrication channel 160 are connected in sequence, and the outlet of the lubrication channel 160 faces the planetary gear bearing 171 of the planetary gear 100.
  • the sun gear shaft 110 is provided with a plurality of fourth oil guide holes 112 connected to the first hollow cavity 111 , wherein an outlet of one of the fourth oil guide holes 112 faces the bearing between the sun gear shaft 110 and the inner gear ring shaft 200 .
  • the lubrication channel 160 of the planetary carrier 120 may be an oil channel opened in the base material of the planetary carrier 120, or may be an oil channel formed by enclosing external components, as long as the lubricating oil can be delivered to the installation location of the planetary gear bearing 171.
  • the planetary gear bearing 171 is a needle bearing, specifically a full needle bearing or a steel cage needle bearing.
  • the planetary gear bearing 171 adopts a double-row needle bearing with a gasket in the middle. The gasket should form a gap with the planetary gear shaft 123 in the radial direction to ensure that the lubricating oil can enter the needle bearing and lubricate the roller surface of the needle bearing.
  • the planet carrier 120 includes a planet carrier shaft 121, a connecting plate 122, and a plurality of planetary gear shafts 123 connected in sequence, the planetary gear 140 is sleeved on the planetary gear shaft 123, a planetary gear bearing 171 is installed between the planetary gear 140 and the planetary gear shaft 123, and the two sides of the planetary gear 140 are respectively meshed with the gear of the sun gear 130 and the gear of the inner gear ring 150 through gears.
  • the planetary carrier shaft 121 is located at the center of the connecting plate 122, and the planetary gear shafts 123 are evenly distributed along the circumference with the planetary carrier shaft 121 as the center.
  • the planetary carrier shaft 121 and the connecting plate 122 can be detachably connected by threaded fasteners, snap-fit structures, etc., or fixed by welding, or the planetary carrier shaft 121 and the connecting plate 122 are an integrated structure. In some embodiments, the planetary carrier shaft 121 is pressed onto the connecting plate 122 by interference fit.
  • the connecting plate 122 and the planetary gear shaft 123 can also be detachably connected by threaded fasteners, snap-fit structures, etc., or welded and fixed, or the connecting plate 122 and the planetary gear shaft 123 are an integrated structure, which is not limited in the present disclosure.
  • the overall external shape and profile of the planetary carrier 120 are also not limited in the present disclosure, for example, the planetary carrier 120 can adopt a cage structure.
  • the planet carrier shaft 121 is provided with a connected oil collecting chamber 124 and a first oil guide hole 125.
  • the oil collecting chamber 124 is located at the center of the planet carrier shaft 121, preferably coaxial with the planet carrier shaft 121.
  • the planetary wheel shaft 123 is provided with a second oil guide hole 126, and the outlet of the second oil guide hole 126 faces the planetary wheel bearing 171 of the planetary gear 100.
  • An oil guide member 20 is provided on the outer side of the connecting plate 122.
  • the first oil guide hole 125, the gap between the oil guide member 20 and the connecting plate 122, and the second oil guide hole 126 are connected in sequence to form a lubrication channel 160.
  • the oil guide member 20 is riveted to the planet carrier 120.
  • the oil guide member 20 The lubricating oil in the oil collecting chamber 124 that is thrown out from the first oil guide hole 125 under the action of centrifugation is guided to the second oil guide hole 126 .
  • an intermediate bearing 174 is provided between the planet carrier shaft 121 and the sun gear shaft 110.
  • the intermediate bearing 174 is a thrust bearing and can withstand a large axial force.
  • One end of the sun gear shaft 110 is against the planet carrier shaft 121 through the thrust bearing.
  • the thrust bearing can meet the working requirement of the planetary gear 100 that there is a speed difference between the planet carrier 120 and the sun gear shaft 110 under certain working conditions.
  • the intermediate bearing 174 is specifically located at the end of the sun gear shaft 110.
  • a concave bearing mounting groove 113 can be provided at the end of the sun gear shaft 110.
  • the bearing mounting groove 113 is connected to the first hollow cavity 111, so that the internal gap of the intermediate bearing 174 is connected to the first hollow cavity 111, and the lubricating oil in the first hollow cavity 111 can enter the intermediate bearing 174.
  • the second oil guide hole 126 may be a channel extending radially and/or axially along the planetary gear shaft 123, or may be a channel extending circumferentially along the planetary gear shaft 123, that is, the second oil guide hole 126 may be an axial straight channel, a radial straight channel, an oblique straight channel, a curved channel, etc., which is not limited in the present disclosure. As shown in FIG.
  • the second oil guide hole 126 includes an axial oil guide hole 1261 extending axially along the planetary gear shaft 123 and at least one radial oil guide hole 1262 extending radially along the planetary gear shaft 123, and the outlet of the radial oil guide hole 1262 constitutes the outlet of the lubrication channel 160.
  • the number of radial oil guide holes 1262 is determined according to the size of the planetary gear bearing 171, and is usually set to more than two. The outlets of the more than two radial oil guide holes 1262 are spaced and evenly distributed along the circumferential surface of the planetary gear shaft 123.
  • the second oil guide hole 126 includes an axial oil guide hole 1261 extending axially along the planetary gear shaft 123 and four radial oil guide holes 1262 extending radially along the planetary gear shaft 123.
  • the four radial oil guide holes 1262 are distributed at 90 degrees to each other to ensure that the oil reaches the planetary gear bearing 171 and avoid sintering of the entire planetary gear row 100 due to insufficient lubrication of the planetary gear bearing 171.
  • the inlet of the axial oil guide hole 1261 is set to be a flared port, and the flared port is preferably a circular flared port to reduce flow resistance.
  • the aperture of the flared port gradually increases from the middle to the end, so as to facilitate the entry of lubricating oil into the axial oil guide hole 1261.
  • a first planetary carrier bearing 172 is mounted on the planetary carrier 120, and the first planetary carrier bearing 172 is arranged in the lubrication channel 160, and the internal gap of the first planetary carrier bearing 172 is connected to the lubrication channel 160 for the circulation of lubricating oil. As shown in FIG. 24 , the first planetary carrier bearing 172 is mounted on the planetary carrier shaft 121 and is close to the connecting plate 122 of the planetary carrier 120.
  • the first planetary carrier bearing 172 is a thrust bearing, and the loose ring of the thrust bearing is in contact with the connecting plate 122, and the tight ring of the thrust bearing is connected and/or in contact with an external fixed member (for example, a housing assembly 300 for mounting the planetary gear 100), so that the planetary gear 100 is axially stable.
  • a channel for the circulation of lubricating oil can be formed between the loose ring and the tight ring, and the roller of the thrust bearing can also be lubricated when the lubricating oil circulates between the loose ring and the tight ring.
  • the first planetary carrier bearing 172 can also be arranged at other positions of the planetary carrier 120, and completely separated from the lubrication channel 160, so as to avoid the internal structure of the first planetary carrier bearing 172 from generating flow resistance.
  • a second planet carrier bearing 173 is further installed on the planet carrier shaft 121.
  • the second planet carrier bearing 173 adopts a needle bearing.
  • the planet carrier 120 is installed in the housing through the second planet carrier bearing 173.
  • the second planet carrier bearing 173 also needs lubrication during operation.
  • the planet carrier shaft 121 is provided with a third oil guide hole 127 connected to the oil collecting chamber 124, and the outlet of the third oil guide hole 127 faces the second planet carrier bearing 173.
  • the sun gear shaft 110 is embedded with an oil guide pipe 10, and the oil guide pipe 10 is installed through the sun gear shaft 110 of the planetary gear row 100, specifically, it is installed through the first hollow cavity 111, and the end of the oil guide pipe 10 near the planetary gear row 100 extends into the oil collecting cavity 124 to guide the oil in the sun gear shaft 110 into the oil collecting cavity 124 of the planetary carrier.
  • the oil guide pipe 10 when the axial oil guide channel is relatively long, the oil guide pipe 10 is used to transfer the lubricating oil from the lubricating oil inlet at the end of the far planetary gear 100 to the planetary carrier 120 of the planetary gear 100, so as to avoid the situation that the oil is thrown out and cannot reach the planetary gear 100 due to the centrifugal force formed by the high-speed operation of the sun gear shaft 110, and the near planetary gear end of the oil guide pipe 10 extends into the oil collecting chamber 124, which can reduce the leakage of the lubricating oil at the gap between the sun gear shaft 110 and the planetary carrier 120.
  • the lubricating oil circulates in the lubrication channel 160 and finally flows to the planetary gear bearing 171 to lubricate the bearings of each planetary gear 140, ensure sufficient oil volume of the bearing, and avoid the safety problem of the whole vehicle caused by the ablation of the entire planetary gear 100.
  • the oil collecting chamber 124 is required to be able to accommodate the end of the oil guide tube 10 near the planetary gear row 100, and store a certain amount of oil to be transported to the third oil guide hole 127.
  • the oil collecting chamber 124 is a stepped hole structure, wherein the large hole section 1241 is used to accommodate the end of the oil guide tube 10 near the planetary gear row 100, and the small hole section 1242 is connected to the third oil guide hole 127, as shown in FIG. 24 .
  • the oil guide tube 10 is provided with a plurality of oil outlet holes 11 spaced apart along the axial direction and/or radial direction of the oil guide tube 10.
  • a plurality of oil outlet holes 11 are usually provided along the axial direction of the oil guide tube, and the diameter and hole spacing of each oil outlet hole 11 are the same.
  • a plurality of oil outlet holes 11 located at the same axial position can also be provided, and the plurality of oil outlet holes 11 located at the same axial position are spaced apart along the circumferential direction, so that the oil can flow evenly into the first hollow cavity 111 of the sun gear shaft 110.
  • An additional oil outlet hole 11 can be provided at the axial position of the oil guide tube 10 corresponding to the installation position of the bearing.
  • the distal planetary gear 100 end of the oil guide tube 10 is provided with more than one oil outlet 12. Since the oil outlet 12 is opened on the tube wall of the oil guide tube 10, oil can be discharged radially, reducing resistance and facilitating oil to enter the lubrication channel 160.
  • the oil outlet 12 can be set as a slot with an opening or a complete hole, for example, the oil outlet 12 can be a U-shaped slot or a round hole.
  • the number of oil outlets 12 is not limited in the present disclosure. For example, if the number of oil outlets 12 is set to 3, the shapes of the 3 oil outlets 12 can be the same or different.
  • At least one bushing 30 is sleeved on the oil guiding tube 10, and the bushing 30 fills the gap between the oil guiding tube 10 and the cavity wall of the first hollow cavity 111.
  • the bushing 30 plays a role in supporting the oil guiding tube 10, and the material of the bushing 30 is copper or composite plastic.
  • the sun gear shaft 110 of the engine input shaft assembly 610 is rotatably connected to the rotor 621 of the generator 620.
  • the rotor 621 of the generator 620 is provided with a second hollow cavity 622 that penetrates along the axial direction, and the second hollow cavity 622 is connected to the first hollow cavity 111.
  • the rotor of the motor assembly 400 is coaxially arranged with the planetary gear 100, and the lubricating oil introduced into the oil inlet channel 303 of the housing assembly 300 passes through the second hollow cavity 622.
  • the first hollow cavity 111 of the planetary gear 100 is introduced, and the oil guide pipe 10 of the planetary gear lubrication structure is installed in the second hollow cavity 622 and the first hollow cavity 111.
  • the far planetary gear 100 end of the oil guide pipe 10 is directly connected to the oil inlet channel 303 of the housing assembly 300, and the near planetary gear 100 end of the oil guide pipe 10 is directly connected to the oil collecting cavity 124 of the planetary carrier 120.
  • the rotor of the motor assembly 400 By connecting the rotor of the motor assembly 400 in series with the internal oil circuit of the planetary gear 100, the rotor of the motor acts as a pipeline for lubricating oil, which simplifies the structure of the lubrication system and improves the integration and vehicle carrying performance of the hybrid electric drive system 1000.
  • FIG30 is an installation structure diagram of the cooling spray pipeline in the hybrid electric drive system of FIG1 .
  • the hybrid electric drive system further includes a cooling spray pipeline 325 , and one of the oil inlet channels 303 of the housing assembly 300 is connected to the cooling spray pipeline 325 .
  • two sets of cooling spray pipelines 325 are required, for example, the stators of the generator 620 and the drive motor 670 are cooled by a set of cooling spray pipelines 325 respectively.
  • the cooling spray pipeline 325 is connected to the oil inlet channel 303 connected thereto by a solenoid valve 370, which is electrically connected to the control board 421 to realize the conduction or disconnection of the stator cooling passage.
  • the solenoid valve 370 is closed so that the coolant does not enter the stator cooling passage.
  • an oil baffle plate 3223 is provided on the left housing 320, and the oil baffle plate 3223 and the left housing 320 are enclosed to form an oil guide area 3224.
  • the oil baffle plate 3223 is arranged in the spraying area of the cooling spray pipeline 325, so that at least one oil hole of the cooling spray pipeline 325 is connected to the oil guide area 3224, and the oil sprayed from the oil hole can be directly collected in the oil guide area 3224.
  • the left housing 320 is provided with a drainage hole 3225 that passes through the inner wall of the left housing 320, and the oil guide area 3224 is connected to the shaft gear cavity through the drainage hole 3225, so that part of the oil in the motor cavity 301 can be introduced into the shaft gear cavity 302 through the drainage hole 3225 to lubricate the bearings that are difficult to fully lubricate by conventional splash lubrication and active lubrication.
  • FIG31 is a schematic diagram of the structure of the oil collecting groove on the left housing in the hybrid electric drive system of FIG1.
  • the inner side walls of the right housing 310 and the left housing 320 are provided with bearing mounting holes 305 and oil collecting grooves 304.
  • the shafts of the speed change mechanism assembly are installed in the bearing mounting holes 305 of the right housing 310 and the left housing 320 at opposite positions through bearings.
  • the communication between the oil collecting groove 304 and the bearing mounting hole 305 is achieved through an oil guide channel opened on the right housing 310 and/or the left housing 320.
  • both the right housing 310 and the left housing 320 are provided with oil collecting grooves 304, and the oil collecting grooves 304 on the right housing 310 and the left housing 320 are positioned opposite to each other, the two oppositely positioned oil collecting grooves 304 can be combined into a complete oil chamber, and the various oil chambers are connected in sequence through the notch 3041 on the groove wall of the oil collecting groove 304, and the oil chamber close to the drainage hole 3225 is connected to the drainage hole 3225, and the oil in the drainage hole 3225 enters the oil chamber connected thereto and fills each oil chamber in sequence to lubricate bearings that are not easy to lubricate, such as the bearing of the drive motor input shaft assembly 660 installed on the right housing 310 and the bearing of the EV intermediate shaft installed on the right housing 310.
  • These two bearings are far away from the differential shaft assembly 640, so the splashing oil is difficult to meet the lubrication needs of the two bearings, especially under the right tilt condition, the lubrication risk of the above two
  • the lubricating power device 340 is an electronic oil pump, which includes a pump body and an oil pump motor.
  • the oil pump motor drives the pump body to rotate and pumps the oil into the oil inlet channel 303.
  • the pump body is immersed in the oil, and the oil pump motor is installed on the housing assembly 300 and partially exposed to the outside, which is convenient for wiring the oil pump motor.
  • the housing assembly 300 is installed with a thermostat (covered by the plug cover 350 shown in Figure 1, which is not visible in the figure) and a radiator 380 for dissipating heat from the oil.
  • the radiator 380 is connected in parallel with the thermostat.
  • the thermostat can change the oil circuit connected to the thermostat itself according to the temperature of the oil, so that when the oil temperature is higher than the set threshold of the thermostat, the oil is dissipated through the radiator 380 to achieve a "large cycle". When the oil temperature is below the set threshold of the thermostat, the oil circulates directly without passing through the radiator 380 to achieve a "small cycle”.
  • the housing assembly 300 is provided with a lubrication power interface for installing the lubrication power device 340 and a thermostat interface for installing the thermostat.
  • the housing assembly 300 is provided with a sensor interface for installing a temperature sensor 360, and the temperature sensor 360 is used to detect the oil temperature.
  • the above interfaces are arranged on the side of the housing assembly 300 close to the engine, and the space between the hybrid electric drive system 1000 and the engine is reasonably utilized.
  • a convex rib 323 is provided on the side of the housing assembly 300 close to the engine to prevent collision of electronic components during vehicle travel and improve the reliability of the hybrid electric drive system.
  • the radiator 380 may be an air-cooled radiator 380 or a water-cooled radiator 380.
  • the radiator 380 is an oil-water heat exchanger, which is connected to the cooling channel of the housing 410.
  • the temperature difference between the cooling temperature of the control component 420 (60°C to 65°C) and the oil temperature of the hybrid transmission mechanism assembly 600 (usually higher than 80°C) is used to cool the lubricating oil with cooling water to reduce energy consumption.
  • a vent plug 390 and a baffle 324 are installed on the housing assembly 300.
  • the vent passage of the vent plug 390 is connected to the motor cavity and/or the shaft tooth cavity.
  • the baffle 324 is arranged in the motor cavity and/or the shaft tooth cavity and is close to the entrance of the vent passage. The baffle 324 can prevent splashing oil from entering the vent passage of the vent plug 390, reduce oil loss, and the gas can smoothly enter the external environment through the vent passage of the vent plug 390.
  • FIG. 32 is a schematic diagram of the structure of a hybrid vehicle according to some embodiments of the present disclosure.
  • the hybrid vehicle includes a vehicle body 2000, an engine 3000, and a hybrid electric drive system 1000 according to the first aspect of the present disclosure.
  • a front engine compartment is provided at the front end of the vehicle body 2000, and the engine 3000 and the hybrid electric drive system 1000 are both installed in the front engine compartment.
  • the speed change mechanism assembly is transmission-connected to the engine, specifically, the engine input shaft assembly 610 is transmission-connected to the engine 3000.
  • the engine input shaft assembly 610 and the engine are also provided with a torque limiting shock absorber.
  • the engine 3000 and the hybrid electric drive system 1000 are arranged side by side along the width direction of the hybrid vehicle, that is, the axial direction of the engine input shaft assembly 610 of the hybrid electric drive system 1000 is parallel to the vehicle width direction.
  • the left side of the hybrid electric drive system 1000 is fixed to the left longitudinal beam of the vehicle body 2000
  • the right side of the hybrid electric drive system 1000 is fixedly connected to the left side of the engine 3000
  • the right side of the engine 3000 is fixed to the right longitudinal beam of the vehicle body 2000.
  • the lower part of the hybrid electric drive system 1000 is fixed to the lower bracket of the vehicle body 2000.
  • Other undescribed structures of the hybrid electric drive system 1000 can refer to The relevant disclosure of the prior art will not be described in detail here.
  • the hybrid electric drive system includes a housing assembly, a motor assembly, a speed change mechanism assembly and a controller assembly.
  • a shaft gear cavity, a motor cavity and an oil storage cavity are arranged inside the housing assembly, which are used to install the speed change mechanism assembly, install the motor assembly and store lubricating oil respectively.
  • the controller assembly is also installed on the housing, and the outer shell of the controller assembly is connected to the housing assembly, so that the distance between the controller assembly and the motor can be shortened, so that the length of the three-phase output copper busbar in the control component and the three-phase input copper busbar of the motor is shortened, and the wiring length between the control component and the low-voltage electronic devices (pumps, sensors, etc.) in the hybrid electric drive system is shortened, which is convenient for pipeline layout.
  • Lubricating oil circuits are provided in the housing assembly, the motor assembly and the speed change mechanism assembly.
  • a lubricating power device is installed on the housing assembly.
  • the lubricating power device drives the lubricating oil to flow in the lubricating oil circuit, thereby realizing active lubrication of each bearing in the speed change mechanism assembly. Since the lubricating oil circuits are provided in the housing assembly, the motor assembly and the speed change mechanism assembly, there is no need to separately provide an oil pipe in the inner cavity of the housing assembly, thereby further reducing the volume of the hybrid electric drive system.
  • the hybrid electric drive system has a motor assembly, a transmission mechanism assembly and a controller assembly which are all fixed and installed by a housing assembly, with high integration and small volume.
  • the distance between the controller assembly and the motor assembly and between the controller assembly and the transmission mechanism assembly is shortened, so that the lengths of the high-voltage copper plate, low-voltage wiring harness, fluid pipeline and other structures are shortened, the structure is streamlined and wiring is convenient; the housing assembly, the motor assembly and the transmission mechanism assembly are all integrated with lubricating oil circuits, and the volume of the hybrid electric drive system is further reduced.
  • the vehicle carrying capacity of the hybrid electric drive system is improved.

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Abstract

一种混合动力电驱动系统(1000)以及混合动力车辆,该混合动力电驱动系统(1000)包括:壳体总成(300)、电机总成、变速机构总成和控制器总成(400);壳体总成内部设置轴齿腔(302)、电机腔(301)和储油腔,分别用于安装变速机构总成、安装电机总成和存储润滑油;电机总成,设于电机腔(301),包括一个以上电机;变速机构总成,设于轴齿腔(302),用于与发动机和电机均传动连接,并且输出动力;控制器总成(400)同样安装于壳体上,控制器总成(400)的外壳(410)连接于壳体总成(300)。

Description

一种混合动力电驱动系统以及混合动力车辆
相关申请的交叉引用
本申请要求于2022年10月24日提交的申请号为202211306021.7的中国专利申请的优先权,其全部内容通过引用并入本文。
技术领域
本公开属于混合动力电驱动系统技术领域,具体涉及一种混合动力电驱动系统以及混合动力车辆。
背景技术
随着当今社会人们对节能环保的意识日渐增强,新能源汽车技术开始迅猛发展。混合动力车辆驱动技术是新能源汽车发展过程的核心阶段。提高燃油经济性、降低排放是混合动力技术面临的重要课题。
目前市场上主流混动电驱动产品还是组装式结构,电机、变速箱、电机控制器分开设计,然后进行组装,导致目前混动电驱动产品结构变得庞大,并且管线较多,搭载性差。
发明内容
为解决上述技术问题,本公开提供一种混合动力电驱动系统以及混合动力车辆,集成度高,整体体积小,搭载性好。
依据本公开的第一方面,提供了一种混合动力电驱动系统,包括:壳体总成,设有轴齿腔、电机腔和储油腔,所述储油腔连通于所述轴齿腔和/或所述电机腔;电机总成,设于所述电机腔,包括一个以上电机;变速机构总成,设于所述轴齿腔,用于与发动机和所述电机均传动连接,并且输出动力;控制器总成,包括设有控制腔的外壳和安装于所述控制腔的控制组件,所述外壳连接于所述壳体总成,所述外壳中设有用于冷却所述控制组件的冷却流道,所述控制组件设有与所述电机的三相输入铜排电连接的三相输出铜排;其中;所述壳体总成上安装有润滑动力装置;所述壳体总成、所述电机总成和所述变速机构总成中均设有润滑油路,所述润滑动力装置通过所述润滑油路连通于所述储油腔。
依据本公开的第二方面还提供了一种混合动力车辆,包括:车体,设有前机舱;发动机,安装于所述前机舱中;上述的混合动力电驱动系统,安装于所述前机舱中,所述变速机构总成与所述发动机传动连接。
附图说明
为了更清楚地说明本公开实施方式中的技术方案,下面将对实施方式描述中所需要使用的附图作简单的介绍。显而易见地,下面描述中的附图仅仅是本公开的一些实施方式,对本领域技术人员来说,在不付出创造性劳动的前提下,还可以根据这些附图获得其他的附图。
为了更完整地理解本公开及其有益效果,下面将结合附图来进行说明。其中,在下面的描述中相同的附图标号表示相同部分。
图1为依据本公开一些实施例的混合动力电驱动系统的立体图;
图2为依据本公开一些实施例的混合动力电驱动系统在第一视角下的结构示意图;
图3为图1的混合动力电驱动系统拆除端盖后的结构示意图;
图4为图1的混合动力电驱动系统拆除右壳体后的结构示意图;
图5为图1的混合动力电驱动系统中控制器总成的结构示意图;
图6为图5的控制器总成的爆炸图;
图7为图5的控制器总成的主视图;
图8为图7的控制器总成沿图7中的剖面线A-A截取的剖视图;
图9为图5的控制器总成的后视图;
图10为图5的控制器总成在拆除壳体后的内部结构图;
图11为图5的控制器总成中上壳体的结构示意图;
图12为图7的控制器总成中上壳体的俯视图;
图13为图8的控制器总成中上壳体沿图12中的剖面线B-B截取的剖视图;
图14为图5的控制器总成中水冷板的结构示意图;
图15为图10的控制器总成中水冷板的主视图;
图16为图10的控制器总成中水冷板的俯视图;
图17为图5的控制器总成中高压转接盒在拆除盒体的顶盖后的结构的俯视图;
图18为图13的控制器总成中高压转接盒的内部结构示意图;
图19为图5的控制器总成中高压转接盒的接线电路图;
图20为图1的混合动力电驱动系统中混合动力变速机构总成的结构示意图;
图21为图20的混合动力变速机构总成在第一视角下的结构示意图;
图22为图20的混合动力变速机构总成在第二视角下的结构示意图;
图23为图20的混合动力变速机构总成中发动机输入轴总成的剖视图;
图24为图23的发动机输入轴总成的内部润滑通道的结构示意图;
图25为图23的发动机输入轴总成中内齿圈轴的结构示意图;
图26为图25的内齿圈轴的剖视图;
图27为图1的混合动力电驱动系统中换挡机构总成的结构示意图;
图28为图1的混合动力电驱动系统中左壳体的安装区的结构示意图;
图29为图1的混合动力电驱动系统的中间板的结构示意图;
图30为图1的混合动力电驱动系统中冷却喷淋管路的安装结构图;
图31为图1的混合动力电驱动系统中左壳体上集油槽的结构示意图;以及
图32为依据本公开一些实施例的混合动力车辆的结构示意图。
附图标记说明:
1000-混合动力电驱动系统;2000-车体;3000-发动机。
300-壳体总成;301-电机腔;302-轴齿腔;303-进油通道;304-集油槽;305-轴承安装孔,3041-缺口;310-右壳体;320-左壳体,321-中间板,3211-轴承孔,3212-避让区,322-安装区,3221-排水孔,3222-销孔,3223-挡油板,3224-导油区,3225-引流孔;323-凸筋;324-挡板;325-冷却喷淋管路;330-端盖;340-润滑动力装置;350-用于覆盖节温器的堵盖;360-温度传感器;370-电磁阀;380-散热器;390-通气塞。
400-控制器总成,401-控制腔,402-高压腔。410-外壳;411-上壳体,4111-顶板,4112-散热结构,4113-容纳部,4114-通孔,4115-第三通孔,4116-安装口;412-水冷板,4121-基板,4122-罩壳,4123-冷却槽,4124-第一通孔,4125-电容安装位,4126-密封槽;413-下壳体,4131-第二通孔,4132-定位销;414-操作窗口;415-防水透气阀;416-盖板;417-入口管;418-出口管;419-密封圈。420-控制组件;421-控制板;422-驱动板;423-IGBT;424-三相输出铜排;425-高压电容;426-电流传感器;427-低压接插件,428-连接排线。430-高压转接盒;431-盒体,4311-盒壁,4312-顶盖,4313-装配口;432-高压连接组件,4321-正极铜排,4322-负极铜排,4323-连接线束;433-电源接插件;434-高压接插件,4341-第一高压接插件,4342-第二高压接插件;435-熔断器;436-安装底座,4361-下沉区,4362-挡板。
500-换挡机构总成;510-换挡电机;520-换挡减速机构;530-换挡毂;540-拨叉。
600-混合动力变速机构总成;610-发动机输入轴总成;620-发电机,621-发电机的转子,622-第二中空腔;630-ICE中间轴总成,631-ICE中间轴,632-第一ICE中间齿轮,633-第二ICE中间齿轮;640-差速器轴总成;650-EV中间轴总成,651-EV中间轴,652-第一EV中间齿轮,653-第二EV中间齿轮;660-驱动电机输入轴总成,661-输入轴,662-传动齿轮;670-驱动电机,671-驱动电机的转子。
200-内齿圈轴,201-内孔;210-轴套部;220-罩部,221-齿套部,222-挡板部,223-内花键;230-第一安装位;240-装配位,241-内孔壁;250-第二安装位;260-限位结构,261-卡簧槽,262-端面,263-凸边,264-孔肩;270-导油孔;280-导油槽。
100-行星排;110-太阳轮轴,111-第一中空腔,1111-储油腔,1112-扩孔段,112-第四导油孔,113-轴承安装槽;120-行星架,121-行星架轴,122-连接板,123-行星轮轴,124-集油腔,1241-大孔段,1242-小孔段,125-第一导油孔,126-第二导油孔,1261-轴向导油孔,1262-径向导油孔,127-第三导油孔;130-太阳轮;140-行星轮;150-内齿圈;160-润滑通道;171-行星轮轴承;172-第一行星架轴承;173-第二行星架轴承;174-中间轴承;175-第一支撑轴承;176-第二支撑轴承;177a-用于安装第一挡位齿轮的滚针轴承,177b-用于安装内齿圈轴的滚针轴承,177c-用于安装第二挡位齿轮的滚针轴承;178-推力轴承;179-球轴承。
10-导油管,11-出油孔,12-出油口;20-导油件;30-衬套;40-执行机构,41-齿毂,42-结合齿,S1-第一执行机构,S2-第二执行机构;50-第一挡位齿轮,51-齿圈部,52-连接部;60-第二挡位齿轮;70-卡簧;80-轴套。
具体实施方式
下面将结合本公开实施方式中的附图,对本公开实施方式中的技术方案进行清楚、完整地描述。显然,所描述的实施方式仅仅是本公开一部分实施方式,而不是全部的实施方式。基于本公开中的实施方式,本领域技术人员在没有作出创造性劳动前提下所获得的所有其他实施方式,都属于本公开保护的范围。
图1为依据本公开一些实施例的混合动力电驱动系统的立体图;图2为依据本公开一些实施例的混合动力电驱动系统在第一视角下的结构示意图;图3为图1的混合动力电驱动系统拆除端盖后的结构示意图;图4为图1的混合动力电驱动系统拆除右壳体后的结构示意图。
依据本公开的第一方面提供了一种混合动力电驱动系统1000,如图1至图4所示,该混合动力电驱动系统1000可以包括壳体总成300、混合动力变速机构总成600和控制器总成400,混合动力变速机构总成600安装于壳体总成300的内部,控制器总成400安装于壳体总成300的外部。
在一些实施例中,壳体总成300的内部设有轴齿腔302、电机腔301和储油腔,储油腔用于存储该混合动力电驱动系统1000所需的润滑油,储油腔与轴齿腔302和/或电机腔301连通。混合动力变速机构总成600由电机总成和变速机构总成构成,电机总成可以包括一个以上电机,也即混合动力电驱动系统1000可以 是单电机混合动力电驱动系统或者多电机混合动力电驱动系统。电机总成安装于电机腔301中,变速机构总成安装于轴齿腔302中。变速机构总成与发动机和一个以上电机均传动连接,并且输出动力至车轮。变速机构总成可以采用现有技术公开的任一结构,例如公开号为CN111873780A的中国发明申请“一种单电机单行星排多档混合动力变速箱、系统和车辆”混合动力变速机构,或者公开号为CN111942138A的中国发明申请“混合动力变速系统、使用方法及混合动力汽车”混合动力变速机构,本公开不做限制。
控制器总成400用于控制电机总成,以及混合动力电驱动系统1000的低压电子器件,例如油泵、散热器、温度传感器360等。控制器总成400包括外壳410和控制组件420,外壳410设有控制腔401,控制组件420安装于控制腔401中。外壳410连接于壳体总成300,外壳410中设有用于冷却控制组件420的冷却流道。控制组件中设有三相输出铜排424,与各电机的三相输入铜排电连接。
壳体总成300的外部安装有润滑动力装置340,润滑动力装置340可以是油泵。壳体总成300、电机总成和变速机构总成中均设有润滑油路,润滑油路可以是通过去除壳或者轴的部分材料得到的空间,或者由多个零件合围形成的空间。润滑动力装置340提供润滑油循环的动力,使得润滑油在润滑油路与储油腔之间循环流动。
为方便混合动力变速机构总成600的安装,壳体总成300采用分体式结构,具体划分方式本公开不做限制,例如壳体总成300可以以水平面进行分割,形成上下两个壳体,或者以竖直面进行分割,形成左中右三个壳体。如图8所示,壳体总成300包括依次连接的右壳体310、左壳体320和端盖330,右壳体310与左壳体320合围成轴齿腔302。左壳体320和端盖330合围成电机腔301。
由于左壳体320位于壳体总成300的中部,并且同时用于安装电机总成和变速机构总成,左壳体320的整体体积相较于右壳体310和端盖330最大。图28为图1的混合动力电驱动系统中左壳体的安装区的结构示意图,如图28所示,在一些实施例中,控制器总成400安装在左壳体320上。如图28所示,左壳体320上设有安装区322,控制器总成400安装于安装区322中。安装区322为一体成型于左壳体320上的槽结构,安装区322的侧壁能够一定程度包裹控制器总成400,提高控制器总成400的安装稳定性。在一些实施例中,安装区322的侧壁设有排水孔3221,便于排出安装区322中存蓄的水,提高用电安全。
为保证控制器总成400的三相输出铜排424与各电机的三相输入铜排精准对中,在一些实施例中,安装区322与外壳410之间设有定位结构,定位结构可采用定位销4132与销孔,或者台阶面配合等结构,本公开不做限制。如图28所示,外壳410的底部设置定位销4132,安装区322中设有销孔3222,安装时将定位销4132插在销孔3222,能够确保三相输出铜排424与各电机的三相输入铜排相对,便于安装高压螺栓。
图5为图1的混合动力电驱动系统中控制器总成的结构示意图;图6为图5的控制器总成的爆炸图;图7为图5的控制器总成的主视图;图8为图7的控制器总成沿图7中的剖面线A-A截取的剖视图;图9为图5的控制器总成的后视图。
如图5至图9所示,为了便于控制组件420的安装,外壳410为分体式结构,具体划分方式本公开不做限制,例如外壳410可以以水平面进行分割,形成上下两个壳体,或者以铅垂面进行分割,形成左中右三个壳体。总的来说,区别于现有的电机控制器,本公开的外壳410中未设置与外壳410相对独立的水冷板,而是在外壳410上直接设置冷却槽4123供冷却液流通,也可理解为本公开是将水冷板作为外壳410的一部分。外壳410包括上壳体411和水冷板412,上壳体411和水冷板412合围成控制腔401,上壳体411和水冷板412上均开设螺栓孔,二者经密封圈419密封后通过螺栓连接固定。水冷板412上设有冷却槽4123,冷却槽4123是水冷板412的顶面向下凹陷形成。在一些实施例中,冷却槽4123的数量与电机的数量相同,为方便布置,各个冷却槽4123沿水平方向均布并依次连通。在另一些实施例中,冷却槽4123也可以是一个通长的槽,通过在槽口上焊接或粘接封板,形成与电机的数量相同的开放式的冷却位。
图10为图5的控制器总成在拆除壳体后的内部结构图。如图6和图10所示,控制组件420包括电连接的控制板421、驱动板422、IGBT423、三相输出铜排424和高压电容425,控制板421、驱动板422、IGBT423和三相输出铜排424依次电连接,高压电容425与IGBT423电连接。控制组件420中,驱动板422、IGBT423和高压电容425均安装于水冷板412上,为充分利用安装空间,IGBT423和高压电容425在水平方向并排设置,驱动板422位于IGBT423的上方、通过螺钉固定在水冷板412上,IGBT423覆盖于冷却槽4123的槽口,以与冷却槽4123合围成冷却流道。
图14为图5的控制器总成中水冷板的结构示意图;图15为图10的控制器总成中水冷板的主视图;图16为图10的控制器总成中水冷板的俯视图。
如图14至图16所示,水冷板412可以包括连接的基板4121和罩壳4122,基板4121大致呈板状,基板4121设有冷却槽4123和供三相输出铜排424穿过的第一通孔4124。基板4121的内部设置流道,流道为开放式结构,形成冷却槽4123。罩壳4122整体呈套状,具有内腔,罩壳4122的内腔通过第一通孔4124连通于外壳410的控制腔401,使得三相输出铜排424与位于控制腔401中的IGBT423电连接后,能够通过第一通孔4124伸入罩壳4122的内腔中,以与伸入罩壳4122的内腔中的电机的三相输入铜排电连接。基板4121和罩壳4122可通过注塑、金属铸造一体成型,或者通过焊接、粘接、螺栓连接等方式固定连接,本实施例中,基板4121和罩壳4122均为铝合金材料,直接铸造成型。
由于冷却槽4123具有开放的槽口,为了保证密封性,基板4121在冷却槽4123的槽口外周设置有密封槽4126,密封槽4126中设置密封圈419,IGBT423具有向外水平延伸的安装边,安装边压紧密封圈419, 实现冷却流道的密封,如图8所示。
图16为图10的控制器总成中水冷板的俯视图。高压电容425安装于IGBT423的旁侧,如图16所示,基板4121上设有电容安装位4125,电容安装位4125可以为凸出于基板4121表面的凸台,或者是与高压电容425匹配的沉槽。为了增加高压电容425与基板4121的接触面积,在一些实施例中,电容安装位4125为沉槽。为了进一步提高散热性能,在一些实施例中,电容安装位4125中设有导热件,例如导热垫或者导热胶,导热件能够快速将高压电容425的热量传递至水冷板412。
如图6和图7所示,在一些实施例中,外壳410还包括用于封闭罩壳4122的内腔的下壳体413,下壳体413设有供电机的三相输入铜排穿过的第二通孔4131,下壳体413与水冷板412的罩壳4122之间设有密封圈419,然后通过螺栓固定连接。在一些实施例中,下壳体413和/或水冷板412上设置定位结构,定位结构可以是定位销或者销孔,在该控制器总成400的安装区域设置相匹配的销孔或者定位销,从而能够实现控制器总成400的安装定位。如图6所示,下壳体413的底面设置有定位销4132,定位销4132与下壳体413可拆卸连接或者一体成型。
基板4121的端部安装有入口管417和出口管418,与冷却槽4123连通。由于混合动力电驱动系统1000与发动机传动连接,发动机具有一套独立的冷却系统,因此可将入口管417和出口管418接入发动机的冷却系统中,在一些实施例中,入口管417和出口管418连通于发动机的冷却系统的管道上,通过发动机的冷却系统的水泵提供冷却水循环动力,冷却水由安装于前机舱中的低温散热器进行散热。
如图8所示,控制组件420中,控制板421连接于外壳410的顶板4111,具体是控制板421安装于上壳体411上,上壳体411的内表面设有若干开设有螺纹孔的立柱,控制板421通过螺钉安装于立柱上,控制板421与驱动板422通过连接排线428电连接。在一些实施例中,控制组件420还包括电流传感器426,电流传感器426与控制板421电连接,电流传感器426设于罩壳4122的内腔,。
在一些实施例中,上壳体411和水冷板412上均设有操作窗口414,其中上壳体411的操作窗口414用于进行连接排线428的接插操作,水冷板412的操作窗口414用于进行三相输出铜排424与电机的三相输入铜排的电连接操作。操作窗口414上设置盖板416,盖板416可采用金属盖板416或者塑料盖板416,盖板416与上壳体411/水冷板412的连接方式可以是螺钉连接、螺纹连接或者卡扣连接等可拆卸方式。
由于控制组件420工作时会发热,因此控制腔401内的压力会发生变化,为了降低气压变化的影响,在一些实施例中,至少一个操作窗口414中安装有防水透气阀415,防水透气阀415能够阻挡水进入控制腔401和罩壳4122的内腔,但是气流能够顺利通过防水透气阀415,以适应控制腔401内气压变化。在另一些实施例中,也可在各操作窗口414上均安装盖板416,在上壳体411或水冷板412的其他部位上安装防水透气阀415,如图9所示。
控制组件420中,驱动板422、IGBT423和三相输出铜排424的数量与电机的数量相同,对于双电机电驱动系统,则需要设置两个驱动板422、两个IGBT423和两组三相输出铜排424。控制板421为集成式PCB板,各个电机的控制芯片均安装于控制板421上。当该控制器总成400应用于混合动力电驱动系统时,特别是具有挡位的混合动力电驱动系统时,则混合动力电驱动系统中的各个传感器、换挡机构也与控制板421电连接,由控制板421直接采集传感器信号、发出换挡控制指令。
因此,为了保证控制板421的正常工作,也需要对控制板421进行冷却降温。可采用在控制板421的芯片上设置散热风扇的方式进行降温,具体结构可参考台式电脑主机CPU的散热结构。在一些实施例中,通过在外壳410的顶板4111(即上壳体411的上板)设置散热结构对控制板421进行冷却降温。
图11为图5的控制器总成中上壳体的结构示意图。如图11所示,顶板4111设有散热结构4112,散热结构4112与控制板421的芯片的位置相对。散热结构4112可采用散热翅片、散热针等结构,本公开不做限制。作为一种实施方式,顶板4111的外表面设有凹槽,凹槽内间隔分布有若干针杆结构,形成散热结构4112,若上壳体411为铸造件,则可将针杆结构一体铸造成型。
为了提高散热效果,在一些实施例中,外壳410中设有导热垫(图中未示出),导热垫的两侧面分别与芯片和散热结构4112接触,导热垫可以是导热胶涂层或者导热性能良好的垫片,通过设置导热垫使得芯片与散热结构4112完全接触。
若控制板421上设置有较大容量的电容,也需要考虑电容的散热。如图11所示,在一些实施例中,外壳410的顶板4111(即上壳体411的上板)设置用于容纳控制板421的电容的容纳部4113,容纳部4113均凸出于顶板4111的上表面,通过设置容纳部4113容纳电容,避免将顶板4111整体抬高,从而降低该控制器总成400的体积。
容纳部4113的尺寸可以大于电容的尺寸或者与电容的形状相适配,容纳部4113的长和宽中的至少一个与电容的尺寸相匹配,以起到一定的限位作用,使得容纳部4113的内型面可以直接构成限位结构,避免电容因震动连接失效。容纳部4113的内腔中设有包裹电容的导热固化胶,使得电容与容纳部4113的内表面充分接触,满足电容的散热需求,并且导热固化胶包裹电容能够进一步稳定电容,保证电容与控制板421稳定电连接。
在一些实施例中,顶板4111上还设置有与控制板421电连接的低压接插件427,低压接插件427用于插接低压线束插头,满足控制器总成400与整车ECU的通信需求。图12为图7的控制器总成中上壳体的俯视图;如图12所示,顶板4111上开设有一通孔4114,低压接插件427安装于该通孔4114,并且同样凸出于 顶板4111的上表面,低压接插件427和容纳部4113并排设置,同时利用对方产生的高度空间,在整体上不会增加控制器总成400外表面的结构凸出高度,不会影响其他结构件的正常使用和安装。在一些实施例中,低压接插件427、容纳部4113和高压转接盒430沿冷却槽4123中流体的流通方向依次设置,充分利用顶板4111的上表面的空间。
在一些实施例中,控制器总成400还可以包括高压转接盒430,高压转接盒430能够实现高压直流电源与高压设备(高压电容425、DCDC、空调压缩机等)的电连接,通过高压转接盒430内部的高压连接组件432实现电源接插件433与高压接插件434的电导通,可根据车辆的高压设备的数量设置对应数量的高压接插件434,使得高压转接盒430充当多通电连接器的作用。
图17为图5的控制器总成中高压转接盒在拆除盒体的顶盖后的结构的俯视图。如图6和图17所示,高压转接盒430可以包括盒体431,以及电连接的高压连接组件432、电源接插件433和至少一个高压接插件434。盒体431与外壳410连接,盒体431设有高压腔402,用于容纳高压连接组件432,盒体431上设有用于安装电源接插件433和/或至少一个高压接插件434的至少一个装配口4313。在一些实施例中,高压接插件434安装于装配口4313中,电源接插件433安装于外壳410或盒体431上。
高压接插件434用于对接车辆中高压设备的接插头,例如DCDC(电压转换器)、空调压缩机、PDU(高压配电盒)、PTC(汽车加热器)、高压电缆等,高压接插件434的数量视实际需要而定。电源接插件433用于对接高压直流电源插头,以从电源(动力电池、燃料电池等)中获得电能。使用时,高压直流电源插头(图中未示出)的正负极铜排伸入高压腔402中,高压直流电源插头的本体通过螺钉固定在外壳410或盒体431上,防止高压直流电源插头松脱。高压电容425从高压直流电源插头中取电,由于高压电容425安装在控制腔401中,因此控制腔401与高压腔402应当设置为相互连通,以使高压电容425的铜排伸入于高压腔402、与高压接插件434电连接。
图13为图8的控制器总成中上壳体沿图12中的剖面线B-B截取的剖视图。如图11,图13和图17所示,高压转接盒430的盒体431为无底的结构,包括顶盖4312和盒壁4311,盒壁4311与上壳体411一体成型,或者通过焊接、粘接等方式固定连接并且密封。在一些实施例中,盒壁4311与上壳体411一体成型,装配口4313设置于盒壁4311上,上壳体411位于盒壁4311所围区域中的部分开设有第三通孔4115,第三通孔4115将高压腔402与控制腔401连通,供高压电容425的铜排伸入于高压腔402。考虑到高压电容425的安装位置相对于高压转接盒430较低,为了方便连接高压电容425的铜排,用于安装电源接插件433的安装口4116设置在上壳体411上,整体高度相对于装配口4313较低,如图11所示。
图15为图10的控制器总成中水冷板的主视图。在一些实施例中,盒壁4311上设有两个装配口4313,相应的高压接插件434的数量为两个,分别为用于与空调压缩机电连接的第一高压接插件4341和用于与DCDC电连接的第二高压接插件4342,如图15所示。两个装配口4313与安装口4116位于不同的侧面,避免第一高压接插件4341、第二高压接插件4342和电源接插件433的对接插头相互干扰。
在一些实施例中,第一高压接插件4341和电源接插件433的轴向分别沿车身宽度方向和车身长度方向,第二高压接插件4342的轴向相对于车身长度方向和车身宽度方向均呈角度设置,即相对车身长度方向和宽度方向,与第二高压接插件4342对接的空调压缩机的高压接插头倾斜出线,能够避让发动机舱的进气歧管等结构设备,避免与之干涉。
图18为图13的控制器总成中高压转接盒的内部结构示意图。为了确保各个高压设备相对独立工作,在一些实施例中,各个高压接插件434均与电源接插件433并联。如图17和图18所示,高压连接组件432包括正极铜排4321、负极铜排4322和若干连接线束4323;正极铜排4321和负极铜排4322均电连接于电源接插件433和高压电容425的铜排,也就是说,正极铜排4321和负极铜排4322分别作为高压连接组件432的正极接入端口和负极接入端口、并且与电源接插件433的正负极电连接,高压电容425的铜排也与电源接插件433的正负极电连接,在一些实施例中,正极铜排4321/负极铜排4322、高压电容425的铜排、电源接插件433的正/负极铜排4322通过一个高压螺栓形成电导通。第一高压接插件4341和第二高压接插件4342通过若干连接线束4323并联接入正极铜排4321和负极铜排4322之间,连接线束4323可采用铜排或者导线。
为了提高用电安全,在一些实施例中,如图18和图9所示,控制组件420还包括熔断器435,熔断器435与高压连接组件432电连接,熔断器435具体可设置于第一高压接插件4341或第二高压接插件4342的连接支路上,本公开不做限制。
为了方便高压连接组件432的安装,如图17和图18所示,在一些实施例中,高压转接盒430还包括设于盒体431内的安装底座436,安装底座436与盒壁4311或上壳体411固定连接,正极铜排4321、负极铜排4322和熔断器435均安装于安装底座436上,连接线束4323具体采用导线,导线具有一定的柔性,方便铜排与接插件的连接。
考虑到电源接插件433需要同时与正极铜排4321/负极铜排4322和高压电容425的铜排的电连接,为了降低铜排的长度,如图18所示,安装底座436具有下沉区4361,下沉区4361与第三通孔4115的位置相对,正极铜排4321、负极铜排4322、电源接插件433和高压电容425的铜排的电连接处位于下沉区4361中,使得电源接插件433和/或高压电容425的铜排可采用直铜排,可直接采购得到,不需要单独设计。正极铜排4321和负极铜排4322则相应设计为弯折结构,由安装底座436的上表面向下弯折并延伸至下沉区4361。
由于下沉区4361与第三通孔4115的位置相对,为了避免连接正极铜排4321、负极铜排4322、电源 接插件433和高压电容425的铜排的螺栓在安装时掉落、进入控制腔401。图14为图5的控制器总成中水冷板的结构示意图,如图14所示,下沉区4361的侧壁设有挡板4362,完全封堵缝隙,或者将缝隙缩小至螺栓无法通过,从而避免螺栓意外掉落的风险。
图20为图1的混合动力电驱动系统中混合动力变速机构总成的结构示意图。在一些实施例中,如图20所示,变速机构总成包括传动连接的发动机输入轴总成610、差速器轴总成640和至少一个中间轴总成,变速机构总成的动力由差速器轴总成640输出至车轮。在变速机构总成中,差速器轴总成640的外圆周的高度最低,因此可以由差速器轴总成640直接与储油腔中的润滑油接触,使得差速器轴总成640转动时搅油,形成对变速机构总成的的齿轮的飞溅润滑。为了简化结构,在一些实施例中,壳体总成300中不单独设置油底壳,将轴齿腔302的底部空间增加,作为储油腔,差速器轴总成至少部分位于储油腔中,实现搅油,在轴齿腔302形成油液飞溅。润滑动力装置340同样可以设置于储油腔中,直接浸没于油液中,为了保证油液的清洁度,润滑动力装置340连通安装有过滤器。
在一些实施例中,变速机构总成中,发动机输入轴总成610与发动机和其中一个电机同时传动连接,为了简化润滑结构,在一些实施例中,发动机输入轴总成610的轴设有贯通的第一中空腔111,与发动机输入轴总成610连接的电机的转子中设有贯通的第二中空腔622,端盖330中设有进油通道303,第一中空腔111、第二中空腔622和进油通道303依次连通,使得进油通道303中流入的润滑油通过电机的转子流入发动机输入轴总成610中,以润滑发动机输入轴总成610中的各个轴承。
在一些实施例中,混合动力变速机构总成600为双电机混合动力变速机构。混合动力变速机构总成600包括传动连接的发动机输入轴总成610、发电机620、ICE中间轴总成630、差速器轴总成640、EV中间轴总成650、驱动电机输入轴总成660和驱动电机670。其中发动机输入轴总成610与发动机传动连接,发动机输入轴总成610设有行星排100、执行机构和挡位齿轮,因此能够实现挡位变换。也即本实施例的混合动力变速机构总成600能实现发动机+电机的混合动力输入,以及混动发动机多挡化。
图21为图20的混合动力变速机构总成在第一视角下的结构示意图;图22为图20的混合动力变速机构总成在第二视角下的结构示意图。如图21和图22所示,针对上述各个总成的位置布置;发动机输入轴总成610与发电机620同轴设置,也即发电机620的转子621直接与发动机输入轴总成610的输入轴(太阳轮轴110、行星架120或内齿圈轴200)传动连接,例如采用键连接、齿轮连接等方式。驱动电机输入轴总成660和驱动电机670同轴设置,也即驱动电机670的转子671直接与驱动电机输入轴总成660的输入轴661传动连接,例如采用键连接、齿轮连接等方式,驱动电机输入轴总成660的输入轴661上一体成型有传动齿轮662。发电机620和驱动电机670位于同侧。以发动机输入轴总成610的轴线平行于车辆宽度方向为例,则发动机输入轴总成610靠近驾驶位的一侧为左侧(记为L),发动机输入轴总成610靠近副驾驶位的一侧为右侧(记为R),则发电机620和驱动电机670同位于发动机输入轴总成610的左侧或同位于发动机输入轴总成610的右侧。图21和图22示出了发电机620和驱动电机670同位于发动机输入轴总成610的左侧时的混合动力变速机构总成600的结构图。
通过将发电机620和驱动电机670设置在发动机输入轴总成610的同一侧,在布置时能够将电机总成(发电机620和驱动电机670)和轴齿总成(发动机输入轴总成610、ICE中间轴总成630、差速器轴总成640、EV中间轴总成650、驱动电机输入轴总成660)分开放置,从而便于冷却润滑系统的设计以及高低电压分区:电机通常采用喷油冷却,并且电机的工作电压较大;轴齿总成的轴承通常采用主动润滑,并且其中换挡电机、传感器等电子器件的电压较小。并且电机与输入轴同轴设置的方案,能够缩小混合动力变速机构总成600的单向尺寸。
上述各个总成中,驱动电机670的轴心位置最高,ICE中间轴总成630和差速器轴总成640的整体高度最低,发动机输入轴总成610的安装高度位于驱动电机670与差速器轴总成640之间,并且发动机输入轴总成610在竖直面上的投影与驱动电机670和差速器轴总成640在竖直面上的投影具有重合部分。因此,发动机输入轴总成610的轴心、驱动电机670的轴心与差速器轴总成640的轴心呈三角形分布,如图20所示。三角形分布结构不仅能够缩小混合动力变速机构总成600的单向尺寸,而且结构稳定,此外,三角形分布能够为ICE中间轴总成630和EV中间轴总成650提供安装空间,能够进一步降低该混合动力变速机构总成600在垂直于发动机输入轴轴线的平面上的尺寸。如图20所示,在一些实施例中,EV中间轴总成650的轴心位于发动机输入轴总成610、驱动电机670和差速器轴总成640的轴心所围的三角形区域中。ICE中间轴总成630的轴心位于发动机输入轴总成610和差速器轴总成640的轴心连线的下方,并且ICE中间轴总成630的轴心的高度最低。
图23为图20的混合动力变速机构总成中发动机输入轴总成的剖视图。发动机输入轴总成610用于连接发动机,发动机的挡位变化也是通过发动机输入轴总成610实现。如图23所示,发动机输入轴总成610包括行星排100、至少一个执行机构、至少一个支撑轴承、至少一个挡位齿轮和内齿圈轴200;内齿圈轴200套设于行星排100外,且内齿圈轴200与行星排100的内齿圈150传动连接,充当行星排100的一部分;至少一个执行机构、至少一个支撑轴承、至少一个挡位齿轮均设置于内齿圈轴200上。通过在发动机输入轴总成610设置有内齿圈轴200,可以同时集成行星排100传动功能、执行机构安装、挡位齿轮安装以及必要的轴向限位功能,从而极大的提高混合动力变速机构总成600的集成度,缩减混合动力变速机构总成600在轴线方向上的功能体积,使其具备更灵活的布置和搭载性能。
进行挡位切换时,换挡机构作用于执行机构,执行机构更改扭矩传递路径,使得不同直径齿轮参与到动力传递中,从而实现挡位变换。发动机输入轴总成610的扭矩由挡位齿轮传输至EV中间轴总成650和ICE中间轴总成630。如图21和图22所示,在一些实施例中,EV中间轴总成650包括EV中间轴651和安装于EV中间轴651上的第一EV中间齿轮652和第二EV中间齿轮653。第一EV中间齿轮652的直径大于第二EV中间齿轮653,由于第二EV中间齿轮653较小,可将第二EV中间齿轮653与EV中间轴651一体成型,第一EV中间齿轮652套装于EV中间轴651上,二者通过键连接。EV中间轴总成650通过第一EV中间齿轮652与发动机输入轴总成610和驱动电机输入轴总成660传动连接,具体是第一EV中间齿轮652与第一挡位齿轮50和驱动电机输入轴总成660的传动齿轮662均啮合;EV中间轴总成650通过第二EV中间齿轮653与差速器轴总成640传动连接。
如图2和图3所示,在一些实施例中,ICE中间轴总成630包括ICE中间轴631和安装于ICE中间轴631上的第一ICE中间齿轮632和第二ICE中间齿轮633。第一ICE中间齿轮632的直径大于第二ICE中间齿轮633,由于第二ICE中间齿轮633较小,可将第二ICE中间齿轮633与ICE中间轴631一体成型,第一ICE中间齿轮632套装于ICE中间轴631上,二者通过键连接。ICE中间轴总成630通过第一ICE中间齿轮632与发动机输入轴总成610传动连接,具体是第一ICE中间齿轮632与第二挡位齿轮60啮合;ICE中间轴总成630通过第二ICE中间齿轮633与差速器轴总成640传动连接。
发动机输入轴总成610是混合动力变速机构总成600中最为重要的轴齿总成,实现发动机动力输入、能量回收、挡位变换的功能。发动机输入轴总成610中内齿圈轴200作为支撑骨架,实现行星排100、至少一个执行机构、至少一个支撑轴承和至少一个挡位齿轮的安装固定。在一些实施例中发动机输入轴总成610仅设置一个行星排100,如图23所示,行星排100包括太阳轮轴110、行星架120、太阳轮130、行星轮140和内齿圈150。太阳轮130安装于太阳轮轴110上,或者与太阳轮轴110一体成型。行星轮140通过行星轮轴承171安装于行星架120的行星轮轴123上,太阳轮130、行星轮140和内齿圈150由内至外依次设置并且依次啮合,内齿圈150与内齿圈轴200传动连接。
如图23所示,该发动机输入轴总成610中,行星排100的太阳轮轴110或行星架轴121与发动机连接,实现发动机动力输入。行星排100的太阳轮轴110或行星架轴121与发电机620连接,实现电机动力输入。内齿圈轴200套设于行星排100的用于进行发动机动力输入的行星架轴121或太阳轮轴110上。例如行星排100采用太阳轮轴110用于发动机输入,则内齿圈轴200和行星架轴121作为输出,内齿圈轴200相应套装于行星架轴121上,内齿圈轴200或行星架轴121上设有用于与发电机620传动连接的连接结构。若行星排100采用行星架轴121输入,则内齿圈轴200和太阳轮轴110作为输出,内齿圈轴200相应套装于太阳轮轴110上,则太阳轮轴110或内齿圈轴200上设有用于与发电机620传动连接的连接结构。在一些实施例中,行星排100采用行星架轴121输入发动机动力,内齿圈轴200和太阳轮轴110输出发动机动力的技术方案,内齿圈轴200套设于太阳轮轴110上。
如图23至图26所示,该内齿圈轴200包括轴套部210和罩部220,轴套部210为轴套结构,能套装于轴上,例如行星排100的太阳轮轴110或行星架轴121。轴套部210的轴向尺寸较长,其上可沿轴向设置若干用于安装执行机构40的第一安装位230,或者用于设置支撑轴承的装配位240、用于设置挡位齿轮的第二安装位250。罩部220与行星排100的内齿圈150传动连接,作为行星排100的一部分参与行星排100的运行,罩部220的内孔型面以及外型面均可作为用于设置支撑轴承的装配位240或用于设置齿轮的第二安装位250。由此,通过设置该内齿圈轴200,可以同时集成行星排100传动功能、执行机构40安装、挡位齿轮安装以及必要的轴向限位功能,从而极大的提高发动机输入轴总成610的集成度,缩减发动机输入轴总成610的功能体积,使得配置有该发动机输入轴总成610的电驱动系统具备更灵活的布置和搭载性能。
内齿圈轴200的罩部220与行星排100的内齿圈150具体可采用一体成型、焊接或键连接。内齿圈轴200、行星架轴121、太阳轮轴110在工作时需要转动,并且某些工况下存在转速差,因此需要在内齿圈轴200与太阳轮轴110或行星架轴121之间安装轴承,轴承的内圈套设于太阳轮轴110或行星架轴121上,内齿圈轴200套设于轴承的外圈上。在一些实施例中,内齿圈轴200通过两个滚针轴承177b套装于太阳轮轴110上,如图23所示。
该内齿圈轴200可以是一体式结构,即轴套部210和罩部220通过铸造或机加工等一体成型。该内齿圈轴200也可以是分体式结构,轴套部210和罩部220可以通过焊接、粘接、螺接等方式固定连接。在一些实施例中,该内齿圈轴200为铸造成型的一体式结构,然后通过机加工加工出内外型面,其材质可以是不锈钢、铸铝等金属材料。
内齿圈轴200的罩部220罩设于行星排100的主体部分上,行星排100的太阳轮130、行星轮140、内齿圈150均位于罩部220的内孔中。在一些实施例中,罩部220包括齿套部221和挡板部222,挡板部222的内环连接轴套部210、外环连接于齿套部221。齿套部221的结构与轴套部210类似,均为轴套结构,齿套部221与行星排100的内齿圈150传动连接。挡板部222可以是环形平板、环形球壳或者由多跟连杆构成的立体结构,挡板部222的具体结构形态本公开不做限制。轴套部210、挡板部222、齿套部221可以是一体式结构,或者通过焊接、粘接、螺接等方式固定连接。齿套部221与内齿圈150可以是一体式结构或者键连接,从而实现动力传动,使得整个内齿圈轴200能够跟随行星排100的内齿圈150共同转动。
如图23所示,在一些实施例中,齿套部221与内齿圈150通过花键连接,齿套部221的内型面设置 内花键223,内齿圈150的内型面为与行星轮140啮合的齿、外型面为外花键,内齿圈150沿轴向卡入内花键223中,内齿圈150的一侧通过挡板部222的内部的端面262轴向限位,在齿套部221的内花键223设有卡簧槽261,卡簧槽261中安装卡簧70后,该卡簧70可对内齿圈150的另一侧进行轴向限位。由此确保齿套部221与内齿圈150不会发生轴向相对移动。并且卡簧70为可拆卸结构,不会影响内齿圈150的安装和拆卸。
内齿圈轴200上的多个构件安装位主要包括用于安装执行机构40的第一安装位230、用于设置支撑轴承的装配位240和用于设置齿轮的第二安装位250。其中执行机构40可以是同步器或离合器,执行机构40可以是空套于内齿圈轴200上,或者是与内齿圈轴200固定连接或传动连接。支撑轴承用于将该内齿圈轴200安装于壳体总成300上。齿轮可以是挡位齿轮或者是仅起传动作用的传动齿轮,齿轮可以是空套于内齿圈轴200上,或者是与内齿圈轴200固定连接或传动连接。在其他实施例中,还可视具体情况在内齿圈轴200设置其他构件安装位,例如用于安装挡油件的构件安装位、用于设置传感器的构件安装位等。
上述构件安装位中,第一安装位230仅设于轴套部210上,主要是因为执行机构40动作是需要一定的轴向空间,而轴套部210相比于罩部220的轴向尺寸更大,能够满足执行机构40动作所需要的轴向空间;另一方面,轴套部210套设于行星排100的太阳轮轴110或行星架轴121上,罩部220套设于行星排100的太阳轮130、行星轮140、内齿圈150上,轴套部210相比于罩部220的径向尺寸更小,便于布置执行机构40。
在一些实施例中,执行机构40的作用是改变行星排100的传动比,例如将行星排100的内齿圈150与太阳轮轴110接合共同转动、将内齿圈150与行星架接合共同转动、将行星架与太阳轮轴110接合共同转动、将内齿圈150锁定、将太阳轮130锁定、将行星轮140锁定等。在一些实施例中,第一安装位230为键连接结构,使得执行机构40与内齿圈轴200传动连接,由于内齿圈轴200与行星排100的内齿圈150传动连接,因此执行机构40可以改变内齿圈150的运动情况,例如将内齿圈150与太阳轮轴110或行星架接合,或者将内齿圈150锁定。
该内齿圈轴200上设有若干用于轴向限位的限位结构260,该限位结构260可以为限位凸台、限位台阶或用于安装卡簧70的凹槽。若限位结构260用于对轴承进行轴向限位,则通常选择限位凸台、限位台阶、结构端面限位;若限位结构260用于对齿轮进行轴向限位,齿轮与内齿圈轴200传动连接,例如花键连接,则通常选择卡簧70进行轴向限位。在限位结构260的设计上,为了方便执行机构40、挡位齿轮、轴承等结构件的安装,在一些实施例中,轴套部210的外型面设计为阶梯轴,具体是自远行星排端至近行星排端,轴套部210的外径呈增大趋势,各结构件逐个套装于轴套部210。阶梯轴自身可形成若干用于轴向定位的限位台阶,此外,该阶梯轴的上还设置有若干凸边263,用于对轴套80、轴承等进行轴向限位。
在第一安装位230上设有用于对执行机构40轴向限位的限位结构260,防止执行机构40与内齿圈轴200之间发生轴向相对转动。具体在在一些实施例中,执行机构40与内齿圈轴200采用花键连接,也即第一安装位230的键连接结构采用外花键,执行机构40的齿毂41和/或结合齿42的内圈设置内花键。针对花键连接,执行机构40与内齿圈轴200采用卡簧70限位,对应的限位结构260为设于外花键的卡簧槽261,卡簧70在执行机构40的齿毂41和/或结合齿42安装到位后卡在卡簧槽261中。
为保证内齿圈轴200安装稳定,在一些实施例中,支撑轴承设置两个,分别为第一支撑轴承175和第二支撑轴承176,第一支撑轴承175和第二支撑轴承176可采用滚珠轴承、滚针轴承、推力轴承等,本实施例采用滚珠轴承。装配位240的数量相应为两个,齿套部221和轴套部210均设有装配位240。如图23所示,第一支撑轴承175和第二支撑轴承176分别安装于轴套部210和罩部220上,第一支撑轴承175设于罩部220的内孔中,第二支撑轴承176通过轴套80设于第一执行机构S1和第二执行机构S2之间,第一支撑轴承175和第二支撑轴承176由于主要起到支撑内齿圈轴200的作用,因此可均采用滚珠轴承。第一支撑轴承175通过第一安装位230的端面262,即罩部220的第一安装位230与支撑位所形成的孔肩264轴向限位;第二支撑轴承176通过轴套80上设置的凸台轴向限位。第一支撑轴承175的内环和第二支撑轴承176的外环分别与壳体总成300的轴承安装孔过盈配合。
对于用于设置支撑轴承的装配位240和用于设置齿轮的第二安装位250,支撑轴承和齿轮的工作形式是转动,不需要发生轴向移动,因此可根据实际需要设置在罩部220和/或轴套部210上。第一支撑轴承175安装于齿套部221的装配位240上,第二支撑轴承176安装于轴套部210的装配位240上。
图25为图23的发动机输入轴总成中内齿圈轴的结构示意图;图26为图25的内齿圈轴的剖视图。如图25和图26所示,罩部220的装配位240为齿套部221的内孔壁241,轴套部210的装配位240为光杆段,第一支撑轴承175与内孔壁241过盈配合,第二支撑轴承176与光杆段过盈配合。齿套部221的装配位240与内齿圈150的安装处之间设有用于对第一支撑轴承175轴向限位的限位结构260,该处的限位结构260可采用端面限位(例如轴肩限位、凸台限位)或者卡簧限位。如图7所示,在一些实施例中,齿套部221的内孔壁241与内花键223之间形成孔肩264,通过孔肩264对内孔壁241上安装的第一支撑轴承175进行轴向限位。
在一些实施例中,轴套部210的装配位240上设有轴套80,一方面可以弥补第二支撑轴承176与光杆段的直径差,另一方面可以用于周围结构件的轴向限位,轴套80与对应的光杆段过盈压装,第二支撑轴承176过盈安装于轴套80上。轴套80用于周围结构件的轴向限位时,周围结构件同样对轴套80起到轴向限位 的作用。
在一些实施例中,发动机输入轴总成610设置为满足发动机四挡,具体是通过两个执行机构40和两个挡位齿轮实现发动机四挡,两个执行机构40和两个挡位齿轮分别记为:第一执行机构S1、第二执行机构S2、第一挡位齿轮50和第二挡位齿轮60。第一执行机构S1、第二执行机构S2均为同步器,第一挡位齿轮50为大齿圈,实现发动机三挡和发动机四挡;第二挡位齿轮60为小齿圈,实现发动机一挡和发动机二挡。
为了适配发动机输入轴总成610的挡位设计,内齿圈轴200的第一安装位230、装配位240、第二安装位250均设有两个。为保证两个第一安装位230上安装的两个执行机构40具有足够的轴向拨动空间,两个第一安装位230分布于轴套部210的两端,需要说明的是,第一安装位230可以安装执行机构40的所有构件,也可以仅用于安装执行机构40的部分构件,例如仅安装同步器的齿毂41或者单侧的结合齿42。为了缩小内齿圈轴200的轴向尺寸,提高设置有该内齿圈轴200的混动变速箱的搭载性能,在一些实施例中,两个装配位240和两个第二安装位250均分别设于轴套部210和罩部220上,如图25所示。
在一些实施例中,第一执行机构S1和第二执行机构S2分布于轴套部210的两端。第一执行机构S1和第二执行机构S2可根据需要采用同步器(单边或双边)或离合器。第一执行机构S1/第二执行机构S2可根据实际需要设置为可选择地连接太阳轮轴110与内齿圈轴200、可选择地连接行星架轴121与内齿圈轴200、可选择地连接内齿圈轴200与第一挡位齿轮50或可选择地连接内齿圈轴200与第二挡位齿轮60。
在一些实施例中,第一执行机构S1采用同步器,具有齿毂41和两侧的结合齿42,第一执行机构S1的齿毂41与第一安装位230传动连接;第一执行机构S1的一侧的结合齿42与第一挡位齿轮50固定连接;第一执行机构S1的另一侧的结合齿42与第二挡位齿轮60固定连接,第一执行机构S1用于将内齿圈轴200可选地与第一挡位齿轮50或第二挡位齿轮60连接。第二执行机构S2同样采用同步器,具有齿毂41和两侧的结合齿42,第二执行机构S2的齿毂41与行星排100的太阳轮轴110传动连接,第二执行机构S2的一侧的结合齿42与轴套部210传动连接,第二执行机构S2的另一侧的结合齿42与壳体总成300固定连接,第二执行机构S2用于将太阳轮轴110可选地与内齿圈轴200或壳体总成300连接,实现行星排100不同的速比输出。为了提高该发动机输入轴总成610的轴向承载能力,第二执行机构S2的齿毂41与壳体总成300之间设有推力轴承,该推力轴承套装于太阳轮轴110上。
第一挡位齿轮50和第二挡位齿轮60分别安装于两个第二安装位250,由于第一挡位齿轮50和第二挡位齿轮60均空套于内齿圈轴200上,因此第一挡位齿轮50和第二挡位齿轮60的内孔均安装有轴承,例如滚珠轴承,如图23所示。在其他实施例中,若挡位齿轮与内齿圈轴200传动连接,则不需要设置轴承。为了降低内齿圈轴200的轴向长度,齿套部221和轴套部210均设有第二安装位250,也即第一挡位齿轮50通过轴承空套于齿套部221上,第二挡位齿轮60通过轴承空套于轴套部210上。
在一些实施例中,如图23所示,第一挡位齿轮50和第二挡位齿轮60均为齿圈,第一挡位齿轮50通过滚针轴承177a空套于罩部220上,第二挡位齿轮60通过滚针轴承177c空套于轴套部210上、且位于第一执行机构S1与第二支撑轴承176之间,第一挡位齿轮50和第二挡位齿轮60均可相对于内齿圈轴200自由转动。在一些实施例中,第一挡位齿轮50为大齿圈,第一挡位齿轮50的内孔径大于第二挡位齿轮60。
第一挡位齿轮50既要满足能够套装于罩部220上的直径要求,又要满足与安装于轴套部210上的第一执行机构S1连接,因此,第一挡位齿轮50具体设置为包括齿圈部51和连接部52,齿圈部51与内齿圈轴200的齿套部221结构相似,均为轴套结构,连接部52与内齿圈轴200的挡板部222结构相似均为环形板结构。齿圈部51和连接部52可以是一体成型结构,或者通过焊接、螺纹紧固件连接固定。齿圈部51通过滚针轴承177a空套于罩部220上,该轴承通过罩部220外型面上设置的凸边263轴向限位。连接部52与第一执行机构S1的一侧的结合齿42固定连接,连接部52与第一执行机构S1的该结合齿42可以是一体成型、焊接固定或者传动连接。第二挡位齿轮60与第一执行机构S1的另一侧的结合齿42固定连接,第二挡位齿轮60与第一执行机构S1的该结合齿42可以是一体成型、焊接固定或者传动连接。第二挡位齿轮60通过第二支撑轴承176的轴套80轴向限位。
为了进一步提高该发动机输入轴总成610的轴向承载能力,如图23所示,连接部52与罩部220之间设有推力轴承178,具体是连接部52与挡板部222之间设有推力轴承178。也就是说,第一挡位齿轮50通过滚针轴承177a和推力轴承178套在内齿圈轴200上,通过推力轴承178以及挡板部222外部的端面262轴向限位。内齿圈轴200的罩部220上设置有贯通壁厚的导油孔270,使得行星排100中飞溅的润滑油能够通过罩部220上的导油孔270进入第一挡位齿轮50与罩部220之间的缝隙中,润滑其中的滚针轴承177a和推力轴承178。
在一些实施例中,混合动力电驱动系统1000还包括换挡机构总成500,换挡机构总成500和混合动力变速机构总成600均安装于壳体总成300中。图27为图1的混合动力电驱动系统中换挡机构总成的结构示意图,如图27所示,换挡机构总成500包括换挡电机510、换挡减速机构520、换挡毂530和拨叉540,换挡电机510、换挡减速机构520和换挡毂530依次传动连接,拨叉540的一端与换挡毂530滑动配合、另一端作用于执行机构。换挡减速机构520500可采用行星减速机构或者其他减速机构,具体结构本公开不做限制。换挡机构总成500的其他未详述结构均可参照现有技术的相关公开,例如公开号为CN108131447A的中国发明申请“一种双离合自动变速器换挡执行机构”。
由于发动机输入轴总成610中轴较多,发电机620的转子621、行星排100的太阳轮轴110、内齿圈 轴200均需要设置轴承进行安装支撑。为了增加轴承安装孔,如图23所示,在一些实施例中,左壳体320设有中间板321,中间板321呈罩体,与左壳体320通过螺纹紧固件或焊接固定连接。中间板321安装有用于支撑发电机620的转子621的球轴承179。图29为图1的混合动力电驱动系统的中间板的结构示意图,如图29所示,为了进一步提高集成度,第二执行机构S2的结合齿42与中间板321固定连接,具体可以是在中间板321上直接加工出第二执行机构S2的结合齿42。在一些实施例中,也可将第二执行机构S2的结合齿42焊接或者过盈压装在中间板321上。
如图29所示,中间板321上开设有用于设置轴承的轴承孔3211和用于避让换挡机构总成500的换挡拨叉540的避让区3212,将中间板321设置在左壳体320后,中间板321既能设置轴承,又能在中间板321与左壳体320之间形成一定的安装空间,可在中间板321与左壳体320之间设置换挡拨叉540安装位,而且换挡拨叉540能够通过中间板321上的避让区3212装入换挡拨叉540安装位,使换挡拨叉540的安装更为方便。进一步地,中间板321上开设有轴承孔3211用于设置发电机620转子的轴承,增加左壳体320整体的轴承安装孔的数量。在一些实施例中,发电机620的转子621通过两个轴承支撑在中间板321和端盖330上,行星排100的行星架轴121通过第一行星架轴承172和第二行星架轴承173支撑在右壳体310上。
由于发动机输入轴总成610的内齿圈轴200上需要安装多个轴承、齿轮,需要保证该多个轴承、齿轮的润滑需求,具体可以采用飞溅润滑或主动润滑的方式,由于内齿圈轴200各个轴承、齿轮布置紧凑,相互形成轴向限位的效果,因此仅通过外部飞溅的润滑油恐难以达到预期的润滑效果,因此,本实施例采用主动润滑方案。
在一些实施例中,如图25和图26所示,轴套部210上设有至少一个贯通轴套部210套壁的导油孔270,导油孔270通常沿周向设置多个,位于同一横截面的多个导油孔270为一组,则轴套部210上沿其轴向可以设置多组导油孔270。在一些实施例中,轴套部210的外型面设有连通于导油孔270的导油槽280,导油槽280与一组导油孔270均连通,导油槽280的具体数量根据实际需要而定。导油槽280为内凹的凹槽,通过设置导油槽280可以将导油孔270流出的润滑油沿周向均匀分布,另外,由于导油槽280为凹槽,该凹槽还可作为内齿圈轴200外型面机加工时的退刀槽。
此外,在一些实施例中,罩部220上也可设置导油孔270,导油孔270可选择设置在齿套部221和/或挡板部222上,便于润滑油进出罩部220的内孔。如图2所示,在一些实施例中,挡板部222上可以设置若干导油孔270,该导油孔270设置为沿飞溅方向向外倾斜,便于行星排100转动时飞溅的润滑油从导油孔270中甩出,润滑内齿圈轴200外部的结构件。
发动机输入轴总成610中,行星排100是功率分流的主要零件,行星排100的润滑是保证该发动机输入轴总成610正常运行的重要条件,行星排100的主要润滑需求在于行星轮轴承171,一方面行星轮轴承171数量多,分布广,另一方面,由于行星轮轴承171的安装位置是位于行星架120所围区域中,并且位于行星轮140与行星轮轴123之间,因此受行星轮140、行星架120的阻挡,润滑油难以进入行星轮轴承171安装处,故而行星轮轴承171容易产生烧蚀,影响整个行星排100的使用。
图24为图23的发动机输入轴总成的内部润滑通道的结构示意图。为了改善行星排100内部的润滑情况,如图24所示,在一些实施例中,行星排100设有润滑通道160,行星排100的太阳轮轴110设有沿轴向贯通的第一中空腔111,太阳轮轴110可以是与行星排100的太阳轮130一体成型,或者键连接,在一些实施例中太阳轮轴110与太阳轮130一体成型。行星排100的行星架120设有集油腔124,第一中空腔111、集油腔124和润滑通道160依次连通,并且润滑通道160的出口朝向行星排100的行星轮轴承171。为了方便润滑太阳轮轴110外部的结构,太阳轮轴110上设有若干与第一中空腔111相连通的第四导油孔112,其中一个第四导油孔112的出口朝向太阳轮轴110与内齿圈轴200之间的轴承。
在一些实施例中,行星架120的润滑通道160可以是开设于行星架120基材中的油道,也可以是由外部元件合围形成的油道,满足能够将润滑油送入行星轮轴承171的安装处即可。在一些实施例中,该行星轮轴承171为滚针轴承,具体可以是满滚针轴承或钢保持架滚针轴承。该行星轮轴承171采用双列滚针轴承,中间设置有垫片,垫片在径向上要与行星轮轴123形成间隙,保证润滑油可以进入滚针轴承中,润滑滚针轴承的滚子表面。
如图24所示,在一些实施例中,行星架120包括依次连接的行星架轴121、连接板122和若干行星轮轴123,行星轮140套在行星轮轴123上,行星轮140与行星轮轴123之间安装有行星轮轴承171,行星轮140两侧分别通过齿轮与太阳轮130的齿轮和内齿圈150的齿轮进行啮合。行星架轴121位于连接板122的中心,行星轮轴123以行星架轴121为中心、沿周向均匀分布。行星架轴121与连接板122可以通过螺纹紧固件、卡扣结构等可拆卸连接,或者焊接固定,或者行星架轴121与连接板122为一体式结构,在一些实施例中,行星架轴121通过过盈压装在连接板122上。连接板122和行星轮轴123也可以通过螺纹紧固件、卡扣结构等可拆卸连接,或者焊接固定,或者连接板122和行星轮轴123为一体式结构,本公开不做限制。行星架120的整体外部形状、轮廓本公开同样不做限制,例如行星架120可以采用笼式结构。
在一些实施例中,如图24所示,行星架轴121设有连通的集油腔124和第一导油孔125,集油腔124位于行星架轴121的中心,优选与行星架轴121共轴线。行星轮轴123设有第二导油孔126,第二导油孔126的出口朝向行星排100的行星轮轴承171。连接板122外侧设有导油件20,第一导油孔125、导油件20与连接板122之间空隙、第二导油孔126依次连通,构成润滑通道160。导油件20与行星架120铆接,导油件20 将集油腔124中在离心作用下由第一导油孔125中甩出的润滑油引导至第二导油孔126。
在一些实施例中,行星架轴121与太阳轮轴110之间设有中间轴承174,中间轴承174采用推力轴承,能够承受较大的轴向力,太阳轮轴110的其中一端通过该推力轴承抵在行星架轴121上,推力轴承能够满足行星排100在某些工况下行星架120与太阳轮轴110之间存在转速差的工作需求。该中间轴承174具体位于太阳轮轴110的端部,在一些实施例中,可在太阳轮轴110的端部设置一个内凹的轴承安装槽113,该轴承安装槽113与第一中空腔111连通,由此使得中间轴承174的内部空隙与第一中空腔111连通,第一中空腔111中的润滑油能够进入中间轴承174。
第二导油孔126可以是沿行星轮轴123径向和/或轴向延伸的通道,也可以是沿行星轮轴123周向延伸的通道,也就是说,第二导油孔126可以是轴向直通道、径向直通道、斜向直通道、曲线通道等,本公开不做限制。如图24所示,在一些实施例中,第二导油孔126包括沿行星轮轴123轴向延伸的轴向导油孔1261和至少一个沿行星轮轴123径向延伸的径向导油孔1262,径向导油孔1262的出口构成润滑通道160的出口。径向导油孔1262的数量根据行星轮轴承171的尺寸而定,通常设置为两个以上,两个以上径向导油孔1262的出口沿行星轮轴123的周向表面间隔、均匀分布,例如第二导油孔126包括沿行星轮轴123轴向延伸的轴向导油孔1261和四个沿行星轮轴123径向延伸的径向导油孔1262,四个径向导油孔1262互呈90°分布,保证油品到达行星轮轴承171,避免由于行星轮轴承171润滑不充分导致整个行星排100烧结。在一些实施例中,轴向导油孔1261的入口设置为扩口,扩口优选圆扩口,降低流阻。沿沿行星轮轴123的轴向,该扩口的孔径自中部向端部逐渐增加,便于润滑油进入轴向导油孔1261。
在一些实施例中,行星架120上安装有第一行星架轴承172,第一行星架轴承172设置于润滑通道160中,第一行星架轴承172的内部空隙与润滑通道160连通,供润滑油流通。如图24所示,该第一行星架轴承172安装于行星架轴121上,并且靠近行星架120的连接板122,该第一行星架轴承172为推力轴承,推力轴承的松环与连接板122接触,推力轴承的紧环与外部固定构件(例如用于安装行星排100的壳体总成300)连接和/或接触,使得行星排轴向稳定。在松环与紧环之间则可形成供润滑油流通的通道,润滑油在松环与紧环之间流通时还可对推力轴承的滚子进行润滑。当然,在其他实施例中,还可将第一行星架轴承172设置在行星架120的其他位置,与润滑通道160完全分离,避免第一行星架轴承172的内部结构产生流阻。
在一些实施例中,为了提高行星架120的转动稳定性,行星架轴121上还安装有第二行星架轴承173,第二行星架轴承173采用滚针轴承,例如行星架120通过第二行星架轴承173安装于壳体中。第二行星架轴承173在工作时同样需要润滑,为此,行星架轴121设有与集油腔124连通的第三导油孔127,第三导油孔127的出口朝向第二行星架轴承173。
由于行星排100的行星架120、太阳轮轴110等存在轴向的制造和加工误差,太阳轮轴110与行星架120之间通常会存在一定的间隙,在某些极限的情况流入此部位的润滑油会通过该间隙大量的泄漏出去。如图23和图24所示,为了解决上述问题,在一些实施例中,太阳轮轴110内嵌入导油管10,导油管10贯通安装于行星排100的太阳轮轴110内部,具体是贯通安装于第一中空腔111中,且导油管10的近行星排100端伸入于集油腔124,以将太阳轮轴110内的油导入到行星架的集油腔124中。通过设置导油管10,在轴向导油通道比较长的情况下,采用导油管10将润滑油从远行星排100端的润滑油入口将油品传递到行星排100的行星架120中,可以避免由于太阳轮轴110高速运转所形成的离心力将油甩出无法到达行星排100的情况,并且导油管10的近行星排端伸入于集油腔124中,能够降低太阳轮轴110与行星架120之间间隙处的润滑油的泄漏量。润滑油在润滑通道160中流通,并最终流动至行星轮轴承171处,润滑各个行星轮140的轴承,保证该轴承的充分油量,避免整个行星排100的烧蚀导致的整车安全问题。
在一些实施例中,集油腔124要求能够容纳导油管10的近行星排100端,并且存储一定油液以输送至第三导油孔127。考虑到第二行星架轴承173所需润滑油相较于行星轮轴承171少,为了保证行星轮轴承171供油充足,在一些实施例中,集油腔124呈阶梯孔的结构,其大孔段1241用于容纳导油管10的近行星排100端,小孔段1242与第三导油孔127连通,如图24所示。
导油管10上设有若干沿导油管10轴向和/或径向间隔分布的出油孔11。沿导游管的轴向,出油孔11通常设置有多个,并且各出油孔11的孔径、孔距均相同。位于同一轴向位置的出油孔11也可设置为多个,多个位于同一轴向位置的出油孔11沿周向间隔分布,使得油液能够均匀的流动至太阳轮轴110的第一中空腔111中。在导油管10的与轴承的安装位置所对应的轴向位置处还可额外开设出油孔11。
在一些实施例中,导油管10的远行星排100端设有一个以上出油口12,由于出油口12开设于导油管10的管壁上,因此能够径向出油,降低阻力,便于油液进入润滑通道160。出油口12可以设置为具有开口的槽或者完整的孔,例如出油口12可以为U型槽或者圆孔。出油口12的数量本公开不做限制,例如出油口12的数量设置为3个,则3个出油口12的形状可以相同或者不同。
由于第一中空腔111的内径大于导油管10的外径,为了保证导油管10稳定安装于第一中空腔111中,在一些实施例中,导油管10上套设有至少一个衬套30,衬套30填充导油管10与第一中空腔111的腔壁之间的间隙。衬套30起支撑导油管10的作用,衬套30的材质为铜或复合塑料。
发动机输入轴总成610的太阳轮轴110与发电机620的转子621转动连接,如图23所示,在一些实施例中,发电机620的转子621设有沿轴向贯通的第二中空腔622,第二中空腔622和第一中空腔111连通,电机总成400的转子与行星排100同轴设置,壳体总成300的进油通道303引入的润滑油经第二中空腔622 引入行星排100的第一中空腔111,行星排润滑结构的导油管10安装于第二中空腔622和第一中空腔111中,导油管10的远行星排100端与壳体总成300的进油通道303直接对接连通,导油管10的近行星排100端与行星架120的集油腔124直接对接连通。通过将电机总成400的转子与行星排100内部油路串联,使得电机的转子充当润滑油的管路,使得润滑系统结构简化,提高了混合动力电驱动系统1000的集成度和整车搭载性。
电机的定子在工作时需要冷却,常用的冷却方式是喷油冷却。图30为图1的混合动力电驱动系统中冷却喷淋管路的安装结构图,如图30所示,在一些实施例中,混合动力电驱动系统还包括冷却喷淋管路325,壳体总成300的其中一条进油通道303连通于冷却喷淋管路325。对于双电机方案,则对应需要两套冷却喷淋管路325,例如发电机620和驱动电机670的定子分别通过一套冷却喷淋管路325进行冷却。
冷却喷淋管路325与与之连通的进油通道303之间连通有电磁阀370,该电磁阀370与控制板421电连接,以实现定子冷却通路的导通或断开,在定子不需要冷却时,关闭电磁阀370,使得冷却液不进入定子冷却通路。通过设置该电磁阀370使得冷却液分别对电机的定子和转子进行冷却,相互不受影响,这样可以根据需要进行冷却,提高了冷却效率,避免了能量的浪费。
在一些实施例中,如图30所示,左壳体320上设有挡油板3223,挡油板3223与左壳体320合围成导油区3224,挡油板3223设置在冷却喷淋管路325喷淋区域中,使得冷却喷淋管路325的至少一个油孔连通于导油区3224,则该油孔喷出的油液能够直接汇集于导油区3224中。左壳体320上设有贯通左壳体320内壁的引流孔3225,导油区3224通过引流孔3225连通于轴齿腔,由此能够通过该引流孔3225将电机腔301中的部分油液引入轴齿腔302中,以润滑采用常规飞溅润滑和主动润滑均难以充分润滑的轴承。
图31为图1的混合动力电驱动系统中左壳体上集油槽的结构示意图。如图30和图31所示,右壳体310和左壳体320的内侧壁均设有轴承安装孔305和集油槽304。轴承安装孔305变速机构总成的各轴通过轴承安装在右壳体310和左壳体320的位置相对的轴承安装孔305中。集油槽304与轴承安装孔305的连通是通过在右壳体310和/或左壳体320上开设的导油通道实现的。由于右壳体310和左壳体320上均设有集油槽304,并且右壳体310和左壳体320上的各集油槽304位置相对,因此位置相对的两个集油槽304可以合围成一个完整的油腔,各个油腔通过集油槽304槽壁上的缺口3041依次连通,并且靠近于引流孔3225的油腔与引流孔3225连通,引流孔3225中的油液进入与之连通的油腔中,并依次充满各个油腔,以润滑不易被润滑的轴承,例如驱动电机输入轴总成660的安装于右壳体310上的轴承以及EV中间轴的安装于右壳体310上的轴承,这两个轴承距离差速器轴总成640的距离较远,因此飞溅的油液难以满足其这两处轴承的润滑需求,尤其是在右倾工况下,上述两处轴承润滑风险高。
润滑油所需的动力由润滑动力装置340提供,在一些实施例中,润滑动力装置340为电子油泵,电子油泵包含泵体和油泵电机,油泵电机驱动泵体旋转,将油液泵入进油通道303中,在一些实施例中,泵体浸没在油液中,油泵电机安装于壳体总成300上,并且部分暴露在外,便于油泵电机接线。在一些实施例中,壳体总成300上安装有节温器(由图1所示的堵盖350覆盖,图中不可见)和用于对油液进行散热的散热器380,散热器380与节温器并联连通,节温器可以根据油液的温度改变节温器自身所接通的油路,从而在油液温度高于节温器的设定阈值时使得油液通过散热器380进行散热,实现“大循环”,在油液温度处于节温器的设定阈值以下时,油液不经过散热器380直接进行循环,实现“小循环”。
相应的,壳体总成300上开设有用于安装润滑动力装置340的润滑动力接口和用于安装节温器的节温器接口,在一些实施例中,壳体总成300上开设有用于安装温度传感器360的传感器接口,温度传感器360用于检测油温。上述接口设置于壳体总成300靠近发动机的一侧,合理利用混合动力电驱动系统1000与发动机之间的空间。在一些实施例中,壳体总成300靠近发动机的一侧设有凸筋323,防止在车辆行进过程中电子元器件的碰撞,提高混合动力电驱动系统的可靠性。
该散热器380可以是风冷散热器380,也可以是水冷散热器380。在一些实施例中,散热器380为油水换热器,油水换热器与外壳410的冷却流道连通,利用控制组件420的冷却温度(60℃~65℃)与混合动力变速机构总成600油液温度(通常高于80℃)之间的温度差值,利用冷却水对润滑油进行降温,降低能耗。
由于润滑油的在工作时温度较高,由此会导致轴齿腔302中气压增加,为了平衡壳体总成300内外压差,如图3和图30所示,壳体总成300上安装有通气塞390和挡板324,通气塞390的通气通道连通于电机腔和/或轴齿腔,挡板324设于电机腔和/或轴齿腔中,并且靠近通气通道的入口。挡板324能够阻挡飞溅的油液进入通气塞390的通气通道中,降低油液损耗,气体能够顺利通过通气塞390的通气通道进入外界环境中。
依据本公开的第二方面还提供一种混合动力车辆。图32为依据本公开一些实施例的混合动力车辆的结构示意图,如图32所示,该混合动力车辆包括车体2000、发动机3000和依据本公开的第一方面的混合动力电驱动系统1000。车体2000的前端设有前机舱,发动机3000和混合动力电驱动系统1000均安装于前机舱中。混合动力电驱动系统1000中,变速机构总成与发动机传动连接,具体是发动机输入轴总成610与发动机3000传动连接,在一些实施例中,发动机输入轴总成610与发动机还设有限扭减震器。
发动机3000和混合动力电驱动系统1000沿该混合动力车辆的宽度方向并排设置,即混合动力电驱动系统1000的发动机输入轴总成610的轴向平行于车宽方向。在一些实施例中,混合动力电驱动系统1000的左侧固定在车体2000的左纵梁上,混合动力电驱动系统1000的右侧与发动机3000的左侧固定连接,发动机3000的右侧固定在车体2000的右纵梁上。为了防止混合动力电驱动系统1000在前机舱中旋转,混合动力电驱动系统1000的下部固定在车体2000的下托架上。该混合动力电驱动系统1000的其他未详述结构均可参照 现有技术的相关公开,此处不展开说明。
由本公开一些实施例的技术方案可知,依据本公开一些实施例的混合动力电驱动系统,包括壳体总成、电机总成、变速机构总成和控制器总成。壳体总成内部设置轴齿腔、电机腔和储油腔,分别用于安装变速机构总成、安装电机总成和存储润滑油。通过将电机总成和变速机构总成均集成于壳体总成中,使得壳体总成内部结构紧凑、体积小。控制器总成同样安装于壳体上,控制器总成的外壳连接于壳体总成,从而能够缩短控制器总成与电机之间的间距,使得控制组件中三相输出铜排与电机的三相输入铜排的长度缩短,并且控制组件与混合动力电驱动系统中的低压电子器件(泵、传感器等)的接线长度缩短,便于管线布置。壳体总成、电机总成和变速机构总成中均设有润滑油路,壳体总成上安装有润滑动力装置,通过润滑动力装置驱动润滑油在润滑油路中流动,实现对变速机构总成中各个轴承的主动润滑,由于润滑油路均设于壳体总成、电机总成和变速机构总成中,因此壳体总成的内腔中不需要单独设置油管,进一步缩小混合动力电驱动系统的体积。
相比于现有技术,依据本公开一些实施例的混合动力电驱动系统,电机总成、变速机构总成和控制器总成均通过壳体总成安装固定,集成度高、体积小,并且控制器总成与电机总成之间以及控制器总成与变速机构总成之间的间距缩短,使得高压铜牌、低压线束、流体管路等结构的长度均缩短,结构精简、便于布线;壳体总成、电机总成和变速机构总成内部均集成润滑油路,且进一步降低混合动力电驱动系统的体积。提高混合动力电驱动系统的整车搭载性。
尽管已描述了本公开的优选实施例,但本领域内的普通技术人员一旦得知了基本创造性概念,则可对这些实施例作出另外的变更和修改。所以,所附权利要求意欲解释为包括优选实施例以及落入本公开范围的所有变更和修改。
显然,本领域的技术人员可以对本公开进行各种改动和变型而不脱离本公开的精神和范围。这样,倘若本公开的这些修改和变型属于本公开权利要求及其等同技术的范围之内,则本公开也意图包含这些改动和变型在内。

Claims (33)

  1. 一种混合动力电驱动系统,包括:
    壳体总成,设有轴齿腔、电机腔和储油腔,所述储油腔连通于所述轴齿腔和/或所述电机腔;
    电机总成,设于所述电机腔,且包括一个以上电机;
    变速机构总成,设于所述轴齿腔,用于与发动机和所述电机均传动连接,并且输出动力;以及
    控制器总成,包括设有控制腔的外壳和安装于所述控制腔的控制组件,所述外壳连接于所述壳体总成,所述外壳中设有用于冷却所述控制组件的冷却流道,所述控制组件设有与所述电机的三相输入铜排电连接的三相输出铜排;
    其中,所述壳体总成上安装有润滑动力装置;所述壳体总成、所述电机总成和所述变速机构总成中均设有润滑油路,所述润滑动力装置通过所述润滑油路连通于所述储油腔。
  2. 如权利要求1所述的混合动力电驱动系统,其中,所述壳体总成包括依次连接的右壳体、左壳体和端盖,所述右壳体与所述左壳体合围成所述轴齿腔,所述左壳体和所述端盖合围成所述电机腔。
  3. 如权利要求2所述的混合动力电驱动系统,其中,所述左壳体上设有安装区,所述控制器总成安装于所述安装区;所述安装区与所述外壳之间设有定位结构;所述安装区的侧壁设有排水孔。
  4. 如权利要求2所述的混合动力电驱动系统,其中,所述变速机构总成包括传动连接的发动机输入轴总成、差速器轴总成和至少一个中间轴总成;所述轴齿腔的底部构成所述储油腔,所述差速器轴总成至少部分位于所述储油腔中;
    所述发动机输入轴总成的轴设有贯通的第一中空腔;所述电机的转子中设有贯通的第二中空腔;所述端盖中设有进油通道,所述第一中空腔、所述第二中空腔和所述进油通道依次连通。
  5. 如权利要求4所述的混合动力电驱动系统,其中,所述电机总成包括两个电机,分别为发电机和驱动电机,所述发电机的转子与发动机输入轴总成的轴传动连接;所述发电机和所述驱动电机的转子均设有贯通的所述第二中空腔,所述第一中空腔、所述发电机的转子的第二中空腔和所述进油通道依次连通;
    所述中间轴总成设有两个,分别为EV中间轴总成和ICE中间轴总成;以及所述变速机构总成还包括与所述驱动电机的转子传动连接的驱动电机输入轴总成。
  6. 如权利要求5所述的混合动力电驱动系统,其中,所述发动机输入轴总成与所述发电机同轴设置,所述驱动电机输入轴总成和所述驱动电机同轴设置;所述发电机和所述驱动电机位于同侧;所述发动机输入轴总成的安装高度位于所述驱动电机与所述差速器轴总成之间,且所述发动机输入轴总成在竖直面上的投影与所述驱动电机和所述差速器轴总成在竖直面上的投影具有重合部分;
    所述EV中间轴总成的轴心位于所述发动机输入轴总成、所述驱动电机和所述差速器轴总成的轴心所围的三角形区域中;所述ICE中间轴总成的轴心的高度最低。
  7. 如权利要求6所述的混合动力电驱动系统,其中,所述EV中间轴总成包括EV中间轴和安装于所述EV中间轴上的第一EV中间齿轮和第二EV中间齿轮,所述EV中间轴总成通过所述第一EV中间齿轮与所述发动机输入轴总成和所述驱动电机输入轴总成传动连接,所述EV中间轴总成通过所述第二EV中间齿轮与所述差速器轴总成传动连接;以及
    所述ICE中间轴总成包括ICE中间轴和安装于所述ICE中间轴上的第一ICE中间齿轮和第二ICE中间齿轮;所述ICE中间轴总成通过所述第一ICE中间齿轮与所述发动机输入轴总成传动连接;所述ICE中间轴总成通过所述第二ICE中间齿轮与所述差速器轴总成传动连接。
  8. 如权利要求5所述的混合动力电驱动系统,其中,所述混合动力电驱动系统还包括冷却喷淋管路,所述冷却喷淋管路连通于所述进油通道,用于向所述发电机和所述驱动电机的定子喷油冷却;所述冷却喷淋管路与所述进油通道之间连通有电磁阀。
  9. 如权利要求8所述的混合动力电驱动系统,其中,所述左壳体上设有挡油板,所述挡油板与所述左壳体合围成导油区,所述冷却喷淋管路的至少一个油孔连通于所述导油区;所述左壳体上设有贯通的引流孔,所述导油区通过所述引流孔连通于所述轴齿腔。
  10. 如权利要求9所述的混合动力电驱动系统,其中,所述右壳体和所述左壳体的内侧壁均设有连通于所述轴齿腔的两个以上轴承安装孔和两个以上集油槽;所述引流孔、所述两个以上集油槽依次连通,至少一个所述集油槽与所述轴承安装孔连通。
  11. 如权利要求4所述的混合动力电驱动系统,其中,所述发动机输入轴总成包括行星排、至少一个执行机构、至少一个支撑轴承、至少一个挡位齿轮和内齿圈轴;所述内齿圈轴套设于所述行星排外,且所述内齿圈轴与所述行星排的内齿圈传动连接;所述至少一个执行机构、所述至少一个支撑轴承、所述至少一个挡位齿轮均设置于所述内齿圈轴上;所述行星排的用于连接发动机的轴设有所述第一中空腔。
  12. 如权利要求11所述的混合动力电驱动系统,其中,所述内齿圈轴通过支撑轴承安装;所述内齿圈轴包括:
    轴套部,用于套设于所述行星排的太阳轮轴或行星架轴上,所述轴套部上设有至少一个用于安装所述执行机构的第一安装位;以及
    罩部,连接于所述轴套部,且用于与所述行星排的内齿圈传动连接;
    其中,所述罩部和/或所述轴套部设有至少一个用于设置所述支撑轴承的装配位;所述罩部和/或所述轴套部设有至少一个用于设置所述挡位齿轮的第二安装位。
  13. 如权利要求12所述的混合动力电驱动系统,其中,所述罩部包括齿套部和挡板部,所述挡板部的内环连接所述轴套部、外环连接于所述齿套部;所述齿套部与所述内齿圈为一体式结构或者键连接;所述轴套部、所述挡板部、所述齿套部为一体式结构。
  14. 如权利要求13所述的混合动力电驱动系统,其中,所述齿套部和所述轴套部均设有所述装配位;所述齿套部的装配位为内孔壁,所述轴套部的装配位上设有用于安装所述支撑轴承的轴套;
    所述齿套部的装配位与所述内齿圈的安装处之间设有用于对所述支撑轴承轴向限位的限位结构;
    所述轴套部和/或所述罩部上设有至少一个贯通的导油孔;所述轴套部的外型面设有连通于所述导油孔的导油槽。
  15. 如权利要求12所述的混合动力电驱动系统,其中,所述至少一个执行机构包括分布于所述轴套部的两端的第一执行机构和第二执行机构;所述至少一个支撑轴承包括第一支撑轴承和第二支撑轴承,所述第一支撑轴承设于所述罩部的内孔中,所述第二支撑轴承通过轴套设于所述第一执行机构和所述第二执行机构之间;所述至少一个挡位齿轮包括第一挡位齿轮和第二挡位齿轮,所述第一挡位齿轮通过轴承空套于所述罩部上,所述第二挡位齿轮通过轴承空套于所述轴套部上、且位于所述第一执行机构与所述第二支撑轴承之间;
    所述第一安装位、所述装配位、所述第二安装位均设有两个;两个所述第一安装位分布于所述轴套部的两端;两个所述装配位和两个所述第二安装位均分别设于所述轴套部和所述罩部上。
  16. 如权利要求15所述的混合动力电驱动系统,其中,所述第一挡位齿轮包括齿圈部和连接部,所述齿圈部通过轴承空套于所述罩部上,所述连接部与所述第一执行机构的一侧的结合齿固定连接;所述第一执行机构的齿毂与所述第一安装位传动连接;所述第一执行机构的另一侧的结合齿与所述第二挡位齿轮固定连接。
  17. 如权利要求11所述的混合动力电驱动系统,其中,所述行星排设有润滑通道,所述润滑通道的出口朝向所述行星排的行星轮轴承;所述行星排的太阳轮轴设有沿轴向贯通的所述第一中空腔,所述行星排的行星架设有集油腔,所述第一中空腔、所述集油腔和所述润滑通道依次连通。
  18. 如权利要求17所述的混合动力电驱动系统,其中,所述行星架包括依次连接的行星架轴、连接板和行星轮轴,所述行星架轴设有连通的所述集油腔和第一导油孔,所述行星轮轴设有第二导油孔;
    所述连接板外侧设有导油件;所述第一导油孔、所述导油件与所述连接板之间空隙和所述第二导油孔依次连通,构成所述润滑通道。
  19. 如权利要求18所述的混合动力电驱动系统,其中,所述发动机输入轴总成还包括导油管,所述导油管安装于所述第二中空腔和所述第一中空腔中,且所述导油管的近行星排端伸入于所述集油腔。
  20. 如权利要求11所述的混合动力电驱动系统,其中,所述混合动力电驱动系统还包括换挡机构总成,所述换挡机构总成安装于所述轴齿腔中;所述换挡机构总成包括换挡电机、换挡减速机构、换挡毂和拨叉,所述换挡电机、所述换挡减速机构和所述换挡毂依次传动连接,所述拨叉的一端与所述换挡毂滑动配合、另一端作用于所述执行机构。
  21. 如权利要求20所述的混合动力电驱动系统,其中,所述左壳体设有中间板,所述中间板呈罩壳,所述中间板上开设有轴承安装孔和用于避让所述拨叉的避让区;
    所述中间板的其中一侧设有用于安装所述执行机构的其中一个结合齿的安装位;或者所述执行机构的其中一个结合齿与所述中间板的其中一侧一体成型。
  22. 如权利要求1-21中任一项所述的混合动力电驱动系统,其中,所述壳体总成靠近所述发动机的一侧设有凸筋、用于安装温度传感器的传感器接口、用于安装所述润滑动力装置的润滑动力接口和用于安装节温器的节温器接口;
    所述壳体总成安装有散热器,所述散热器与所述节温器并联连通,并且均连通于所述润滑动力装置和所述壳体总成的润滑油路之间;
    所述壳体总成安装有通气塞和挡板,所述通气塞的通气通道连通于所述电机腔和/或所述轴齿腔,所述挡板设于所述电机腔和/或所述轴齿腔中,并且靠近所述通气通道的入口。
  23. 如权利要求22所述的混合动力电驱动系统,其中,所述散热器为油水换热器,所述油水换热器与所述外壳的冷却流道连通。
  24. 如权利要求1-21中任一项所述的混合动力电驱动系统,其中,所述外壳包括上壳体和水冷板,所述上壳体和水冷板合围成所述控制腔,所述水冷板上设有冷却槽;
    所述控制组件包括电连接的控制板、驱动板、IGBT、所述三相输出铜排和高压电容,所述驱动板、所述IGBT和所述高压电容均安装于所述水冷板上,所述控制板安装于所述上壳体上,所述控制板与所述驱动板通过连接排线电连接,所述IGBT覆盖于所述冷却槽的槽口,以与所述冷却槽合围成所述冷却流道。
  25. 如权利要求24所述的混合动力电驱动系统,其中,所述水冷板包括连接的基板和罩壳,所述基板设有所述冷却槽和供所述三相输出铜排穿过的第一通孔;所述罩壳的内腔通过所述第一通孔连通于所述控制腔;所述壳体还包括用于封闭所述罩壳的内腔的下壳体,所述下壳体设有供电机的三相输入铜排穿过的第二通孔。
  26. 如权利要求24所述的混合动力电驱动系统,其中,所述上壳体和所述水冷板上均设有操作窗口;所述上壳体或所述水冷板上设有防水透气阀,或者至少一个所述操作窗口中安装有防水透气阀。
  27. 如权利要求24所述的混合动力电驱动系统,其中,所述控制器总成还包括高压转接盒,所述高压转接盒包括盒体,以及电连接的高压连接组件、电源接插件和至少一个高压接插件,所述盒体设于所述壳体、且设有连通的高压腔和至少一个装配口,所述高压连接组件设于所述高压腔中,所述高压接插件安装于所述装配口中;所述电源接插件安装于所述壳体或所述盒体上;所述控制腔与所述高压腔连通,以使所述高压电容的铜排伸入于所述高压腔、与所述高压接插件电连接。
  28. 如权利要求27所述的混合动力电驱动系统,其中,所述盒体包括顶盖和与所述上壳体一体成型的盒壁,所述装配口设置于所述盒壁上,所述上壳体上设有用于安装所述电源接插件的安装口;
    所述盒壁上设有两个所述装配口,两个所述装配口与所述安装口位于不同的侧面;所述高压接插件的数量为两个,分别为用于与空调压缩机电连接的第一高压接插件和用于与DCDC电连接的第二高压接插件。
  29. 如权利要求28所述的混合动力电驱动系统,其中,所述高压连接组件包括正极铜排、负极铜排和若干连接线束;所述正极铜排和负极铜排均电连接于所述电源接插件和所述高压电容的铜排,所述第一高压接插件和所述第二高压接插件通过所述若干连接线束并联接入所述正极铜排和所述负极铜排之间;所述控制组件还包括与所述高压连接组件电连接的熔断器。
  30. 如权利要求29所述的混合动力电驱动系统,其中,所述高压转接盒还包括设于所述盒体内的安装底座,所述正极铜排、所述负极铜排和所述熔断器均安装于所述安装底座;所述安装底座具有下沉区,所述正极铜排、所述负极铜排、所述电源接插件和所述高压电容的铜排的电连接处位于所述下沉区;所述下沉区的侧壁设有挡板。
  31. 如权利要求24所述的混合动力电驱动系统,其中,所述控制板连接于所述壳体的顶板;所述顶板设有散热结构、与所述控制板电连接的低压接插件和用于容纳所述控制板的电容的容纳部,所述散热结构与所述控制板的芯片的位置相对,所述低压插接件和所述容纳部均凸出于所述顶板的上表面。
  32. 一种混合动力车辆,包括:
    车体,设有前机舱;
    发动机,安装于所述前机舱中;以及
    权利要求1-31中任一项所述的混合动力电驱动系统,安装于所述前机舱中,所述变速机构总成与所述发动机传动连接。
  33. 如权利要求32所述的混合动力车辆,其中,所述混合动力电驱动系统的左侧固定在所述车体的左纵梁上,所述混合动力电驱动系统的右侧与所述发动机的左侧固定连接,所述发动机的右侧固定在所述车体的右纵梁上;所述混合动力电驱动系统的下部固定在所述车体的下托架上。
PCT/CN2023/095714 2022-10-24 2023-05-23 一种混合动力电驱动系统以及混合动力车辆 WO2024087601A1 (zh)

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