Acceleration control method for dct vehicle
US-2019202461-A1 · Jul 4, 2019 · US
US11498559B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11498559-B2 |
| Application number | US-202117458963-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 27, 2021 |
| Priority date | Feb 23, 2021 |
| Publication date | Nov 15, 2022 |
| Grant date | Nov 15, 2022 |
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A launch control method for a vehicle may include a step of increasing clutch torque of a clutch according to a decrease in braking pressure, a step of maintaining a current level of the clutch torque for a first reference duration, a step of gradually reducing the clutch torque within a range which is lower than the first reference torque level and is equal to or greater than a second reference torque level which is lower than the first reference torque level, a step of gradually increasing the clutch torque until the clutch torque reaches a third reference torque level which is higher than the first reference torque level, and a step of bringing the control to a stop when a state in which a clutch slip is less than a predetermined critical synchronous slip is maintained for a predetermined critical synchronization duration or longer than the predetermined critical synchronization duration.
Opening claim text (preview).
What is claimed is: 1. A vehicle launch control method comprising the steps of: increasing clutch torque of a clutch according to a decrease in braking pressure when a launch control operation is initiated; maintaining the clutch torque at a current torque level for a first reference duration when the clutch torque reaches or exceeds a first reference torque level; after a lapse of the first reference duration, when a wheel slip ratio exceeds a first reference slip ratio, reducing the clutch torque in a range which is lower than the first reference torque level and is equal to or greater than a second reference torque level which is lower than the first reference torque level; when the wheel slip ratio is equal to or less than a second reference slip ratio which is less than the first reference slip ratio or when a second reference duration elapses after the clutch torque reaches or exceeds the first reference torque level, increasing the clutch torque until the clutch torque reaches a third reference torque level which is higher than the first reference torque level; and stopping the launch control operation when a state in which a clutch slip remains less than a predetermined critical synchronous slip is maintained for a predetermined critical synchronization duration or longer than the predetermined critical synchronization duration. 2. The method according to claim 1 , wherein the launch control operation is initiated when a driver makes an input to select a launch control option and depresses an accelerator pedal and a brake pedal until an engine speed increases and reaches a reference engine speed. 3. The method according to claim 2 , wherein the clutch torque is maintained at a preparation torque level until the engine speed reaches the reference engine speed. 4. The method according to claim 1 , wherein in the increasing clutch torque of the clutch according to the decrease in the braking pressure, the clutch torque is reduced when the braking pressure is equal to or greater than a first reference braking pressure, and the clutch torque is increased at a rate corresponding to a first gradient when the braking pressure is lower than the first reference braking pressure. 5. The method according to claim 4 , wherein when an accelerator pedal remains depressed down to below a position that corresponds to a predetermined reference accelerator pedal sensor (APS) value, and the braking pressure becomes equal to or lower than a second reference braking pressure which is lower than the first reference braking pressure, the clutch torque is increased at a rate corresponding to a second gradient until the clutch torque reaches the first reference torque level. 6. The method according to claim 1 , wherein in the reducing the clutch torque in the range which is lower than the first reference torque level and is equal to or greater than the second reference torque level, the clutch torque is reduced while a feedback control to reduce the wheel slip ratio is performed. 7. The method according to claim 1 , wherein in the reducing the clutch torque in the range which is lower than the first reference torque level and is equal to or greater than the second reference torque level, when the wheel slip ratio is less than the first reference slip ratio, the clutch torque is not reduced but is maintained. 8. The method according to claim 1 , wherein in the increasing the clutch torque until the clutch torque reaches the third reference torque level, the clutch torque is reduced while a feedback control to reduce the wheel slip ratio is performed. 9. A vehicle launch control method comprising: (i) increasing clutch torque of a clutch of a vehicle according to a decrease in braking pressure when a launch control operation is initiated; (ii) maintaining the clutch torque at a current torque level for a first reference duration when the clutch torque reaches or exceeds a first reference torque level; (iii) after a lapse of the first reference duration, when a wheel slip ratio exceeds a first reference slip ratio, reducing the clutch torque within a range which is lower than the first reference torque level and is equal to or greater than a second reference torque level which is lower than the first reference torque level; (iv) when the wheel slip ratio is equal to or less than a second reference slip ratio which is less than the first reference slip ratio or when a second reference duration elapses after the clutch torque reaches or exceeds the first reference torque level, increasing the clutch torque until the clutch torque reaches a third reference torque level which is higher than the first reference torque level; and (v) stopping the launch control operation when a state in which a clutch slip remains less than a predetermined critical synchronous slip is maintained for a predetermined critical synchronization duration or longer than the predetermined critical synchronization duration, wherein after the step (iv), when the clutch slip is equal to or less than a first reference clutch slip, an average speed of driven wheels of the vehicle is equal to or greater than a first reference speed, and the wheel slip ratio is equal to or less than a third reference wheel slip ratio, a step of increasing the clutch torque toward a fourth reference torque level is performed. 10. The method according to claim 9 , wherein when the average speed of the driven wheels is equal to or greater than a second reference speed or when the clutch slip remains lower than the predetermined critical synchronous slip for the predetermined critical synchronization duration or longer than the predetermined critical synchronization duration, the launch control operation is brought into a stop. 11. The method according to claim 9 , wherein during each of the (i), (ii), (iii), (iv) and (v) steps, activation of a driving wheel spin prevention control function is prohibited. 12. A vehicle comprising: a transmission; an engine, wherein an output power of the engine undergoes an upshift or a downshift through the transmission; a clutch mounted between the engine and the transmission; and a controller electrically connected to the transmission and the clutch, wherein the controller is configured for: increasing clutch torque of the clutch according to a decrease in braking pressure when a launch control operation of the vehicle is initiated; maintaining the clutch torque at a current torque level for a first reference duration when the controller determines that the clutch torque reaches or exceeds a first reference torque level; after a lapse of the first reference duration, when a wheel slip ratio exceeds a first reference slip ratio, reducing the clutch torque in a range which is lower than the first reference torque level and is equal to or greater than a second reference torque level which is lower than the first reference torque level; when the wheel slip ratio is equal to or less than a second reference slip ratio which is less than the first reference slip ratio or when a second reference duration elapses after the clutch torque reaches or exceeds the first reference torque level, increasing the clutch torque until the clutch torque reaches a third reference torque level which is higher than the first reference torque level; and stopping the launch control operation when the controller determines that a state in which a clutch slip remains less than a predetermined critical synchronous slip is maintained for a predetermined critical synchronization duration or longer than the predetermined critical synchronization duration. 13. The vehicle according to claim 12 , wherein the controller is
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