Method and Control Unit for Operating a Drive Train of a Vehicle
US-2024068563-A1 · Feb 29, 2024 · US
US9625031B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9625031-B2 |
| Application number | US-201414912298-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 7, 2014 |
| Priority date | Aug 19, 2013 |
| Publication date | Apr 18, 2017 |
| Grant date | Apr 18, 2017 |
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A method and apparatus for modifying the shift map of an automatically controlled vehicle transmission having individually selectable speed ratios. A calibrator determines launch ratio from a plurality of speed ratios and is responsive to ambient pressure and/or ambient temperature. The calibrator may be further responsive to engine speed, engine temperature, transmission temperature, gradient and direction of gradient.
Opening claim text (preview).
The invention claimed is: 1. A method of determining a launch speed ratio of an automatically controlled multi-speed vehicle transmission having a shift map to determine a ratio selection, the method comprising: providing in the transmission a plurality of speed ratios for vehicle launch, and determining which one of the plurality of speed ratios is to be selected in the transmission as the launch speed ratio by reference to ambient temperature. 2. A method according to claim 1 comprising determining which one of the plurality of speed ratios is to be selected in the transmission as the launch speed ratio by reference to ambient pressure. 3. A method according to claim 2 comprising determining a first launch speed ratio when the ambient pressure is below a pre-determined ambient pressure or determining a second launch speed ratio when the ambient pressure is above a pre-determined ambient pressure and wherein the second launch speed ratio is higher than the first launch speed ratio. 4. A method according to claim 3 applied to gasoline and diesel engined variants, and wherein said pre-determined ambient pressure is lower for the gasoline engined variant than for the diesel engined variant. 5. A method according to claim 1 applied to a gasoline engined variant, comprising determining a lower launch speed ratio when the ambient temperature is below a pre-determined ambient temperature. 6. A method according to claim 5 wherein said pre-determined ambient temperature is dependent on ambient pressure. 7. A method according to claim 6 , wherein said pre-determined ambient temperature progressively increases as ambient pressure progressively decreases. 8. A method according to claim 7 applied to ambient temperature in a range from −25° C. to 39° C., and an ambient pressure in a range from 1050 to 750 mbar. 9. A method according to claim 1 applied to a diesel engined variant, comprising determining a lower launch speed ratio when the ambient temperature is above a pre-determined ambient temperature. 10. A method according to claim 9 wherein said pre-determined ambient temperature is dependent on ambient pressure. 11. A method according to claim 10 wherein said pre-determined ambient temperature progressively decreases as ambient pressure progressively decreases. 12. A method according to claim 11 applied to ambient temperature in a range from 41° C. to 14° C., and ambient pressure in a range from 1050 to 800 mbar. 13. A method according to claim 1 comprising determining a lower launch speed ratio when the ambient temperature is below a first ambient temperature and subsequently maintaining said launch speed ratio until the ambient temperature is above a second ambient temperature. 14. A method according to claim 13 wherein the first ambient temperature is in a range from −15° C. to −6° C. and the second ambient temperature is in a range from −5° C. to 0° C. 15. A method according to claim 1 including determining a first numerical factor in a range from 50-100 relating ambient pressure and ambient temperature, said first factor having a lowest numerical value for high temperature and low pressure, and a highest numerical value for low temperature and high pressure; determining a second numerical factor relating said first factor and gradient in a range from −30% to 20%, said second factor being indicative of a minimum vehicle engine speed at which a lower launch speed ratio is permitted; and commanding launch in said lower launch speed ratio should engine speed be less than the numerical value of the second factor. 16. A method according to claim 1 including relating a temperature of the vehicle transmission in a range from −30° C. to +30° C. to a temperature of a vehicle engine for said transmission in a range from −30° C. to +40° C., to give a threshold engine speed below which a lower launch speed ratio is commanded, said threshold engine speed being highest for the lowest transmission temperature and lowest engine temperature in combination, and lowest for the highest transmission temperature and highest engine temperature in combination. 17. A calibrator for application to the shift map of an automatically controlled multi-speed vehicle transmission, said calibrator comprising a processor and memory for implementing the method of claim 1 . 18. An electronic control unit for automatically selecting a speed ratio of a multi-speed vehicle transmission according to a shift map, said shift map including a calibrator for implementing the method of claim 1 . 19. An automatically controlled multi-speed transmission of a vehicle having a plurality of speed ratios, a shift map for determining speed ratio selection, and a calibrator according to claim 18 applied to said shift map. 20. An automatically controlled multi-speed transmission of a vehicle having an electronic control unit according to claim 18 . 21. A vehicle incorporating the transmission of claim 20 .
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