Patent · US Active

Engine control apparatus and method

US8560206B2 · kind B2 · utility

2Cited by
11References
7Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 22, 2010
Grant dateOct 15, 2013
Priority date
Expiry dateSep 17, 2031

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T10/40
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

By using a model of a transient response characteristic of an engine and a model of a steady-state characteristic of the engine, a disturbance estimate value is calculated. By using this disturbance estimate value, initial command values of a nozzle opening degree of a Variable Nozzle Turbo and a valve opening degree of a Exhaust Gas Recirculator are adjusted in order to reduce model errors and appropriately handle the disturbance. Hence, it is possible to cause Mass Air Flow and Manifold Air Pressure to follow their target values stably.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.