IP Library Granted Patent US 7,658,098
Granted Patent B2
US 7,658,098 · App. 11/967,353 · Granted Feb 9, 2010

Method for controlling vehicle emissions

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Quick Facts
Patent No.
US 7,658,098
App. No.
11/967,353
Granted
Feb 9, 2010
Kind
B2
Abstract

A method and system is provided for determining non-sensed vehicle operating parameters of a vehicle system. The method and system further provide for determining an engine air mass flow rate using the non-sensed vehicle operating parameters. A plurality of vehicle operating set-points may be determined using the non-sensed vehicle system operating parameters and the non-sensed engine air mass flow rate. A controller may use the vehicle operating set-points in order to control emissions of the vehicle system.

Claims (290)

1. A method for controlling emissions of a vehicle system, the method comprising:

determining a plurality of non-sensed vehicle operating parameters; the said plurality of non-sensed vehicle operating parameters includes a non-sensed air intake mass flow rate, the non-sensed air intake mass flow rate being determined using a volumetric efficiency ratio, a vehicle engine speed, a sensed intake manifold pressure, a displacement volume, and a sensed intake manifold temperature;

determining an engine air mass flow rate of the vehicle system using the non-sensed vehicle operating parameters; and

determining vehicle operating set-points for use in controlling emissions of the vehicle system, the vehicle operating set-points being determined using the non-sensed vehicle operating parameters and the determined engine air mass flow rate.

2. The method according to claim 1 , further comprising determining at least a portion of the non-sensed vehicle operating parameters from a number of sensed vehicle operating parameters.

3. The method according to claim 1 , wherein the non-sensed air intake mass flow rate is determined using the following relationship:

M

intake

=

V

disp

RPM

engine

*

I

M

P

120

*

R

gas

*

I

M

T

η

vol

wherein: M intake is the non-sensed intake mass flow rate, V disp is a displacement volume of the vehicle system, RPM engine is the sensed vehicle engine speed, IMP is the sensed intake manifold pressure, R gas is a gas constant, IMT is the sensed intake manifold temperature, and N vol is the volumetric efficiency ratio.

4. The method according to claim 3 , wherein the volumetric efficiency is determined using the following relationship:

η vol =α(RPM engine ,PR engine )η vol — map (RPM engine ,ρ intake )

wherein: α is a function determined using the vehicle engine speed and an engine pressure ratio; and N vol — map is a function determined using the vehicle engine speed and an engine intake density.

5. The method according to claim 1 , wherein the plurality of non-sensed vehicle operating parameters includes a non-sensed EGR mass flow rate, the non-sensed EGR mass flow rate being determined using a non-sensed turbine inlet temperature, a non-sensed turbine inlet pressure, an EGR valve discharge coefficient, and an engine pressure differential.

6. The method according to claim 5 , wherein the non-sensed EGR mass flow rate is determined using the following relationship:

M

EGR

2

*

T

T

I

T

P

I

*

Disc

C

2

=

C

1

*

Δ

P

+

C

2

wherein: M EGR is the non-sensed EGR mass flow rate, TTI is the non-sensed turbine inlet temperature, TPI is the non-sensed turbine inlet pressure, DisC is an EGR valve discharge coefficient, C 1 is a constant value dependent upon the vehicle system, C 2 is a function of a sensed vehicle engine speed and a vehicle engine load, and ΔP is the engine pressure differential.

7. The method according to claim 1 , wherein the plurality of non-sensed vehicle operating parameters includes a non-sensed turbine mass flow rate, the non-sensed turbine mass flow rate being determined using a reduced turbine mass flow rate, a non-sensed turbine inlet temperature, and a non-sensed turbine inlet pressure.

8. The method according to claim 7 , wherein the non-sensed turbine mass flow rate is determined using the following relationship:

M

turbine

=

M

turbine_reduced

*

T

P

I

T

T

I

wherein: M turbine is the non-sensed turbine mass flow rate, M turbine — reduced is the reduced turbine mass flow rate, TTI is the non-sensed turbine inlet temperature, and TPI is the non-sensed turbine inlet pressure.

9. The method according to claim 8 , wherein the reduced turbine mass flow rate is determined using the following relationship:

M turbine — reduced =f turbine — map ( S ,PR turbine )

wherein: M turbine — reduced is the reduced turbine mass flow rate, f turbine — map is a mapped turbine function, S is a VGT vane pulse width modulation value, and PR turbine is a VGT pressure ratio.

10. The method according to claim 1 , wherein the plurality of non-sensed vehicle operating parameters includes a non-sensed turbine inlet temperature, the non-sensed turbine inlet temperature being determined using a sensed intake manifold temperature, an engine exhaust energy fraction, a mass fueling rate, and the non-sensed intake mass flow rate.

11. The method according to claim 10 , wherein the non-sensed turbine inlet temperature is determined using the following relationship:

T

T

I

=

I

M

T

+

L

H

V

*

F

exh_energy

*

M

fueling

Cp

exh

*

M

intake

wherein: TTI is the non-sensed inlet turbine temperature, IMT is the sensed intake manifold temperature, LHV is a lower heat value of the fuel, F exh — energy is the engine exhaust energy fraction, M fueling is the mass fueling rate, Cp exh is a specific heat of the exhaust gas, and M intake is the non-sensed intake mass flow rate.

12. The method according to claim 1 , wherein a non-sensed turbine inlet pressure is determined using a non-sensed turbine inlet temperature, a mass fueling rate, a non-sensed intake mass flow rate, a non-sensed EGR mass flow rate, and the non-sensed turbine mass flow rate.

13. The method according to claim 12 , wherein the non-sensed turbine inlet pressure is determined using the following relationship:

·

V

exh_manifold

R

exh_gas

t

(

T

P

I

T

T

I

)

=

M

fueling

+

M

intake

-

M

EGR

-

M

turbine

wherein: V exh — manifold is a exhaust manifold volume, R exh — gas is an exhaust gas constant, TPI is the non-sensed turbine inlet pressure, TTI is the non-sensed turbine inlet temperature, M Fueling is the mass fueling rate, M intake is the non-sensed intake mass flow rate, M EGR is the non-sensed EGR mass flow rate, and M turbine is the non-sensed turbine mass flow rate.

14. A method for controlling emissions of a vehicle system, the method comprising:

determining a non-sensed EGR mass flow rate, a non-sensed air intake mass flow rate, a non-sensed turbine mass flow rate, a non-sensed turbine inlet temperature, and a non-sensed turbine inlet pressure using a plurality of sensed vehicle operating parameters;

determining an engine air mass flow rate of the engine using the non-sensed EGR mass flow rate, the non-sensed air intake mass flow rate, the non-sensed turbine mass flow rate, the non-sensed turbine inlet temperature, and the non-sensed turbine inlet pressure;

determining a plurality of vehicle operating set-points using the non-sensed EGR mass flow rate, the non-sensed air intake mass flow rate, the non-sensed turbine mass flow rate, the non-sensed turbine inlet temperature, the non-sensed turbine inlet pressure, and the engine air mass flow rate; and

determining future operations of the vehicle system using the determined vehicle operating set-points, wherein the determined future operations are used to modify the determined vehicle operating set-points in order to control the emissions of the vehicle system.

15. The method according to claim 14 , wherein the sensed vehicle operating parameters include an intake manifold pressure, an intake manifold temperature, and a vehicle engine speed.

16. A system for use in controlling emissions of a vehicle system, the system comprising:

a plurality of hardware sensors providing a plurality of sensed vehicle operating parameters, the plurality of hardware sensors including an intake manifold pressure sensor, an intake manifold temperature sensor, and a vehicle engine speed sensor; and

a controller configured for:

determining a plurality of non-sensed vehicle operating parameters based upon the data provided from the plurality of sensed vehicle operating parameters;

determining a non-sensed engine air mass flow rate based upon the determined non-sensed vehicle operating parameters;

determining a plurality of vehicle operating set-points using the non-sensed vehicle operating parameters and the non-sensed engine air mass flow rate; and

controlling emissions of the vehicle system using the determined vehicle operating set-points.

17. The method according to claim 16 , wherein the non-sensed vehicle operating parameters include a non-sensed air intake mass flow rate, the non-sensed air intake mass flow rate being determined using the following relationship:

M

intake

=

V

disp

RPM

engine

*

I

M

P

120

*

R

gas

*

I

M

T

η

vol

wherein: M intake is the non-sensed intake mass flow rate, V disp is a displacement volume, RPM engine is a sensed vehicle engine speed, IMP is a sensed intake manifold pressure, R gas is a gas constant, IMT is a sensed intake manifold temperature, and N vol is a volumetric efficiency ratio.

18. The method according to claim 16 , wherein the non-sensed vehicle operating parameters include a non-sensed EGR mass flow rate, the non-sensed EGR mass flow rate being determined using the following relationship:

M

EGR

2

*

T

T

I

T

P

I

*

Disc

C

2

=

C

1

*

Δ

P

+

C

2

wherein: M EGR is the non-sensed EGR mass flow rate, TTI is a non-sensed turbine inlet temperature, TPI is a non-sensed turbine inlet pressure, DisC is an EGR valve discharge coefficient, C 1 is a constant value dependent upon the vehicle system, C 2 is a function of a sensed vehicle engine speed and a vehicle engine load, and ΔP is a engine pressure differential.

19. The method according to claim 16 , wherein the non-sensed vehicle operating parameters include a non-sensed turbine mass flow rate, the non-sensed turbine mass flow rate being determined using the following relationship:

M

turbine

=

M

turbine_reduced

*

T

P

I

T

T

I

wherein: M turbine is the non-sensed turbine mass flow rate, M turbine — reduced is a reduced turbine mass flow rate, TTI is a non-sensed turbine inlet temperature, and TPI is a non-sensed turbine inlet pressure.

Assignments (1)
CONFIRMATORY LICENSE Recorded Aug 3, 2015
From: DETROIT DIESEL CORPORATION
To: ENERGY, UNITED STATES DEPARTMENT OF
Reel/Frame 036274/0206 →
Continuity (1)
Related Publication 20090165544A1 · Jul 2, 2009