Turbocompound internal combustion engine

• US 6,681,575 B2
• Filed: 10/05/2001
• Issued: 01/27/2004
• Est. Priority Date: 10/06/2000
• Status: Expired due to Fees

• Current Assignee: FPT Motorenforschung AG (Iveco Group NV)
• Original Assignee: Iveco Fiat SpA (Iveco Group NV), Iveco Motorenforschung AG
• Inventors: Zaehner, Werner, Dellora, Giancarlo
• Primary Examiner(s): Denion, Thomas
• Assistant Examiner(s): TRIEU, THAI BA
• Application Number:
  US09/971,817
• Publication Number:
  US 20020062646A1
• Time in Patent Office: 844 Days
• Field of Search: 606/24, 606/14, 606/02
• US Class Current: 60/624
• CPC Class Codes: F02B 37/005 Exhaust driven pumps being combined with an exhaust driven auxiliary apparatus, e.g. a ventilator
• CPC Class Codes: F02B 37/24 by using pumps or turbines with adjustable guide vanes
• CPC Class Codes: F02B 41/10 in exhaust turbines use of exhaust turbines for charging F02B37/00
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies

Abstract

A turbocompound internal combustion engine having a turbocharger with a variable-geometry turbine; and an auxiliary turbine, which is located downstream from the turbine of the turbocharger, provides for recovering energy from the exhaust gas, and is connected mechanically to the drive shaft of the engine via a transmission; a control device compares the rotation speed of the auxiliary turbine, detected by means of a sensor, with a range of permissible speeds calculated on the basis of the speed of the drive shaft, and controls fuel supply to the engine and the geometry of the variable-geometry turbine to maintain the speed of the auxiliary turbine within predetermined limits in the event of a fault on the transmission.

Claims

1. A turbocompound internal combustion engine comprising:

a drive shaft;

a turbocharger comprising;

a turbine and

a compressor;

an auxiliary turbine located along the path of the exhaust gas, downstream from said turbine of said turbocharger; and

transmission means between said auxiliary turbine and said drive shaft

said engine further comprising;

a first angular speed sensor for detecting the rotation speed of said auxiliary turbine; and

a control device for controlling the rotation speed of said auxiliary turbine, and which is connected to said first angular speed sensor and in turn comprises;

calculating means for calculating a range of permissible values of said rotation speed of said auxiliary turbine,

comparing means for comparing the rotation speed of said auxiliary turbine measured by said first sensor with said range of permissible values, and

control means for controlling operating parameters of the engine in response to an enabling signal generated by said comparing means, so as to maintain said speed of said auxiliary turbine within said range of permissible values;

said calculating means for calculating said range of permissible values including a second angular speed sensor for detecting the rotation speed of the drive shaft; and

processing means for calculating at least a maximum value of the speed of said auxiliary turbine on the basis of the speed of the drive shaft.

2. The engine as claimed in claim 1, characterized in that said turbine of said turbocharger is a variable-geometry type;

said control means for controlling operating parameters of the engine comprising means for varying the geometry of said variable-geometry turbine.

3. The engine as claimed in claim 2, characterized in that said means for varying the geometry of the variable-geometry turbine comprise means for setting a full-open condition of said variable-geometry turbine.

4. The engine as claimed in claim 1, characterized in that said control means for controlling operating parameters of the engine comprise means for varying fuel supply, to maintain said speed of said auxiliary turbine within said maximum value.

5. The engine as claimed in claim 1, characterized in that said control device includes means for determining the plausibility of a signal received from said first sensor;

and disabling means for disabling said control means for controlling operating parameters of the engine in response to detection of an implausibility condition of said signal.

6. A method of controlling a turbocompound internal combustion engine comprising:

a drive shaft;

a turbocharger comprising;

a turbine and

a compressor;

an auxiliary turbine located along the path of the exhaust gas, downstream from said turbine of said turbocharger; and

transmission means between said auxiliary turbine and said drive shaft;

said method including the steps of;

measuring the rotation speed of said auxiliary turbine by means of a first sensor;

calculating a range of permissible values of said rotation speed of said auxiliary turbine;

comparing the rotation speed of said auxiliary turbine measured by said first sensor with said range of permissible values; and

controlling operating parameters of the engine in response to the outcome of said comparing step, so as to maintain said speed of said auxiliary turbine within said range of permissible values,

said operating parameters including the geometry of said turbine of said turbocharger and fuel supply of said engine.

7. The method as claimed in claim 6, characterized in that said step of controlling operating parameters of the engine comprises the operations of setting said turbine of said turbocharger to a full-open condition;

and modulating fuel supply to maintain the rotation speed of the auxiliary turbine within a maximum limit.

8. The method as claimed in claim 6, characterized by comprising the steps of determining the plausibility of a signal received from said first sensor;

and disabling said step of controlling said operating parameters of the engine in response to an implausibility condition of said signal.

9. A method of controlling a turbocompound internal combustion engine comprising:

a drive shaft;

a turbocharger comprising;

a turbine and

a compressor;

an auxiliary turbine located along the path of the exhaust gas, downstream from said turbine of said turbocharger; and

transmission means between said auxiliary turbine and said drive shaft;

said method including the steps of;

measuring the rotation speed of said auxiliary turbine by means of a first sensor;

calculating a range of permissible values of said rotation speed of said auxiliary turbine;

measuring the rotation speed of the drive shaft of said engine by means of a second angular speed sensor;

calculating a range of permissible values of the speed of said auxiliary turbine on the basis of the speed of the drive shaft, said range being defined by at least a maximum value of the speed of said auxiliary turbine;

comparing the rotation speed of said auxiliary turbine measured by said first sensor with said range of permissible values; and

controlling operating parameters of the engine in response to the outcome of said comparing step, so as to maintain said speed of said auxiliary turbine within said range of permissible values.