Methanol fueled turbocharged diesel cycle internal combustion engine

• US 5,269,144 A
• Filed: 09/10/1991
• Issued: 12/14/1993
• Est. Priority Date: 09/10/1991
• Status: Expired due to Term

• Current Assignee: MTU America, Inc. (Rolls-Royce Holdings Plc)
• Original Assignee: Detroit Diesel Corporation (Daimler Truck Holding AG)
• Inventors: Hawkins, Jeffery S., Tasky, David P., Winsor, Richard E., Weisman, Steven M., Savonen, Craig L., Miller, Stanley P.
• Primary Examiner(s): KOCZO JR, MICHAEL
• Application Number:
  US07/757,720
• Time in Patent Office: 826 Days
• Field of Search: 60/609, 60/611, 91/362, 123/564, 417/310
• US Class Current: 60/609
• CPC Class Codes: F02B 1/02 with positive ignition with non-timed positive ignition F02B9/06
• CPC Class Codes: F02B 2075/025 two
• CPC Class Codes: F02B 2275/32 Miller cycle
• CPC Class Codes: F02B 3/06 with compression ignition compression ignition engines using air or gas for blowing fuel into compressed air in cylinder F02B13/02
• CPC Class Codes: F02B 33/38 of Roots type
• CPC Class Codes: F02B 33/446 having valves for admission of atmospheric air to engine, e.g. at starting
• CPC Class Codes: F02B 37/04 Engines with exhaust drive and other drive of pumps, e.g. with exhaust-driven pump and mechanically-driven second pump
• CPC Class Codes: F02B 37/12 Control of the pumps
• CPC Class Codes: F02B 37/16 by bypassing charging air
• CPC Class Codes: F02B 39/16 Other safety measures for, or other control of, pumps
• CPC Class Codes: F02B 67/00 Engines characterised by the arrangement of auxiliary apparatus not being otherwise provided for, e.g. the apparatus having different functions; Driving auxiliary apparatus from engines, not otherwise provided for
• CPC Class Codes: F02B 7/02 the fuel in the charge being liquid
• CPC Class Codes: F02B 75/22 with cylinders in V, fan, or star arrangement
• CPC Class Codes: F02D 2009/0237 Increasing combustion chamber gas temperature
• CPC Class Codes: F02D 2009/0249 Starting engine, e.g. closing throttle in Diesel engine to reduce starting torque
• CPC Class Codes: F02D 23/02 the engines being of fuel-injection type
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies

Abstract

The combination of an intake air supply system with an internal combustion engine having a charge air cooler, a cylinder charging air intake and an exhaust discharge is provided. The intake air supply system includes a Roots-type positive displacement blower having inlet and outlet means and an exhaust gas driven turbo-compressor connected in series with the blower. The intake air supply system further includes a bypass passage connecting the blower inlet and outlet and a valve in the bypass passage to control the flow of fluid through the bypass. The valve is operative to open and close the bypass passage in response to engine operating parameters and to modulate the flow area of the passage in response to the same engine operating parameters so as to infinitely vary the flow area between the open and closed positions of the valve. The valve is modulated to operatively maintain the bypass passage at least partially open at engine idle, whereby the valve means permits bypass flow to recirculate air flow from the blower outlet to the inlet to reduce or limit the engine power absorbed by the blower or to conduct additional air flow around the blower directly from the turbo-compressor to the engine intake to avoid the restriction of the blower to increased charging air flow. A single valve means thus provides a dual function capability.

Claims

1. The combination of an intake air supply system with an internal combustion engine having a charge air cooler, a cylinder charging air intake and an exhaust discharge, the intake air supply system including:

an engine driven positive displacement blower having inlet and outlet means and an exhaust gas driven turbo-compressor connected in series whereby the compressor discharges to the blower inlet and the blower outlet discharges to the charge air cooler and to the engine air intake;

a bypass passage connecting the blower inlet and outlet;

control means including an electronic control module for calculating a required flow area of said bypass passage in response to continually sensed engine operating parameters including engine speed, boost air pressure at the turbo-compressor outlet and operator demand;

valve means in the bypass passage to control the flow of fluid through the bypass;

said valve means being operative to modulate said flow area as calculated from a fully open position to a fully closed position of said bypass passage thereby infinitely varying the flow area between the fully open and fully closed positions of said valve means; and

said valve means being modulated to operatively maintain said bypass passage at least partially open at engine idle, whereby said valve means permits bypass flow, either (a) to recirculate air flow from the blower outlet to the inlet to reduce or limit the engine power absorbed by the blower or (b) to conduct additional air flow around the blower directly from the turbo-compressor to the engine intake to avoid the restriction of the blower to increased charging air flow, thereby providing a dual function capability in a single valve means.

2. The combination of claim 1 wherein said control means includes means for (1) maintaining said passage partially closed at engine idle and low load-low speed conditions, (2) maintaining said passage fully closed at low speed-high load conditions and (3) maintaining said passage fully open at high speed-high load conditions.

3. The combination of claim 2 wherein said control means maintains said passage fully closed under heavy acceleration of said engine when the turbo-compressor discharge pressure is insufficient to maintain acceptable air/fuel ratios.

4. The combination of claim 1 wherein said control means includes means for (1) maintaining said passage between 40% and 70% closed at engine idle and low load-low speed conditions, (2) maintaining said passage fully closed at low speed-high load conditions and (3) maintaining said passage fully open at high speed-high load conditions.

5. The combination of claim 4 wherein said control means maintains said passage fully closed under heavy acceleration of said engine when the turbo-compressor discharge pressure is insufficient to maintain acceptable air/fuel ratios.

6. The combination of claim 5 wherein said internal combustion engine is a two cycle compression-ignition engine having at least one piston cylinder and associated compression chamber,

said engine having a compression ratio within the combustion chamber ranging from about 20:

1 to about 25;

1.

7. The combination of claim 6 wherein said blower includes a second said bypass passage to thereby provide a pair of bypass passages,

said blower including a main housing rotatably supporting a pair of mating impellers in an enclosed chamber having inlet and outlet zones respectively connected with the compressor and the charge air cooler and the engine air intake, and further including an air inlet housing having a main air inlet portion leading directly into said inlet zone and a pair of outlet ports, one each of said outlet ports leading directly to a respective one of said bypass passages,

a valve within each said outlet port and affixed to a common actuating member, each said valve being actuable from a position fully closing said outlet port to a position fully opening said outlet port.

8. The combination of claim 7 wherein the geometric compression ratio within said combustion chamber is about 23:

1.

9. The combination of claim 1 wherein said blower includes a second said bypass passage to thereby provide a pair of bypass passages,

said blower including a main housing rotatably supporting a pair of mating impellers in an enclosed chamber having inlet and outlet zones respectively connected with the compressor and the charge air cooler and the engine air intake, and further including an air inlet housing having a main air inlet portion leading directly into said inlet zone and a pair of outlet ports, one each of said outlet ports leading directly to a respective one of said bypass passages,

a valve within each said outlet port and affixed to a common actuating member, each said valve being actuable from a position fully closing said outlet port to a position fully opening said outlet port.

10. The combination of claim 1 wherein said internal combustion engine is a two cycle compression-ignition engine having at least one piston cylinder and associated compression chamber,

said engine having a geometric compression ratio within the combustion chamber ranging from about 20:

1 to about 25;

1.

11. The combination of claim 10 wherein the geometric compression ratio within said combustion chamber is about 23:

1.

12. The combination of claim 1 further comprising:

a solenoid valve actuator for controlling said control valve means;

means for generating an input control signal based on engine speed, boost air pressure as sensed at the outlet of said turbo-compressor and operator demand;

means for supplying a feedback signal representing the actual angular position of the control valve means to the means for generating the input control signal.