Method and system for controlling pressure in a tuned pipe of a two stroke engine

Patent metadata

Field	Value
Publication number	US-11236668-B2
Application number	US-201916692628-A
Country	US
Kind code	B2
Filing date	Nov 22, 2019
Priority date	Dec 7, 2018
Publication date	Feb 1, 2022
Grant date	Feb 1, 2022

Abstract

An engine system and method of operating the same includes a two stroke engine, an exhaust manifold coupled to the two-stroke engine, a tuned pipe coupled to the exhaust manifold coupled to the exhaust manifold, a stinger pipe coupled to the tuned pipe, a silencer coupled to the tuned pipe and an exhaust pipe, and an exhaust bypass valve. Exhaust gases are directed from the two stroke engine through an exhaust manifold and through a tuned pipe. An opening of the exhaust bypass valve is changed to redirect exhaust gases away from the tuned pipe to change a pressure within the tuned pipe. In response to changing the opening of the exhaust bypass valve, the airflow through the engine is changed.

First claim

What is claimed is:

1. An engine system comprising:
a two stroke engine;
an exhaust manifold coupled to the two stroke engine;
a tuned pipe coupled to the exhaust manifold;
a stinger pipe coupled to the tuned pipe;
a common housing having a common wall dividing the common housing into a first silencer and a second silencer;
a turbocharger coupled to the stinger pipe, said turbocharger comprising a turbine inlet coupled to the stinger pipe and a turbine outlet coupled to the first silencer;
said first silencer coupled to the tuned pipe through the stinger pipe, a first exhaust path to atmosphere is provided sequentially from the tuned pipe through the stinger pipe, through the turbocharger and through the first silencer;
said second silencer coupled to an exhaust bypass valve and atmosphere, said second silencer having a second exhaust path completely separated from the first exhaust path of the first silencer by the common wall, said second exhaust path communicating exhaust gasses between the exhaust bypass valve and atmosphere; and
the exhaust bypass valve bypassing exhaust away from the stinger pipe to the second silencer.

2. The engine system as recited in claim 1 , wherein the exhaust bypass valve controls a pressure within the tuned pipe to control airflow through the engine.

3. The engine system as recited in claim 1 wherein the exhaust bypass valve is directly coupled to the exhaust manifold.

4. The engine system as recited in claim 1 wherein the tuned pipe comprises a diverging portion, a converging portion and a center portion therebetween, wherein said exhaust bypass valve is coupled to one of said diverging portion, said center portion or said converging portion.

5. The engine system as recited in claim 1 wherein the tuned pipe comprises a diverging portion, a converging portion and a center portion therebetween, wherein said exhaust bypass valve is directly coupled to one of said diverging portion, said center portion or said converging portion.

6. The engine system as recited in claim 1 wherein the tuned pipe comprises a diverging portion, a converging portion and a center portion therebetween, wherein said exhaust bypass valve is coupled to said center portion through a standoff pipe.

7. The engine system as recited in claim 1 further comprising a bypass pipe comprising a first end coupled to the exhaust bypass valve and a second end coupled to the second silencer.

8. The engine system as recited in claim 7 wherein the exhaust bypass valve comprises a wastegate.

9. The engine system as recited in claim 1 further comprising a bypass pipe comprising a first end coupled to the exhaust bypass valve and a second end of the bypass pipe is coupled to the second silencer separate from an exhaust pipe.

10. The engine system as recited in claim 1 further comprising a controller and a position sensor coupled to the exhaust bypass valve and generating a position signal corresponding to a position of the exhaust bypass valve, said controller positioning the exhaust bypass valve in response to the position signal.

11. The engine system as recited in claim 1 further comprising a controller coupled to a boost pressure sensor generating a boost pressure signal, said controller controlling a position of the exhaust bypass valve in response to the boost pressure signal.

12. The engine system as recited in claim 1 further comprising a controller coupled to a boost pressure sensor generating a boost pressure signal and an atmospheric pressure sensor generating an atmospheric pressure signal, said controller controlling a position of the exhaust bypass valve in response to the boost pressure signal and the atmospheric pressure signal.

13. The engine system as recited in claim 1 further comprising a controller coupled to an engine speed sensor generating an engine speed signal and a throttle position sensor generating a throttle position signal, said controller controlling a position of the exhaust bypass valve in response to the engine speed signal and the throttle position signal.

14. The engine system as recited in claim 13 further comprising an atmospheric sensor generating an atmospheric pressure signal and wherein the controller controls the position of the exhaust bypass valve in response to the engine speed signal, the throttle position signal and the atmospheric pressure signal.

Assignees

• Polaris Inc

Inventors

• Buchwitz James H
• Hedlund Darren J
• Brandt Jon P
• Hanson Reed A
• Salfer Lucas R
• Zimney Derek

Classifications

• Y02T10/12

  Improving ICE efficiencies · CPC title

• F01N2590/00

  Exhaust or silencing apparatus adapted to particular use, e.g. for military applications, airplanes, submarines · CPC title

• F01N2900/1406

  Exhaust gas pressure · CPC title

• Y02T10/40

  Engine management systems · CPC title

• F02B37/186 Primary

  Arrangements of actuators or linkage for bypass valves · CPC title