IP Library Granted Patent US 9,010,099
Granted Patent B2
US 9,010,099 · App. 13/681,616 · Granted Apr 21, 2015

Exhaust system for two-stroke internal combustion engine

Inventor: Stephen B. Schultz (Denver, IA)
F01N3/00F01N13/08F02B27/04F01N2470/20F01N2470/24
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Quick Facts
Patent No.
US 9,010,099
App. No.
13/681,616
Granted
Apr 21, 2015
Kind
B2
Abstract

An exhaust pipe for two-stroke, internal-combustion engines in which there are multiple exhaust expansion chambers, each within one another, used in combination, the multiple chambers allow for the combustible fuel/air mixture to be delivered in more optimal reflective pressure waves throughout the RPM range of the engine. By changing the number of the chambers, their size and shape, the design of the exhaust pipe can be tuned for torque and power while requiring a minimum of space.

Claims (11)

1. An exhaust system for a two-stroke internal combustion engine having one or more exhausts ports, said exhaust system comprising:

a hollow outer tube having an inlet end adapted to be connected to one or more exhaust ports of the internal combustion engine and an outlet end for conducting the exhaust gases to the atmosphere;

the outer tube having an inlet section, an expansion section, a transition section, a reflector section and an outlet section joined together in sequence and providing for continuous flow of the exhaust through the sections;

the inlet section of the outer tube being of uniform diameter along its length, the expansion section gradually increasing in diameter along its length until its joinder with the transition section, the transition section being of a uniform diameter along its length, the reflector section gradually decreasing in diameter along its length from the transition section until its joinder with the outlet section, the outlet section being of uniform diameter along its length; and

a first hollow inner tube positioned fully inside the outer tube and having an open inlet end and an open outlet end, the first hollow inner tube forming annular chambers with the outer tube through at least one of the transition, reflector and outlet sections of the outer tube so that the radial distance between the inner tube and outer tube at any given point along the length of at least one of the transition, reflector and outlet sections of the outer tube remains the same, whereby the exhaust gases can flow though the chambers.

2. The exhaust system of claim 1 in which a second hollow inner tube is positioned fully inside the first inner tube, the second inner tube having an open inlet end and an open outlet end and forming annular chambers with the first inner tube through at least the transition, reflector and outlet sections of the first inner tube.

3. The exhaust system of claim 2 in which the second inner tube is configured with sections comparable to the sections of the first inner tube so as to form annular chambers between the sections of the second inner tube and the first inner tube which chambers are uniform in size along their lengths.

4. The exhaust system of claim 2 in which an exhaust tube is combined with the outlet end of the first inner tube to conduct the exhaust gases in the first inner tube directly to the atmosphere.

5. The exhaust system of claim 1 in which the first inner tube forms annular chambers with the outer tube through all of the inlet section, the expansion section, the transition section, the reflector section and the outlet section.

6. The exhaust system of claim 5 in which the first hollow inner tube is configured with sections comparable to the sections of the outer tube so as to form annular chambers between the sections of the outer tube and the first inner tube which chambers are uniform in size along their lengths.

7. The exhaust system of claim 5 in which a second hollow inner tube is positioned fully inside the first inner tube, the second inner tube having an open′ inlet end and an open outlet end and forming annular chambers with the first inner tube through the inlet section, the expansion section, the transition section, the reflector section, and the outlet section of the first inner tube.

Continuity (2)
Provisional Application 61562792 · Nov 22, 2011
Related Publication 20130125535A1 · May 23, 2013