The Expansion Chamber Designing ( TRY YOU OWN )

 

Description:

The expansion chamber design software is used to design the tuned pipe for the exhaust system of the micro car engine. One can choose to design a single stage, two-stage or a three-stage diffuser chamber according to their requirements. This section details the various parameters and design formulae, which have been implemented in the software design project.

Sections of a Tuned Pipe:

Header - Attaches to the engine and is the straight or slightly divergent (opens up 2-3 degrees) section of the pipe. It helps to suck the exhaust gases out of the engine. The header pipe cross-sectional area should be 10-15% greater than the exhaust port window for when maximum output at maximum RPM's is desired. In some cases the area of the header pipe may have a cross-sectional area 150% of the exhaust port area. The length should be 6-8 of its diameters for maximum horsepower, for a broader power curve 11 times pipe diameter may be used. The part you trim off to tune.

Divergent (Diffuser) Cone - The section of the pipe that attaches to the header and opens up at an angle like a megaphone. It intensifies and lengthens the returning sound waves thus broadening the power curve. The steeper the angle the more intense the negative wave returns, but also the shorter the duration. The lesser the angle, of course, returns a less intense wave, but for a longer period of time (duration). The outlet area should be 6.25 times the inlet area. 7-10 degree taper angle.

Belly - Located between the divergent and convergent cones, it's length determines the relative timing of the negative and positive waves. The shorter the belly the shorter the distance positive waves travel and the narrower the RPM range. This is good for operating at HIGH RPM only. The longer the belly the broader the RPM range. The diameter of the belly has little or no effect.

Convergent (Baffle) Cone - Located after the belly and before the stinger, reflects the positive waves back to the open exhaust port and forces the fresh fuel mixture back into the combustion chamber as the exhaust port closes. The steeper the angle the more intense the positive wave and the gentler the angle the less intense. 14-20 degree taper angle. The taper angle primarily influences the shape of the power curve past the point at which maximum power is obtained.

Stinger - Located at the opposite end of the pipe from the header and after the convergent cone, it is the "pressure relief valve" of the pipe where the exhaust gasses eventually leave the pipe. The back pressure in the pipe is caused by the size (diameter) or length of the stinger. A smaller stinger causes more back pressure and thus a denser medium for the sound waves to travel in. Sound waves love denser mediums and thus travel better. A draw back to a small stinger is heat build up in the pipe and engine. The stinger diameter should be 0.58--0.62 times that of the header pipe and a length equal to 12 of it's own diameters.

When the engine fires it detonates the fuel mixture in the combustion chamber, pushes the piston down, opens the exhaust port and allows the burnt gases to escape along with the sound wave produced when the engine fired. The negative sound waves pull the exhaust gasses out of the exhaust port. The positive sound waves, reflected back from the convergent (baffle) cone, force the fresh fuel mixture back into the combustion chamber through the exhaust port thus super-charging your engine.

Common Engine Parameters to be calculated:

BMEP =

Average Exhaust Temperature based on BMEP

BMEP, bar	Avg. Exhaust Temp
11 +	650
8	500
9-10	600
5	350

Speed of Sound A₀ =

Where g is specific heat ratio of air i.e. 1.4

R is the Gas Constant of air i.e. 287

T_exc is exhaust gas temperature

The values for k₁ and k ₂ are ranges depending on the type of engine. k₁ ranges from 1.05 to 1.125 while k ₂ ranges from 2.125 to 3.25.

Finally the tuned length

L_{t =}

Where q _ep is exhaust port open duration in degrees

Single Stage Diffuser Expansion Chamber Design:

Design Formulae:

L_t =

Where L_t is tuned length

E_o is exhaust-open period

V_s is sonic wave speed

N is crankshaft speed

L₁ =

L₂ =

L₃ = D₁ x (6 to11)

L₄ =

L₅ = L₁ - (L₃ + L₄)

L₆ =

L₇ = D₃ x 12

D₁ is 10 to 15% greater than exhaust port window

D₂ =

D₃ = D₁ x (0.58 to 0.62)

A₁ = (half the diffuser's angle of divergence)

A2 = (half the baffle-cone's angle of divergence)

Two Stage Diffuser Expansion Chamber Design:

 D₁ = K₁.EXD

D₃ = K₂.EXD

D₄ = K₀.EXD

LP01 = 0.10L_T

LP12 = 0.41L_T

LP23 = 0.14L_T

LP34 = 0.11L_T

LP45 = 0.24L_T

LP56 = LP45

Three Stage Diffuser Expansion Chamber Design:

D₄ = K₂.EXD

D₅ = K₀.EXD

D₁ = K₁.EXD

D₂ =

D₃ =

 Notice also that an extra coefficient has been introduced. This coefficient K_h is called the horn coefficient, with typical values between one and two. Small values of K_h are best suited to Grand Prix engines with narrow power bands, larger values are for wider more flexible engines.

LP01 = 0.10LT
LP12 = 0.275LT
LP23 = 0.183LT
LP34 = 0.092LT
LP45 = 0.11LT
LP56 = 0.24LT
LP67 = LP56  

DOWNLOAD ZIP    :MOTA 2 STROKE EXPANSION DESIGN SOFTWARE:

CONE LAYOUT  ZIP:Cone Layout is a program to unfold a frustum of a cone and generate a sheet cutting layout or flat pattern projection that can be rolled or bend up into a truncated cone shape.( Trial Version)

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