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I want to share and discuss with every forum posters here a new concept on piston heads, which by the way is not as brainy as you may think.
The new concept is concerned with spark ignition engines. Everybody know that combustion process have two main stages in this kind of engines.
Once the mixture has entered into the chamber with moderate turbulence, the spark ignites it and enhances a premixed flame. The very first instant of ignition is governed by laminar considerations, and it is the so called "laminar" stage. The process of ignition depends upon local thermodynamic variables and has low dependence with turbulence as it was checked by Taylor et al. There is a finite ignition energy threshold which has to be reached by the spark energy inflow in order to burn the mixture. The crank angle occupied by this stage will be [tex] \theta_l[/tex].
Once the ignition has occurred there is a turbulent transportation of the flame to the rest of the chamber. Because of this transportation there are effects of "cyclic dispersions", as the cycles represented in a PV diagram vary continously due to successes and failures of the flame. Each eddie transports the flame to parts where there are reactants. So that, this stage is strongly influenciated by turbulence, and is the so-called "turbulent" stage.
We will call the crank angle occupied by this stage [tex] \theta_t[/tex].
There are many ways of increasing turbulence in order to exploit the combustion process and make it to last the least. Pollutant generation and power bonus would be some of these profits. New concepts, like the GDI Mitshubishi engine makes use of the "tumble" movement of the mixture, designing a piston head which points directly the intake mixture towards the plug.
The turbulence is modified by the angular velocity [tex] n [/tex]. In fact, the more [tex] n [/tex] the more [tex] \theta_t[/tex] but the time of combustion remains the same, so nothing exceptional is achieved.
You may now open the figure attached. I only have drawn a quarter of the piston surface due to the axilsymmetry.
My concept is concerned with the next:
i) the entire piston has two movements: one of spinning around its axis of symmetry and the typical up and down movement.
ii) the head piston is shaped and mechanized in such a form that there are small blades disposed radially. So that, as the piston spins, the flow is forced to swirl, and so increasing strongly the turbulence and mixing.
iii) Therefore, this design has two main consecuences: (a) it increases the global volumetric efficiency because of the suction effect of the blades. Remain that the volumetric efficiency of a heat engine is defined as [tex] \eta_v=m_a / (\rho_{at}Q)[/tex] the quotient between the air mass accepted by the combustion chamber and the reference mass adopted (here it is the multiplication of the atmospheric density and the total volume of the chamber). Such increasing of volumetric efficiency will enhance an increasing of total power, ceteris paribus. (b) It decreases the time of the turbulent stage, because [tex] \theta_t=nt[/tex] and [tex] n [/tex] is constant. This decreasing enhances a less combustion duration, so that the gas expansion stage will take away less power to the chemical reaction. Also, the pollutant generation due to further flame cooling by means of the expansion will not occur, because the flame will end well before the point it nowadays does. More power will be available.
What are your opinions? Negative comments are allowed, only and only if they are not very offensive
.
The new concept is concerned with spark ignition engines. Everybody know that combustion process have two main stages in this kind of engines.
Once the mixture has entered into the chamber with moderate turbulence, the spark ignites it and enhances a premixed flame. The very first instant of ignition is governed by laminar considerations, and it is the so called "laminar" stage. The process of ignition depends upon local thermodynamic variables and has low dependence with turbulence as it was checked by Taylor et al. There is a finite ignition energy threshold which has to be reached by the spark energy inflow in order to burn the mixture. The crank angle occupied by this stage will be [tex] \theta_l[/tex].
Once the ignition has occurred there is a turbulent transportation of the flame to the rest of the chamber. Because of this transportation there are effects of "cyclic dispersions", as the cycles represented in a PV diagram vary continously due to successes and failures of the flame. Each eddie transports the flame to parts where there are reactants. So that, this stage is strongly influenciated by turbulence, and is the so-called "turbulent" stage.
We will call the crank angle occupied by this stage [tex] \theta_t[/tex].
There are many ways of increasing turbulence in order to exploit the combustion process and make it to last the least. Pollutant generation and power bonus would be some of these profits. New concepts, like the GDI Mitshubishi engine makes use of the "tumble" movement of the mixture, designing a piston head which points directly the intake mixture towards the plug.
The turbulence is modified by the angular velocity [tex] n [/tex]. In fact, the more [tex] n [/tex] the more [tex] \theta_t[/tex] but the time of combustion remains the same, so nothing exceptional is achieved.
You may now open the figure attached. I only have drawn a quarter of the piston surface due to the axilsymmetry.
My concept is concerned with the next:
i) the entire piston has two movements: one of spinning around its axis of symmetry and the typical up and down movement.
ii) the head piston is shaped and mechanized in such a form that there are small blades disposed radially. So that, as the piston spins, the flow is forced to swirl, and so increasing strongly the turbulence and mixing.
iii) Therefore, this design has two main consecuences: (a) it increases the global volumetric efficiency because of the suction effect of the blades. Remain that the volumetric efficiency of a heat engine is defined as [tex] \eta_v=m_a / (\rho_{at}Q)[/tex] the quotient between the air mass accepted by the combustion chamber and the reference mass adopted (here it is the multiplication of the atmospheric density and the total volume of the chamber). Such increasing of volumetric efficiency will enhance an increasing of total power, ceteris paribus. (b) It decreases the time of the turbulent stage, because [tex] \theta_t=nt[/tex] and [tex] n [/tex] is constant. This decreasing enhances a less combustion duration, so that the gas expansion stage will take away less power to the chemical reaction. Also, the pollutant generation due to further flame cooling by means of the expansion will not occur, because the flame will end well before the point it nowadays does. More power will be available.
What are your opinions? Negative comments are allowed, only and only if they are not very offensive
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