Main Page: Difference between revisions

From formulasearchengine
Jump to navigation Jump to search
mNo edit summary
No edit summary
 
(725 intermediate revisions by more than 100 users not shown)
Line 1: Line 1:
{{thermodynamics|cTopic=Processes and Cycles}}
This is a preview for the new '''MathML rendering mode''' (with SVG fallback), which is availble in production for registered users.
<!-- BEFORE EDITING THIS PAGE:
    Note that there is a separate page on the Diesel *engine*.
    If you are going to describe glow plugs, differences between fuels, use in
    trucks etc, that is the place for your contribution. -->
The '''Diesel cycle''' is a combustion process of a reciprocating [[internal combustion engine]]. In it, [[fuel]] is ignited by heat generated during the compression of air in the combustion chamber, into which fuel is then injected. This is in contrast to igniting the fuel-air mixture with a [[spark plug]] as in the [[Otto cycle]] (four-stroke/petrol) engine. Diesel engines ([[heat engine]]s using the Diesel cycle) are used in [[automobile]]s, [[power generation]], [[Diesel-electric transmission|diesel-electric]] [[locomotive]]s, and [[submarines]]. {{dubious|date=November 2014}}


The [[thermodynamic cycle]] which approximates the Diesel cycle [[pressure]] and [[Volume (thermodynamics)|volume]] of the [[combustion chamber]] of the [[diesel engine]], was invented by [[Rudolph Diesel]] in 1897. It is assumed to have constant pressure during the initial part of the "combustion" phase (<math>V_2</math> to <math>V_3</math> in the diagram, below). This is an idealized mathematical model: real physical diesels do have an increase in pressure during this period, but it is less pronounced than in the Otto cycle. In contrast, the idealized [[Otto cycle]] of a [[four-stroke cycle|gasoline engine]] approximates a constant volume process during that phase.
If you would like use the '''MathML''' rendering mode, you need a wikipedia user account that can be registered here [[https://en.wikipedia.org/wiki/Special:UserLogin/signup]]
* Only registered users will be able to execute this rendering mode.
* Note: you need not enter a email address (nor any other private information). Please do not use a password that you use elsewhere.


== The Idealized Diesel Cycle ==
Registered users will be able to choose between the following three rendering modes:  
[[Image:DieselCycle PV.svg|thumb|300px|left|p-V Diagram for the ideal Diesel cycle. The cycle follows the numbers 1-4 in clockwise direction.]]


The image on the left shows a p-V diagram for the ideal Diesel cycle; where <math>p</math> is [[pressure]] and V the volume or <math>v</math> the [[specific volume]] if the process is placed on a unit mass basis. The ideal Diesel cycle follows the following four distinct processes:
'''MathML'''
:<math forcemathmode="mathml">E=mc^2</math>


* Process 1 to 2 is [[isentropic]] compression of the fluid (blue)
<!--'''PNG'''  (currently default in production)
* Process 2 to 3 is [[Reversible process (thermodynamics)|reversible]] constant pressure heating (red)
:<math forcemathmode="png">E=mc^2</math>
* Process 3 to 4 is isentropic expansion (yellow)
* Process 4 to 1 is reversible constant volume cooling (green)<ref>Eastop & McConkey 1993, ''Applied Thermodynamics for Engineering Technologists'', Pearson Education Limited, Fifth Edition, p.137</ref>


The Diesel engine is a heat engine: it converts [[heat]] into [[Work (thermodynamics)|work]].  During the bottom isentropic processes (blue), energy is transferred into the system in the form of work <math>W_{in}</math>, but by definition (isentropic) no energy is transferred into or out of the system in the form of heat. During the constant pressure (red, [[isobaric process |isobaric]]) process, energy enters the system as heat <math>Q_{in}</math>. During the top isentropic processes (yellow), energy is transferred out of the system in the form of <math>W_{out}</math>, but by definition (isentropic) no energy is transferred into or out of the system in the form of heat. During the constant volume (green, [[isochoric process|isochoric]]) process, some of energy flows out of the system as heat through the right depressurizing process <math>Q_{out}</math>. The work that leaves the system is equal to the work that enters the system plus the difference between the heat added to the system and the heat that leaves the system; in other words, net gain of work is equal to the difference between the heat added to the system and the heat that leaves the system.
'''source'''
:<math forcemathmode="source">E=mc^2</math> -->


* Work in (<math>W_{in}</math>) is done by the piston compressing the air (system)
<span style="color: red">Follow this [https://en.wikipedia.org/wiki/Special:Preferences#mw-prefsection-rendering link] to change your Math rendering settings.</span> You can also add a [https://en.wikipedia.org/wiki/Special:Preferences#mw-prefsection-rendering-skin Custom CSS] to force the MathML/SVG rendering or select different font families. See [https://www.mediawiki.org/wiki/Extension:Math#CSS_for_the_MathML_with_SVG_fallback_mode these examples].
* Heat in (<math>Q_{in}</math>) is done by the [[combustion]] of the fuel
* Work out (<math>W_{out}</math>) is done by the working fluid expanding and pushing a piston (this produces usable work)
* Heat out (<math>Q_{out}</math>) is done by venting the air
* Net work produced = <math>Q_{in}</math> - <math>Q_{out}</math>


The net work produced is also represented by the area enclosed by the cycle on the P-V diagram. The net work is produced per cycle and is also called the useful work, as it can be turned to other useful types of energy and propel a vehicle ([[kinetic energy]]) or produce electrical energy. The summation of many such cycles per unit of time is called the developed power. The <math>W_{out}</math> is also called the gross work, some of which is used in the next cycle of the engine to compress the next charge of air.
==Demos==


Here are some [https://commons.wikimedia.org/w/index.php?title=Special:ListFiles/Frederic.wang demos]:


{{clear}}


=== Maximum thermal efficiency ===
* accessibility:
The maximum thermal efficiency of a Diesel cycle is dependent on the compression ratio and the cut-off ratio. It has the following formula under cold [[Standard state|air standard]] analysis:  
** Safari + VoiceOver: [https://commons.wikimedia.org/wiki/File:VoiceOver-Mac-Safari.ogv video only], [[File:Voiceover-mathml-example-1.wav|thumb|Voiceover-mathml-example-1]], [[File:Voiceover-mathml-example-2.wav|thumb|Voiceover-mathml-example-2]], [[File:Voiceover-mathml-example-3.wav|thumb|Voiceover-mathml-example-3]], [[File:Voiceover-mathml-example-4.wav|thumb|Voiceover-mathml-example-4]], [[File:Voiceover-mathml-example-5.wav|thumb|Voiceover-mathml-example-5]], [[File:Voiceover-mathml-example-6.wav|thumb|Voiceover-mathml-example-6]], [[File:Voiceover-mathml-example-7.wav|thumb|Voiceover-mathml-example-7]]
** [https://commons.wikimedia.org/wiki/File:MathPlayer-Audio-Windows7-InternetExplorer.ogg Internet Explorer + MathPlayer (audio)]
** [https://commons.wikimedia.org/wiki/File:MathPlayer-SynchronizedHighlighting-WIndows7-InternetExplorer.png Internet Explorer + MathPlayer (synchronized highlighting)]
** [https://commons.wikimedia.org/wiki/File:MathPlayer-Braille-Windows7-InternetExplorer.png Internet Explorer + MathPlayer (braille)]
** NVDA+MathPlayer: [[File:Nvda-mathml-example-1.wav|thumb|Nvda-mathml-example-1]], [[File:Nvda-mathml-example-2.wav|thumb|Nvda-mathml-example-2]], [[File:Nvda-mathml-example-3.wav|thumb|Nvda-mathml-example-3]], [[File:Nvda-mathml-example-4.wav|thumb|Nvda-mathml-example-4]], [[File:Nvda-mathml-example-5.wav|thumb|Nvda-mathml-example-5]], [[File:Nvda-mathml-example-6.wav|thumb|Nvda-mathml-example-6]], [[File:Nvda-mathml-example-7.wav|thumb|Nvda-mathml-example-7]].
** Orca: There is ongoing work, but no support at all at the moment [[File:Orca-mathml-example-1.wav|thumb|Orca-mathml-example-1]], [[File:Orca-mathml-example-2.wav|thumb|Orca-mathml-example-2]], [[File:Orca-mathml-example-3.wav|thumb|Orca-mathml-example-3]], [[File:Orca-mathml-example-4.wav|thumb|Orca-mathml-example-4]], [[File:Orca-mathml-example-5.wav|thumb|Orca-mathml-example-5]], [[File:Orca-mathml-example-6.wav|thumb|Orca-mathml-example-6]], [[File:Orca-mathml-example-7.wav|thumb|Orca-mathml-example-7]].
** From our testing, ChromeVox and JAWS are not able to read the formulas generated by the MathML mode.


<math>\eta_{th}=1-\frac{1}{r^{\gamma-1}}\left ( \frac{\alpha^{\gamma}-1}{\gamma(\alpha-1)} \right )</math>
==Test pages ==


where
To test the '''MathML''', '''PNG''', and '''source''' rendering modes, please go to one of the following test pages:
:<math>\eta_{th} </math> is [[thermal efficiency]]
*[[Displaystyle]]
:<math>\alpha</math> is the cut-off ratio <math>\frac{V_3}{V_2}</math> (ratio between the end and start volume for the combustion phase)
*[[MathAxisAlignment]]
:{{math|r}} is the [[compression ratio]] <math>\frac{V_1}{V_2}</math>
*[[Styling]]
:<math>\gamma </math> is ratio of [[specific heat capacity|specific heats]] (C<sub>p</sub>/C<sub>v</sub>)<ref>[http://230nsc1.phy-astr.gsu.edu/hbase/thermo/diesel.html The Diesel Engine]</ref>
*[[Linebreaking]]
*[[Unique Ids]]
*[[Help:Formula]]


The cut-off ratio can be expressed in terms of temperature as shown below:
*[[Inputtypes|Inputtypes (private Wikis only)]]
:<math>\frac{T_2}{T_1} ={\left(\frac{V_1}{V_2}\right)^{\gamma-1}} = r^{\gamma-1}</math>
*[[Url2Image|Url2Image (private Wikis only)]]
 
==Bug reporting==
:<math> \displaystyle {T_2} ={T_1} r^{\gamma-1} </math>
If you find any bugs, please report them at [https://bugzilla.wikimedia.org/enter_bug.cgi?product=MediaWiki%20extensions&component=Math&version=master&short_desc=Math-preview%20rendering%20problem Bugzilla], or write an email to math_bugs (at) ckurs (dot) de .
 
:<math>\frac{V_3}{V_2} = \frac{T_3}{T_2}</math>
 
:<math>\alpha = \left(\frac{T_3}{T_1}\right)\left(\frac{1}{r^{\gamma-1}}\right)</math>
 
<math>T_3</math> can be approximated to the flame temperature of the fuel used. The flame temperature can be approximated to the [[adiabatic flame temperature]] of the fuel with corresponding air-to-fuel ratio and compression pressure, <math>p_3</math>.
<math>T_1</math> can be approximated to the inlet air temperature.
 
This formula only gives the ideal thermal efficiency. The actual thermal efficiency will be significantly lower due to heat and friction losses. The formula is more complex than the Otto cycle (petrol/gasoline engine) relation that has the following formula;
 
<math>\eta_{otto,th}=1-\frac{1}{r^{\gamma-1}}</math>
 
The additional complexity for the Diesel formula comes around since the heat addition is at constant pressure and the heat rejection is at constant volume. The Otto cycle by comparison has both the heat addition and rejection at constant volume.
 
Comparing the two formulae it can be seen that for a given compression ratio ({{math|r}}), the ideal Otto cycle will be more efficient. However, a [[diesel engine]] will be more efficient overall since it will have the ability to operate at higher compression ratios.  If a petrol engine were to have the same compression ratio, then knocking (self-ignition) would occur and this would severely reduce the efficiency, whereas in a diesel engine, the self ignition is the desired behavior.  Additionally, both of these cycles are only idealizations, and the actual behavior does not divide as clearly or sharply.  And the ideal Otto cycle formula stated above does not include throttling losses, which do not apply to diesel engines.
 
== Applications ==
===Diesel engines ===
{{main|Diesel engine}}
Diesel engines have the lowest [[specific fuel consumption (shaft engine)|specific fuel consumption]] of any large internal combustion engine employing a single cycle, 0.26&nbsp;lb/hp·h (0.16&nbsp;kg/kWh) for very large marine engines (combined cycle power plants are more efficient, but employ two engines rather than one). Two-stroke diesels with high pressure forced induction, particularly [[turbocharging]], make up a large percentage of the very largest diesel engines.
 
In [[North America]], diesel engines are primarily used in large trucks, where the low-stress, high-efficiency cycle leads to much longer engine life and lower operational costs. These advantages also make the diesel engine ideal for use in the heavy-haul railroad environment.
 
=== Other internal combustion engines without spark plugs ===
Many [[model airplane]]s use very simple "glow" and "diesel" engines.  Glow engines use [[glow plug]]s.  "Diesel" model airplane engines have variable compression ratios.  Both types depend on special fuels.
 
Some 19th-century or earlier experimental engines used external flames, exposed by valves, for ignition, but this becomes less attractive with increasing compression.  (It was the research of [[Nicolas Léonard Sadi Carnot]] that established the thermodynamic value of compression.) A historical implication of this is that the diesel engine could have been invented without the aid of electricity.
<br /> See the development of the  [[hot bulb engine]] and [[indirect injection]] for historical significance.
 
== References ==
<references/>
 
== See also ==
* [[Diesel engine]]
* [[Hot bulb engine]]
* [[Mixed/dual cycle]]
{{Thermodynamic cycles|state=uncollapsed}}
 
{{DEFAULTSORT:Diesel Cycle}}
[[Category:Thermodynamic cycles]]

Latest revision as of 23:52, 15 September 2019

This is a preview for the new MathML rendering mode (with SVG fallback), which is availble in production for registered users.

If you would like use the MathML rendering mode, you need a wikipedia user account that can be registered here [[1]]

  • Only registered users will be able to execute this rendering mode.
  • Note: you need not enter a email address (nor any other private information). Please do not use a password that you use elsewhere.

Registered users will be able to choose between the following three rendering modes:

MathML


Follow this link to change your Math rendering settings. You can also add a Custom CSS to force the MathML/SVG rendering or select different font families. See these examples.

Demos

Here are some demos:


Test pages

To test the MathML, PNG, and source rendering modes, please go to one of the following test pages:

Bug reporting

If you find any bugs, please report them at Bugzilla, or write an email to math_bugs (at) ckurs (dot) de .