Warning: foreach() argument must be of type array|object, bool given in /var/www/html/web/app/themes/studypress-core-theme/template-parts/header/mobile-offcanvas.php on line 20

Do diesel or gasoline engines operate at higher compression ratios? Why?

Short Answer

Expert verified
Answer: Diesel engines operate at higher compression ratios compared to gasoline engines. This is due to their operational principles (relying on autoignition), better fuel efficiency, and higher resistance to knocking.

Step by step solution

01

Understand the concepts of gasoline and diesel engines

A gasoline engine works with a mixture of fuel and air that is compressed and ignited by a spark from a spark plug. In contrast, a diesel engine uses only air for compression, and the fuel is injected afterward when the air is already compressed and therefore hot enough to ignite the fuel without the need for a spark plug. We need to analyze the differences in their operating principles to understand which engine type has a higher compression ratio.
02

Learn about the compression ratio

The compression ratio in internal combustion engines is the ratio of the maximum volume of the cylinder when the piston is at the bottom of its stroke (BDC) to the minimum volume when the piston is at the top of its stroke (TDC). A higher compression ratio means that the fuel-air mixture or air are compressed more in the cylinder, leading to higher pressure and temperature.
03

Compare compression ratios in both engines

Diesel engines usually have a higher compression ratio compared to gasoline engines. The compression ratios for diesel engines range approximately between 14:1 to 24:1, while gasoline engines have compression ratios ranging from 8:1 to 12:1.
04

Understand the reasons for the difference

The reasons for the higher compression ratio in diesel engines are as follows: 1. Autoignition: Diesel engines rely on the heat generated during compression to ignite the fuel, whereas gasoline engines use a spark plug. Higher compression ratios result in higher temperatures in the cylinder, which is crucial for effective autoignition of the fuel in diesel engines. 2. Fuel efficiency: A higher compression ratio leads to better fuel efficiency, as more energy is extracted from the combustion process. 3. Reducing engine knocking: Diesel fuel has a higher resistance to knocking (premature combustion), allowing for higher compression ratios without causing harmful effects on the engine. In gasoline engines, too high compression ratios can lead to knocking, which can damage the engine. So diesel engines operate at higher compression ratios due to their operational principles, fuel efficiency, and avoiding knocking.

Unlock Step-by-Step Solutions & Ace Your Exams!

  • Full Textbook Solutions

    Get detailed explanations and key concepts

  • Unlimited Al creation

    Al flashcards, explanations, exams and more...

  • Ads-free access

    To over 500 millions flashcards

  • Money-back guarantee

    We refund you if you fail your exam.

Over 30 million students worldwide already upgrade their learning with Vaia!

One App. One Place for Learning.

All the tools & learning materials you need for study success - in one app.

Get started for free

Most popular questions from this chapter

Exhaust gases from the turbine of a simple Brayton cycle are quite hot and may be used for other thermal purposes. One proposed use is generating saturated steam at \(110^{\circ} \mathrm{C}\) from water at \(30^{\circ} \mathrm{C}\) in a boiler. This steam will be distributed to several buildings on a college campus for space heating. A Brayton cycle with a pressure ratio of 6 is to be used for this purpose. Plot the power produced, the flow rate of produced steam, and the maximum cycle temperature as functions of the rate at which heat is added to the cycle. The temperature at the turbine inlet is not to exceed \(2000^{\circ} \mathrm{C}\)

How does the ideal Diesel cycle differ from the ideal Otto cycle?

An ideal diesel engine has a compression ratio of 20 and uses air as the working fluid. The state of air at the beginning of the compression process is \(95 \mathrm{kPa}\) and \(20^{\circ} \mathrm{C}\). If the maximum temperature in the cycle is not to exceed \(2200 \mathrm{K}\) determine \((a)\) the thermal efficiency and \((b)\) the mean effective pressure. Assume constant specific heats for air at room temperature.

A gas-turbine power plant operates on the regenerative Brayton cycle between the pressure limits of 100 and \(700 \mathrm{kPa}\). Air enters the compressor at \(30^{\circ} \mathrm{C}\) at a rate of \(12.6 \mathrm{kg} / \mathrm{s}\) and leaves at \(260^{\circ} \mathrm{C}\). It is then heated in a regenerator to \(400^{\circ} \mathrm{C}\) by the hot combustion gases leaving the turbine. A diesel fuel with a heating value of \(42,000 \mathrm{kJ} / \mathrm{kg}\) is burned in the combustion chamber with a combustion efficiency of 97 percent. The combustion gases leave the combustion chamber at \(871^{\circ} \mathrm{C}\) and enter the turbine whose isentropic efficiency is 85 percent. Treating combustion gases as air and using constant specific heats at \(500^{\circ} \mathrm{C}\), determine (a) the isentropic efficiency of the compressor, ( \(b\) ) the effectiveness of the regenerator, \((c)\) the air-fuel ratio in the combustion chamber, \((d)\) the net power output and the back work ratio, \((e)\) the thermal efficiency, and \((f)\) the second-law efficiency of the plant. Also determine \((g)\) the second-law efficiencies of the compressor, the turbine, and the regenerator, and \((h)\) the rate of the energy flow with the combustion chamber with a combustion efficiency of 97 percent. The combustion gases leave the combustion chamber at \(871^{\circ} \mathrm{C}\) and enter the turbine whose isentropic efficiency is 85 percent. Treating combustion gases as air and using constant specific heats at \(500^{\circ} \mathrm{C}\), determine (a) the isentropic efficiency of the compressor, (b) the effectiveness of the regenerator, (c) the air-fuel ratio in the combustion chamber, \((d)\) the net power output and the back work ratio, \((e)\) the thermal efficiency, and \((f)\) the second-law efficiency of the plant. Also determine \((g)\) the second-law efficiencies of the compressor, the turbine, and the regenerator, and \((h)\) the rate of the energy flow with the combustion gases at the regenerator exit.

Electricity and process heat requirements of a manufacturing facility are to be met by a cogeneration plant consisting of a gas turbine and a heat exchanger for steam production. The plant operates on the simple Brayton cycle between the pressure limits of 100 and 1000 kPa with air as the working fluid. Air enters the compressor at \(20^{\circ} \mathrm{C}\). Combustion gases leave the turbine and enter the heat exchanger at \(450^{\circ} \mathrm{C},\) and leave the heat exchanger of \(325^{\circ} \mathrm{C},\) while the liquid water enters the heat exchanger at \(15^{\circ} \mathrm{C}\) and leaves at \(200^{\circ} \mathrm{C}\) as a saturated vapor. The net power produced by the gas-turbine cycle is \(1500 \mathrm{kW}\). Assuming a compressor isentropic efficiency of 86 percent and a turbine isentropic efficiency of 88 percent and using variable specific heats, determine \((a)\) the mass flow rate of air, \((b)\) the back work ratio and the thermal efficiency, and \((c)\) the rate at which steam is produced in the heat exchanger. Also determine \((d)\) the utilization efficiency of the cogeneration plant, defined as the ratio of the total energy utilized to the energy supplied to the plant.

See all solutions

Recommended explanations on Physics Textbooks

View all explanations

What do you think about this solution?

We value your feedback to improve our textbook solutions.

Study anywhere. Anytime. Across all devices.

Sign-up for free