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

Why are the external surfaces of a lawn mower engine covered with fins?

Short Answer

Expert verified
Fins increase surface area for heat dissipation, preventing engine overheating and ensuring reliable performance.

Step by step solution

01

- Understand the Role of the Fins

Fins are extensions on the surface of an engine. They are designed to increase the surface area available for heat dissipation.
02

- Explain Heat Dissipation

When the engine operates, it generates heat. The fins help in transferring this heat from the engine to the air, thus keeping the engine at an optimal temperature.
03

- Reasons for Efficient Cooling

Efficient cooling is crucial to maintain the engine's performance and longevity. Overheating can damage engine components and reduce efficiency.
04

- Convection Process

The heat dissipation process mainly happens through convection, where heat is transferred from the fins to the moving air around them.
05

- Practical Impact

By preventing overheating, the fins ensure that the lawn mower engine runs smoothly, providing reliable performance and reducing the risk of wear and tear.

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!

Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Engine Cooling Mechanisms
In engines, heat is generated whenever they operate due to combustion or friction. To ensure the engine remains efficient and does not overheat, cooling mechanisms are essential. One simple yet effective cooling mechanism is the use of fins. These fins are designed to extend from the main body of the engine, increasing the surface area for cooling.

Fins work by providing a larger area for heat to escape from the engine to the surrounding air. Overheating can lead to significant damage to engine parts and decrease the overall efficiency. Therefore, mechanisms like fins play a crucial role in maintaining engine health and performance. They are a passive cooling method—meaning they don't require additional energy to function, unlike active cooling systems like fans or coolant circulation.
Heat Transfer
Heat transfer is the process of moving heat from one place to another. In the case of engines, it's moving heat generated inside the engine to the outside environment. This process can occur in three ways: conduction, convection, and radiation. Conduction involves heat transfer through direct contact, like how heat moves through metal. Radiation is heat transfer through electromagnetic waves, like the heat from the sun.

However, in engines, convection is the primary method of heat dissipation. The fins on the lawn mower engine enhance this process significantly. By increasing the surface area, more heat can escape into the surrounding air, effectively cooling the engine. This principle of heat transfer is essential for all types of engine cooling mechanisms.
Convection Process
Convection is a type of heat transfer that occurs through the movement of fluids, which can be either liquids or gases. In the context of a lawn mower engine, the fluid is the air surrounding the engine. When the engine generates heat, the fins on its surface heat up. The heated fins then transfer heat to the cooler air around them.

As the air close to the engine becomes warm, it rises and is replaced by cooler air from the surroundings. This continuous flow of air around the fins helps to dissipate the heat away from the engine. This natural movement of air due to temperature differences is why an understanding of convection is critical in designing efficient engine cooling systems. The fins maximize the convection process, ensuring the engine remains at a safe operational temperature.

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

Air enters the diffuser of a ramjet engine at \(40 \mathrm{kPa}, 240 \mathrm{~K}\), with a velocity of \(2500 \mathrm{~km} / \mathrm{h}\) and decelerates to negligible velocity. On the basis of an air-standard analysis, the heat addition is \(1080 \mathrm{~kJ}\) per \(\mathrm{kg}\) of air passing through the engine. Air exits the nozzle at \(40 \mathrm{kPa}\). Determine (a) the pressure at the diffuser exit, in \(\mathrm{kPa}\). (b) the velocity at the nozzle exit, in \(\mathrm{m} / \mathrm{s}\). Neglect kinetic energy except at the diffuser inlet and the nozzle exit.

Consider an ideal air-standard Brayton cycle with minimum and maximum temperatures of \(300 \mathrm{~K}\) and \(1500 \mathrm{~K}\), respectively. The pressure ratio is that which maximizes the net work developed by the cycle per unit mass of air flow. On a cold air-standard basis, calculate (a) the compressor and turbine work per unit mass of air flow, each in \(\mathrm{kJ} / \mathrm{kg}\). (b) the thermal efficiency of the cycle. (c) Plot the thermal efficiency versus the maximum cycle temperature ranging from 1200 to \(1800 \mathrm{~K}\).

A two-stage air compressor operates at steady state, compressing \(10 \mathrm{~m}^{3} / \mathrm{min}\) of air from \(100 \mathrm{kPa}, 300 \mathrm{~K}\), to \(1200 \mathrm{kPa}\). An intercooler between the two stages cools the air to \(300 \mathrm{~K}\) at a constant pressure of \(350 \mathrm{kPa}\). The compression processes are isentropic. Calculate the power required to run the compressor, in \(\mathrm{kW}\), and compare the result to the power required for isentropic compression from the same inlet state to the same final pressure.

The inlet to a gas turbine aircraft engine must provide air to the compressor with as little a drop in stagnation pressure and with as small a drag force on the aircraft as possible. The inlet also serves as a diffuser to raise the pressure of the air entering the compressor while reducing the air velocity. Write a paper discussing the most common types of inlet designs for subsonic and supersonic applications. Include a discussion of how engine placement affects diffuser performance.

Using Interactive Thermodynamics: \(I T\), generate tables of the same normal shock functions as in Table \(9.2\) for specific heat ratios of \(1.2,1.3,1.4\), and \(1.67\) and Mach numbers ranging from 1 to 5

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