Cessna fuel systems vs. Piper PA-28 Cherokee’s Fuel Systems

Purpose

Background: Cessna 150’s fuel system

The purpose of the report is to compare Cessna 150’s fuel system with that of Piper PA-28 Cherokee with regards to performance, efficiency, and cost. Both machines are classified as light aircrafts.

Major manufacturers

Piper PA-28 Cherokee’s System: Mechanism Descriptions

Cessna 150’s fuel system

System Appearance

Cessna 150’s fuel tank

Fuel filter used in priming

Cherokee’s fuel tank

fuel system was first designed in 1951 when the production of the aircraft started. It was designed by Reims Aviation. The production of the aircraft’s fuel system was done in the United States.

Cessna 150’s fuel shut-off

Cessna 150’s fuel strainer

Cherokee’s electric fuel pump

The most prominent features of the system include the fuel tanks [1]. They are located in both wings. As such, they assume the design of these structures. The aircraft has larger wings compared to Cessna 150.

The Components of Cessna 150’s Fuel System

Appearance of Cessna 150’s fuel system

The major components of Cessna 150’s fuel system include the right and left fuel tanks, the shut-off valve, the strainer, and the carburetor [3]. Other parts include the intake manifold, the sump trains, and the fuel gauges.

Operations of Cessna 150’s Fuel System

The operation of the system involves drawing fuel from the tanks. The shut-off valve regulates the amount of fuel drawn from the tanks for passage into the engine cylinders. The fuel passing through the shut-off valve moves to the strainer before it is injected into the engine cylinders.

Most of the components of the system are contained in the wings [5]. The fuel tanks are fitted with outlets that lead to the engine. The tanks are designed to fit into the wings of the aircraft. As such, they are shallow and wide in appearance. They are filled through a hole on their top surface.

The Components of Cessna 150’s Fuel System

The major components of Cessna 150’s fuel system include the right and left fuel tanks, the shut-off valve, the strainer, and the carburetor. Other parts include the intake manifold, the sump trains, and the fuel gauges.

Major manufacturers

Operations of Piper PA-28 Cherokee’s System

The tanks act as the storage for the aircraft’s fuel reserve. Each of them has its own gauge to monitor fuel levels [1]. Fuel is normally drawn from the tanks by the pumps. The sump drains play a role in the removal of waste fuel that settles at the bottom of the tanks.

cost of the fuel systems

The estimated cost of the aircraft’s fuel system is US$1000. Most of the cost is related to the purchase of the tanks, which are the major components of the system. Each tank costs US$450.

Reims Aviation and Dawson Aircraft Inc. are involved in the manufacture of the aircraft’s fuel system [5]. Most of the production activities occur within the United States of America.

Piper PA-28 Cherokee’s fuel system

Comparative Analysis

Invention

Operational Goal

Performance

Cost

The tank is the most expensive part of an aircraft’s fuel system. All the other components of the system are attached to the tank.

The fuel system of an aircraft plays a major part in its propulsion. It plays the role of storing and delivering fuel to the engine cylinders.

There is a close relationship between the performance of an aircraft and its fuel system. Cessna 150 carries a considerably smaller amount of fuel compared to Piper PA-28 Cherokee.

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The system was invented in 1960 when the aircraft was first produced [1]. It was invented by the Piper Aircraft in the United States of America

Socio-economic context

The system is associated with efficient use of fuel. As a result, flight costs are reduced, which makes it desirable, especially in relation to private flights.

Cessna fuel systems vs. Piper PA-28 Cherokee’s Fuel Systems