Design and Analysis of Wind Speeds and Pressure on the Inlet of the CMF56-7B Engine to Enhance Performance
Disciplines
Aerodynamics and Fluid Mechanics | Computer-Aided Engineering and Design | Propulsion and Power
Abstract (300 words maximum)
The CMF56-7B, a high-bypass turbofan engine developed by CFM International in collaboration with General Electric and Safran Aircraft Engines, represents a cornerstone in modern aviation propulsion, extensively powering aircraft models like the Airbus A320, Boeing 737 NG, and Embraer E-Jet families. The aviation industry is grappling with multifaceted challenges, including those related to environmental sustainability, rising fuel costs, and higher competitiveness. Continuous improvements in aircraft and engine economy are essential to meet these challenges. The objective of the research is to identify opportunities to enhance the performance and efficiency of the CMF56-7B engine, one of the most popular engines in the market. With the intention of modifying the inlet's profile to increase pressure inside the intake, an examination of wind speeds and pressure on the CMF56-7B engine's inlet is presented. The efficiency and performance of the engine can be increased by optimizing the airflow through the inlet, which can result in less fuel being used and fewer pollutants. The size and shape of the inlet nacelle are modified in this research. The goal is to determine the optimal combination of these parameters that will help maximize the air pressure before the compressor. This will help increase inlet and compressor efficiency and overall engine performance. Anyone concerned with the design and upkeep of aircraft propulsion systems, including aerospace engineers, aircraft manufacturers, and others, will be interested in the conclusions of this paper. The knowledge gained from this research will help to enhance aeronautics technology and open the door for future air travel that is more efficient and sustainable.
Academic department under which the project should be listed
SPCEET - Mechanical Engineering
Primary Investigator (PI) Name
Adeel Khalid
Design and Analysis of Wind Speeds and Pressure on the Inlet of the CMF56-7B Engine to Enhance Performance
The CMF56-7B, a high-bypass turbofan engine developed by CFM International in collaboration with General Electric and Safran Aircraft Engines, represents a cornerstone in modern aviation propulsion, extensively powering aircraft models like the Airbus A320, Boeing 737 NG, and Embraer E-Jet families. The aviation industry is grappling with multifaceted challenges, including those related to environmental sustainability, rising fuel costs, and higher competitiveness. Continuous improvements in aircraft and engine economy are essential to meet these challenges. The objective of the research is to identify opportunities to enhance the performance and efficiency of the CMF56-7B engine, one of the most popular engines in the market. With the intention of modifying the inlet's profile to increase pressure inside the intake, an examination of wind speeds and pressure on the CMF56-7B engine's inlet is presented. The efficiency and performance of the engine can be increased by optimizing the airflow through the inlet, which can result in less fuel being used and fewer pollutants. The size and shape of the inlet nacelle are modified in this research. The goal is to determine the optimal combination of these parameters that will help maximize the air pressure before the compressor. This will help increase inlet and compressor efficiency and overall engine performance. Anyone concerned with the design and upkeep of aircraft propulsion systems, including aerospace engineers, aircraft manufacturers, and others, will be interested in the conclusions of this paper. The knowledge gained from this research will help to enhance aeronautics technology and open the door for future air travel that is more efficient and sustainable.