Macroeconomics

Fuel efficiency

Gas compressor

World Wide Web

Engineering

Ecology

Aerospace engineering

Biology

Sustainability

Exergy efficiency

Operating system

Turbofan

Economics

Computer science

Waste management

Mechanical engineering

Environmental engineering

Organic chemistry

Index (typography)

Aviation

Thrust specific fuel consumption

Combustion

Productivity

Automotive engineering

Environmental science

Environmental Sustainability Index

Chemistry

Idle

Exergy

Energy

In this paper, JT15D turbofan engine and its main subcomponents are assessed with the aviation, energy, exergy, environmental, and sustainability analyses. In the first stage, the system's specific thrust and specific fuel consumption of the engine are found as 315.9 N s/kg and 15.8 g/kN.s, respectively. Then, system's energetic efficiency is estimated as 21.15% and exergetic efficiency is accounted to be 19.919%. The system's exergetic improvement potential rate, productivity lack ratio and fuel exergy waste ratio are determined as 1573.535 kW, 402.024% and 80.081%, respectively. The ecological and environmental effect factors of the turbofan system are computed to be 5.020 and 4.020, respectively, while the sustainable efficiency factor and exergetic sustainability index rates are found as 1.249 and 0.249, respectively. Finally, among the system parts, the Combustion Chamber (CC) has minimum rates of sustainable efficiency factor, exergetic efficiency and sustainability index, while it has utmost rates of ecological and environmental effect factors, fuel exergy waste ratio, irreversibility and productivity lack ratios. As a general conclusion, the combustion chamber and low pressure compressor components should be optimized for better performance of the system.

Turbofan engine performances from aviation, thermodynamic and environmental perspectives