AIRCRAFT ENGINE DEVELOPMENTS CENTRE ON IMPROVED PERFORMANCE, HIGHER EFFICIENCY
William H. Sens
Abstract
William H. Sens
Abstract
Means are described of improving the fuel consumption of current engines by as much as 5 percent through improved component performance and reduced engine deterioration. The advanced turbofan configuration, however, has the potential of providing a 20 percent reduction in fuel burned relative to todays designs for high bypass ration turbofans for 1990. Modifications to the JT8D and JT9D engines which improve their fuel consumption are described. Comments are also made on Pratt and Whitney's long term turbofan engine technology development. The optimum direct operating costs are also discussed.
A significance statement is not available in the OpenAlex record.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
Means are described of improving the fuel consumption of current engines by as much as 5 percent through improved component performance and reduced engine deterioration. The advanced turbofan configuration, however, has the potential of providing a 20 percent reduction in fuel burned relative to todays designs for high bypass ration turbofans for 1990. Modifications to the JT8D and JT9D engines which improve their fuel consumption are described. Comments are also made on Pratt and Whitney's long term turbofan engine technology development. The optimum direct operating costs are also discussed.
Key concepts: Turbofan, Fuel efficiency, Automotive engineering, Thrust specific fuel consumption, Engineering, Environmental science