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Propulsive efficiency comparison for various gas turbine engine configurations. In the 1970s, Hamilton Standard described its propfan as "a small diameter, highly loaded multiple bladed variable pitch propulsor having swept blades with thin advanced airfoil sections, integrated with a nacelle contoured to retard the airflow through the blades thereby reducing compressibility losses and ...
[3] [4] Three broad classes of distributed propulsion system have been identified: [4] Distributed exhaust, such as jet flaps. Multiple discrete propulsors (fans, propellers or jets), which may be powered individually or by remote drive from fewer engines. Cross-flow fans, which are a type of horizontal-axis rotor.
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The axial fan is often contained within a short section of cylindrical ductwork, to which inlet and outlet ducting can be connected. Axial fan types have fan wheels with diameters that usually range from less than a foot (0.3 meters) to over 30 feet (9.1 m), although axial cooling tower fan wheels may exceed 82 feet (25 m) in diameter.
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The core of the NK-93 was to form the foundation of a family of direct-drive turbofans and geared propfans, ranging from 11,000 to 22,000 kilograms-force (24,000 to 49,000 pounds-force; 110 to 220 kilonewtons) in thrust. [9] It was the last major project of Kuznetsov Design Bureau founder Nikolai Dmitriyevich Kuznetsov. [10]
Fan disks must withstand the centrifugal force of the attached fan blades. Because of their size and weight, a failed fan disk can severely damage an aircraft, as happened with United Airlines Flight 232 in 1989. [4] While operating there is increased aerodynamic loading on the fan disk while the fan blade tips are traveling faster than sound. [5]