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Pratt & Whitney JT8D
Pratt & Whitney JT8D
Cutaway showing the configuration: twin fan, axial compressor stages, cannular combustors and 4-stage turbine
Cutaway showing the configuration: twin fan, axial compressor stages, cannular combustors and 4-stage turbine
Cannular combustor
Cannular combustor
20 in (510 mm) diameter rotor and bypass stator
20 in (510 mm) diameter rotor and bypass stator
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Chevrons on an Air India Boeing 787 GE GEnx engine
Chevrons on an Air India Boeing 787 GE GEnx engine
Rolls-Royce Conway low-bypass turbofan from a Boeing 707. The bypass air exits from the fins, while the exhaust from the core exits from the central n
Rolls-Royce Conway low-bypass turbofan from a Boeing 707. The bypass air exits from the fins, while the exhaust from the core exits from the central nozzle. This fluted jetpipe design is a noise-reducing method devised by Frederick Greatorex at Rolls-Royce
General Electric GEnx-2B turbofan engine as used on a Boeing 747–8. View into the bypass duct looking forward from the bypass nozzle and showing fan e
General Electric GEnx-2B turbofan engine as used on a Boeing 747–8. View into the bypass duct looking forward from the bypass nozzle and showing fan exit stators/fan blades
The widely produced Pratt & Whitney JT8D used on many early narrowbody jetliners. The fan is located behind the inlet guide vanes.
The widely produced Pratt & Whitney JT8D used on many early narrowbody jetliners. The fan is located behind the inlet guide vanes.