Infinite photos and videos for every Wiki article · Find something interesting to watch in seconds
History
Page
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
Page
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.