Pratt & Whitney F119

Diameter

965.2 mm

Length

4978.4 mm

Dry Weight

2267.962 kg

Thrust To Weight

5.2

Architecture

Fan	Fan Stages —	Fan Blades —	Fan Technology —	Fan Pressure Ratio —
Gearbox	Geared Fan No	Gear —	Reduction Ratio —
LP compressor	Low-Pressure Compressor Stages —	Low-Pressure Compressor Technology —	BP Compressor Pressure Ratio —
IP compressor	Intermediary-Pressure Compressor Stages —	Intermediary-Pressure Compressor Technology —	IP Compressor Pressure Ratio —
HP compressor	High-Pressure Compressor Stages —	High-Pressure Compressor Technology —	HP Compressor Pressure Ratio —
Combustor	Combustion Chamber Annular combustor
HP turbine	High Pressure Compressor Stages —	High-Pressure Turbine Technology —
IP turbine	Intermediary-Pressure Turbine Stages —	Intermediary-Pressure Turbine Technology —
LP turbine	Low-Pressure Turbine Stages —	Low-Pressure Turbine Technology —
Whole engine	Streams 2	Bypass Ratio —	Overall Pressure Ratio —	Afterburner No

No pictures yet for this family.

Name	Aircraft Engine	Number of Engines	Length (m)	Flat Wing Span (m)
Lockheed Martin F-22 Raptor	Pratt & Whitney F119	2	18.92	13.56

All data (15 fields)

Name: Pratt & Whitney F119
Aircraft Engine Manufacturer: Pratt & Whitney
Aircraft Engine Type: Turbofan
Dry Weight (kg): 2267.962
Diameter (mm): 965.2
Length (mm): 4978.4
Wikipedia Article (URL): en.wikipedia.org/wiki/Pratt_%26_Whitney_F119
Fuel: JP-8
Geared Fan: No
Combustion Chamber: Annular combustor
Afterburner: No
Streams: 2
Thrust To Weight: 5.2
Compressor Description: 3-stage fan, 6-stage high-pressure compressor; Bypass ratio: 0.30:1
Turbine Description: 1-stage high-pressure, 1-stage low-pressure counterrotating turbines; Nozzle: 2-dimensional vectoring convergent-divergent