Rolls-Royce RB.183 Tay

Turbofan · Rolls-Royce

Maximum Takeoff Thrust

63 kN

Bypass Ratio

3.04

Diameter

1117.6 mm

Length

2405.38 mm

Dry Weight

1501.391 kg

Thrust To Weight

4.2

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 10 can-annular combustion chambers
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 3.04	Overall Pressure Ratio —	Afterburner No

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Name	Aircraft Engine	Number of Engines	Length (m)	Flat Wing Span (m)	Max Seating
Fokker 70	Rolls-Royce RB.183 Tay	2	30.91	28.08
Gulfstream IV	Rolls-Royce RB.183 Tay		26.8224	23.4696	19
Gulfstream X-54	Rolls-Royce RB.183 Tay	2

Name	Aircraft Engine Manufacturer	Maximum Takeoff Thrust (kN)	Bypass Ratio	Overall Pressure Ratio
TAY Mk611-8	Rolls-Royce	61.6	3	16.1	Compare
TAY Mk620-15	Rolls-Royce	61.6	3	16.1	Compare
TAY 611-8C	Rolls-Royce	61.61	3.2	15.75	Compare
TAY611-8C	Rolls-Royce	61.6	3.26	15.88	Compare
TAY 650	Rolls-Royce	67.2	3	15.9	Compare
TAY Mk650-15	Rolls-Royce	67.2	3	16.4	Compare

All data (16 fields)

Name: Rolls-Royce RB.183 Tay
Aircraft Engine Manufacturer: Rolls-Royce
Aircraft Engine Type: Turbofan
Dry Weight (kg): 1501.391
Diameter (mm): 1117.6
Length (mm): 2405.38
Wikipedia Article (URL): en.wikipedia.org/wiki/Rolls-Royce_RB.183_Tay
Geared Fan: No
Combustion Chamber: 10 can-annular combustion chambers
Afterburner: No
Streams: 2
Bypass Ratio: 3.04
Maximum Takeoff Thrust (kN): 63
Thrust To Weight: 4.2
Compressor Description: Single-stage fan plus a 3-stage IP compressor (Same shaft.) and a 12-stage HP compressor
Turbine Description: 2 stage HP turbine, 3 stage LP turbine