Rolls-Royce AE 3007

AE 3007

AE 3007 mounted on a Cessna Citation X
Type	Turbofan
National origin	United States
Manufacturer	Allison Engine Company Rolls-Royce North America
First run	1991^[1]
Major applications	Cessna Citation X Embraer ERJ 145 family RQ-4 Global Hawk MQ-4C Triton

The Rolls-Royce AE 3007 is a high-bypass turbofan engine produced by Rolls-Royce. In military service it is designated as F137.

Design and development

The engine was initially developed by the Allison Engine Company for use on the Cessna Citation X. The engine provides up to 9,440 lbf (42 kN) of thrust. It consists of a fan, 14-stage high-pressure compressor, 2-stage high-pressure turbine and 3-stage low-pressure turbine. It shares a common core with the AE 1107C-Liberty and AE 2100.

Variants

AE 3007C, C1, C2 for the Cessna Citation X
AE 3007H (F137) for the Northrop Grumman GlobalHawk and Triton
AE 3007A, A1, A1/1, A1/3, A3, A1P, A1E, A2 for the Embraer ERJ Family of Jets

Applications

Rolls-Royce AE 3007 installed on a Cessna Citation X undergoing maintenance

A Rolls-Royce AE 3007 installed on an Embraer ERJ 145

Specifications (AE 3007)

Data from

General characteristics

Type: Turbofan
Length: 106.5 in (2,705 mm)
Diameter: 38.5 in (978 mm)
Dry weight: 1,585 lb (719 kg)

Components

Compressor: 14-stage high pressure axial compressor and single-stage fan
Turbine: 2-stage high pressure and 3-stage low pressure

Performance

Maximum thrust: 6,495–9,440 lbf (28.9–42.0 kN)
Overall pressure ratio: 18–20:1
Bypass ratio: 5.1^[1]
Air mass flow: 240–280 lb/s (109–127 kg/s)
Turbine inlet temperature: 994℃
Thrust-to-weight ratio: : 4.1–5.6

References

1 2 "Baby big fan". Flight Global. 10 April 1996.

Leyes II, Richard A.; William A. Fleming (1999). The History of North American Small Gas Turbine Aircraft Engines. Washington, DC: Smithsonian Institution. ISBN 1-56347-332-1.

External links

Wikimedia Commons has media related to Rolls-Royce AE 3007.

Rolls-Royce plc aero engines
Turbofans	Advance 2 Advance 3 AE 3007 BR700† EJ200† F136† RB183 RB282 RB401 RJ500† Spey Junior Tay Trent series (Trent 500 Trent 700 Trent 800 Trent 900 Trent 1000 Trent XWB Trent 7000) V2500
Turboprops/Turboshafts	501 AE 2100 M250 MTR390† RR300 RR500 T56 T406 T800† TP400†
Other fan-type engines	RB2011 RB3011 LiftSystem
Aero-derivative industrial and marine engines	Gas turbines: MT30 MT7 WR-21
† Joint development aero engines See also Rolls-Royce Limited aero engines

United States military gas turbine aircraft engine designation system
Turbojets	J30 J31 J32 J33 J34 J35 J36 J37 XJ38 J39 J40 XJ41 J42 J43 J44 J45 J46 J47 J48 XJ49 J51 J52 J53 J54 J55 J56 J57 J58 J59 J60 J61 J63 J65 J67 J69 J71 J73 J75 J79 J81 J83 J85 J87 J89 J91 YJ93 J95 J97 J99 J100 YJ101 J102 J400 J401 J402 J403 J700
Turboprops/ Turboshafts	T30 T31 T33 T34 T35 T36 T37 T38 T39 T40 T41 T42 T43 T44 T45 T46 T47 T48 T49 T50 T51 T52 T53 T54 T55 T56 T57 T58 T60 T61 T62 T63 T64 T65 T66 T67 T68 T69 T70 T71 T72 T73 T74 T76 T78 T80 T100 T101 T400 T405 T406 T407 T408 T700 T701 T702 T703 T706 T708 T800
Turbofans	TF30 TF31 TF32 TF33 TF34 TF35 TF37 TF39 TF41 F100 F101 F102 F103 F104 F105 F106 F107 F108 F109 F110 F112 F113 F117 F118 F119 YF120 F121 F122 F124 F125 F126 F127 F128 F129 F135 F136 F137 F138 F400 F401 F402 F404 F405 F408 F412 F414 F415

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