Rolls-Royce AE 3007

The Rolls-Royce AE 3007 (formerly Allison 3007 AE ) is a two-shaft turbofan engine (engl. Turbofan ) of Rolls-Royce , which in business aircraft is in the thrust range of 30 to 40 kN thrust used.

development

Rolls-Royce AE 3007

The first tests of the engine began in 1991 and its maiden flight took place in 1996. The engine consists of a fan driven by a three-stage low-pressure turbine and a 14-stage high-pressure compressor , which is driven by a two -stage high -pressure turbine. The Rolls-Royce AE 3007 shares the engine core with the AE 1107C-Liberty and the AE 2100 , from which it was derived.

The AE 3007 found in aircraft such as the Embraer ERJ 135, ERJ 140, ERJ 145 and Legacy as well as the Cessna Citation X 's application. In military aviation, the Northrop Grumman RQ-4 Global Hawk drone (as AE 3007H ), Boeing MQ-25 ( AE 3007N ) and the military variants of the ERJ 145 (Embraer R-99A, R-99B and P-99 ) used.

Technical specifications

Type	Thrust (kN)	By- pass ratio at start	Total pressure ratio	Fan diameter (m)	Length (m)	Dry matter (kg)	Admission	Used at
AE 3007 A, A1, A1 / 1, A1P, A1 / 3, A3	31.11-33.69	4.8-4.98: 1	18-21: 1	0.98	2.705	719.4	1995	ERJ 135/140/145 Legacy
AE 3007 A1E	36.1	4.8: 1	18-20: 1	0.98	2.705	752	2002	ERJ 145 XR
AE 3007 C1	30.09	4.8: 1	24: 1	0.98	2.705	717	2002	Cessna Citation X

Web links

• Manufacturer's website (viewed on August 7, 2010)
• EASA-TCDS-E.044 - Type certification of the AE 3007