TP400-D6
Design, development and manufacturing activities for the TP400-D6 engine are carried out by the Europrop International (EPI) consortium established jointly by MTU Aero Engines, Snecma, Rolls-Royce and Rolls-Royce ITP Aero. TEI participates in this project as the risk and revenue partner with Rolls-Royce ITP Aero.
The first flight of the engine was performed with A400M aircraft in Seville, Spain in late 2009, and it was released to service in late 2013.
The 7th of A400M (ATLAS) aircraft out of the 10 pieces, planned to be
procured by the Turkish Air Forces, were delivered in 2019.
The 7th of A400M (ATLAS) aircraft out of the 10 pieces, planned to be
procured by the Turkish Air Forces, were delivered in 2019.
TEI is responsible for design, development, prototype production, assembly, testing, mass production and post-sales support of the following work packages:
- Front Bearing Structure Module,
- Propeller Gearbox Supporting Bars,
- Primary Exhaust Nozzle,
- Exhaust Cone,
- Special to Project Test Equipment - SPTE
- Preparation of the Component Maintenance Manual (CMM) as necessary to perform the maintenance activities for the Front Bearing Structure Module at TEI MRO
- Service support engineering activities to resolve any problems arising in the post-sales process with respect to the modules under TEI's responsibility
Technical Specifications
- Engine Type: Turboprop
- Engine Power: Approx. 11,000 shp (sea level)
- Pressure Ratio: 25
- Weight: Approx. 1,900 kg (dry)
- Length: 3,5 m
- Diameter: 0,92 m
- Compressor: 5 intermediate-pressure stages, 6 high-pressure stages
- Turbine: 1 high-pressure stage, 1 intermediate-pressure stage, 3 low-pressure stages
General Specifications
- The most powerful turboprop engine of the Western Europe
- High growth potential
- Low lifecycle cost
- Component technology endurable for military and commercial applications
Gallery
