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(Linear Innovative Thrust Reversal Actuation System)
The thrust reverser flaps of a commercial aircraft are to be electrically driven contrary to the previous hydraulic drive method.
Highly utilized double-sided, transverse force-free linear motor in short stator design.
Active volume 4,5 l (0,0045 m³)
Possible power for short-term 12000 N
The drive task requires 7000 N for a short time at a limited current.
The force density corresponds to approx. 50 – 60 % of a hydraulic cylinder, with equal forces in both directions.
Oil free (environment, risk of fire)
High control dynamics
Design freedom for other geometries
This project has received funding from the Clean Sky 2 Joint Undertaking (JU) under grant agreement No 887163. The JU receives support from the European Union’s Horizon 2020 research and innovation programme and the Clean Sky 2 JU members other than the Union.