Mtu Aero Engines Ag

Eckart Heinrich

Manfred Feldmann

Hermann Klingels

Werner Humhauser

Rudolf Stanka

Norbert Huebner

Erich Steinhardt

Hans-Peter Hackenberg

Karl Maar

Stefan Hagen Weber

Jochen Gier

Klaus Peter Rued

Claus Riegler

A turbofan aircraft engine having a primary duct (C), including a combustion chamber (BK), a first turbine (HT) disposed downstream of the combustion chamber, a compressor (HC) disposed upstream of the combustion chamber and coupled (W) to the first turbine, and a second turbine (L) disposed downstream of the first turbine and coupled (W) via a speed reduction mechanism (G) to a fan (F) for feeding a secondary duct (B) of the turbofan aircraft engine. A square of a ratio of a maximum blade diameter (D) of the fan to a maximum blade diameter (D) of the second turbine is at least 3.5, in particular at least 4.

Turbofan aircraft engine

Growing community of inventors

Germering, Germany

Eckart Heinrich