GAS-TURBINE ENGINE, TWO-MOTOR HELICOPTER, FITTED WITH SUCH A GAS-TURBINE ENGINE, AND METHOD FOR OPTIMIZING A SUPERGASM MODE WITH ZERO POWER OF SUCH TWO-AND-TWO

摘要

The invention relates to a turboshaft engine comprising a gas generator (5) that is capable of being rotated, and a free turbine (6) that is rotated by the gases of said gas generator (5), characterized in that it comprises a device (20) for spontaneously mechanically coupling said gas generator (5) and said free turbine (6) that is capable of mechanically and spontaneously connecting said gas generator (5) and said free turbine (6) as soon as the ratio of the rotational speed (NGG) of said gas generator to the rotational speed (NTL) of said free turbine reaches a predetermined threshold value.