A method for converting a turbofan aircraft - - engine in an engine unit for a not - purpose and apparatus for carrying out the method

摘要

described is a antriebsmaschinenanlage (10) with a first compressor (20) for generating a stromabwu00e4rtigen axial flow, a second compressor (22), downstream of the first compressor (20) is arranged, and a combustion chamber (24), the downstream of the second ca rdichters (22) is arranged.a first turbine (28) is arranged downstream of the combustion chamber (24) and the second compressor (22) on a first shaft (32) antriebsmu00e4u00dfig connected. a second turbine (36) is downstream of the first turbine (28) arranged with the first compressor (20) on a second shaft (40) antriebsmu00e4u00dfig connected.the antriebsmaschinenanlage (10) is connected to the second shaft (40) with a drehbelastung connected. described is also capable of converting an flugzeugturbofantriebwerks in an engine for a nichtflugtechnischen purpose by removing the fan and replacing the same by a strain.