| 摘要 |
<p>The gas turbine engine can be used in the aircraft engineering and in motor car engineering. The engine operates on a lighter mode and has better cooling and suffers minimum heat losses, its construction being light-weight and simple. It comprises a housing (5) which houses a shaft (7), resting on one of its ends on bearing bodies (13), to which a compressor (10) is fitted having radially positioned blades. A turbine (8) is fitted to the compressor (10) and to shaft (7), so that the compressor (10) and the turbine (8) have a common rear wall (11). At the outlet of the compressor (10) a guiding apparatus (4) is mounted, fitted in the inlet of a combustion chamber (1) in which a torch (2) is fitted. At the outlet of chamber (1) and torch (2) the guiding apparatus (12) of the turbine (8) is fitted. Guiding apparatuses (4 and 12) have a common partition wall (14), which also continues into the volume of the combustion chamber (1). The common partition wall (14), the guiding apparatus (4) of the compressor (10) and the guiding apparatus (12) of turbine (8) and the internal partition wall (3) operate as a regeneration chamber of the gas turbine engine. The common rear wall (11) at the same time serves for cooling the blades of turbine (8). 1 claim, 1 figure</p> |
