| 摘要 |
<p>The aircraft gas turbine engine is held in position be a flexible connecting ring which is made of metal in sectors (56,60). One end (56a,60a) of the ring is fixed (50,52) to the combustion chamber and the second end, which forms a flange, is fixed (54,58) to the envelope. The ring can be bolted to the combustion chamber. the connecting ring can be apertured for ventilation.</p> |
