| 摘要 |
<p>The flow alignment stage for an aircraft gas turbine has an exterior shroud (5) and an inner concentric shroud connected by fixed vanes (60-62...). Each shroud has a functional side (500) and a non-functional side (501), and can have ports (50-52...) to allow passage of the vane ends. The vane ends have deformable formations (601, 603,604) to lock them to the shrouds. <??>Claims include a method of assembly of a turbine.</p> |
