首页> 外国专利> Mounting for aircraft gas turbine flow guides has flow guide sectors bolted directly in place on carrier and with sealing sectors to cover impingement surfaces

Mounting for aircraft gas turbine flow guides has flow guide sectors bolted directly in place on carrier and with sealing sectors to cover impingement surfaces

机译:飞机燃气轮机导流装置的安装中,导流扇形部分直接用螺栓固定在支架上,并带有密封扇形块以覆盖撞击表面

摘要

The mounting for the sectors of a flow guide in an aircraft gas turbine has the sectors (11) provided with ribs (13) which engage directly on the carrier (14) and are bolted (16) to them. The suspension hooks (21) on the opposite side is movable on the carrier. The sealing sectors (17) adjacent to the guide sectors can completely cover the impingement faces of the guide sectors.
机译:用于飞机燃气涡轮机中的导流器的扇形件的安装具有扇形件(11),扇形件(11)具有肋(13),肋直接接合在托架(14)上并通过螺栓(16)固定在托架上。相对侧的吊钩(21)可在支架上移动。与导向区段相邻的密封区段(17)可以完全覆盖导向区段的冲击面。

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