首页> 外国专利> Intake manifold for aircraft engine, has closing device for closing air intake opening, where closing device includes flap that pivots simultaneously between closed position and open position

Intake manifold for aircraft engine, has closing device for closing air intake opening, where closing device includes flap that pivots simultaneously between closed position and open position

机译:飞机发动机的进气歧管,具有用于关闭进气孔的关闭装置,其中关闭装置包括可同时在关闭位置和打开位置之间旋转的挡板

摘要

The manifold (80) has an air intake opening (81) and a closing device for closing the air intake opening, where the device is arranged partially in the opening. The closing device includes a flap (82) ready to pivot between a closed position in which the opening is closed and an open position in which the opening is open. Another flap (84) extends parallel to the former flap and pivots simultaneously with the former flap between the closed position and the open position, where the flaps are spaced apart by washers (90).
机译:歧管(80)具有进气口(81)和用于关闭进气口的关闭装置,其中该装置部分地布置在该开口中。该关闭装置包括一个挡板(82),该挡板准备在一个关闭该开口的关闭位置和一个打开该开口的打开位置之间枢转。另一个挡板(84)平行于前挡板延伸,并与前挡板同时在关闭位置和打开位置之间枢转,其中挡板由垫圈(90)隔开。

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