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Device for connecting inner wall and outer wall of bypass filter channel of turbojet engine unit, has two wall-like supporting elements, which are partially arranged in assembled state in direction of fluid flow in bypass filter channel
Device for connecting inner wall and outer wall of bypass filter channel of turbojet engine unit, has two wall-like supporting elements, which are partially arranged in assembled state in direction of fluid flow in bypass filter channel
The device (11) has two wall-like supporting elements (15,16), which are partially arranged behind one another in an assembled state in a direction of a fluid flow (21) in a bypass filter channel. The sections (15A,16A) overlap the supporting elements in the areas of side surfaces (15B,16B) running in the direction of the fluid flow. The supporting elements of a support device (12) are adjustable executed to each other in mutually facing areas (22,23).
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