The panel (10) has stiffening elements (18) in pockets (16) along its edges.
In an embodiment, a guardrail can comprise: an outer wall and stiffening elements, wherein the guardrail comprises a plastic.
The intermediate section comprises a plurality of stiffening elements.
A second series of elongated sections (14) is then laid, completing the manufacture of the carcass ply (3) with the formation of axially outer terminal zones (16) which are superimposed on the stiffening elements (20).
This wavy central portion improves the rigidity of the blades and allows their thickness to be decreased and their length increased without having to resort to stiffening elements which have the disadvantage of causing the curds to crumble.
The stiffener elements include at least some stiffener elements that are disposed at an angle to at least some of the other stiffener elements.
The second face sheet is disposed against the second edges of the stiffener elements and the first and second face sheets are autogenously welded to the edges of the stiffener elements.
The first and second stiffening members can be disposed in an overlapping and spaced relationship. .
Each of the stiffening may also define a means for maintaining the position of the stiffening members during the molding process to ensure that the stiffening member is properly located in the wing.
A support member can optionally be disposed between the first and second stiffening members.
After the device is delivered and expanded additional stiffening struts can be inserted into these pockets.
The end edges and the lateral edges of the sheet are rigidified respectively by a transverse (22) and longitudinal rigidifying members (24).
The stiffener elements each have a first edge disposed against the first face sheet and an opposed second edge.
Further provided integral with the boot (12) are retention members (106a, 106b) that isolate the malleoli from the stiffening members (104a, 104b) for the comfort of the wearer.
The pulley further comprises stiffening means (46) of the outer portion coming into contact with a bore (40b) of said portion.
Alternatively, the second stiffening member can be disposed distal to the first stiffening member such that a gap is defined between the stiffening members.
Optional stiffening members may be attached to the backpan to provide additional structural rigidity, as well as to support a front panel for the array.
The present invention relates to a novel connection means between members of a metal roof truss, namely the connection between chord members (20,22,24) and stiffening members (12,14,16,18).
Each half-shell structure (30, 50) is an integral or unitary member that includes at least a portion of the outer skin (16) of the airfoil as well as stiffener members (34, 54) and connection members (38, 58).
A plurality of stiffening members is disposed around the second lumen, the plurality of stiffening members being engageable to selectively stiffen the catheter body.
Requêtes fréquentes français :1-200, -1k, -2k, -3k, -4k, -5k, -7k, -10k, -20k, -40k, -100k, -200k, -500k, -1000k,
Requêtes fréquentes anglais :1-200, -1k, -2k, -3k, -4k, -5k, -7k, -10k, -20k, -40k, -100k, -200k, -500k, -1000k,
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