Composite material wall reinforced for limiting crack propagation in one direction
A technology of composite materials and reinforcements, which is applied in the direction of synthetic resin layered products, thin material processing, power devices on aircraft, etc., and can solve problems such as not being used to contact aerodynamic flow
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[0069] According to a preferred embodiment, the metal reinforcement 20 has a width of approximately 30 mm and a thickness of approximately 0.5 mm, the struts and crosspieces have a width of approximately 2 mm to 4 mm, the grooves are regularly spaced and have a dimension L1 of 30 mm to 35 mm and a dimension L2 close to 25mm.
[0070] Such as Figure 8 and 9 As shown, in case the reflective wall 16 of the sound-absorbing panel 10 is a tubular portion with an axis 30 , the stiffeners 20 should be (preferably regularly) distributed on the circumference in a direction parallel to the axis 30 . Advantageously, on the cylindrical wall of the air inlet, 12 to 35 stiffeners should be regularly distributed on the periphery, forming an angle between them varying substantially from 10° to 30°. Advantageously, 16 to 18 reinforcements should be provided.
[0071] For the walls of the pressurized fuselage, not only should the spread of cracks be limited, but also the sealing of the walls...
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