Method and device for series production of components made of a fiber-reinforced composite material
US-2016375613-A1 · Dec 29, 2016 · US
US9211684B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9211684-B2 |
| Application number | US-201314076847-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 11, 2013 |
| Priority date | Nov 13, 2012 |
| Publication date | Dec 15, 2015 |
| Grant date | Dec 15, 2015 |
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A method for manufacturing a radial shaft of a gas-turbine engine which is made up of +/−45° layers, zero layers and +/−30° layers of carbon fiber composite and connected to load-input end pieces via sinusoidal connecting areas.
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What is claimed is: 1. A method for manufacturing a radial shaft of an aircraft gas-turbine engine comprising: providing a conical, rod-shaped core with end areas at both sides, said end areas each having around their circumference a sinusoidal structure with convex and concave areas extending in a longitudinal direction of the respective end area, placing structured rods into the concave areas of the sinusoidal structure, wrapping the core and the end areas with flat and spl…
Operations & Transport · mapped topic
Operations & Transport · mapped topic
Operations & Transport · mapped topic
Operations & Transport · mapped topic
Operations & Transport · mapped topic
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