Improved method for producing a transmission shaft, preferably for an accessory box system of an aircraft turbomachine
US-2015377282-A1 · Dec 31, 2015 · US
US10022919B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10022919-B2 |
| Application number | US-201615204377-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 7, 2016 |
| Priority date | Dec 9, 2011 |
| Publication date | Jul 17, 2018 |
| Grant date | Jul 17, 2018 |
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A die and method for impregnating at least one fiber roving with a polymer resin are disclosed. The die includes an impregnation section. The impregnation section includes an impregnation zone configured to impregnate the roving with the resin. The impregnation zone includes a plurality of contact surfaces. At least one of the plurality of contact surfaces is configured such that a normal force of the roving is less than or equal to a lift force of the resin at an impregnation location on the contact surface during impregnation of the roving with the resin by the contact surface.
Opening claim text (preview).
What is claimed is: 1. A method for impregnating at least one fiber roving with a polymer resin, the method comprising: flowing a polymer resin through a manifold assembly of a die, the manifold assembly comprising a plurality of branched runners; coating at least one fiber roving with the resin; and traversing the coated roving through an impregnation zone of the die to impregnate the roving with the resin, the impregnation zone comprising a plurality of contact surfaces, wherein a normal force of the roving is less than or equal to a lift force of the resin at an impregnation location on at least one of the plurality of contact surfaces during impregnation of the roving with the resin by the at least one of the plurality of contact surfaces. 2. The method of claim 1 , wherein the at least one of the plurality of contact surfaces is a final contact surface in a run direction of the roving. 3. The method of claim 1 , wherein no contact occurs between the roving and the at least one of the plurality of contact surfaces during impregnation of the roving with the resin by the contact surface. 4. The method of claim 1 , wherein the impregnation location comprises a peak of the contact surface. 5. The method of claim 1 , wherein the normal force is calculated using the equation: a =sin( A )* h wherein a is the normal force, A is an angle at which the roving traverses the at least one of the plurality of contact surfaces, and his a tension of the roving. 6. The method of claim 1 , wherein the lift force is calculated using the equation: F =(((6η UL )/ h 2 )*((( h o −h )*( h−h L ))/( h o 2 −h L 2 )))* C *( w*L ) wherein F is the lift force, η is a viscosity of the resin, U is a speed of the roving, L is a length of the impregnation location, h is a height of resin within the impregnation location, C is a porosity factor, and w is a width of the roving. 7. The method of claim 1 , wherein each of the plurality of contact surfaces is configured such that the roving traverses the contact surface at an angle in the range between 1 degree and 30 degrees. 8. The method of claim 1 , wherein the at least one of the plurality of contact surfaces is configured such that the roving traverses the at least one of the plurality of contact surfaces at an angle that is less than the angle of the remainder of the plurality of contact surfaces. 9. The method of claim 1 , wherein each of the plurality of contact surfaces comprises a curvilinear contact surface.
combined with compression moulding · CPC title
in the die zone, e.g. to create flow homogeneity · CPC title
the work being a web, band, strip or the like · CPC title
of preformed parts, e.g. inserts, retaining their shape during the extrusion process · CPC title
with a matrix in liquid form, e.g. as melt, solution or latex · CPC title
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