Method for manufacturing a composite platform for a fan of an aircraft turbine engine
US-2024060460-A1 · Feb 22, 2024 · US
US12508747B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-12508747-B2 |
| Application number | US-202217978053-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 31, 2022 |
| Priority date | Oct 31, 2022 |
| Publication date | Dec 30, 2025 |
| Grant date | Dec 30, 2025 |
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A manufacturing method is provided. A preform is arranged over a surface of an inner mold line. The preform is folded over sides of the inner mold line. An end of the preform is clamped to a floating plate using a bladder-activated clamp. The floating plate is translated in a first direction to tension the preform into a shaped body. A plurality of compressing bladders are activated to apply compressive forces to the preform.
Opening claim text (preview).
What is claimed is: 1 . A manufacturing method, comprising: arranging a preform over a surface of an inner mold line; folding the preform over sides of the inner mold line; positioning an end of the preform over a floating plate coupled to a side of the inner mold line; clamping the end of the preform to the floating plate, wherein the clamping is provided by activating a clamping bladder to apply a first clamping force to the preform to secure the end of the preform with respect to the floating plate; translating the floating plate in a first direction to apply a first tension on the preform into a shaped body; and activating a first compressing bladder to apply a first compressive force to the preform. 2 . The manufacturing method of claim 1 , wherein the floating plate is coupled to a tensioning system through the side of the inner mold line. 3 . The manufacturing method of claim 2 , wherein the tensioning system is at least one of a gear rack-based tensioning system or a screw-based tensioning system. 4 . The manufacturing method of claim 3 , wherein the floating plate is coupled to the tensioning system through one or more pockets in the side of the inner mold line. 5 . The manufacturing method of claim 1 , wherein the first compressing bladder is activated by inflating the first compressing bladder with a fluid. 6 . The manufacturing method of claim 1 , wherein the first compressing bladder is mounted to a caul plate moveable with respect to the inner mold line, and wherein the caul plate has a different rigidity than the first compressing bladder. 7 . The manufacturing method of claim 1 , further comprising activating a second compressing bladder to apply a second compressive force to the preform, wherein the second compressing bladder is activated after the first compressing bladder. 8 . The manufacturing method of claim 1 , further comprising: increasing the first compressive force coupled with increasing the first tension. 9 . The manufacturing method of claim 1 , further comprising: activating a second compressing bladder to apply a second compressive force to the preform; and activating a third compressing bladder to apply a third compressive force to the preform. 10 . The manufacturing method of claim 9 , wherein the first compressing bladder, the second compressing bladder, and the third compressing bladder are activated sequentially along a second direction. 11 . The manufacturing method of claim 9 , wherein the first compressing bladder, the second compressing bladder, and the third compressing bladder are activated starting from a center of the preform and working outward toward a periphery of the preform.
Inflatable bladders using gas or fluid and related details · CPC title
with means for positioning, fastening or clamping the material to be formed or preforms inside the mould · CPC title
Bags, bleeder sheets or cauls for isostatic pressing · CPC title
Deforming tubular bodies (corrugating tubes by applying fluid pressure B21D15/03, B21D15/10) · CPC title
Details of caul plates, e.g. materials or shape · CPC title
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