Key tool and composite panel in particular for an aircraft engine nacelle manufactured by means of such tool
US-2016167316-A1 · Jun 16, 2016 · US
US11235494B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11235494-B2 |
| Application number | US-201716466274-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 30, 2017 |
| Priority date | Dec 1, 2016 |
| Publication date | Feb 1, 2022 |
| Grant date | Feb 1, 2022 |
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A seal member formed in a line shape having ends is inserted in a seal groove formed on at least one of adjacent side surfaces of segments. A lip portion is provided on a seal upper portion of the member so at least a tip end thereof projects to an outside of the seal groove when the member is inserted in the groove. The seal member is hollow or includes a concave portion on at least a seal bottom portion thereof. When assembling the segments as a single structure, the adjacent side surfaces of the segments are coupled to each other, and the seal member is crushed in a cross sectional direction by the side surface of the other segment to seal between the segments. With this, complication of manufacturing steps can be suppressed or avoided while realizing a satisfactory sealed state between the adjacent segments of a mold.
Opening claim text (preview).
The invention claimed is: 1. A method of manufacturing a hollow composite material structure including a skin constituted by at least a thermosetting resin composition and a fiber material, the method using a mold located in the hollow composite material structure, the mold being constituted by a plurality of segments and kept as a single structure by coupling adjacent side surfaces of the segments to each other, the method comprising: laminating a prepreg on an outer peripheral surface of the mold, the prepreg being configured to become the skin by thermal curing; forming a vacuum bag after the prepreg is laminated, the vacuum bag being configured to seal an outside of the mold; and inserting seal members in seal grooves each provided on at least one of the adjacent side surfaces of the segments, each of the seal members being formed in a line shape having ends, wherein: a part of the seal member which part contacts a bottom surface of the seal groove when the seal member is inserted in the seal groove is referred to as a seal bottom portion; a part of the seal member which part is opposed to the seal bottom portion is referred to as a seal upper portion; a lip portion is provided at the seal upper portion such that at least a tip end of the lip portion projects to an outside of the seal groove when the seal member is inserted in the seal groove; the seal member is hollow therein or includes a concave portion on at least the seal bottom portion of the seal member; and when assembling the segments as the single structure, the adjacent side surfaces of the segments are coupled to each other, and the seal member provided at one of the segments is crushed in a cross sectional direction by the side surface of the other segment to seal between the segments, the method further comprising while subjecting an inside of the vacuum bag to vacuum suction, subjecting the prepreg to the thermal curing while being pressurized by autoclaving of the entire mold, wherein: a surface of the segment which surface constitutes an outer peripheral surface of the single structure is referred to as a front surface of the segment; both end portions of the seal groove are bent toward the front surface of the segment; a length of the seal member is set such that when the seal member is inserted in the seal groove, end portions of the seal member are exposed from respective end portions of the seal groove, i.e., from the front surface of the segment; after the seal member is inserted in the seal groove, the end portions of the seal member are cut near the front surface of the segment; and end portion pressing members are then fixed to the segment and press the respective end portions of the seal member such that the end portions of the seal member are not exposed from the front surface of the segment. 2. The method according to claim 1 , wherein: the composite material structure includes a skeleton member in addition to the skin; the skeleton member is attached to the outer peripheral surface of the mold, and the prepreg is laminated on an outside of the skeleton member; and a caul plate covering the prepreg is attached to an outside of the prepreg. 3. The method according to claim 1 , wherein: after the end portions of the seal member are cut near the front surface of the segment, the end portions of the seal member are covered with bonding members to be bonded to the front surface of the segment; and the end portions of the seal members are then pressed by the respective end portion pressing members. 4. The method according to claim 1 , wherein the plurality of segments are fixed to a pair of annular holding members to be kept as the single structure. 5. The method according to claim 4 , wherein the plurality of segments include: a segment having the side surface on which the seal groove is provided; and a segment having the side surface on which the seal groove is not provided. 6. The method according to claim 5 , wherein: the segments includes two types of segments that are first segments each having such a shape that when the first segment is arranged horizontally with the front surface facing upward, each of both side surfaces of the first segment faces a horizontal direction or a direction inclined upward relative to the horizontal direction, and second segments each having such a shape that when the second segment is arranged horizontally with the front surface facing upward, each of both side surfaces of the second segment faces a direction inclined downward relative to the horizontal direction; the first segments and the second segments are alternately arranged such that the second segments are first fixed at every other fixing positions of the annular holding members, each of the first segments is inserted between the second segments, and the side surfaces of the first and second segments are coupled to each other; and the seal grooves are provided only on the side surfaces of the first segments. 7. The method according to claim 6 , wherein: a plurality of concave portions into which skeleton materials are fitted are formed on the front surfaces of the first and second segments; and the skeleton materials are first attached to the first and second segments, and the first and second segments are then fixed to the annular holding members. 8. The method according to claim 1 , wherein: the lip portion projects in a normal direction of the seal upper portion or projects so as to be inclined relative to the normal direction of the seal upper portion; and one of a width of the seal upper portion and a width of the seal bottom portion in a cross section of the seal member is larger than the other. 9. The method according to claim 1 , wherein the concave portion is also formed on the seal upper portion so as to be located close to the lip portion.
Seals preventing pressurized fluid to escape from the mould cavity · CPC title
using bags surrounding the moulding material {or using membranes contacting the moulding material} · CPC title
Perforating, cutting or machining during or after moulding · CPC title
using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding · CPC title
Assembling a large number of mould elements to constitute one cavity · CPC title
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