# US 10,479,066 B2 · Composite tool having vacuum integrity and method of making the same > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 10,479,066 B2 - Document ID: US10479066B2 - Status: Granted - Kind: B2 - Application number: 15/269,916 - Filed: 2016-09-19 - Published: 2017-01-12 - Granted: 2019-11-19 - Earliest claimed: 2012-10-31 - Assignees: The Boeing Company - Applicants: The Boeing Company - Inventors: Charles William Thomas - Web page: https://patentgrep.com/patent/US10479066B2 ## CPC - B32B 37/10: characterised by the pressing technique, e.g. using action of vacuum or fluid pressure - B29C 33/38: characterised by the material or the manufacturing process (B29C33/44 takes precedence) - B29C 70/44: using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding - B29D 7/00: Producing flat articles, e.g. films or sheets (B29D24/00 takes precedence) - B32B 37/1009: {using vacuum and fluid pressure} - B32B 37/1018: {using only vacuum} - Y10T 156/10: Methods of surface bonding and/or assembly therefor - Y10T 156/1052: with cutting, punching, tearing or severing - B32B: LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM - B29C: SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING (making preforms B29B11/00; making laminated products by combining previously unconnected layers which become one product whose layers will remain together B32B37/00 - B32B41/00) - B29D: PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE (making granules B29B9/00; making preforms B29B11/00) - Y10T: TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION ## Abstract A composite tool for vacuum bag processing composite parts comprises a plurality of laminated composite plies, including a facesheet adapted to have a composite part placed thereon. A gas impermeable barrier layer sandwiched between the composite plies prevents air leaks through the tool. ## Claims ### Claim 1 A method of fabricating a composite tool used for vacuum bag processing composite parts, comprising: forming a first composite tool portion; forming a second composite tool portion comprising a tool surface for forming a composite part; preventing air leaks through the composite tool via placing a membrane between the first and second composite tool portions, the membrane being impermeable to gas; and forming a groove surrounding the tool surface and extending down to the membrane, the groove serving as a vacuum manifold around the tool surface, placing the membrane on a surface of the first composite tool portion; and adhering membrane to the surface of the first composite tool portion by placing a vacuum bag over the membrane and the first composite tool portion, and, using the vacuum bag, compressing the membrane against the surface of the first composite tool portion. ### Claim 2 (depends on 1) The method of claim 1, further comprising: forming the first composite tool portion comprising laying up a first set of composite pre-preg plies; placing the membrane includes laying up the membrane on the first set of composite pre-preg plies; and forming the second composite tool portion includes laying up a second set of composite pre-preg plies over the membrane. ### Claim 3 (depends on 2) The method of claim 2, further comprising: framing the groove surrounding the tool surface with a peripheral shoulder. ### Claim 4 (depends on 3) The method of claim 3, further comprising framing the groove comprising machining, at an offset within a perimeter of the second composite tool portion, the second composite tool portion down to the membrane. ### Claim 5 A method of fabricating a composite tool having vacuum integrity, the method comprising: laying up a first set of composite pre-preg plies; laying up a second set of composite pre-preg plies; placing a membrane between the first and second sets of composite pre-preg plies to prevent through-the-tool leaks, the membrane being impermeable to gas; laminating the first and second sets of composite pre-preg plies and the membrane; and forming a groove surrounding a tool surface of the second set of composite pre-preg plies and extending down to the membrane, the groove forming a vacuum manifold around the tool surface when using the tool surface for vacuum bag processing a composite part. ### Claim 6 (depends on 5) The method of claim 5, further comprising: forming the groove after laminating the second set of composite pre-preg plies wherein the laminating includes co-curing the first and second sets of composite pre-preg plies and vulcanizing the membrane. ### Claim 7 (depends on 5) The method of claim 5, further comprising: curing each of the first and second sets of composite pre-preg plies, forming cured first and second sets of composite pre-preg plies, such that the laminating comprises adhesively bonding the membrane to each of the cured first and second sets of composite pre-preg plies. ### Claim 8 (depends on 5) The method of claim 5, further comprising forming the groove via machining in a face of the second set of composite pre-preg plies surrounding the tool surface. ### Claim 9 (depends on 5) The method of claim 5, wherein: placing the membrane includes placing a sheet of b-staged rubber on a ply forming part of the second set of composite pre-preg plies, and the laminating includes vulcanizing the sheet of b-staged rubber. ### Claim 10 A method of fabricating a composite laminate tool comprising vacuum integrity used for vacuum bag processing a composite part, the method comprising: laying up a first set of composite pre-preg plies; laying up a second set of composite pre-preg plies; preventing through-the-tool gas leaks via placing a flexible material between the first set of composite pre-preg plies and the second set of composite pre-preg plies, the flexible material being impermeable to gas; and curing the first and second sets of composite pre-preg plies and the flexible material into the composite laminate tool, such that the laminate composite tool comprises: a first set of cured composite plies; a second set of cured composite plies forming a facesheet comprising a tool surface adapted for receiving the composite part; a barrier layer comprising the flexible material sandwiched between the first set of cured composite plies and the second set of cured composite plies, such that a first face of the barrier layer contacts a last composite ply of the second set of cured composite plies and a second face of the barrier layer contacts a first composite ply of the first set of cured composite plies, in which the first face is opposite the second face; and an edge breather groove in the facesheet extending down to the barrier layer and surrounding the tool surface. ### Claim 11 (depends on 10) The method of claim 10, further comprising the edge breather groove serving as a vacuum manifold around the tool surface when vacuum processing the composite part on the tool surface. ### Claim 12 (depends on 10) The method of claim 10, further comprising locating the facesheet on a side, away from the flexible material, of the second set of cured composite plies. ### Claim 13 (depends on 11) The method of claim 11, further comprising forming the tool surface via machining the facesheet. ### Claim 14 (depends on 11) The method of claim 11, further comprising forming a peripheral shoulder comprising a perimeter portion of the second set of composite pre-preg plies surrounding the edge breather groove. ### Claim 15 (depends on 14) The method of claim 14, further comprising forming the peripheral shoulder via machining the edge breather groove into the second set of composite pre-preg plies around the perimeter portion of the tool surface. ### Claim 16 (depends on 1) The method of claim 1, further comprising the membrane comprising a flexible material. ### Claim 17 (depends on 16) The method of claim 16, further comprising the flexible material comprising one of: rubber, nylon, and silicone. ### Claim 18 (depends on 1) The method of claim 1, further comprising placing the membrane between the first and second composite tool portions comprising placing a sheet of b-staged rubber on the first composite tool portion and hot vacuum forming the b-staged rubber onto a face of the first composite tool portion. ### Claim 19 (depends on 18) The method of claim 18, further comprising vulcanizing the sheet of b-staged rubber. ### Claim 20 (depends on 1) The method of claim 1, further comprising placing the membrane between the first and second composite tool portions comprising adhesively bonding the membrane to the first and second composite tool portions.