# US 10,307,943 B2 · Method and system for vacuum bagging > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 10,307,943 B2 - Document ID: US10307943B2 - Status: Granted - Kind: B2 - Application number: 15/204,575 - Filed: 2016-07-07 - Published: 2017-01-12 - Granted: 2019-06-04 - Earliest claimed: 2015-07-08 - Assignees: Airbus Operations GmbH - Applicants: Airbus Operations GmbH - Inventors: Paulin Fideu Siagam; Hauke Seegel; Claus Fastert - Web page: https://patentgrep.com/patent/US10307943B2 ## CPC - B29C 43/56: Compression moulding under special conditions, e.g. vacuum - B29C 70/342: {using isostatic pressure} - B29C 70/44: using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding - B29D 99/0014: {provided with ridges or ribs, e.g. joined ribs} - Y02T 50/40: Weight reduction - 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) - Y02T: CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION ## Abstract A vacuum bagging system for vacuum bagging a fiber-reinforced polymer component for an aircraft or spacecraft includes a vacuum bagging film or membrane which is configured to cover and seal the component during molding. The vacuum bagging film or membrane is pre-formed, e.g. thermoformed, to a shape or to an external geometry of the component to be molded. A method of vacuum bagging a fiber-reinforced polymer component of an aircraft or space-craft, includes the steps of: arranging a component to be molded in a vacuum bagging assembly for forming a fiber-reinforced polymer component; pre-forming a vacuum bagging film or membrane to a shape or external geometry of the component; and arranging the vacuum bagging film or membrane on or over the component in the vacuum bagging assembly such that the film or membrane form-fittingly covers the component. ## Claims ### Claim 1 A method of vacuum bagging a fiber-reinforced polymer component of an aircraft or spacecraft, comprising: arranging a component to be molded in a vacuum bagging assembly for molding the component; pre-forming a vacuum bagging film or membrane to a shape or an external geometry of the component to be molded; and arranging or laying the vacuum bagging film or membrane on or over the component to be molded in the vacuum bagging assembly such that the film or membrane form-fittingly covers the component during molding; wherein arranging or laying the vacuum bagging film or membrane on or over a tool for the pre-forming comprises: extruding a sheet of the film or membrane onto the tool, whereby an extruder assembly is movable relative to the tool and/or the tool is movable relative to the extruder assembly, or drawing or extending a sheet of the film or membrane from a supply roll. ### Claim 2 (depends on 1) The method of claim 1, wherein pre-forming the vacuum bagging film or membrane to the shape or external geometry of the component comprises arranging the vacuum bagging film or membrane on or over a pre-forming tool having the shape or external geometry of the component to be molded. ### Claim 3 (depends on 1) The method of claim 1, wherein pre-forming the vacuum bagging film or membrane to the shape or external geometry of the component comprises thermoforming the film or membrane by applying heat to the film or membrane for softening and forming or shaping same to the external geometry of the component. ### Claim 4 (depends on 1) The method of claim 1, wherein pre-forming the vacuum bagging film or membrane to the shape or external geometry of the component comprises applying positive pressure to an upper surface of the film or membrane. ### Claim 5 (depends on 1) The method of claim 1, wherein pre-forming the vacuum bagging film or membrane to the shape or external geometry of the component includes applying a vacuum to at least partially evacuate a space between a tool for the pre-forming and the film or membrane. ### Claim 6 (depends on 1) The method of claim 1, wherein the component comprises at least one elongate structural member, the shape or the external geometry of which is substantially uniform along a length thereof, wherein the film or membrane is pre-formed to the shape or the external geometry of the at least one elongate structural member. ### Claim 7 (depends on 6) The method of claim 6, wherein the component comprises a plurality of elongate structural members and wherein the vacuum bagging film or membrane is pre-formed to the shape or the external geometry of the plurality of elongate structural members. ### Claim 8 (depends on 1) The method of claim 1, comprising fixing a periphery or an edge region of the film or membrane prior to and/or during pre-forming the film or membrane to the shape or the external geometry of the component. ### Claim 9 (depends on 2) The method of claim 2, wherein pre-forming the vacuum bagging film or membrane to the shape or external geometry of the component comprises laying the vacuum bagging film or membrane on or over a pre-forming tool having the shape or external geometry of the component to be molded. ### Claim 10 (depends on 4) The method of claim 4, wherein applying positive pressure to the upper surface of the film or membrane is performed via a blower device for directing a heated air stream onto the film or membrane. ### Claim 11 (depends on 4) The method of claim 4, wherein applying positive pressure to an upper surface of the film or membrane is performed via a pressure applicator device for contacting the film or membrane to press same locally against the external geometry of the component. ### Claim 12 A method of vacuum bagging a fiber-reinforced polymer component of an aircraft or spacecraft, comprising: arranging a component to be molded in a vacuum bagging assembly for molding the component; pre-forming a vacuum bagging film or membrane to a shape or an external geometry of the component to be molded; and arranging or laying the vacuum bagging film or membrane on or over the component to be molded in the vacuum bagging assembly such that the film or membrane form-fittingly covers the component during molding; wherein pre-forming the vacuum bagging film or membrane to the shape or external geometry of the component comprises applying positive pressure to an upper surface of the film or membrane via a blower device for directing a heated air stream onto the film or membrane or via a pressure applicator device for contacting the film or membrane to press same locally against the external geometry of the component.