# US 4,379,013 A · Fine film pressure bags forming composite structures > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 4,379,013 A - Document ID: US4379013A - Status: Granted - Kind: A - Application number: 06/192,571 - Filed: 1980-09-30 - Granted: 1983-04-05 - Earliest claimed: 1980-09-30 - Assignees: The Boeing Company - Inventors: William C. Tambussi - Web page: https://patentgrep.com/patent/US4379013A ## CPC - B29D 99/0028: {hollow blades} - B29C 33/448: {destructible (B29C33/52 takes precedence; in particular used in injection moulding B29C45/4457)} - B29C 43/3642: {Bags, bleeder sheets or cauls for isostatic pressing} - B29C 70/34: and shaping or impregnating by compression {, i.e. combined with compressing after the lay-up operation} - B29L 2031/082: {Blades, e.g. for helicopters} - B29D: PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE (making granules B29B9/00; making preforms B29B11/00) - 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) - B29L: INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES ## Abstract This invention relates to a method and apparatus for fabricating a composite structure and, in particular, to a method and apparatus for fabricating a hollow composite structure having a dense laminated wall formed by bonding and curing a plurality of resin-preimpregnated fiber sheets or tapes under heat and pressure. Hollow composite structures may be formed by applying layers of resin-impregnated fabric material onto a pressure bag covering a rigid mandrel, disposing the assembly of the mandrel, pressure bag, and uncured composite layers within an outer mold, transmitting heat to the composite material to cure the resin and applying pressure within the flexible pressure bag to act against the composite material during the curing operation to assure proper dimensions, density, structural properties and wall thickness of the cured composite structure. ## Claims ### Claim 1 In an apparatus for curing a tubular composite structure of laminated, resin-impregnated fibrous material which includes structure retaining means having a contoured inner surface adjacent the outer surface of the composite structure and pressure bag means disposed within and extending between opposite ends of the composite structure, for applying pressure to the inner surface of the composite structure, the improvement wherein the pressure bag means comprises at least one pressure bag formed of a material having inherent release characteristics and adapted to be connected to a pressure source, and the pressure bag includes at least one overlapped folded portion extending between the opposite ends of the adjacent composite structure, to allow the pressure bag to expand radially against the inner surface of the composite structure when the pressure bag is connected to the pressure source. ### Claim 2 (depends on 1) An apparatus, as described in claim 1, wherein the pressure bag means comprises two pressure bags, one disposed within the other. ### Claim 3 (depends on 2) An apparatus, as described in claim 2, wherein adjacent ends of the two pressure bags are sealed together to form a common end portion which is connected to the pressure source. ### Claim 4 (depends on 1) An apparatus, as described in claim 1, wherein said at least one pressure bag is formed of thin film PVF material. ### Claim 5 (depends on 1) An apparatus, as described in claim 1, wherein said at least one overlapped folded portion comprises a plurality of said overlapped folded portions which are uniformly spaced about the pressure bag. ### Claim 6 In an expandable pressure bag assembly for continuously applying pressure to the inner surface of a tubular composite structure during curing of the composite structure, which is closely disposed about a rigid mandrel and is adapted to be connected to a pressure source, wherein the pressure bag assembly includes an outer layer of a material having inherent release characteristics, about which contoured straps of layered, resin-impregnated fibrous material are disposed to form the composite, structure, the improvement wherein the pressure bag assembly comprises: an inner expandable pressure bag, closely disposed about the mandrel and adapted to be connected to the pressure source; and an outer pressure bag of material having inherent release characteristics, which is disposed about and conforms closely to the inner pressure bag, wherein the outer pressure bag includes at least one overlapped folded portion extending between opposite ends of the adjacent composite structure, to allow the outer pressure bag to expand radially against, and continuously apply pressure to, the inner surface of the composite structure when the inner pressure bag is connected to the pressure source. ### Claim 7 (depends on 6) A pressure bag assembly, as described in claim 6, wherein the inner pressure bag is formed of material having inherent release characteristics, and includes at least one overlapped folded portion extending between opposite ends of the mandrel, to allow the inner pressure bag to expand radially against, and continuously apply pressure to, the outer pressure bag during curing of the composite structure. ### Claim 8 (depends on 7) A pressure bag assembly, as described in claim 7, wherein adjacent ends of the inner and outer pressure bags are sealed together to form a common end portion which is adapted to be connected to the pressure source. ### Claim 9 (depends on 8) A pressure bag assembly, as described in claim 8, wherein the inner and outer pressure bags are formed of thin film PVF material. ### Claim 10 In a method for curing a tubular composite structure which includes the steps of forming an elongated mandrel assembly comprising a rigid mandrel and an expandable pressure bag assembly which is closely disposed about the mandrel, has an outer layer of material having inherent release characteristics and is adapted to be connected to a pressure source, laying contoured straps of layered, resin-impregnated fiber material about the mandrel assembly to form the uncured composite structure, disposing an outer mold or die assembly having a contoured inner surface about the uncured composite structure, and simultaneously applying heat and pressure to the composite structure for a predetermined time to effect curing thereof, which includes connecting the expandable pressure bag assembly to the pressure source to effect continuous application of pressure to the inner surface of the composite structure during curing thereof, the improvement wherein the step of forming an elongated mandrel assembly includes: forming first and second elongate pressure bags of thin film material having inherent release characteristics, each having a longitudinal length and a transverse inner perimeter larger than the longitudinal length and maximum transverse perimeter of the mandrel, and each having an open end and an opposite closed end; inserting the mandrel into the first pressure bag; folding the first pressure bag so that it is closely disposed about the mandrel, including forming at least one overlapped folded portion or pleat which extending longitudinally between opposite ends of the mandrel; inserting the assembly of the first pressure bag and the mandrel into the second pressure bag; folding the second pressure bag so that it is closely disposed about the first pressure bag, including forming at least one overlapped folded portion or pleat which extends longitudinally between opposite ends of the mandrel; closing the open end of the second pressure bag by sealing the two pressure bags together adjacent their open ends; and sealing the open end of the first pressure bag about a pressure fitting adapted to be connected to the pressure source. ### Claim 11 (depends on 10) The method of curing a tubular composite structure, as described in claim 10, wherein the steps of folding the first and second pressure bags to form at least one longitudinally-expending pleat in each bag comprises forming a plurality of said pleats which are uniformly spaced about each pressure bag.