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公开(公告)号:US20200094450A1
公开(公告)日:2020-03-26
申请号:US16141127
申请日:2018-09-25
Applicant: Bell Helicopter Textron Inc.
Inventor: James A. Cordell , Suvankar Mishra , Andrew Paul Haldeman , Jesse J. Wrabel , Dalton T. Hampton
Abstract: A method is provided in one example embodiment and may include positioning at least one nozzle within a hollow portion of a rotor blade at a distance associated with a span of the rotor blade and providing, via the at least one nozzle, a liquid foam mixture in the hollow portion, wherein the liquid foam expands and becomes a solid foam material that fills the hollow portion of the rotor blade. Another method is provided in another example embodiment and may include providing a plurality of openings for a rotor blade that are positioned proximate to a hollow portion of the rotor blade and providing a liquid foam mixture in the hollow portion of the rotor blade through at least one opening of the rotor blade, wherein the liquid foam mixture expands and becomes a solid foam material that fills the hollow portion of the rotor blade.
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公开(公告)号:US20190084207A1
公开(公告)日:2019-03-21
申请号:US15710797
申请日:2017-09-20
Applicant: Bell Helicopter Textron Inc.
Inventor: David G. Carlson , Douglas K. Wolfe , James A. Cordell
Abstract: In one embodiment, a method may comprise heating a composite material into a viscous form, wherein the composite material comprises a thermoplastic and a plurality of reinforcement fibers, wherein the plurality of reinforcement fibers is randomly arranged within the thermoplastic. The method may further comprise extruding a plurality of strands of the composite material, wherein extruding the plurality of strands causes the plurality of reinforcement fibers within each strand to align. The method may further comprise arranging the plurality of strands of the composite material to form an assembly fixture, wherein the assembly fixture comprises an anisotropic thermal expansion property, and wherein the anisotropic thermal expansion property is based on an orientation of the plurality of reinforcement fibers within the assembly fixture.
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公开(公告)号:US11027465B2
公开(公告)日:2021-06-08
申请号:US16141127
申请日:2018-09-25
Applicant: Bell Helicopter Textron Inc.
Inventor: James A. Cordell , Suvankar Mishra , Andrew Paul Haldeman , Jesse J. Wrabel , Dalton T. Hampton
Abstract: A method is provided in one example embodiment and may include positioning at least one nozzle within a hollow portion of a rotor blade at a distance associated with a span of the rotor blade and providing, via the at least one nozzle, a liquid foam mixture in the hollow portion, wherein the liquid foam expands and becomes a solid foam material that fills the hollow portion of the rotor blade. Another method is provided in another example embodiment and may include providing a plurality of openings for a rotor blade that are positioned proximate to a hollow portion of the rotor blade and providing a liquid foam mixture in the hollow portion of the rotor blade through at least one opening of the rotor blade, wherein the liquid foam mixture expands and becomes a solid foam material that fills the hollow portion of the rotor blade.
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公开(公告)号:US20210308926A1
公开(公告)日:2021-10-07
申请号:US17242014
申请日:2021-04-27
Applicant: Bell Helicopter Textron Inc.
Inventor: David G. Carlson , Douglas K. Wolfe , James A. Cordell
IPC: B29C48/05 , B29C63/00 , B64C11/16 , B32B27/02 , B64C3/00 , B29C70/52 , B29C64/118 , B29C33/38 , B64F5/10 , B29C65/78 , B29C65/00 , B25B11/02 , B29C70/54
Abstract: In one embodiment, a method includes fastening a plurality of components of a composite structure in an assembly fixture, wherein the assembly fixture comprises a plurality of strands of a fiber-reinforced thermoplastic material, wherein the fiber-reinforced thermoplastic material comprises a thermoplastic embedded with a plurality of reinforcement fibers, wherein the plurality of reinforcement fibers is aligned within each strand of the plurality of strands, and wherein the assembly fixture further comprises an anisotropic thermal expansion property based on an orientation of the plurality of reinforcement fibers within the assembly fixture; and heating the assembly fixture in an autoclave to bond the plurality of components of the composite structure.
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公开(公告)号:US11077596B2
公开(公告)日:2021-08-03
申请号:US16814622
申请日:2020-03-10
Applicant: Bell Helicopter Textron Inc.
Inventor: David G. Carlson , Douglas K. Wolfe , James A. Cordell
IPC: B29C65/00 , B29C48/05 , B29C63/00 , B64C11/16 , B32B27/02 , B64C3/00 , B29C70/52 , B29C64/118 , B29C33/38 , B64F5/10 , B29C65/78 , B25B11/02 , B29C70/54 , B29K105/10 , B29K105/14 , B29L31/00 , B29L31/08 , B29L31/30
Abstract: In one embodiment, an assembly fixture may include a base structure including a plurality of strands of a fiber-reinforced thermoplastic material comprising a thermoplastic embedded with a plurality of reinforcement fibers, wherein the plurality of reinforcement fibers is aligned within each strand of the plurality of strands, and wherein the base structure further comprises an anisotropic thermal expansion property based on an orientation of the plurality of reinforcement fibers within the base structure, The assembly fixture may further include a plurality of fastening structures coupled to the base structure, wherein the plurality of fastening structures is configured to fasten a plurality of components of a composite structure for assembly using a heated bonding process.
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公开(公告)号:US20200346382A1
公开(公告)日:2020-11-05
申请号:US16814622
申请日:2020-03-10
Applicant: Bell Helicopter Textron Inc.
Inventor: David G. Carlson , Douglas K. Wolfe , James A. Cordell
Abstract: In one embodiment, an assembly fixture may include a base structure including a plurality of strands of a fiber-reinforced thermoplastic material comprising a thermoplastic embedded with a plurality of reinforcement fibers, wherein the plurality of reinforcement fibers is aligned within each strand of the plurality of strands, and wherein the base structure further comprises an anisotropic thermal expansion property based on an orientation of the plurality of reinforcement fibers within the base structure, The assembly fixture may further include a plurality of fastening structures coupled to the base structure, wherein the plurality of fastening structures is configured to fasten a plurality of components of a composite structure for assembly using a heated bonding process.
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公开(公告)号:US10654208B2
公开(公告)日:2020-05-19
申请号:US15710797
申请日:2017-09-20
Applicant: Bell Helicopter Textron Inc.
Inventor: David G. Carlson , Douglas K. Wolfe , James A. Cordell
IPC: B29C41/02 , B29C48/05 , B29C63/00 , B64C11/16 , B32B27/02 , B64C3/00 , B29C70/52 , B29C64/118 , B29C33/38 , B29K105/10 , B29K105/14 , B29L31/00
Abstract: In one embodiment, a method may comprise heating a composite material into a viscous form, wherein the composite material comprises a thermoplastic and a plurality of reinforcement fibers, wherein the plurality of reinforcement fibers is randomly arranged within the thermoplastic. The method may further comprise extruding a plurality of strands of the composite material, wherein extruding the plurality of strands causes the plurality of reinforcement fibers within each strand to align. The method may further comprise arranging the plurality of strands of the composite material to form an assembly fixture, wherein the assembly fixture comprises an anisotropic thermal expansion property, and wherein the anisotropic thermal expansion property is based on an orientation of the plurality of reinforcement fibers within the assembly fixture.
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