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公开(公告)号：US10723438B2
公开(公告)日：2020-07-28
申请号：US14015576
申请日：2013-08-30
Applicant: Bell Helicopter Textron Inc.
Inventor： Ronald J. Measom , Mitchell Elvin Rains
Abstract: A composite assembly has an outer spar component having an outer spar component inner profile, an inner spar component having an inner spar component outer profile substantially complementary to the outer spar component inner profile, and an adhesive disposed between the outer spar component and the inner spar component.
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公开(公告)号：US20170217109A1
公开(公告)日：2017-08-03
申请号：US15492274
申请日：2017-04-20
Applicant: Bell Helicopter Textron Inc.
Inventor： Ronald J. Measom , James R. Stamper , Robert Self , Paul Sherrill , Paul K. Oldroyd , Neil Edward Morrow , Russell Cole
CPC classification number: B29C70/342 , B23P15/04 , B29C70/46 , B29C70/541 , B29K2063/00 , B29K2105/0881 , B29K2307/04 , B29L2031/082 , B64C27/473 , B64C2027/4736 , B64F5/10 , F01D5/282 , Y10T29/49337
Abstract: A method of constructing a cured composite assembly includes positioning a composite assembly within a bonding tool, wherein the composite assembly comprises an uncured composite spar and a skin and performing a curing cycle on the composite assembly to simultaneously cure the uncured composite spar and bond the skin to the cured composite spar.
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公开(公告)号：US10005242B2
公开(公告)日：2018-06-26
申请号：US15492274
申请日：2017-04-20
Applicant: Bell Helicopter Textron Inc.
Inventor： Ronald J. Measom , James R. Stamper , Robert Self , Paul Sherrill , Paul K. Oldroyd , Neil Edward Morrow , Russell Cole
IPC: B23P15/04 , B29C41/00 , B29C70/34 , B64C11/26 , B64C27/46 , B64C27/473 , B64F5/10 , B29C70/46 , B29C70/54 , B29L31/08 , B29K105/08 , B29K307/04 , B29K63/00
CPC classification number: B29C70/342 , B23P15/04 , B29C70/46 , B29C70/541 , B29K2063/00 , B29K2105/0881 , B29K2307/04 , B29L2031/082 , B64C27/473 , B64C2027/4736 , B64F5/10 , F01D5/282 , Y10T29/49337
Abstract: A method of constructing a cured composite assembly includes positioning a composite assembly within a bonding tool, wherein the composite assembly comprises an uncured composite spar and a skin and performing a curing cycle on the composite assembly to simultaneously cure the uncured composite spar and bond the skin to the cured composite spar.
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公开(公告)号：US20170291701A1
公开(公告)日：2017-10-12
申请号：US15625598
申请日：2017-06-16
Applicant: Bell Helicopter Textron Inc.
Inventor： Robert Wardlaw , Werner Idler , John R. McCullough , Patrick Ryan Tisdale , Frank Bradley Stamps , James L. Braswell, JR. , Ronald J. Measom , Paul K. Oldroyd
CPC classification number: B29C70/30 , B29C70/202 , B29C70/38 , B29C70/382 , B29L2031/08 , B29L2031/082 , B32B5/12 , B32B5/22 , B32B5/26 , B32B37/02 , B32B37/16 , B32B37/18 , B32B38/1808 , B32B2603/00 , B64C11/02 , B64C11/04 , B64C11/12 , B64C27/32 , B64C27/33 , B64C27/48 , F01D5/02 , H05K999/99 , Y10T29/49316 , Y10T156/1062
Abstract: An apparatus comprising a soft in plane rotor yoke comprising two longitudinal side portions connected together via two outboard portions, wherein the outboard portions comprise a plurality of first layers formed of a first composite fabric material having a plurality of first fibers oriented in a first direction, and a plurality of second layers formed of a second composite fabric material having a plurality of second fibers oriented in a second direction. Included is an apparatus comprising a soft in plane rotor comprising two longitudinal side portions connected together via two outboard portions, wherein the outboard portions comprise a plurality of first layers formed of a first composite fabric material, and a plurality of second layers formed of a second composite fabric material, wherein the soft in plane rotor yoke does not comprise any narrow steered slit tape or filament windings.
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公开(公告)号：US09638048B2
公开(公告)日：2017-05-02
申请号：US13840881
申请日：2013-03-15
Applicant: Bell Helicopter Textron Inc.
Inventor： Ronald J. Measom , James R. Stamper, Jr. , Robert Self , Paul Sherrill , Paul Oldroyd , Neil Edward Morrow , Russell Cole
CPC classification number: B29C70/342 , B23P15/04 , B29C70/46 , B29C70/541 , B29K2063/00 , B29K2105/0881 , B29K2307/04 , B29L2031/082 , B64C27/473 , B64C2027/4736 , B64F5/10 , F01D5/282 , Y10T29/49337
Abstract: A method of constructing a cured composite assembly includes positioning a composite assembly within a bonding tool, wherein the composite assembly comprises an uncured composite spar and a skin and performing a curing cycle on the composite assembly to simultaneously cure the uncured composite spar and bond the skin to the cured composite spar.
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Patent Agency Ranking
公开(公告)号：US20150064013A1
公开(公告)日：2015-03-05
申请号：US14015576
申请日：2013-08-30
Applicant: Bell Helicopter Textron Inc.
Inventor： Ronald J. Measom , Mitchell Elvin Rains
IPC: B64C11/26
Abstract: A composite assembly has an outer spar component having an outer spar component inner profile, an inner spar component having an inner spar component outer profile substantially complementary to the outer spar component inner profile, and an adhesive disposed between the outer spar component and the inner spar component.
Abstract translation: 复合组件具有外部翼梁部件，其具有外部翼梁部件内部轮廓，内部翼梁部件具有与外部翼梁部件内部轮廓基本上互补的内部翼梁部件外部轮廓，以及设置在外部翼梁部件和内部翼梁之间的粘合剂 零件。
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公开(公告)号：US20140271215A1
公开(公告)日：2014-09-18
申请号：US13840881
申请日：2013-03-15
Applicant: Bell Helicopter Textron Inc.
Inventor： Ronald J. Measom , James R. Stamper, JR. , Robert Self , Paul Sherrill , Paul Oldroyd , Neil Edward Morrow , Russell Cole
CPC classification number: B29C70/342 , B23P15/04 , B29C70/46 , B29C70/541 , B29K2063/00 , B29K2105/0881 , B29K2307/04 , B29L2031/082 , B64C27/473 , B64C2027/4736 , B64F5/10 , F01D5/282 , Y10T29/49337
Abstract: A method of constructing a cured composite assembly includes positioning a composite assembly within a bonding tool, wherein the composite assembly comprises an uncured composite spar and a skin and performing a curing cycle on the composite assembly to simultaneously cure the uncured composite spar and bond the skin to the cured composite spar.
Abstract translation: 一种构建固化的复合组件的方法包括将复合组件定位在焊接工具内，其中复合组件包括未固化的复合材料翼梁和皮肤，并在复合组件上执行固化循环，以同时固化未固化的复合材料翼梁并粘合皮肤 到固化的复合材料翼梁。
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8.发明申请Fiber Orientation to Allow for Automated Ply Placement With Composite Rotor Yokes 有权纤维方向允许使用复合转子轭自动铺层公开(公告)号：US20140271209A1
公开(公告)日：2014-09-18
申请号：US13801666
申请日：2013-03-13
Applicant: BELL HELICOPTER TEXTRON INC.
Inventor： Robert Wardlaw , Werner Idler , John R. McCullough , Patrick Ryan Tisdale , Frank Bradley Stamps , James L. Braswell, JR. , Ronald J. Measom , Paul K. Oldroyd
CPC classification number: B29C70/30 , B29C70/202 , B29C70/38 , B29C70/382 , B29L2031/08 , B29L2031/082 , B32B5/12 , B32B5/22 , B32B5/26 , B32B37/02 , B32B37/16 , B32B37/18 , B32B38/1808 , B32B2603/00 , B64C11/02 , B64C11/04 , B64C11/12 , B64C27/32 , B64C27/33 , B64C27/48 , F01D5/02 , H05K999/99 , Y10T29/49316 , Y10T156/1062
Abstract: An apparatus comprising a soft in plane rotor yoke comprising two longitudinal side portions connected together via two outboard portions, wherein the outboard portions comprise a plurality of first layers formed of a first composite fabric material having a plurality of first fibers oriented in a first direction, and a plurality of second layers formed of a second composite fabric material having a plurality of second fibers oriented in a second direction. Included is an apparatus comprising a soft in plane rotor comprising two longitudinal side portions connected together via two outboard portions, wherein the outboard portions comprise a plurality of first layers formed of a first composite fabric material, and a plurality of second layers formed of a second composite fabric material, wherein the soft in plane rotor yoke does not comprise any narrow steered slit tape or filament windings.
Abstract translation: 一种包括一个平面内的转子磁轭的装置，包括通过两个外侧部分连接在一起的两个纵向侧部分，其中外侧部分包括由第一复合织物材料形成的多个第一层，所述第一复合织物材料具有沿第一方向取向的多个第一纤维， 以及由具有在第二方向上定向的多个第二纤维的第二复合织物材料形成的多个第二层。 包括一种装置，包括一个平面内的平面转子，包括通过两个外侧部分连接在一起的两个纵向侧部分，其中外侧部分包括由第一复合织物材料形成的多个第一层，以及由第二层 复合织物材料，其中所述软平面转子轭不包括任何窄的转向切割带或细丝绕组。
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公开(公告)号：US10059064B2
公开(公告)日：2018-08-28
申请号：US15625598
申请日：2017-06-16
Applicant: Bell Helicopter Textron Inc.
Inventor： Robert Wardlaw , Werner Idler , John R. McCullough , Patrick Ryan Tisdale , Frank Bradley Stamps , James L. Braswell, Jr. , Ronald J. Measom , Paul K. Oldroyd
IPC: B29C70/30 , B29C70/20 , B32B37/02 , B32B37/16 , B32B37/18 , B32B5/12 , B32B5/26 , B64C11/02 , B64C11/04 , B64C11/12 , B64C27/33 , B64C27/48 , B29C70/38 , F01D5/02 , B32B38/18 , B32B5/22 , B64C27/32 , B29L31/08
CPC classification number: B29C70/30 , B29C70/202 , B29C70/38 , B29C70/382 , B29L2031/08 , B29L2031/082 , B32B5/12 , B32B5/22 , B32B5/26 , B32B37/02 , B32B37/16 , B32B37/18 , B32B38/1808 , B32B2603/00 , B64C11/02 , B64C11/04 , B64C11/12 , B64C27/32 , B64C27/33 , B64C27/48 , F01D5/02 , H05K999/99 , Y10T29/49316 , Y10T156/1062
Abstract: An apparatus comprising a soft in plane rotor yoke comprising two longitudinal side portions connected together via two outboard portions, wherein the outboard portions comprise a plurality of first layers formed of a first composite fabric material having a plurality of first fibers oriented in a first direction, and a plurality of second layers formed of a second composite fabric material having a plurality of second fibers oriented in a second direction. Included is an apparatus comprising a soft in plane rotor comprising two longitudinal side portions connected together via two outboard portions, wherein the outboard portions comprise a plurality of first layers formed of a first composite fabric material, and a plurality of second layers formed of a second composite fabric material, wherein the soft in plane rotor yoke does not comprise any narrow steered slit tape or filament windings.
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公开(公告)号：US09714086B2
公开(公告)日：2017-07-25
申请号：US13801666
申请日：2013-03-13
Applicant: Bell Helicopter Textron Inc.
Inventor： Robert Wardlaw , Werner Idler , John R. McCullough , Patrick Ryan Tisdale , Frank Bradley Stamps , James L. Braswell, Jr. , Ronald J. Measom , Paul K. Oldroyd
CPC classification number: B29C70/30 , B29C70/202 , B29C70/38 , B29C70/382 , B29L2031/08 , B29L2031/082 , B32B5/12 , B32B5/22 , B32B5/26 , B32B37/02 , B32B37/16 , B32B37/18 , B32B38/1808 , B32B2603/00 , B64C11/02 , B64C11/04 , B64C11/12 , B64C27/32 , B64C27/33 , B64C27/48 , F01D5/02 , H05K999/99 , Y10T29/49316 , Y10T156/1062
Abstract: An apparatus comprising a soft in plane rotor yoke comprising two longitudinal side portions connected together via two outboard portions, wherein the outboard portions comprise a plurality of first layers formed of a first composite fabric material having a plurality of first fibers oriented in a first direction, and a plurality of second layers formed of a second composite fabric material having a plurality of second fibers oriented in a second direction. Included is an apparatus comprising a soft in plane rotor comprising two longitudinal side portions connected together via two outboard portions, wherein the outboard portions comprise a plurality of first layers formed of a first composite fabric material, and a plurality of second layers formed of a second composite fabric material, wherein the soft in plane rotor yoke does not comprise any narrow steered slit tape or filament windings.
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