-
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.
-
公开(公告)号：US20160089844A1
公开(公告)日：2016-03-31
申请号：US14496271
申请日：2014-09-25
Applicant: Bell Helicopter Textron Inc.
Inventor： Suvankar Mishra , Jesse Wrabel , John R. McCullough , Randall Willnow , Carl May
CPC classification number: B29C73/10 , B29C44/1214 , B29C44/1276 , B29C44/128 , B29C44/18 , B29C66/02241 , B29C73/02 , B29C73/04 , B29C73/06 , B29C2073/264 , B29L2031/082 , B29L2031/3076 , B29L2031/3085 , B29L2031/3088 , B29L2031/608 , B64F5/40
Abstract: A method of repairing a core stiffened structure can include removing a damaged portion of the core stiffened structure; creating a cutout in a portion of a repair core member; fitting the repair core member onto an existing core member such that the cutout mates with a portion of the existing core member; bonding the repair core member to the existing core member; and placing a skin patch over the repair core member.
Abstract translation: 修复芯加固结构的方法可以包括去除芯加固结构的损坏部分; 在修复核心部件的一部分中形成切口; 将修复芯构件装配到现有的芯构件上，使得切口与现有芯构件的一部分配合; 将修复芯构件粘合到现有的芯构件上; 并将皮肤贴片放置在修复芯部件上。
-
公开(公告)号：US10814567B2
公开(公告)日：2020-10-27
申请号：US16244295
申请日：2019-01-10
Applicant: Bell Helicopter Textron Inc.
Inventor： David G. Carlson , John R. McCullough , Douglas K. Wolfe , Andrew G. Baines , George R. Decker
IPC: B29C70/34 , B64C1/12 , B29C70/30 , B64F5/10 , B64C3/24 , B29C35/02 , B29C70/06 , B29C70/54 , B29D99/00 , B64C3/26 , B64C29/00 , B29C65/48 , B32B3/12 , B32B7/12 , B64C3/18 , B64F5/00 , B29L31/30
Abstract: In one aspect, there is a method of making a pre-cured laminate having a total number of plies in a mold, the mold having a cavity with a periphery defined by a forward edge, an aft edge, and outboard ends. The method includes selecting a first plurality of resin impregnated plies that continuously extend beyond the periphery of the cavity, the first plurality of resin impregnated plies includes at least 50 percent of the total number of plies; laying the plies in a mold; compacting the plies in a mold; and pre-curing the plies to form a pre-cured laminate, which can extend beyond the periphery of the cavity. In an embodiment, a pre-cured laminate includes a first plurality of resin impregnated plies that continuously extend beyond the periphery of the cavity.
-
公开(公告)号：US10589850B2
公开(公告)日：2020-03-17
申请号：US15936866
申请日：2018-03-27
Applicant: Bell Helicopter Textron Inc.
Inventor： Jeffrey Paul Nissen , John R. McCullough
IPC: B64C27/473 , F01D5/28 , F04D29/22 , B64C29/00
Abstract: An erosion protection system (EPS) has a first erosion protection unit (EPU) having a first ligament and a first scale attached to the first ligament, the first scale having an outer hardness that is greater than a hardness of the first ligament. The EPS also has a second EPU having a second ligament and a second scale attached to the second ligament, the second scale having an outer hardness that is greater than a hardness of the second ligament. The EPS also has an interstitial space between the first ligament and the second ligament wherein at least one of (1) the first scale overlaps at least a portion of the second EPU and (2) the second scale overlaps at least a portion of the first EPU.
-
公开(公告)号：US20190143613A1
公开(公告)日：2019-05-16
申请号：US16244295
申请日：2019-01-10
Applicant: Bell Helicopter Textron Inc.
Inventor： David G. Carlson , John R. McCullough , Douglas K. Wolfe , Andrew G. Baines , George R. Decker
Abstract: In one aspect, there is a method of making a pre-cured laminate having a total number of plies in a mold, the mold having a cavity with a periphery defined by a forward edge, an aft edge, and outboard ends. The method includes selecting a first plurality of resin impregnated plies that continuously extend beyond the periphery of the cavity, the first plurality of resin impregnated plies includes at least 50 percent of the total number of plies; laying the plies in a mold; compacting the plies in a mold; and pre-curing the plies to form a pre-cured laminate, which can extend beyond the periphery of the cavity. In an embodiment, a pre-cured laminate includes a first plurality of resin impregnated plies that continuously extend beyond the periphery of the cavity.
-
Patent Agency Ranking
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.
-
公开(公告)号：US20170225769A1
公开(公告)日：2017-08-10
申请号：US15423888
申请日：2017-02-03
Applicant: Bell Helicopter Textron Inc.
Inventor： David G. Carlson , John R. McCullough , Douglas K. Wolfe , George R. Decker , Keith A. Stanney
CPC classification number: B29C70/34 , B29C35/02 , B29C65/48 , B29C70/06 , B29C70/30 , B29C70/545 , B29C2793/009 , B29D99/001 , B29D99/0089 , B29L2031/3076 , B29L2031/3085 , B32B3/12 , B32B7/12 , B32B2250/05 , B32B2305/024 , B32B2605/18 , B64C1/12 , B64C3/185 , B64C3/24 , B64C3/26 , B64C29/0033 , B64F5/00 , B64F5/10 , Y02T50/43
Abstract: A method of manufacturing a tiltrotor wing structure including providing a spar mold having a plurality of bores extending from an exterior surface of the mold to an interior surface of the mold, the plurality of bores corresponding to a plurality of primary coordination holes in a spar member, the spar mold having a periphery defined by a top edge, a bottom edge and outboard ends; selecting a plurality of resin impregnated plies to ensure that the plies continuously extend beyond the periphery of the spar mold; laying the plies in the spar mold; curing the plies in the mold to form a cured spar member that extends beyond the periphery of the spar mold; and accurately drilling a plurality of primary coordination holes in the cured spar member in the spar mold using a tool positioned in the plurality of bores.
-
公开(公告)号：US09550334B2
公开(公告)日：2017-01-24
申请号：US14496271
申请日：2014-09-25
Applicant: Bell Helicopter Textron Inc.
Inventor： Suvankar Mishra , Jesse Wrabel , John R. McCullough , Randall Willnow , Carl May
IPC: B29C44/12 , B29C73/02 , B29C73/04 , B29C73/06 , B29C73/10 , B29C65/00 , B29C44/18 , B64F5/00 , B29L31/30 , B29L31/08 , B29L31/60 , B29C73/26
CPC classification number: B29C73/10 , B29C44/1214 , B29C44/1276 , B29C44/128 , B29C44/18 , B29C66/02241 , B29C73/02 , B29C73/04 , B29C73/06 , B29C2073/264 , B29L2031/082 , B29L2031/3076 , B29L2031/3085 , B29L2031/3088 , B29L2031/608 , B64F5/40
Abstract: A method of repairing a core stiffened structure can include removing a damaged portion of the core stiffened structure; creating a cutout in a portion of a repair core member; fitting the repair core member onto an existing core member such that the cutout mates with a portion of the existing core member; bonding the repair core member to the existing core member; and placing a skin patch over the repair core member.
Abstract translation: 修复芯加固结构的方法可以包括去除芯加固结构的损坏部分; 在修复核心部件的一部分中形成切口; 将修复芯构件装配到现有的芯构件上，使得切口与现有芯构件的一部分配合; 将修复芯构件粘合到现有的芯构件上; 并将皮肤贴片放置在修复芯部件上。
-
公开(公告)号：US20160300003A1
公开(公告)日：2016-10-13
申请号：US15092969
申请日：2016-04-07
Applicant: Bell Helicopter Textron Inc.
Inventor： Jonathan A. Knoll , Jeffrey P. Nissen , John R. McCullough
IPC: G06F17/50
CPC classification number: G06F17/5018 , G06F17/5086
Abstract: A method of performing structural analysis relating to a component having CAD-based geometry, refined CAD-based geometry and CAD-based FEA data associated therewith. The method includes scanning the component to obtain scan-based point cloud geometry of the component, aligning the scan-based point cloud geometry with the CAD-based geometry of the component, generating scan-based geometry of the component by refining the scan-based point cloud geometry, comparing the scan-based geometry with the refined CAD-based geometry of the component to quantify geometric differences therebetween, generating scan-based FEA geometry of the component by meshing the scan-based geometry, performing finite element analysis on the scan-based FEA geometry to obtain scan-based FEA data and comparing the scan-based FEA data with the CAD-based FEA data of the component to quantify the effect of geometric difference therebetween.
Abstract translation: 执行关于具有基于CAD的几何，基于精简的基于CAD的几何和与其相关联的基于CAD的FEA数据的组件的结构分析的方法。 该方法包括扫描组件以获得组件的基于扫描的点云几何，使基于扫描的点云几何与组件的基于CAD的几何对齐，通过精炼基于扫描的基于扫描的点云几何 将基于扫描的几何与基于组件的基于CAD的几何组合进行比较，以量化其间的几何差异，通过网格化基于扫描的几何形状生成基于扫描的FEA几何形状，对扫描进行有限元分析 的FEA几何，以获得基于扫描的FEA数据，并将基于扫描的FEA数据与组件的基于CAD的FEA数据进行比较，以量化其间几何差异的影响。
-
30.发明授权Method of repairing, splicing, joining, machining, and stabilizing honeycomb core using pourable structural foam and a structure incorporating the same 有权使用可流动的结构泡沫体进行修复，拼接，接合，加工和稳定蜂窝芯的方法以及结合其的结构公开(公告)号：US09149999B2
公开(公告)日：2015-10-06
申请号：US13664010
申请日：2012-10-30
Applicant: Bell Helicopter Textron Inc.
Inventor： Ramesh Thiagarajan , Theodore W. Ingram, III , John R. McCullough , Suvankar Mishra , Carl May
CPC classification number: B32B3/12 , B29C73/06 , B29C73/10 , B29C2073/264 , B29L2031/082 , B29L2031/608 , Y10T428/24008 , Y10T428/24157 , Y10T428/249953
Abstract: A method of the present disclosure includes of repairing a core stiffened structure with structural foam. Another method includes splicing core members together using structural foam. Another method includes joining a core member to a structure using structural foam. Another method includes using structural foam to stabilize a core member during a machining process. Another method includes stabilizing a core member with structural foam to prevent the core member from crushing in autoclave pressure. The present disclosure further includes a core stiffened structure have a core member with structural foam therein.
Abstract translation: 本公开的方法包括用结构泡沫修复芯加固结构。 另一种方法包括使用结构泡沫将芯部件拼接在一起。 另一种方法包括使用结构泡沫将芯构件连接到结构上。 另一种方法包括在加工过程中使用结构泡沫来稳定芯构件。 另一种方法包括用结构泡沫稳定芯部件以防止芯件在高压釜压力下破碎。 本公开还包括具有在其中具有结构泡沫的芯构件的芯加强结构。
-
-
-
-
-
-
-
-
-
Search Results
38
records
(took 0.02 seconds)
