公开(公告)号：WO2006130454A2

公开(公告)日：2006-12-07

申请号：PCT/US2006/020377

申请日：2006-05-26

Applicant: BELL HELICOPTER TEXTRON INC. ,  OLDROYD, Paul, K.

Inventor： OLDROYD, Paul, K.

CPC classification number: B64D15/12 ,  B32B5/024 ,  B32B5/12 ,  B32B5/26 ,  B32B2250/03 ,  B32B2250/20 ,  B32B2250/40 ,  B32B2255/02 ,  B32B2255/205 ,  B32B2260/023 ,  B32B2260/046 ,  B32B2262/101 ,  B32B2262/106 ,  B32B2307/54 ,  B32B2603/00 ,  G06F1/1628 ,  G06F1/1632 ,  H05B3/347 ,  H05B2203/007 ,  H05B2203/014 ,  H05B2203/017

Abstract: A rotor blade of a helicopter is presented. In an embodiment, the rotor blade includes a body; and a heating mat arranged in the body and configured to supply heat to said body. The heating mat includes a first plurality of fibers and a second plurality of fibers electrically connected to the first plurality of fibers. The first plurality of fibers define a positive angle smaller than about +45° relative to a first direction perpendicular to a longitudinal direction of the body. The second plurality of fibers define a negative angle greater than about -45° relative to the first direction.

Abstract translation: 呈现直升机的转子叶片。 在一个实施例中，转子叶片包括主体; 以及加热垫，其布置在所述主体中并且被配置为向所述主体供应热量。 加热垫包括第一多根纤维和与第一多根纤维电连接的第二多个纤维。 所述第一多根纤维相对于垂直于所述主体的纵向方向的第一方向限定小于约+ 45°的正角度。 第二多根纤维相对于第一方向限定大于约-45°的负角度。

公开(公告)号：WO2006086147A3

公开(公告)日：2006-12-07

申请号：PCT/US2006002413

申请日：2006-01-24

Applicant: BELL HELICOPTER TEXTRON INC ,  STAMPS FRANK B ,  TISDALE PATRICK R ,  BRASWELL JAMES L ,  BASKIN CHARLES L JR ,  CAMPBELL TOM ,  LEDBETTER TIMOTHY K ,  ZIERER JOSEPH J ,  REDDY D J ,  WIINIKKA MARK A ,  MARTIN RONNIE L ,  HAYNIE DAVID A ,  SADLER STANLEY GENE ,  MEASOM RON ,  OLDROYD PAUL ,  HIROS TRICIA ,  HARSE JIM ,  MULLINS BOB

Inventor： STAMPS FRANK B ,  TISDALE PATRICK R ,  BRASWELL JAMES L ,  BASKIN CHARLES L JR ,  CAMPBELL TOM ,  LEDBETTER TIMOTHY K ,  ZIERER JOSEPH J ,  REDDY D J ,  WIINIKKA MARK A ,  MARTIN RONNIE L ,  HAYNIE DAVID A ,  SADLER STANLEY GENE ,  MEASOM RON ,  OLDROYD PAUL ,  HIROS TRICIA ,  HARSE JIM ,  MULLINS BOB

IPC: B64C27/33 ,  B64C27/51

CPC classification number: B64C27/48 ,  B64C27/33

Abstract: An assembly for providing flexure to a blade of a rotary blade system, the assembly including an upper support plate (22) having an upper curved surface (37) , a lower support plate (24) having a lower curved surface (37) , and a yoke (120) positioned therebetween. At least one of the upper and lower yoke surfaces (37) having a layer of cushioning material (56) positioned thereon and secured thereto. The layer of cushioning material (56) extending along and following the general contour of yoke surface (37) , and the layer of cushioning material (56) directly contacting a support plate (22,24) . Another embodiment is an assembly for providing flexure to a blade of a rotary blade system, including, an upper support plate (22) having an upper curved surface (27) , a lower support plate (24) having a lower curved surface (37) , and a yoke (120) positioned therebetween and directly contacting the support plates wherein one of the curved surfaces (37) is a non-circular arc that does not form part of the circumference of a circle.

Abstract translation: 一种用于向旋转叶片系统的叶片提供挠曲的组件，所述组件包括具有上曲面（37）的上支撑板（22），具有下弯曲表面（37）的下支撑板（24），以及 位于其间的轭架（120）。 上和下轭表面（37）中的至少一个具有定位在其上并固定到其上的缓冲材料层（56）。 缓冲材料层（56）沿轭铁表面（37）的一般轮廓延伸并且跟随着磁体表面（37）的一般轮廓，缓冲材料层（56）直接接触支撑板（22,24）。 另一个实施例是用于向旋转刀片系统的刀片提供弯曲的组件，包括具有上曲面（27）的上支撑板（22），具有下弯曲表面（37）的下支撑板（24） 以及位于其间并直接接触支撑板的磁轭（120），其中一个弯曲表面（37）是不形成圆周的一部分的非圆弧。

公开(公告)号：WO2006130454A3

公开(公告)日：2007-08-09

申请号：PCT/US2006020377

申请日：2006-05-26

Applicant: BELL HELICOPTER TEXTRON INC ,  OLDROYD PAUL K

Inventor： OLDROYD PAUL K

IPC: B64D15/12 ,  B32B5/12 ,  H05B3/20 ,  H05B3/34

CPC classification number: B64D15/12 ,  B32B5/024 ,  B32B5/12 ,  B32B5/26 ,  B32B2250/03 ,  B32B2250/20 ,  B32B2250/40 ,  B32B2255/02 ,  B32B2255/205 ,  B32B2260/023 ,  B32B2260/046 ,  B32B2262/101 ,  B32B2262/106 ,  B32B2307/54 ,  B32B2603/00 ,  G06F1/1628 ,  G06F1/1632 ,  H05B3/347 ,  H05B2203/007 ,  H05B2203/014 ,  H05B2203/017

Abstract: A rotor blade of a helicopter is presented. In an embodiment, the rotor blade (100) includes a body (105) ; and a heating mat (301) arranged in the body (105) and configured to supply heat to said body. The heating mat (301) includes a first (505) plurality of fibers (400) and a second (510) plurality of fibers (400) electrically connected to the first plurality of fibers. The first plurality of fibers define a positive angle smaller than about +45° relative to a first direction perpendicular to a longitudinal direction of the body. The second plurality of fibers define a negative angle greater than about -45° relative to the first direction.

Abstract translation: 呈现直升机的转子叶片。 在一个实施例中，转子叶片（100）包括主体（105）; 以及布置在所述主体（105）中并且被配置为向所述主体供应热量的加热垫（301）。 加热垫（301）包括电连接到第一多根纤维的第一（505）多个纤维（400）和第二（510）多个纤维（400）。 所述第一多根纤维相对于垂直于所述主体的纵向方向的第一方向限定小于约+ 45°的正角度。 第二多根纤维相对于第一方向限定大于约-45°的负角度。

公开(公告)号：WO2012091695A1

公开(公告)日：2012-07-05

申请号：PCT/US2010/062211

申请日：2010-12-28

Applicant: BELL HELICOPTER TEXTRON INC. ,  MCCULLOUGH, John, R. ,  CARLSON, David, Gordon ,  HETHCOCK, James, Donn ,  OLDROYD, Paul, K. ,  MAY, Carl, A.

Inventor： MCCULLOUGH, John, R. ,  CARLSON, David, Gordon ,  HETHCOCK, James, Donn ,  OLDROYD, Paul, K. ,  MAY, Carl, A.

IPC: B64C3/18

CPC classification number: B64C1/12 ,  B29C65/4835 ,  B29C65/5021 ,  B29C65/5057 ,  B29C65/5078 ,  B29C65/5085 ,  B29C65/562 ,  B29C66/1122 ,  B29C66/1142 ,  B29C66/1162 ,  B29C66/1282 ,  B29C66/12881 ,  B29C66/43441 ,  B29C66/721 ,  B29C66/72525 ,  B29C66/8416 ,  B29D99/001 ,  B29L2031/3076 ,  B64C1/06 ,  B64C2001/0072 ,  F16B5/01 ,  F16B5/12 ,  F16B17/00 ,  Y02T50/43 ,  Y10T29/49622 ,  Y10T403/70

Abstract: A structural joint includes a first member having a first base portion and a first leg portion. The structural joint further includes a second member having a second base portion and a second base portion. The first base portion and the second base portion are coupled together at an overlapping portion. The first leg portion and the second leg portion form a cavity for structurally coupling to a structural member.

Abstract translation: 结构接头包括具有第一基部和第一腿部的第一构件。 结构接头还包括具有第二基部和第二基部的第二构件。 第一基部和第二基部在重叠部分处连接在一起。 第一腿部分和第二腿部部分形成用于结构上结合到结构构件的空腔。

公开(公告)号：WO2010027361A1

公开(公告)日：2010-03-11

申请号：PCT/US2008/075336

申请日：2008-09-05

Applicant: BELL HELICOPTER TEXTRON INC. ,  RELLER, Dan ,  OLDROYD, Paul

Inventor： RELLER, Dan ,  OLDROYD, Paul

IPC: B05C5/04

CPC classification number: B32B7/12 ,  B32B3/12 ,  B32B5/02 ,  B32B5/147 ,  B32B5/24 ,  B32B9/007 ,  B32B9/04 ,  B32B15/04 ,  B32B15/20 ,  B32B27/06 ,  B32B27/16 ,  B32B27/34 ,  B32B2262/101 ,  B32B2307/102 ,  B32B2307/50 ,  B32B2307/718 ,  B32B2405/00 ,  B32B2603/00 ,  B32B2605/00 ,  B32B2605/18 ,  C09J7/26 ,  C09J2201/20 ,  C09J2201/36 ,  Y10T156/1057 ,  Y10T428/24298 ,  Y10T428/24331

Abstract: A present system of the present application provides for reticulating adhesive to the surface network of cellular core. As such, the present invention allows for substantial improvements over prior systems. The present invention may be implemented with any aircraft, wind turbine, rocket, space satellite, or land vehicle, but there is nothing within the spirit and scope of the present invention limiting it to any particular application. The teachings of the present invention are useful to any composite structure utilizing cellular core.

Abstract translation: 本申请的本发明系统提供将粘合剂网状结合到蜂窝芯的表面网络上。 因此，本发明允许相对于现有系统的实质性改进。 本发明可以用任何飞行器，风力涡轮机，火箭，太空卫星或陆上车辆来实现，但是在本发明的精神和范围内没有任何限制于任何特定应用。 本发明的教导对于利用细胞核的任何复合结构是有用的。

公开(公告)号：WO2009096964A1

公开(公告)日：2009-08-06

申请号：PCT/US2008/052546

申请日：2008-01-31

Applicant: BELL HELICOPTER TEXTRON INC. ,  HIROS, Tricia ,  STAMPS, Frank, Bradley ,  TISDALE, Pat ,  MEASOM, Ron ,  BRASWELL, Jim ,  CAMPBELL, Tom ,  OLDROYD, Paul, K. ,  BARBOUR, Richard

Inventor： HIROS, Tricia ,  STAMPS, Frank, Bradley ,  TISDALE, Pat ,  MEASOM, Ron ,  BRASWELL, Jim ,  CAMPBELL, Tom ,  OLDROYD, Paul, K. ,  BARBOUR, Richard

IPC: B64C27/00

CPC classification number: B64C27/32 ,  B64C27/33

Abstract: A method of making a rotor yoke includes preparing a cured composite rotor yoke preform on a single-sided curing tool and machining at least one portion of the cured rotor yoke preform to form a rotor yoke. In one embodiment, preparing the cured composite rotor yoke is accomplished by applying successive layers of uncured polymeric composite material to a single-sided tool in a configuration to produce an uncured rotor yoke preform; disposing a semi-rigid caul to an untooled side of the uncured rotor yoke preform; enclosing the uncured rotor yoke preform and the semi-rigid caul by substantially hermetically sealing a vacuum bag to the tool; substantially evacuating a volume defined by the vacuum bag and the tool of air; and heating the uncured rotor yoke preform, sometimes under pressure, to form the cured composite rotor yoke preform.

Abstract translation: 制造转子轭铁的方法包括在单侧固化工具上制备固化的复合转子轭预制件，并且对固化的转子轭预制件的至少一部分进行加工以形成转子轭。 在一个实施方案中，通过将未固化的聚合物复合材料的连续层施加到单面工具以制备未固化的转子轭预制件的构型来实现固化的复合转子轭的制备; 将半刚性盖子设置在未固化转子轭预制件的未固定侧; 通过将真空袋基本气密地密封到所述工具上来封装未固化的转子轭预制件和半刚性盖子; 基本上排空由真空袋和空气工具限定的体积; 有时在压力下加热未固化的转子轭预制件，以形成固化的复合转子轭预制件。

公开(公告)号：WO2009078871A1

公开(公告)日：2009-06-25

申请号：PCT/US2007/087931

申请日：2007-12-18

Applicant: BELL HELICOPTER TEXTRON INC. ,  MARHSALL, Bryan ,  SHERRIL, Paul ,  BASKIN, Bryan, K. ,  HIROS, Tricia ,  OLDROYD, Paul, K.

Inventor： MARHSALL, Bryan ,  SHERRIL, Paul ,  BASKIN, Bryan, K. ,  HIROS, Tricia ,  OLDROYD, Paul, K.

IPC: B64C11/16 ,  B64C27/46

CPC classification number: B64C27/473 ,  B64C2027/4736

Abstract: A helicopter rotor blade includes a structural composite skin defining a cavity therein; a composite spar disposed within the cavity and adhesively bonded to the skin, a portion of the spar exhibiting a C-shape in cross section; and a foam core disposed within the cavity and adhesively bonded to the skin. The structural composite skin forms an external, closed box structure configured to transmit mechanical loads encountered by the rotor blade.

Abstract translation: 直升机转子叶片包括在其中限定腔室的结构复合皮肤; 复合翼梁，其设置在所述腔体内并且粘合地粘合到所述皮肤上，所述翼梁的一部分呈横截面为C形; 以及泡沫芯，其设置在所述腔内并且粘合到所述皮肤上。 结构复合皮肤形成外部封闭的箱体结构，其构造成传递由转子叶片遇到的机械载荷。

公开(公告)号：WO2011097433A1

公开(公告)日：2011-08-11

申请号：PCT/US2011/023681

申请日：2011-02-04

Applicant: BELL HELICOPTER TEXTRON INC. ,  HETHCOCK, James, D. ,  NUNN, Kenneth, E. ,  OLDROYD, Paul

Inventor： HETHCOCK, James, D. ,  NUNN, Kenneth, E. ,  OLDROYD, Paul

IPC: B32B3/26

CPC classification number: B32B5/26 ,  B32B3/12 ,  B32B3/20 ,  B32B5/12 ,  B32B5/28 ,  B32B7/04 ,  B32B7/12 ,  B32B27/04 ,  B32B27/12 ,  B32B2250/40 ,  B32B2255/02 ,  B32B2255/26 ,  B32B2260/021 ,  B32B2260/046 ,  B32B2262/0269 ,  B32B2262/106 ,  B32B2307/50 ,  D04C3/48 ,  Y10T428/24074 ,  Y10T428/31504

Abstract: A composite core includes a plurality of tubes, each the plurality of tubes comprising a plurality of fibers disposed in a polymeric matrix. Adjacent tubes of the plurality of tubes are adhesively bonded to one another along sides of the adjacent tubes. A method of making a composite core includes the steps of providing a plurality of tubes, each of the plurality of tubes including a plurality of fibers disposed in a polymeric matrix, and adhesively bonding adjacent tubes of the plurality of tubes along sides of the adjacent tubes. A method of making a composite core such that a removable band is included in the core, the removable band being configured to be removable through a procedure subsequent to the cure of the composite core, thereby producing gaps in the core.

Abstract translation: 复合芯包括多个管，每个管包括设置在聚合物基体中的多根纤维。 多个管的相邻管沿着相邻管的侧面彼此粘合。 制造复合芯的方法包括提供多个管的步骤，多个管中的每一个包括设置在聚合物基体中的多根纤维，并且沿着相邻管的侧面粘附多个管的相邻管 。 一种制造复合芯的方法，使得芯中包含可移除带，可移除带被配置为通过复合芯固化之后的过程可移除，从而在芯中产生间隙。

公开(公告)号：WO2006086147A2

公开(公告)日：2006-08-17

申请号：PCT/US2006/002413

申请日：2006-01-24

Applicant: BELL HELICOPTER TEXTRON, INC. ,  STAMPS, Frank, B. ,  TISDALE, Patrick, R. ,  BRASWELL, James, L. ,  BASKIN, Charles, L., Jr. ,  CAMPBELL, Tom ,  LEDBETTER, Timothy, K. ,  ZIERER, Joseph, J. ,  REDDY, D., J. ,  WIINIKKA, Mark, A. ,  MARTIN, Ronnie, L. ,  HAYNIE, David, A. ,  SADLER, Stanley, Gene ,  MEASOM, Ron ,  OLDROYD, Paul ,  HIROS, Tricia ,  HARSE, Jim ,  MULLINS, Bob

Inventor： STAMPS, Frank, B. ,  TISDALE, Patrick, R. ,  BRASWELL, James, L. ,  BASKIN, Charles, L., Jr. ,  CAMPBELL, Tom ,  LEDBETTER, Timothy, K. ,  ZIERER, Joseph, J. ,  REDDY, D., J. ,  WIINIKKA, Mark, A. ,  MARTIN, Ronnie, L. ,  HAYNIE, David, A. ,  SADLER, Stanley, Gene ,  MEASOM, Ron ,  OLDROYD, Paul ,  HIROS, Tricia ,  HARSE, Jim ,  MULLINS, Bob

IPC: B64C27/33 ,  B64C27/51

CPC classification number: B64C27/48 ,  B64C27/33

Abstract: An assembly for providing flexure to a blade of a rotary blade system, the assembly including an upper support plate having an upper curved surface, a lower support plate having a lower curved surface, and a yoke positioned therebetween. At least one of the upper and lower yoke surfaces having a layer of cushioning material positioned thereon and secured thereto. The layer of cushioning material extending along and following the general contour of yoke surface, and the layer of cushioning material directly contacting a support plate. Another embodiment is an assembly for providing flexure to a blade of a rotary blade system, including, an upper support plate having an upper curved surface, a lower support plate having a lower curved surface, and a yoke positioned therebetween and directly contacting the support plates wherein one of the curved surfaces is a non-circular arc that does not form part of the circumference of a circle.

Abstract translation: 一种用于向旋转叶片系统的叶片提供挠曲的组件，该组件包括具有上曲面的上支撑板，具有下弯曲表面的下支撑板和位于其间的轭。 上和下磁轭表面中的至少一个具有定位在其上并固定到其上的缓冲材料层。 缓冲材料层沿着轭铁表面的一般轮廓延伸并且沿着磁体表面的一般轮廓延伸，并且缓冲材料层直接接触支撑板。 另一个实施例是用于向旋转刀片系统的刀片提供弯曲的组件，包括具有上曲面的上支撑板，具有下弯曲表面的下支撑板和位于其间的直接接触支撑板 其中一个弯曲表面是不形成圆周的一部分的非圆弧。