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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
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。
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公开(公告)号:BR102012023612A2
公开(公告)日:2014-12-09
申请号:BR102012023612
申请日:2012-09-19
Applicant: BELL HELICOPTER TEXTRON INC
Inventor: OLDROYD PAUL , HETHCOCK JAMES DONN , FEWS ROBERT CLIVE
Abstract: The shear bonding method of the present application is configured to facilitate bonding of structures in an out-of-autoclave environment. The shear bonding method is configured to bond a plurality of frame members to the interior of a tapered tailboom (103). The frames (113a-113f) are located on a bayonet type tool (701). An adhesive pack (501) having a plurality of adhesive film layers is applied to each frame. The bayonet type tool (701) is inserted into the tailboom until the adhesive packs (501) come into contact with the interior walls of the tailboom. Conductive heating tiles (317a-317d) are applied to the exterior of the tailboom. The conductive heating tiles are controlled to first achieve and maintain viscosity of the adhesive packs. During this period the bayonet tool (701) is actuated so that the frames (113) are translated in relation to the tailboom. The heating tiles (317) are then controlled to achieve and maintain the adhesive at a requisite curing temperature.
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公开(公告)号:CA2788205C
公开(公告)日:2014-07-29
申请号:CA2788205
申请日:2012-08-29
Applicant: BELL HELICOPTER TEXTRON INC
Inventor: OLDROYD PAUL , HETHCOCK JAMES DONN , FEWS ROBERT CLIVE
Abstract: The shear bonding method of the present application is configured to facilitate bonding of structures in an out-of-autoclave environment. The shear bonding method is configured to bond a plurality of frame members to the interior of a tapered tailboom. The frames are located on a bayonet type tool. An adhesive pack having at least one adhesive layer is applied to the faying surfaces of each frame. The bayonet type tool is inserted into the tailboom until the adhesive packs come into contact with the interior walls of the tailboom. Conductive heating tiles are applied to the exterior of the tailboom. The conductive heating tiles are controlled to first achieve and maintain viscosity of the adhesive packs. During this period the bayonet tool is actuated so that the frames are translated in relation to the tailboom, thereby smearing the viscous adhesive and creating positive mechanical pressure at the bondline until the frames are located in the final position. The heating tiles are then controlled to achieve and maintain the adhesive at a requisite curing temperature.
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公开(公告)号:CA2596322C
公开(公告)日:2016-09-13
申请号:CA2596322
申请日:2006-01-24
Applicant: BELL HELICOPTER TEXTRON INC
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
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.
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公开(公告)号:CA2846669C
公开(公告)日:2016-07-26
申请号:CA2846669
申请日:2014-03-13
Applicant: BELL HELICOPTER TEXTRON INC
Inventor: MEASOM RONALD , STAMPER JAMES R , SELF ROBERT , SHERRILL PAUL , OLDROYD PAUL , MORROW NEIL EDWARD , COLE RUSSELL
IPC: B29C70/30
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:CA2786737C
公开(公告)日:2016-04-19
申请号:CA2786737
申请日:2011-02-04
Applicant: BELL HELICOPTER TEXTRON INC
Inventor: HETHCOCK JAMES D , NUNN KENNETH E , OLDROYD PAUL
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.
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公开(公告)号:CA2803434C
公开(公告)日:2015-04-07
申请号:CA2803434
申请日:2013-01-24
Applicant: BELL HELICOPTER TEXTRON INC
Inventor: LEE WEI-YUEH , OLDROYD PAUL
Abstract: The present application relates a core member for a core-stiffened structural assembly. The core member includes a plurality of cell members oriented a direction to provide a tailored stiffness in a certain direction. The core member can further include one or more planar members that can aid in shear transfer between cell members. The cell members can be made from bonding a plurality of corrugated layers together. The core-stiffened structure can be a rotor blade for an aircraft. In such an embodiment, the torsional stiffness of the rotor blade can be tailored in at least one of the chordwise and spanwise directions to provide tailor a torsional stiffness at any give location in the rotor blade.
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公开(公告)号:CA2788205A1
公开(公告)日:2013-04-13
申请号:CA2788205
申请日:2012-08-29
Applicant: BELL HELICOPTER TEXTRON INC
Inventor: OLDROYD PAUL , HETHCOCK JAMES DONN , FEWS ROBERT CLIVE
Abstract: The shear bonding method of the present application is configured to facilitate bonding of structures in an out-of-autoclave environment. The shear bonding method is configured to bond a plurality of frame members to the interior of a tapered tailboom. The frames are located on a bayonet type tool. An adhesive pack having a plurality of adhesive film layers is applied to the faying surfaces of each frame. The bayonet type tool is inserted into the tailboom until the adhesive packs come into contact with the interior walls of the tailboom. Conductive heating tiles are applied to the exterior of the tailboom. The conductive heating tiles are controlled to first achieve and maintain viscosity of the adhesive packs. During this period the bayonet tool is actuated so that the frames are translated in relation to the tailboom, thereby smearing the viscous adhesive and creating positive mechanical pressure at the bondline until the frames are located in the final position. The heating tiles are then controlled to achieve and maintain the adhesive at a requisite curing temperature.
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公开(公告)号:CA2596322A1
公开(公告)日:2006-08-17
申请号:CA2596322
申请日:2006-01-24
Applicant: BELL HELICOPTER TEXTRON INC
Inventor: ZIERER JOSEPH J , REDDY D J , LEDBETTER TIMOTHY K , TISDALE PATRICK R , STAMPS FRANK B , WIINIKKA MARK A , OLDROYD PAUL , HIROS TRICIA , MEASOM RON , MARTIN RONNIE L , CAMPBELL TOM , BRASWELL JAMES L , BASKIN CHARLES L JR , HARSE JIM , MULLINS BOB , SADLER STANLEY GENE , HAYNIE DAVID A
Abstract: An assembly for providing flexure to a blade of a rotary blade system includes 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 has a layer of cushioning material positioned thereon and secured thereto. An alternate embodiment includes 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. Another alternate embodiment includes a similar assembly having a twist-shank type of yoke for providing rotation of attached blades about their respective pitch axes.
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公开(公告)号:CA2846010C
公开(公告)日:2018-01-02
申请号:CA2846010
申请日:2014-03-12
Applicant: BELL HELICOPTER TEXTRON INC
Inventor: HETHCOCK JAMES DONN , WOLTHUIS SCOTT , BRACK ROBERT , OLDROYD PAUL
Abstract: A method of manipulating a thin-walled structure includes providing a thin-walled structure in a first unconstrained configuration, constraining the thin-walled structure to a first constrained configuration in which a first feature of the thin-walled structure is spatially located relative to the a second feature of the thin-walled structure in a predetermined manner, wherein an open volume of the thin-walled structure is constrained to maintain a predetermined open volume shape, and machining the thin-walled structure to a second constrained configuration in which the first feature of the thin-walled structure remains spatially located relative to the second feature of the thin-walled structure in the predetermined manner.
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