CLOSING MEMBER FOR OPENING
    1.
    发明申请
    CLOSING MEMBER FOR OPENING 有权
    关闭会员开放

    公开(公告)号:US20120325967A1

    公开(公告)日:2012-12-27

    申请号:US13577754

    申请日:2011-02-09

    申请人: Hideto Motohashi

    发明人: Hideto Motohashi

    IPC分类号: B64D45/02 B64C1/14

    CPC分类号: B64C3/34 B64D37/32 B64D45/02

    摘要: An object of the invention is to provide a low-cost closing member for an opening having an excellent lightning protection capability.A door body 30, a clamp ring 40 made of a composite material, and an opening 12 of a wing panel 11 made of the composite material are electrically connected by surface bonding of conductive materials in a butt section of an abutment surface 34 of the door body 30 and a tapered surface 40c of the clamp ring 40 and a butt section of a tapered surface 40d of the clamp ring 40 and an abutment surface 14 of the opening 12.

    摘要翻译: 本发明的目的是提供一种具有优良的防雷能力的用于开口的低成本闭合件。 门体30,由复合材料制成的夹紧环40以及由复合材料制成的翼片11的开口12通过导电材料的表面粘接电连接在门的邻接表面34的对接部分 主体30和夹紧环40的锥形表面40c以及夹紧环40的锥形表面40d的对接部分和开口12的邻接表面14。

    WING PANEL AND AIRCRAFT MAIN WING
    2.
    发明申请

    公开(公告)号:US20120211603A1

    公开(公告)日:2012-08-23

    申请号:US13399393

    申请日:2012-02-17

    IPC分类号: B64C3/00

    摘要: There is provided a wing panel having improved formability at the time when the wing panel is curvedly formed by the peen forming method, and an aircraft main wing provided with the said wing panel. For a stringer member 20, a base part 21 is formed, and the neutral axis position N in the cross-sectional direction is located on the wing panel 11 side from the center position C in the height direction of a web part 22. When the peen forming method is carried out by projecting metal shots to a portion near a flange part 23 in the tip end portion of the stringer member 20, the tensile strain developing in the portion near a flange part 23 acts in a state in which the moment length around the neutral axis position N is kept long

    摘要翻译: 提供了一种翼板,其在翼板通过喷丸成形方法弯曲形成时具有改进的成形性,以及设置有所述翼板的飞机主翼。 对于纵梁构件20,形成基部21,并且横截面方向上的中性轴线位置N在腹板部22的高度方向上位于中心位置C的翼板11侧。当 通过将金属镜头投射到纵梁构件20的前端部中的凸缘部23附近的部分进行喷丸成形方法,在凸缘部23附近的部分中产生的拉伸应变作用在其中力矩长度 围绕中立轴位置N保持很长

    Vent stringer and aircraft main wing
    3.
    发明授权
    Vent stringer and aircraft main wing 有权
    排气纵梁和飞机主翼

    公开(公告)号:US08672269B2

    公开(公告)日:2014-03-18

    申请号:US13353703

    申请日:2012-01-19

    IPC分类号: B64C3/18

    CPC分类号: B64C3/182 B64D37/06

    摘要: A vent stringer 20 is formed by a pair of ribs 21 rising in the direction perpendicular to an inner surface 11a of a wing panel 11, and a cover 22 provided in the tip end portions of the ribs 21. With rivets 23 unexposed to an outer surface 11b of the wing panel 11, a spark is prevented from occurring in a fuel tank 30, which is provided in a main wing 10, through the rivet 23 at the time of a lightning strike. Formed by being machined integrally with the wing panel 11, the rib 21 is formed with high accuracy so as to match the curved shape of the wing panel 11. The cover 22 has only to be formed by curving a strap member so as to match the shapes of the wing panel 11 and the ribs 21.

    摘要翻译: 排气纵梁20由在翼板11的内表面11a垂直的方向上上升的一对肋21和设置在肋21的前端部的盖22形成。铆钉23未暴露于外部 翼片11的表面11b,在雷击时防止在设置在主翼10中的燃料箱30中通过铆钉23发生火花。 通过与翼板11一体地加工而形成,肋21被形成为具有与翼板11的弯曲形状相匹配的高精度。盖22仅通过弯曲带部件而形成,以便匹配 翼板11和肋21的形状。

    Method for producing structural member and structural member
    4.
    发明授权
    Method for producing structural member and structural member 有权
    生产结构件和结构件的方法

    公开(公告)号:US08986804B2

    公开(公告)日:2015-03-24

    申请号:US13578129

    申请日:2011-02-09

    IPC分类号: B32B3/14 B29D99/00 B64C3/18

    摘要: A narrow prepreg sheet 20N is bonded along a ridge C, and wide prepreg sheet 20W is bonded to other portions, whereby the wide prepreg sheet 20W having no cut line is bonded to both side portions of the ridge C.In a portion in which a spar 10 is curved, the narrow prepreg sheet 20N is bonded in an axial direction of the spar 10 while divided into plural pieces, and a length of the narrow prepreg sheet 20N is adjusted according to a radius of curvature of the curved portion in the axial direction of the spar 10, whereby various radii of curvature are easily dealt with.

    摘要翻译: 窄的预浸薄片20N沿着脊C接合,并且将宽的预浸料片20W与其它部分接合,由此将没有切割线的宽的预浸料片20W接合到脊C的两侧部分。在其中 翼片10弯曲,窄预成型片20N沿着翼梁10的轴向接合而分成多个,并且根据弯曲部分在轴向上的曲率半径来调整窄预浸薄片20N的长度 翼梁10的方向,从而容易地处理各种曲率半径。

    Closing member for opening
    5.
    发明授权
    Closing member for opening 有权
    关闭会员开放

    公开(公告)号:US08752792B2

    公开(公告)日:2014-06-17

    申请号:US13577754

    申请日:2011-02-09

    申请人: Hideto Motohashi

    发明人: Hideto Motohashi

    CPC分类号: B64C3/34 B64D37/32 B64D45/02

    摘要: An object of the invention is to provide a low-cost closing member for an opening having an excellent lightning protection capability.A door body 30, a clamp ring 40 made of a composite material, and an opening 12 of a wing panel 11 made of the composite material are electrically connected by surface bonding of conductive materials in a butt section of an abutment surface 34 of the door body 30 and a tapered surface 40c of the clamp ring 40 and a butt section of a tapered surface 40d of the clamp ring 40 and an abutment surface 14 of the opening 12.

    摘要翻译: 本发明的目的是提供一种具有优良的防雷能力的用于开口的低成本闭合件。 门体30,由复合材料制成的夹紧环40以及由复合材料制成的翼片11的开口12通过导电材料的表面粘接电连接在门的邻接表面34的对接部分 主体30和夹紧环40的锥形表面40c以及夹紧环40的锥形表面40d的对接部分和开口12的邻接表面14。

    VENT STRINGER AND AIRCRAFT MAIN WING
    6.
    发明申请
    VENT STRINGER AND AIRCRAFT MAIN WING 有权
    飞行员和飞机主飞

    公开(公告)号:US20120187246A1

    公开(公告)日:2012-07-26

    申请号:US13353703

    申请日:2012-01-19

    CPC分类号: B64C3/182 B64D37/06

    摘要: A vent stringer 20 is formed by a pair of ribs 21 rising in the direction perpendicular to an inner surface 11a of a wing panel 11, and a cover 22 provided in the tip end portions of the ribs 21. With rivets 23 unexposed to an outer surface 1 lb of the wing panel 11, a spark is prevented from occurring in a fuel tank 30, which is provided in a main wing 10, through the rivet 23 at the time of a lightning strike. Formed by being machined integrally with the wing panel 11, the rib 21 is formed with high accuracy so as to match the curved shape of the wing panel 11. The cover 22 has only to be formed by curving a strap member so as to match the shapes of the wing panel 11 and the ribs 21.

    摘要翻译: 排气纵梁20由在翼板11的内表面11a垂直的方向上上升的一对肋21和设置在肋21的前端部的盖22形成。铆钉23未暴露于外部 翼片11的表面1lb,在雷击时通过铆钉23防止在设置在主翼10中的燃料箱30中发生火花。 通过与翼板11一体地加工而形成,肋21被形成为具有与翼板11的弯曲形状相匹配的高精度。盖22仅通过弯曲带部件而形成,以便匹配 翼板11和肋21的形状。

    Closing member for opening
    7.
    发明授权
    Closing member for opening 有权
    关闭会员开放

    公开(公告)号:US08840068B2

    公开(公告)日:2014-09-23

    申请号:US13577733

    申请日:2011-02-09

    申请人: Hideto Motohashi

    发明人: Hideto Motohashi

    CPC分类号: B64C3/34 B64D37/32 B64D45/02

    摘要: An object of the invention is to provide a low-cost closing member for an opening having an excellent lightning protection capability. In a door body 30, an outer surface 31a of a plate part 31 is formed by a composite material layer 60, and a side of an inner surface 31b and a flange part 32 are formed by a metallic material layer 61. The door body 30, a clamp ring 40, and an opening 12 of a wing panel 11 are electrically connected by surface bonding of conductive materials in a butt section of an abutment surface 34 of the door body 30 and a tapered surface 40c of the clamp ring 40 and a butt section of a tapered surface 40d of the clamp ring 40 and an abutment surface 14 of the opening 12.

    摘要翻译: 本发明的目的是提供一种具有优良的防雷能力的用于开口的低成本闭合件。 在门体30中,板部31的外表面31a由复合材料层60形成,内表面31b和凸缘部32的一侧由金属材料层61形成。门体30 通过在门体30的邻接表面34的对接部分和夹紧环40的锥形表面40c之间的导电材料的表面粘合来电连接翼片11的夹环40和开口12, 夹紧环40的锥形表面40d的对接部分和开口12的邻接表面14。

    METHOD FOR PRODUCING STRUCTURAL MEMBER AND STRUCTURAL MEMBER
    8.
    发明申请
    METHOD FOR PRODUCING STRUCTURAL MEMBER AND STRUCTURAL MEMBER 有权
    生产结构构件和结构构件的方法

    公开(公告)号:US20120328819A1

    公开(公告)日:2012-12-27

    申请号:US13578129

    申请日:2011-02-09

    摘要: A narrow prepreg sheet 20N is bonded along a ridge C, and wide prepreg sheet 20W is bonded to other portions, whereby the wide prepreg sheet 20W having no cut line is bonded to both side portions of the ridge C.In a portion in which a spar 10 is curved, the narrow prepreg sheet 20N is bonded in an axial direction of the spar 10 while divided into plural pieces, and a length of the narrow prepreg sheet 20N is adjusted according to a radius of curvature of the curved portion in the axial direction of the spar 10, whereby various radii of curvature are easily dealt with.

    摘要翻译: 窄的预浸料片20N沿着脊C接合,并且宽的预浸料片20W与其它部分接合,由此将没有切割线的宽的预浸料片20W粘合到脊C的两侧部分。在其中 翼片10弯曲,窄预成型片20N沿着翼梁10的轴向接合而分成多个,并且根据弯曲部分在轴向上的曲率半径来调整窄预浸薄片20N的长度 翼梁10的方向,从而容易地处理各种曲率半径。

    PANEL MEMBER, AIRCRAFT MAIN WING, AND METHOD FOR FORMING PANEL MEMBER
    9.
    发明申请
    PANEL MEMBER, AIRCRAFT MAIN WING, AND METHOD FOR FORMING PANEL MEMBER 审中-公开
    面板会员,飞机主席,以及形成面板会员的方法

    公开(公告)号:US20120219818A1

    公开(公告)日:2012-08-30

    申请号:US13402099

    申请日:2012-02-22

    IPC分类号: B32B3/30 B23P13/00

    摘要: There is provided a panel member capable of restraining an increase in weight of a wing panel while restraining wasteful work in the manufacturing process, an aircraft main wing, and a method for forming the panel member. A wing panel 10 is formed with ridges 20 each having a dimension larger than the machining tolerance in the boundary portions between areas A1, A2, . . . Therefore, the worker who handles the wing panel 10 can visually confirm the step portions of the areas A1, A2, . . . easily. Thereby, if a flaw or the like is found in the areas A1, A2, . . . , corrective actions can be properly taken on the actually existing flaw without mistaking the flaw for the step portion of the areas A1, A2, . . . .

    摘要翻译: 提供一种面板构件,能够抑制机翼面板的重量增加,同时抑制制造过程中的浪费工作,飞行器主翼以及用于形成面板构件的方法。 翼板10形成有各自具有比区域A1,A2之间的边界部分中的加工公差大的尺寸的脊20。 。 。 因此,处理翼板10的工人可以在视觉上确认区域A1,A2的台阶部分。 。 。 容易。 因此,如果在区域A1,A2,...中发现缺陷等。 。 。 可以对实际存在的缺陷适当地采取纠正措施,而不会误认区域A1,A2的台阶部分的缺陷。 。 。 。

    CLOSING MEMBER FOR OPENING
    10.
    发明申请
    CLOSING MEMBER FOR OPENING 有权
    关闭会员开放

    公开(公告)号:US20130015294A1

    公开(公告)日:2013-01-17

    申请号:US13577733

    申请日:2011-02-09

    申请人: Hideto Motohashi

    发明人: Hideto Motohashi

    IPC分类号: B64C1/14 B64D37/02

    CPC分类号: B64C3/34 B64D37/32 B64D45/02

    摘要: An object of the invention is to provide a low-cost closing member for an opening having an excellent lightning protection capability. In a door body 30, an outer surface 31a of a plate part 31 is formed by a composite material layer 60, and a side of an inner surface 31b and a flange part 32 are formed by a metallic material layer 61. The door body 30, a clamp ring 40, and an opening 12 of a wing panel 11 are electrically connected by surface bonding of conductive materials in a butt section of an abutment surface 34 of the door body 30 and a tapered surface 40c of the clamp ring 40 and a butt section of a tapered surface 40d of the clamp ring 40 and an abutment surface 14 of the opening 12.

    摘要翻译: 本发明的目的是提供一种具有优良的防雷能力的用于开口的低成本闭合件。 在门体30中,板部31的外表面31a由复合材料层60形成,内表面31b和凸缘部32的一侧由金属材料层61形成。门体30 通过在门体30的邻接表面34的对接部分和夹紧环40的锥形表面40c之间的导电材料的表面粘合来电连接翼片11的夹环40和开口12, 夹紧环40的锥形表面40d的对接部分和开口12的邻接表面14。