| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 61 | 包装盒（扭力杆） | CN201930548937.6 | 2019-10-10 | CN305741528S | 2020-04-28 | 王彬威 |
| 1.本外观设计产品的名称：包装盒（扭力杆）。 2.本外观设计产品的用途：用于包装扭力杆的包装盒。 3.本外观设计产品的设计要点：在于形状与图案的结合。 4.最能表明设计要点的图片或照片：主视图。 | ||||||
| 62 | 包装盒(扭力扳手) | CN200930261510.4 | 2009-09-30 | CN301244360S | 2010-06-02 | 李书山 |
| 俯视图与仰视图对称，省略俯视图；右视图与左视图相同，省略右视图。 | ||||||
| 63 | 包装盒（扭力胶心） | CN200330112108.2 | 2003-11-15 | CN3382891D | 2004-08-04 | 陈启泰 |
| 64 | 包装盒（扭力胶芯） | CN201730121990.9 | 2017-04-13 | CN304339595S | 2017-11-03 | 吴清源; 吴英真 |
| 1．本外观设计产品的名称：包装盒（扭力胶芯）； 2．本外观设计产品的用途：本外观设计产品用于物品的包装； 3．本外观设计产品的设计要点：在于产品外观设计的形状、图案及其结合； 4．最能表明本外观设计设计要点的图片或照片：立体图。 | ||||||
| 65 | 包装盒(扭力胶芯) | CN201530476417.0 | 2015-11-18 | CN303639324S | 2016-04-13 | 赵素伟 |
| 1.本外观设计产品的名称：包装盒(扭力胶芯)。2.本外观设计产品的用途：主要用于产品的外包装。3.本外观设计的设计要点：图案和色彩的结合。4.本外观设计以主视图最能表明设计要点。5.本外观设计产品仰视无保护要点，故省略仰视图；后视图与主视图相同，故省略后视图。6.本外观设计请求保护色彩。 | ||||||
| 66 | 包装盒（扭力工具） | CN201130394096.1 | 2011-10-31 | CN302495119S | 2013-07-10 | 张健儿 |
| 1．本外观设计产品的名称：包装盒（扭力工具）。2．本外观设计产品的用途：一种包装盒，尤其涉及扭力工具的包装盒。3．本外观设计的设计要点：该外观设计产品的外观形状。4．最能表明设计要点的图片或者照片：设计1主视图。 | ||||||
| 67 | 包装盒(扭力衬套) | CN02350081.6 | 2002-07-15 | CN3291180D | 2003-04-30 | 陈启泰 |
| 后视图与主视图相同，故省略后视图。 | ||||||
| 68 | 扭力扳手套装包装盒 | CN202230427188.3 | 2022-07-07 | CN307721031S | 2022-12-13 | 苏华强 |
| 1.本外观设计产品的名称：扭力扳手套装包装盒。 2.本外观设计产品的用途：用作工具箱，用于收纳手工锤、钻头、螺丝刀等工具。 3.本外观设计产品的设计要点：在于内部形状，收纳陈设。 4.最能表明设计要点的图片或照片：打开状态图1。 | ||||||
| 69 | 包装盒(扭力胶芯) | CN201230242221.1 | 2012-06-12 | CN302173734S | 2012-11-14 | 杨丽玉 |
| 1.本外观设计产品的名称：包装盒(扭力胶芯)。2.本外观设计产品的用途：主要用于产品的外包装。3.本外观设计的设计要点：图案。4.本外观设计以主视图最能表明设计要点。5.本外观设计产品底部无保护要点，故省略仰视图；后视图与主视图相同，故省略后视图。 | ||||||
| 70 | COMPOSITE STRUCTURAL ELEMENT AND TORSION BOX | US14627255 | 2015-02-20 | US20150239207A1 | 2015-08-27 | Sergey SELYUGIN; Jan-Ronald BALZER |
| This relates to a composite structural element, in particular a rib or a spar, specifically for use in a torsion box of an aircraft structure such as a vertical tailplane, wherein the structural element defines a coordinate system with a first axis “a” wherein the structural element comprises a substantially planar main section defining a coordinate system with a first axis “a” extending along the longitudinal axis “L” of the structural element and a second axis “b” extending perpendicular to said longitudinal axis “L” within the planar main section and defining an angle of +90° with the first axis “a”, wherein the structural element contains a lay-up of single plies consisting of a fiber-reinforced composite material with a substantially unidirectional fiber orientation. | ||||||
| 71 | MULTI-SPAR TORSION BOX STRUCTURE | US15160957 | 2016-05-20 | US20160340022A1 | 2016-11-24 | Carlos Garcia Nieto; Soledad Crespo Pena; Jesus Javier Vazquez Castro |
| The present disclosure refers to a multi-spar torsion box structure comprising a plurality of spars of composite material arranged to form a multi-cell structure with two or more cells extending span-wise at the torsion box, and upper and lower skin covers of composite material respectively joined to upper and lower surfaces of the multi-cell structure. The structure further comprises at least one belt-like reinforcing element extending on the outer perimeter of the torsion box, and fixed to the upper and lower surfaces of the multi-cell structure, and transversely arranged with respect to the span-wise direction of the torsion box. The belt-like reinforcing element is made of a metallic or a composite material. The present disclosure can advantageously be used in the manufacture of aircrafts lifting surfaces, such as horizontal tail planes (HTP) or wings. | ||||||
| 72 | HORIZONTAL TAIL PLANE WITH A MULTI-RIB TORSION BOX | EP15382231.7 | 2015-05-05 | EP3090940B1 | 2017-12-06 | Pereira Mosqueira, Fernando; Marasco, Andrea-Ivan |
| The present invention relates to an aircraft horizontal tail plane (HTP) having a multi-rib torsion box formed by first (1a) and second (1b) lateral torsion boxes symmetrically arranged with respect to a plane of symmetry (X-X) of the horizontal tail plane (8). A group of ribs (4a,4b) are substantially parallel to the plane of symmetry (X-X) of the horizontal tail plane (8), and stringers (7a,7b) are arranged so as to define an angle within the range 80°-100° with respect to the plane of symmetry (X-X) of the horizontal tail plane (8). Due to this relative arrangement of the ribs (4a,4b) and stringers (7a,7b), the stringers (7a,7b) are not continuous through ribs (4a,4b), thus the ribs (4a,4b) can be manufactured without mouse holes. The HTP (8) of the invention can be manufactured easier and faster than traditional HTP designs. | ||||||
| 73 | HORIZONTAL TAIL PLANE WITH A MULTI-RIB TORSION BOX | EP15382231.7 | 2015-05-05 | EP3090940A1 | 2016-11-09 | Pereira Mosqueira, Fernando; Marasco, Andrea-Ivan |
The present invention relates to an aircraft horizontal tail plane (HTP) having a multi-rib torsion box formed by first (1a) and second (1b) lateral torsion boxes symmetrically arranged with respect to a plane of symmetry (X-X) of the horizontal tail plane (8). A group of ribs (4a,4b) are substantially parallel to the plane of symmetry (X-X) of the horizontal tail plane (8), and stringers (7a,7b) are arranged so as to define an angle within the range 80°-100° with respect to the plane of symmetry (X-X) of the horizontal tail plane (8). Due to this relative arrangement of the ribs (4a,4b) and stringers (7a,7b), the stringers (7a,7b) are not continuous through ribs (4a,4b), thus the ribs (4a,4b) can be manufactured without mouse holes. The HTP (8) of the invention can be manufactured easier and faster than traditional HTP designs.
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| 74 | HORIZONTAL TAIL PLANE WITH A MULTI-RIB TORSION BOX | US15147202 | 2016-05-05 | US20160325822A1 | 2016-11-10 | Fernando Pereira Mosqueira; Andrea-Ivan Marasco |
| The present disclosure generally refers to an aircraft horizontal tail plane (HTP) having a multi-rib torsion box formed by first and second lateral torsion boxes symmetrically arranged with respect to a plane of symmetry of the horizontal tail plane. A group of ribs are substantially parallel to the plane of symmetry of the horizontal tail plane, and the stringers are arranged as to define an angle within the range 80°-100° with respect to the plane of symmetry of the horizontal tail plane. Due to this relative arrangement of the ribs and stringers, the stringers are not continuous through ribs, thus the ribs can be manufactured without mouse holes. The HTP of the invention can be manufactured easier and faster than traditional HTP designs. | ||||||
| 75 | Pale en matériaux composites, à structure bilongeron et bicaisson, et à revêtements stratifiés à sandwich de nid d'abeilles, et son procédé de fabrication | EP87401748.6 | 1987-07-27 | EP0256916B1 | 1989-11-02 | Bost, Michel |
| 76 | 一种电机扭力测试工装 | CN201810841572.0 | 2018-07-27 | CN108613767A | 2018-10-02 | 孙伟; 郭文西; 陆富贵; 张国扬 |
| 本发明公开了一种电机扭力测试工装，包括基座，基座上设有电控盒和竖向设置的扭力传感器，扭力传感器与基座固定连接；扭力传感器的上端连接有联轴器，扭力传感器的外围设有支撑架，支撑架上位于联轴器的上方设有电机固定板，电机固定板的中部对应联轴器处开设有供待测电机的输出轴穿过的通孔；电控盒内设有扭力测试仪，扭力传感器与扭力测试仪电连接，扭力测试仪包括扭力显示面板，扭力显示面板设于电控盒的上表面上，电控盒上设有正反转切换开关、电容接线柱和电机接线柱。本发明的电机扭力测试工装，测试过程方便，测试速度快，能够满足批量检测。 | ||||||
| 77 | 一种汽车非金属零件抗扭力测试装置 | CN202310840213.4 | 2023-07-10 | CN116929741A | 2023-10-24 | 李文丰; 孙迪 |
| 本发明公开了一种汽车非金属零件抗扭力测试装置，属于汽车非金属零件测试技术领域，包括抗扭力测试柜台，所述抗扭力测试柜台的顶部连接有抗扭力测试架，所述抗扭力测试架的支撑面上开设有多个抗扭力测试口，多个抗扭力测试口内均套装有抗扭力测试组件。本发明中，抗扭力测试轴在抗扭力测试弹簧复位弹性力的作用下完成复位动作，工业电机继续工作，对下一个待测试非金属零件做扭力测试，接着相关工作人员将已完成扭力测试的汽车非金属零件取出，并将新的待测试非金属零件放入对应的下层抗扭力测试盒内等待下一个循环测试，实现连续对多个汽车非金属零件进行扭力测试，有效提升了汽车非金属零件抗扭力测试的工作效率，且结构简单，实用性强。 | ||||||
| 78 | 分离式成像装置 | CN201710330661.4 | 2017-05-11 | CN107229210B | 2020-05-22 | 林嘉信; 高然星 |
| 本发明涉及一种分离式成像装置包含感光组体、墨粉盒体及至少一个扭力弹簧。感光组体包含壳件及感光鼓。壳件具有容置槽。感光鼓装设于壳件，并位于容置槽的一侧。墨粉盒体可脱离地位于容置槽。扭力弹簧位于容置槽。扭力弹簧的一段装设于壳件，且扭力弹簧的相对一段抵靠于墨粉盒体背向感光鼓的一侧，以使墨粉盒体朝感光鼓靠近。 | ||||||
| 79 | 分离式成像装置 | CN201710330661.4 | 2017-05-11 | CN107229210A | 2017-10-03 | 林嘉信; 高然星 |
| 本发明涉及一种分离式成像装置包含感光组体、墨粉盒体及至少一个扭力弹簧。感光组体包含壳件及感光鼓。壳件具有容置槽。感光鼓装设于壳件，并位于容置槽的一侧。墨粉盒体可脱离地位于容置槽。扭力弹簧位于容置槽。扭力弹簧的一段装设于壳件，且扭力弹簧的相对一段抵靠于墨粉盒体背向感光鼓的一侧，以使墨粉盒体朝感光鼓靠近。 | ||||||
| 80 | 一种用于适配对开门车型的车辆结构及汽车 | CN202211294493.5 | 2022-10-21 | CN115593516A | 2023-01-13 | 张印; 赵栋; 付立杰 |
| 本发明提供了一种用于适配对开门车型的车辆结构及汽车，车辆结构沿整车坐标系X0轴对称布置，包括：车辆结构沿X0轴依次布置有前防撞梁模块、前扭力盒总成模块、电池包模块、后扭力盒总成模块及后防撞梁模块；其中，电池包模块分别连接于前扭力盒总成模块及后扭力盒总成模块的X向顶部，与前扭力盒总成模块及后扭力盒总成模块在Z向的高度一致；电池包模块的底部设置有安装空间，安装空间以电池包模块的底部为Z向平面，以前扭力盒总成模块及后扭力盒总成模块朝向电池包模块一侧为X向面。通过本发明提供的车辆结构及汽车，使得对开门机构的布置不占用电池包及门槛结构，增加了车辆的续航，同时地板结构的离地高度提高，降低了车辆的行驶风险。 | ||||||
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