会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 22. 发明授权
    • Mechanism for arming, disarming and activating airplane emergency slide
evacuation systems
    • 布防,解除和激活飞机紧急滑行疏散系统的机制
    • US5738303A
    • 1998-04-14
    • US441283
    • 1995-05-15
    • Tomio HamataniDavid BrockmeyerKatsuya IkedaHisao Kondo
    • Tomio HamataniDavid BrockmeyerKatsuya IkedaHisao Kondo
    • A62B1/20A62B99/00B64C1/14B64D25/14B64C1/34
    • B64D25/14Y10S244/905
    • A mechanism(10) arms, disarms, and activates an airplane emergency evacuation system having a slide with one end connected to a girt bar (16). The mechanism includes floor fittings (18) mountable below and at each edge of the airplane door (14). Each floor fitting includes a base (32) defining a notch (40) for receiving the girt bar and a pawl (42) mounted to the base. The pawl rotates relative to the base from a locked position preventing removal of the girt bar from the notch, and to an unlocked position permitting removal of the girt bar. Support fittings (20) mountable to the door, engages the floor fittings when the door is closed and locked. A first jaw (58) extends downwardly to one side of the notch, and faces generally towards the notch from the support fitting. First and second linkage members (60) and (70) connect to one another and rotatably mount to the support fitting. A second jaw (94) extends from the second linkage member and faces generally towards the first jaw. The mechanism operates to rotate the second jaw towards the first jaw to capture the girt bar therebetween, and to rotate the pawl to the unlocked position to disarm the system and allow normal use of the door. To arm the system, the second jaw is rotated in the opposite direction which releases the girt bar and causes the pawl to securely lock the girt bar to the floor of the airplane.
    • 一种机构(10)臂,分离和激活具有滑动件的飞机紧急撤离系统,其一端连接到密封条(16)。 该机构包括安装在飞机门(14)的每个边缘下方和下方的地板配件(18)。 每个地板配件包括限定用于接收衬垫条的凹口(40)的底座(32)和安装到基座的棘爪(42)。 棘爪相对于基座从锁定位置旋转,从而防止将缝线从凹口移除,并且到解锁位置,从而能够移除棉条。 当门关闭并锁定时,可安装到门上的支撑配件(20)与地板配件接合。 第一钳口(58)向下延伸到凹口的一侧,并且大致朝向来自支撑配件的凹口面对。 第一和第二连杆构件(60)和(70)彼此连接并可旋转地安装到支撑配件。 第二钳口(94)从第二连杆构件延伸并且大致面向第一钳口。 该机构用于使第二钳口朝向第一钳口旋转,以在其间捕获间隙棒,并且将棘爪旋转到解锁位置以解除系统并允许门的正常使用。 为了操纵系统,第二钳口沿相反的方向旋转,释放出细条,并使棘爪牢牢地锁定到飞机的地板上。
    • 29. 发明授权
    • Window assembly manufacturing method and window pane
    • 窗户装配制造方法和窗格
    • US07754128B2
    • 2010-07-13
    • US10563374
    • 2004-06-14
    • Katsuyuki AmanoAkihiro SuzukiTatsuya TamuraHisao Kondo
    • Katsuyuki AmanoAkihiro SuzukiTatsuya TamuraHisao Kondo
    • A61M25/00
    • B29C45/14377B29C45/14311B29C45/14434B29C45/14778B29C2045/0093B29K2709/08B29L2031/7782B60J1/004
    • An adhesive agent is uniformly applied to a back surface of a window pane, the application made to an area where a covering member is planned to be adhered and to an area where a positioning fixture and a holding portion are planned to be adhered, the application is also made continuously such that adhesive agent layers of both planned adhesion areas being continuous with an adhesive agent continuous area in between. After that, the window pane and the positioning fixture are set in an injection mold and a polymer material is injected in the mold. This results that the covering member and the holding portion are formed into a shape where they are connected by a connection portion for material flow, which connection portion is formed at a position other than the adhesive agent continuous area. The forming results that the covering member and the holding portion are adhered and fixed to the back surface of the window pane with the adhesive agent layers in between. After the forming process above, the connection portion for material flow is removed.
    • 将粘合剂均匀地施加到窗玻璃的后表面上,将涂布物制成覆盖部件被计划粘附的区域和计划粘贴定位夹具和保持部分的区域,该应用 也使得两个计划的粘合区域的粘合剂层与其间的粘合剂连续区域连续地连续地制成。 之后,将窗玻璃和定位夹具放置在注射模具中,并将聚合物材料注入模具中。 因此,覆盖部件和保持部形成为通过用于材料流动的连接部连接的形状,该连接部形成在粘接剂连续区域以外的位置。 形成结果是,覆盖构件和保持部分粘合并固定到窗玻璃的后表面,其间具有粘合剂层。 在上述成形过程之后,物料流的连接部分被去除。