Method for forming aircraft engine nacelle exhaust mixers and similar
products
    1.
    发明授权
    Method for forming aircraft engine nacelle exhaust mixers and similar products 失效
    形成飞机发动机舱排气混合器和类似产品的方法

    公开(公告)号:US5444912A

    公开(公告)日:1995-08-29

    申请号:US145944

    申请日:1993-10-29

    申请人: Carroll W. Folmer

    发明人: Carroll W. Folmer

    IPC分类号: B23P15/00 F02K1/48

    摘要: A method for forming aircraft nacelle mixers by rolling and welding a cylinder of metal to a predetermined diameter and then taper machining to an empirically determined thickness which allows it to be end sealed, longitudinally end loaded, and pressure formed to a preform die before final pressure forming to a finish die.

    摘要翻译: 通过将金属圆筒滚动并焊接到预定直径,然后将加工加工成根据经验确定的厚度来形成飞机机舱混合器的方法,该厚度允许其端部密封,纵向端部加载,并且在最终压力 成型成精模。

    Method for forming large 360 degree sheet metal shapes using
longitudinal end loading
    3.
    发明授权
    Method for forming large 360 degree sheet metal shapes using longitudinal end loading 失效
    使用纵向端部加载形成大型360度金属板形状的方法

    公开(公告)号:US5388440A

    公开(公告)日:1995-02-14

    申请号:US95686

    申请日:1993-07-21

    申请人: Carroll W. Folmer

    发明人: Carroll W. Folmer

    CPC分类号: B21D26/047

    摘要: A method for reshaping 360.degree. sheet metal cylinders by longitudinal end loading simultaneous with gas pressure applied to the inside of the cylinder directing the metal into dies resulting in new shapes without thinning, in a clean atmosphere.

    摘要翻译: 一种通过纵向端部加载重新整形360°金属板的方法,同时将气体压力施加到气缸内部,将金属导入模具中,从而在清洁的气氛中形成新的形状而不变薄。

    Method for sheet metal and thermoplastic adhesive bonded assemblies and
brazed bonded assemblies in 360.degree. shapes
    4.
    发明授权
    Method for sheet metal and thermoplastic adhesive bonded assemblies and brazed bonded assemblies in 360.degree. shapes 失效
    钣金和热塑性粘合剂组合方法和360度形状的钎焊接合组件

    公开(公告)号:US5445310A

    公开(公告)日:1995-08-29

    申请号:US95108

    申请日:1993-07-21

    申请人: Carroll W. Folmer

    发明人: Carroll W. Folmer

    CPC分类号: B32B37/146

    摘要: A method for Sheet Meta) and Thermoplastic Adhesive Bonded Assemblies and Brazed Bonded Assemblies in 360.degree. Shapes.Abstract: A method for preparing and bonding Sheet Metal Adhesive Bond Shapes and Thermoplastic Bond Shapes and Brazed Bonded Shapes utilizing forming dies as bond tools and using the sheet metal inner shape as a pressure vessel for effecting an adhesive or brazed bond.

    摘要翻译: 一种Meta的方法)和热塑性粘合剂粘合组件和钎焊粘结组件在360°形状。 摘要:利用成形模具作为粘结工具,并使用金属板内部形状作为压力容器来制造和粘合钣金粘合剂形状和热塑性粘合剂形状和钎焊粘结形状的方法,以实现粘合剂或钎焊粘结。

    Reverser door mechanisms
    6.
    发明授权
    Reverser door mechanisms 失效
    反转门机构

    公开(公告)号:US4313581A

    公开(公告)日:1982-02-02

    申请号:US74823

    申请日:1979-09-12

    CPC分类号: F02K1/72 F02K1/76 Y02T50/671

    摘要: An improved deployment mechanism for deploying blocker doors between a stowed and a deployed position. At least a pair of operable blocker doors are utilized. These doors are pivotally attached to fixed cowl structure surrounding a turbo fan engine. A yoke member having adjacent curvilinear tracks is carried by a rear translatable cowl section. Sliders are provided that follow the adjacent tracks. A drag link is connected between a slider and fixed aircraft structure and a door deploying link is connected between each blocker door and is associated slider. In a second configuration, more than one blocker door is actuated by a link connected to a single slider, coupled by more than one door deploying link. When the translatable cowl section is translated rearward by conventional actuation, a peripheral outflow passage is formed between the cowl sections and the blocker doors now being deployed redirect the fan air through the peripheral opening.

    摘要翻译: 改进的部署机构,用于在收起位置和部署位置之间部署阻挡门。 至少使用一对可操作的阻挡门。 这些门枢转地连接到围绕涡轮风扇发动机的固定罩盖结构上。 具有相邻曲线轨道的轭构件由后可平移的整流罩部分承载。 提供了跟随相邻轨道的滑块。 拖动连杆连接在滑块和固定的飞行器结构之间,并且门部分连杆连接在每个阻挡门之间并且是相关联的滑块。 在第二种配置中,通过连接到单个滑块的链路致动多于一个阻塞门,该链路通过多于一个的门部署链路联接。 当可平移整流罩部分通过常规致动向后平移时,在整流罩部分和现在被展开的阻塞门之间形成外围流出通道,从而将风扇空气重新引导通过周边开口。

    Cowl door latch adjustment fitting assembly
    7.
    发明授权
    Cowl door latch adjustment fitting assembly 失效
    导管门闩锁调整配件组件

    公开(公告)号:US4320912A

    公开(公告)日:1982-03-23

    申请号:US73706

    申请日:1979-09-10

    IPC分类号: E05B15/02 E05C21/00

    CPC分类号: E05B15/025 Y10T292/705

    摘要: An adjustable, flush mounted over center hook-latch assembly of the general type employed to secure abutting aircraft panels in flight ready condition. The device, the tension on the internal hook and eye structure, is adjustable from the external surface of the aircraft skin. Precision alignment pins and apertures cooperating therewith provide for proper alignment of the two abutting panel structures prior to their latched flight ready condition.

    摘要翻译: 一种可调节的齐平安装的中心钩形闩锁组件,其通常用于将飞行器面板固定在飞行就绪状态。 该装置,内部钩和眼睛结构上的张力可从飞机皮肤的外表面调节。 与其配合的精密对准销和孔提供两个邻接的面板结构在其锁定的飞行就绪状态之前的正确对准。