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    AIRCRAFT SUPPLEMENTAL THRUST DEVICE AND METHOD OF OPERATING THE SAME
    1.
    发明申请
    AIRCRAFT SUPPLEMENTAL THRUST DEVICE AND METHOD OF OPERATING THE SAME 审中-公开
    飞机辅助装置及其操作方法

    公开(公告)号：WO2014113444A3

    公开(公告)日：2015-02-05

    申请号：PCT/US2014011633

    申请日：2014-01-15

    Applicant: OTTO WILLIAM M

    Inventor： OTTO WILLIAM M

    IPC: B64D41/00

    CPC classification number: B64D33/02 ,  B64C9/16 ,  B64C9/20 ,  B64C25/14 ,  B64C2025/125 ,  F02C6/12 ,  Y02T50/32 ,  Y02T50/44 ,  Y02T50/672

    Abstract: A supplemental thrust system for an airplane comprising a submerged inlet duct, a diffuser section in communication with the inlet duct, and a duct outlet in communication with the diffuser section, an outlet nozzle in communication with the duct outlet, a turbocharger unit comprising one or more turbochargers in communication with each other to provide compressed air to the engine and the cabin, a heat exchanger unit comprising a plurality of heat exchangers in the diffuser section to provide cooling liquid to cool pressurized air in the cabin, engine intake air and the engine jacket, where each turbocharger is coupled to the intake manifold of an engine to increase the power of the engine by introducing compressed air into the manifold.

    Abstract translation: 一种用于飞机的辅助推力系统，包括浸没入口管道，与入口管道连通的扩散器部分和与扩散器部分连通的管道出口，与管道出口连通的出口喷嘴，涡轮增压器单元，包括一个或 更多的涡轮增压器彼此连通以向发动机和舱室提供压缩空气，热交换器单元包括在扩散器部分中的多个热交换器，以提供冷却液体来冷却舱室中的加压空气，发动机进气和发动机 夹套，其中每个涡轮增压器联接到发动机的进气歧管，以通过将压缩空气引入歧管来增加发动机的功率。

    DOUBLE SLOTTED FOWLER WING FLAP WITH CHAIN
    3.
    发明申请
    DOUBLE SLOTTED FOWLER WING FLAP WITH CHAIN 审中-公开
    双链缝合翅膀与链条

    公开(公告)号：WO2014168661A3

    公开(公告)日：2014-11-27

    申请号：PCT/US2014011641

    申请日：2014-01-15

    Applicant: OTTO WILLIAM M

    Inventor： OTTO WILLIAM M

    IPC: B64C9/20 ,  B64C13/00 ,  B64C13/34

    CPC classification number: B64C25/20 ,  B64C1/00 ,  B64C1/065 ,  B64C1/069 ,  B64C1/10 ,  B64C3/185 ,  B64C3/26 ,  B64C3/58 ,  B64C5/02 ,  B64C5/16 ,  B64C9/02 ,  B64C9/16 ,  B64C9/20 ,  B64C13/30 ,  B64C25/02 ,  B64C25/10 ,  B64C25/12 ,  B64C25/14 ,  B64C25/18 ,  B64C25/22 ,  B64C2025/125 ,  B64D33/10 ,  B64D37/04 ,  F02B37/001 ,  Y02T50/32 ,  Y02T50/44

    Abstract: A wing flap control system on a wing comprising at least two control plates having an opening sized to accommodate a drive shaft, a drive shaft that engages each of the openings in each of the plurality of plates, a sprocket rotatively affixed the drive shaft with the drive shaft penetrating the other control plate, at least two idler sprockets between the control plates, a chain wrapped around the sprocket and idler sprockets, a support arm rotatively coupled to the chain by a chain shoe and to a foreflap, a link arm rotatively coupled to the support arm and to a flap, where movement of the drive shaft causes the foreflap and flap to extend and retract to increase or decrease the surface area of the wing.

    Abstract translation: 一种机翼上的机翼翼片控制系统，包括至少两个控制板，该控制板的开口尺寸适于容纳驱动轴;驱动轴，其接合多个板中的每一个中的每个开口;链轮，其将驱动轴与 驱动轴穿过另一个控制板，控制板之间至少有两个空转链轮，围绕链轮和惰轮链轮缠绕的链条，支撑臂通过链条可转动地联接到链条和前翼，连杆臂可旋转地联接 到支撑臂和翼片，其中驱动轴的运动导致前翼和翼片延伸和缩回以增加或减小机翼的表面积。

    AIRCRAFT SUPPLEMENTAL THRUST DEVICE AND METHOD OF OPERATING THE SAME
    4.
    发明申请
    AIRCRAFT SUPPLEMENTAL THRUST DEVICE AND METHOD OF OPERATING THE SAME 审中-公开
    飞机辅助装置及其操作方法

    公开(公告)号：WO2014113444A2

    公开(公告)日：2014-07-24

    申请号：PCT/US2014/011633

    申请日：2014-01-15

    Applicant: OTTO, William M.

    Inventor： OTTO, William M.

    IPC: B64D33/02

    CPC classification number: B64D33/02 ,  B64C9/16 ,  B64C9/20 ,  B64C25/14 ,  B64C2025/125 ,  F02C6/12 ,  Y02T50/32 ,  Y02T50/44 ,  Y02T50/672

    Abstract: A supplemental thrust system for an airplane comprising a submerged inlet duct, a diffuser section in communication with the inlet duct, and a duct outlet in communication with the diffuser section, an outlet nozzle in communication with the duct outlet, a turbocharger unit comprising one or more turbocharges in communication with each other to provide compressed air to the engine and the cabin, a heat exchanger unit comprising a plurality of heat exchangers in the diffuser section to provide cooling liquid to cool pressurized air in the cabin, engine intake air and the engine jacket, where each turbocharger is coupled to the intake manifold of an engine to increase the power of the engine by introducing compressed air into the manifold.

    Abstract translation: 一种用于飞机的辅助推力系统，包括浸没入口管道，与入口管道连通的扩散器部分和与扩散器部分连通的管道出口，与管道出口连通的出口喷嘴，涡轮增压器单元，包括一个或 更多的涡轮增压彼此连通以向发动机和舱室提供压缩空气;热交换器单元，包括在扩散器部分中的多个热交换器，以提供冷却液体，以冷却舱室内的加压空气，发动机进气和发动机 夹套，其中每个涡轮增压器联接到发动机的进气歧管，以通过将压缩空气引入歧管来增加发动机的功率。

    AIRCRAFT WING FLAP DEVICE AND METHOD OF OPERATING THE SAME
    7.
    发明申请
    AIRCRAFT WING FLAP DEVICE AND METHOD OF OPERATING THE SAME 审中-公开
    飞机翼片装置及其操作方法

    公开(公告)号：WO2014168661A2

    公开(公告)日：2014-10-16

    申请号：PCT/US2014/011641

    申请日：2014-01-15

    Applicant: OTTO, William M.

    Inventor： OTTO, William M.

    IPC: B64C13/34

    CPC classification number: B64C25/20 ,  B64C1/00 ,  B64C1/065 ,  B64C1/069 ,  B64C1/10 ,  B64C3/185 ,  B64C3/26 ,  B64C3/58 ,  B64C5/02 ,  B64C5/16 ,  B64C9/02 ,  B64C9/16 ,  B64C9/20 ,  B64C13/30 ,  B64C25/02 ,  B64C25/10 ,  B64C25/12 ,  B64C25/14 ,  B64C25/18 ,  B64C25/22 ,  B64C2025/125 ,  B64D33/10 ,  B64D37/04 ,  F02B37/001 ,  Y02T50/32 ,  Y02T50/44

    Abstract: A wing flap control system on a wing comprising at least two control plates having an opening sized to accommodate a drive shaft, a drive shaft that engages each of the openings in each of the plurality of plates, a sprocket rotatively affixed the drive shaft with the drive shaft penetrating the other control plate, at least two idler sprockets between the control plates, a chain wrapped around the sprocket and idler sprockets, a support arm rotatively coupled to the chain by a chain shoe and to a foreflap, a link arm rotatively coupled to the support arm and to a flap, where movement of the drive shaft causes the foreflap and flap to extend and retract to increase or decrease the surface area of the wing.

    Abstract translation: 一种机翼上的机翼翼片控制系统，包括至少两个控制板，该控制板的开口尺寸适于容纳驱动轴;驱动轴，其接合多个板中的每一个中的每个开口;链轮，其将驱动轴与 驱动轴穿过另一个控制板，控制板之间至少有两个空转链轮，围绕链轮和惰轮链轮缠绕的链条，支撑臂通过链条可转动地联接到链条和前翼，连杆臂可旋转地联接 到支撑臂和翼片，其中驱动轴的运动导致前翼和翼片延伸和缩回以增加或减小机翼的表面积。

    AUTOMATICALLY RETRACTING MOTORCYCLE KICKSTAND
    8.
    发明申请
    AUTOMATICALLY RETRACTING MOTORCYCLE KICKSTAND 审中-公开
    自动回放摩托车踢球

    公开(公告)号：WO1990010569A1

    公开(公告)日：1990-09-20

    申请号：PCT/US1990001314

    申请日：1990-03-09

    Applicant: OTTO, William, M. ,  CABABA, Edmund, R.

    IPC: B62H01/02

    CPC classification number: B62H1/02

    Abstract: A kickstand for a motorcycle which automatically retracts partially from its fully-extended position when the motorcycle is brought to an upright position from a leaning position in order to prevent the kickstand from interfering with the ground during the operation of the motorcycle in the event that the rider forgets to return the kickstand to its retracted position prior to operating the motorcycle. The kickstand uses a coil spring (38) connected to a mounting bracket (12) and support arm (18) to urge the arm to a fully-retracted position. The spring also engages a pivot bolt (34) to increase spring tension as the arm is moved to its fully-extended position.

    Abstract translation: 当摩托车从倾斜位置到达直立位置时，摩托车的自动缩回部分地从其完全伸出的位置缩回，以防止在摩托车的操作过程中脚蹬干扰地面 在操作摩托车之前，骑手忘记将脚手架返回其缩回位置。 支架使用连接到安装支架（12）和支撑臂（18）的螺旋弹簧（38），以将臂推动到完全缩回的位置。 当臂移动到其完全伸出位置时，弹簧还接合枢转螺栓（34）以增加弹簧张力。

    AIRCRAFT FUSELAGE
    9.
    发明申请
    AIRCRAFT FUSELAGE 审中-公开
    飞机熔接

    公开(公告)号：WO2014113464A1

    公开(公告)日：2014-07-24

    申请号：PCT/US2014/011670

    申请日：2014-01-15

    Applicant: OTTO, William M.

    Inventor： OTTO, William M.

    IPC: B64C1/00

    CPC classification number: B64C25/20 ,  B64C1/00 ,  B64C1/065 ,  B64C1/069 ,  B64C1/10 ,  B64C3/185 ,  B64C3/26 ,  B64C3/58 ,  B64C5/02 ,  B64C5/16 ,  B64C9/02 ,  B64C9/16 ,  B64C9/20 ,  B64C13/30 ,  B64C25/02 ,  B64C25/10 ,  B64C25/12 ,  B64C25/14 ,  B64C25/18 ,  B64C25/22 ,  B64C2025/125 ,  B64D33/10 ,  B64D37/04 ,  F02B37/001 ,  Y02T50/32 ,  Y02T50/44

    Abstract: A fuselage for an airplane including a frame comprising an upper truss and a lower truss extending from a front end of the fuselage towards the rear end of the fuselage, wherein the lower truss comprises one or more forward box beams, a plurality of support rings attached to the upper truss and lower truss, a front bulkhead connected to a first end of the upper truss and lower truss, a main bulkhead connected to the upper truss and lower truss, a pressure vessel adapted to fit within the frame between the front bulkhead and main bulkhead, and a skin adapted to fit over the frame.

    Abstract translation: 一种用于飞机的机身，包括框架，该框架包括从机身的前端朝向机身的后端延伸的上桁架和下桁架，其中下桁架包括一个或多个前箱梁，多个支撑环连接 连接到上桁架和下桁架的前隔板，连接到上桁架和下桁架的第一端的前隔板，连接到上桁架和下桁架的主隔板，适于装配在前隔板和前隔板之间的框架内的压力容器 主要隔板和适于装配在框架上的皮肤。

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