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    GEODESIC STRUCTURE FORMING SYSTEMS AND METHODS
    5.
    发明申请
    GEODESIC STRUCTURE FORMING SYSTEMS AND METHODS 有权
    地质构造系统与方法

    公开(公告)号：US20170057029A1

    公开(公告)日：2017-03-02

    申请号：US14840845

    申请日：2015-08-31

    Applicant: THE BOEING COMPANY

    Inventor： Sina Golshany ,  Junghyun Ahn ,  Derek Alderks ,  Todd William Erickson

    IPC: B23P23/04 ,  B21J15/30 ,  B23B41/00 ,  B21J15/14

    CPC classification number: B23B41/00 ,  B21J15/142 ,  B21J15/30 ,  B23B2215/04 ,  B64C1/08 ,  B64C1/12 ,  B64F5/10 ,  Y10T29/49616 ,  Y10T29/49622 ,  Y10T29/49867 ,  Y10T29/49943 ,  Y10T29/49947 ,  Y10T29/49956

    Abstract: A system and method determine a size and a shape for identical geodesic modules that are used to form a structure. The system and method may include analyzing input data regarding a size and a shape of the structure to be formed, and determining the size and the shape for each of the identical geodesic modules based on the size and the shape of the structure to be formed. The structure may include a framework including the identical geodesic modules. Each of the geodesic modules has a size and a shape that are the same as all of the other of the geodesic modules. A forming system and method position a framework and a covering skin of the structure in relation to a mandrel, and drill and rivet the framework to the covering skin with a plurality of operating heads.

    Abstract translation: 系统和方法确定用于形成结构的相同测地板模块的尺寸和形状。 系统和方法可以包括分析关于要形成的结构的尺寸和形状的输入数据，并且基于要形成的结构的尺寸和形状来确定每个相同测地模块的尺寸和形状。 该结构可以包括包括相同测地板模块的框架。 每个测地线模块具有与所有其他测地线模块相同的尺寸和形状。 成形系统和方法将结构的框架和覆盖层相对于心轴定位，并用多个操作头钻孔并将框架铆接到覆盖表皮上。

    Laterally reinforced variable pitch rotor
    6.
    发明授权
    Laterally reinforced variable pitch rotor 有权

    公开(公告)号：US10018058B2

    公开(公告)日：2018-07-10

    申请号：US14798788

    申请日：2015-07-14

    Applicant: The Boeing Company

    Inventor： Sina Golshany ,  Todd W. Erickson

    IPC: F01D25/06 ,  F01D7/00 ,  B64C11/32

    CPC classification number: F01D7/00 ,  B64C11/32 ,  F01D25/06

    Abstract: A propulsion unit having reduced noise employs a rotor having a plurality of variable pitch blades. A tensioning joint mechanism is carried within each blade and a tension element is engaged by the tension joint mechanism. The tension element is configured to maintain tension between the blades in the rotor and the tensioning joint mechanism adapted to allow variation of pitch of the blades without altering tension in the tension element.

    Systems and methods for determining sizes and shapes of geodesic modules
    7.
    发明授权
    Systems and methods for determining sizes and shapes of geodesic modules 有权

    公开(公告)号：US09965582B2

    公开(公告)日：2018-05-08

    申请号：US14840802

    申请日：2015-08-31

    Applicant: THE BOEING COMPANY

    Inventor： Sina Golshany ,  Junghyun Ahn ,  Derek Alderks ,  Todd William Erickson

    IPC: G06F19/00 ,  B64C1/00 ,  B64D7/00 ,  G06F17/50

    CPC classification number: G06F17/5095 ,  G06F17/50

    Abstract: A system and method determine a size and a shape for identical geodesic modules that are used to form a structure. The system and method may include analyzing input data regarding a size and a shape of the structure to be formed, and determining the size and the shape for each of the identical geodesic modules based on the size and the shape of the structure to be formed. The structure may include a framework including the identical geodesic modules. Each of the geodesic modules has a size and a shape that are the same as all of the other of the geodesic modules. A forming system and method position a framework and a covering skin of the structure in relation to a mandrel, and drill and rivet the framework to the covering skin with a plurality of operating heads.

    SYSTEMS AND METHODS FOR DETERMINING SIZES AND SHAPES OF GEODESIC MODULES
    9.
    发明申请
    SYSTEMS AND METHODS FOR DETERMINING SIZES AND SHAPES OF GEODESIC MODULES 有权
    用于确定地球模块尺寸和形状的系统和方法

    公开(公告)号：US20170061068A1

    公开(公告)日：2017-03-02

    申请号：US14840802

    申请日：2015-08-31

    Applicant: THE BOEING COMPANY

    Inventor： Sina Golshany ,  Junghyun Ahn ,  Derek Alderks ,  Todd William Erickson

    IPC: G06F17/50 ,  G05B15/02

    CPC classification number: G06F17/5095 ,  G06F17/50

    Abstract: A system and method determine a size and a shape for identical geodesic modules that are used to form a structure. The system and method may include analyzing input data regarding a size and a shape of the structure to be formed, and determining the size and the shape for each of the identical geodesic modules based on the size and the shape of the structure to be formed. The structure may include a framework including the identical geodesic modules. Each of the geodesic modules has a size and a shape that are the same as all of the other of the geodesic modules. A forming system and method position a framework and a covering skin of the structure in relation to a mandrel, and drill and rivet the framework to the covering skin with a plurality of operating heads.

    Abstract translation: 系统和方法确定用于形成结构的相同测地板模块的尺寸和形状。 系统和方法可以包括分析关于要形成的结构的尺寸和形状的输入数据，并且基于要形成的结构的尺寸和形状来确定每个相同测地模块的尺寸和形状。 该结构可以包括包括相同测地板模块的框架。 每个测地线模块具有与所有其他测地线模块相同的尺寸和形状。 成形系统和方法将结构的框架和覆盖层相对于心轴定位，并用多个操作头钻孔并将框架铆接到覆盖表皮上。

    LATERALLY REINFORCED VARIABLE PITCH ROTOR
    10.
    发明申请
    LATERALLY REINFORCED VARIABLE PITCH ROTOR 有权
    侧向加固可变式转脚转子

    公开(公告)号：US20170016337A1

    公开(公告)日：2017-01-19

    申请号：US14798788

    申请日：2015-07-14

    Applicant: The Boeing Company

    Inventor： Sina Golshany ,  Todd W. Erickson

    IPC: F01D7/00 ,  F01D25/06

    CPC classification number: F01D7/00 ,  B64C11/32 ,  F01D25/06

    Abstract: A propulsion unit having reduced noise employs a rotor having a plurality of variable pitch blades. A tensioning joint mechanism is carried within each blade and a tension element is engaged by the tension joint mechanism. The tension element is configured to maintain tension between the blades in the rotor and the tensioning joint mechanism adapted to allow variation of pitch of the blades without altering tension in the tension element.

    Abstract translation: 具有降低噪声的推进单元采用具有多个可变桨距叶片的转子。 在每个叶片内承载张紧关节机构，并且张紧元件由张力接合机构接合。 张力元件构造成保持转子中的叶片和张紧接头机构之间的张力，该张紧接头机构适于允许叶片间距的变化而不改变张力元件的张力。

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