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    NOSE LANDING GEAR ARRANGEMENTS AND METHODS FOR MAKING THE SAME
    2.
    发明申请
    NOSE LANDING GEAR ARRANGEMENTS AND METHODS FOR MAKING THE SAME 有权
    NOSE接地齿轮安装及其制造方法

    公开(公告)号：US20150251750A1

    公开(公告)日：2015-09-10

    申请号：US14201345

    申请日：2014-03-07

    Applicant: Gulfstream Aerospace Corporation

    Inventor： Brian Cook ,  John Louis ,  Thomas Van de Ven ,  Robert M. Vieito ,  Mehdi R. Khorrami

    IPC: B64C25/16 ,  B64C25/18 ,  B64C25/04 ,  B64C23/00 ,  B64C25/00

    CPC classification number: B64C25/16 ,  B64C23/005 ,  B64C25/001 ,  B64C25/04 ,  B64C25/18 ,  B64C2025/003 ,  Y10T29/4984

    Abstract: Nose landing gear arrangements including a folding follow-up door for reducing airflow noise for aircrafts, aircrafts including such nose landing gear arrangements, and methods for making such nose landing gear arrangements are provided herein. In one example, a nose landing gear arrangement includes a wheel assembly and a main strut. The main strut is operatively coupled to the wheel assembly and is configured to extend outside of the fuselage substantially along a generally vertical plane. A folding follow-up door is pivotally coupled to the main strut and extends to the fuselage. The folding follow-up door includes a first door section and a second door section that extend outwardly in directions away from each other to define an unfolded position. The folding follow-up door is foldable to move the first and second door sections towards each other about the generally vertical plane to define a folded position

    Abstract translation: 这里提供了包括用于减少飞行器的气流噪声的折叠后跟门，包括这种前起落架装置的飞机以及用于制造这种前起落架装置的方法的鼻子起落架布置。 在一个示例中，前起落架布置包括车轮组件和主支柱。 主支柱可操作地联接到车轮组件并且构造成基本上沿着大致垂直的平面延伸到机身的外部。 折叠的后跟门枢转地连接到主支柱并延伸到机身。 折叠后续门包括第一门部分和第二门部分，该第一门部分和第二门部分沿彼此远离的方向向外延伸以限定展开位置。 折叠后续门是可折叠的，以使第一和第二门部分围绕大体上垂直的平面朝向彼此移动以限定折叠位置

    Interactive aircraft cabin environment
    3.
    发明授权
    Interactive aircraft cabin environment 有权

    公开(公告)号：US12243538B2

    公开(公告)日：2025-03-04

    申请号：US17446701

    申请日：2021-09-01

    Applicant: Gulfstream Aerospace Corporation

    Inventor： Brian Cook ,  Tongan Wang

    IPC: G10L17/22 ,  B64D11/00 ,  G10L17/18

    Abstract: The interactive aircraft cabin environment control system employs at least one microphone array disposed within the cabin to capture spoken utterances from a passenger and is configured to provide an estimation of passenger location within the cabin based on arrival time analysis of the spoken utterances. A data source onboard the aircraft provides flight context information. Such data sources include sensors measuring real-time parameters on the aircraft, the current flight plan of the aircraft, singly and in combination. A control processor, coupled to the microphone array, is configured to ascertain passenger identity based on the spoken utterances. The control processor is programmed and configured to learn and associate passenger preference to passenger identity. The control processor is receptive of the estimation of passenger location and is coupled to provide supervisory control over at least one device forming a part of the cabin environment according to passenger location, passenger preference obtained from passenger identity and flight context information.

    NOSE LANDING GEAR ARRANGEMENTS INCLUDING A FLEXIBLE SHEET AND METHODS FOR MAKING THE SAME
    4.
    发明申请
    NOSE LANDING GEAR ARRANGEMENTS INCLUDING A FLEXIBLE SHEET AND METHODS FOR MAKING THE SAME 有权
    包括柔性片的SE ING ING ING AR ET ET ET AME AME AME AME AME AME AME AME AME

    公开(公告)号：US20160200423A1

    公开(公告)日：2016-07-14

    申请号：US14623972

    申请日：2015-02-17

    Applicant: Gulfstream Aerospace Corporation

    Inventor： Brian Cook ,  John Louis ,  Thomas Van de Ven ,  Robert M. Vieito

    IPC: B64C25/14 ,  B64C25/34

    CPC classification number: B64C25/14 ,  B64C25/001 ,  B64C25/34 ,  B64C2025/003

    Abstract: Nose landing gear arrangements for aircrafts, aircrafts including such nose landing gear arrangements, and methods for making such nose landing gear arrangements are provided. In one example, a nose landing gear arrangement includes a wheel assembly and a main strut. The main strut is operatively coupled to the wheel assembly and is configured to move between an extended position and a retracted position. The main strut in the extended position extends outside of the fuselage substantially along a generally vertical plane to position the wheel assembly for takeoff and/or landing of the aircraft. The main strut in the retracted position is disposed inside the fuselage. A flexible sheet is disposed adjacent to the main strut and is configured such that when the main strut is in the extended position the flexible sheet is positioned substantially around the main strut.

    Abstract translation: 提供了用于飞机的鼻子起落架装置，包括这种前起落架装置的飞机，以及用于制造这种前起落架装置的方法。 在一个示例中，前起落架布置包括车轮组件和主支柱。 主支柱可操作地联接到车轮组件并且构造成在延伸位置和缩回位置之间移动。 延伸位置的主支柱基本上沿着大致垂直的平面延伸到机身外部，以定位车轮组件以使飞行器起飞和/或降落。 在缩回位置的主支柱设置在机身内部。 柔性片被布置成与主支柱相邻，并且构造成使得当主支柱处于伸出位置时，柔性片基本上围绕主支柱定位。

    INTERACTIVE AIRCRAFT CABIN ENVIRONMENT
    5.
    发明申请
    INTERACTIVE AIRCRAFT CABIN ENVIRONMENT 有权

    公开(公告)号：US20230073759A1

    公开(公告)日：2023-03-09

    申请号：US17446701

    申请日：2021-09-01

    Applicant: Gulfstream Aerospace Corporation

    Inventor： Brian Cook ,  Tongan Wang

    IPC: G10L17/22 ,  G10L17/18 ,  B64D11/00

    Abstract: The interactive aircraft cabin environment control system employs at least one microphone array disposed within the cabin to capture spoken utterances from a passenger and is configured to provide an estimation of passenger location within the cabin based on arrival time analysis of the spoken utterances. A data source onboard the aircraft provides flight context information. Such data sources include sensors measuring real-time parameters on the aircraft, the current flight plan of the aircraft, singly and in combination. A control processor, coupled to the microphone array, is configured to ascertain passenger identity based on the spoken utterances. The control processor is programmed and configured to learn and associate passenger preference to passenger identity. The control processor is receptive of the estimation of passenger location and is coupled to provide supervisory control over at least one device forming a part of the cabin environment according to passenger location, passenger preference obtained from passenger identity and flight context information.

    Nose landing gear arrangements and methods for making the same
    8.
    发明授权
    Nose landing gear arrangements and methods for making the same 有权
    鼻子起落架布置和制作方法

    公开(公告)号：US09290263B2

    公开(公告)日：2016-03-22

    申请号：US14201345

    申请日：2014-03-07

    Applicant: Gulfstream Aerospace Corporation

    Inventor： Brian Cook ,  John Louis ,  Thomas Van de Ven ,  Robert M. Vieito ,  Mehdi R. Khorrami

    IPC: B64C25/10 ,  B64C25/16 ,  B64C23/00 ,  B64C25/00 ,  B64C25/04 ,  B64C25/18

    CPC classification number: B64C25/16 ,  B64C23/005 ,  B64C25/001 ,  B64C25/04 ,  B64C25/18 ,  B64C2025/003 ,  Y10T29/4984

    Abstract: Nose landing gear arrangements including a folding follow-up door for reducing airflow noise for aircrafts, aircrafts including such nose landing gear arrangements, and methods for making such nose landing gear arrangements are provided herein. In one example, a nose landing gear arrangement includes a wheel assembly and a main strut. The main strut is operatively coupled to the wheel assembly and is configured to extend outside of the fuselage substantially along a generally vertical plane. A folding follow-up door is pivotally coupled to the main strut and extends to the fuselage. The folding follow-up door includes a first door section and a second door section that extend outwardly in directions away from each other to define an unfolded position. The folding follow-up door is foldable to move the first and second door sections towards each other about the generally vertical plane to define a folded position.

    Abstract translation: 这里提供了包括用于减少飞行器的气流噪声的折叠后跟门，包括这种前起落架装置的飞机以及用于制造这种前起落架装置的方法的鼻子起落架布置。 在一个示例中，前起落架布置包括车轮组件和主支柱。 主支柱可操作地联接到车轮组件并且构造成基本上沿着大致垂直的平面延伸到机身的外部。 折叠的后跟门枢转地连接到主支柱并延伸到机身。 折叠后续门包括第一门部分和第二门部分，该第一门部分和第二门部分沿彼此远离的方向向外延伸以限定展开位置。 折叠后续门是可折叠的，以使第一和第二门部分围绕大致垂直的平面朝向彼此移动以限定折叠位置。

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