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    SYSTEMS AND METHODS FOR MANUFACTURE OF A MODULAR AIRCRAFT
    1.
    发明公开
    SYSTEMS AND METHODS FOR MANUFACTURE OF A MODULAR AIRCRAFT 审中-公开

    公开(公告)号：US20230390969A1

    公开(公告)日：2023-12-07

    申请号：US18090136

    申请日：2022-12-28

    申请人： Blended Wing Aircraft, Inc.

    发明人： Mark Allan Page

    IPC分类号： B29C33/30 ,  B64F5/10 ,  B29C70/30

    CPC分类号： B29C33/301 ,  B64F5/10 ,  B29C70/30 ,  B29K2307/04

    摘要： A system for manufacturing modular aircraft includes at least at least a common tooling component, including at least one or more of a first component in a shape of a nose and a second component in a shape of a wing. The system further including at least a modular tooling component in a shape of a main body, wherein connecting the at least a common tooling components to the at least modular component forms a mold in a shape of at least a portion of a blended wing body (BWB) aircraft with no clear demarcation between the shape of the wing and a shape of a main body along an edge of the shape of the BWB.

    Systems and methods for manufacture of a modular aircraft
    4.
    发明授权
    Systems and methods for manufacture of a modular aircraft 有权

    公开(公告)号：US11541576B1

    公开(公告)日：2023-01-03

    申请号：US17478493

    申请日：2021-09-17

    申请人： Blended Wing Aircraft, Inc.

    发明人： Mark Allan Page

    IPC分类号： B29C33/30 ,  B64F5/10 ,  B29C70/30 ,  B29K307/04 ,  B29L31/30 ,  B29K105/08

    摘要： A system for manufacturing modular aircraft includes at least a common tooling component, wherein the at least a common tooling component is configured to manufacture at least a flight component. The system includes at least a modular tooling component, wherein the at least modular tooling component wherein the at least a modular tooling component is configured to manufacture at least a fuselage component and a collar component. The system includes at least a tooling interface component, wherein the at least a tooling interface component is configured to mechanically connect the at least a common tooling component at a first end to the at least a modular tooling component at a second end.

    SYSTEMS AND METHODS FOR MODULAR AIRCRAFT
    5.
    发明申请
    SYSTEMS AND METHODS FOR MODULAR AIRCRAFT 有权

    公开(公告)号：US20230092771A1

    公开(公告)日：2023-03-23

    申请号：US17478406

    申请日：2021-09-17

    申请人： Blended Wing Aircraft, Inc.

    发明人： Mark Allan Page

    IPC分类号： B64C1/06 ,  B64C39/10 ,  B64C9/00 ,  B64C7/02 ,  B64F5/10 ,  B64C39/00

    摘要： A system for modular aircraft includes at least a common component, wherein the at least a common component includes at least a flight component. The system includes at least a modular component, wherein the at least modular component includes at least a fuselage component and a collar component. The system includes at least an interface component, wherein the at least an interface component is configured to connect the at least a common component at a first end to the at least a modular component at a second end.

    NON-COUPLED LANDING GEAR APPARATUS AND METHODS OF USE
    7.
    发明公开
    NON-COUPLED LANDING GEAR APPARATUS AND METHODS OF USE 审中-公开

    公开(公告)号：US20240025536A1

    公开(公告)日：2024-01-25

    申请号：US17870365

    申请日：2022-07-21

    申请人： Blended Wing Aircraft, Inc.

    发明人： Mark Allan Page

    IPC分类号： B64C25/50 ,  B64C25/06

    CPC分类号： B64C25/50 ,  B64C25/06

    摘要： A non-coupled landing gear for an aircraft includes at least a nose gear and at least a main gear. The at least a nose gear disposed forward of a neutral point of an aircraft by a first distance and the at least a main gear disposed aft of the neutral point of the aircraft by a second distance. The at least a nose gear and the at least a main gear are uncoupled from each other.

    Blended wing body aircraft with transparent panels
    9.
    发明授权
    Blended wing body aircraft with transparent panels 有权

    公开(公告)号：US11565811B1

    公开(公告)日：2023-01-31

    申请号：US17586988

    申请日：2022-01-28

    申请人： Blended Wing Aircraft, Inc.

    发明人： Mark Allan Page

    IPC分类号： B64C39/10 ,  B64C1/14 ,  B64D47/02 ,  B64C1/06 ,  B60Q3/43 ,  B64D11/00

    摘要： The present disclosure is directed to a blended wing body aircraft including a blended wing body, wherein the blended wing body is characterized by having no clear dividing line between wings and a main body along a leading edge of the aircraft; a cabin located within the main body and a transitional portion of the blended wing body; and a plurality of transparent panels in a ceiling of the cabin configured to transmit light from outside the blended wing body aircraft to inside the cabin.