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    Modular container transport systems
    1.
    发明授权
    Modular container transport systems 有权

    公开(公告)号：US11167682B2

    公开(公告)日：2021-11-09

    申请号：US15877309

    申请日：2018-01-22

    Applicant: Biosphere Aerospace, LLC

    Inventor： Elie Helou, Jr.

    IPC: B65D88/12 ,  B60K7/00 ,  B60P3/42 ,  B65D88/00 ,  B65D90/00 ,  B60P3/11 ,  B65D90/02 ,  B65D88/14 ,  B65D88/02 ,  B64D9/00 ,  B64C1/22 ,  B64D7/08 ,  B65D90/18 ,  B62D61/12

    Abstract: Disclosed are apparatus, systems, and methods, including a ground transport drive container comprising an outer container having a cuboid shape and comprising a plurality of fittings for securing the outer container to another apparatus; and a drive wheel assembly. The drive wheel assembly comprises one or more wheels and a deployment mechanism secured to the one or more wheels. An actuating member actuates the drive wheel assembly between a stowed configuration and one or more deployed configurations. In the stowed configuration, the drive wheel assembly is housed entirely within the outer container. In the one or more deployed configurations, the drive wheel assembly extends from the outer container.

    MODULAR CONTAINER TRANSPORT SYSTEMS
    5.
    发明申请
    MODULAR CONTAINER TRANSPORT SYSTEMS 有权

    公开(公告)号：US20220203880A1

    公开(公告)日：2022-06-30

    申请号：US17521721

    申请日：2021-11-08

    Applicant: Biosphere Aerospace, LLC

    Inventor： Elie Helou, JR.

    IPC: B60P3/42 ,  B65D88/00 ,  B65D88/12 ,  B65D90/00 ,  B60K7/00 ,  B60P3/11 ,  B65D90/02 ,  B65D88/14 ,  B65D88/02 ,  B64D9/00 ,  B64C1/22 ,  B64D7/08 ,  B65D90/18 ,  B62D61/12

    Abstract: Disclosed are apparatus, systems, and methods, including a ground transport drive container comprising an outer container having a cuboid shape and comprising a plurality of fittings for securing the outer container to another apparatus; and a drive wheel assembly. The drive wheel assembly comprises one or more wheels and a deployment mechanism secured to the one or more wheels. An actuating member actuates the drive wheel assembly between a stowed configuration and one or more deployed configurations. In the stowed configuration, the drive wheel assembly is housed entirely within the outer container. In the one or more deployed configurations, the drive wheel assembly extends from the outer container.

    Space shuttle orbiter and return system
    6.
    发明授权
    Space shuttle orbiter and return system 有权

    公开(公告)号：US10549868B2

    公开(公告)日：2020-02-04

    申请号：US15451001

    申请日：2017-03-06

    Applicant: Biosphere Aerospace LLC

    Inventor： Elie Helou, Jr.

    IPC: B64G1/00 ,  B64G1/14 ,  B64G1/22 ,  B64G1/40 ,  B64G1/58 ,  B64G1/62 ,  B64G1/10

    Abstract: A launch system comprises a nose section comprising a nose coupling surface, a tail section comprising a tail coupling surface facing the nose coupling surface and a mast coupling the nose and tail sections. The mast is configured to expand and retract to displace the nose and tail sections within a range of distances from one another. In a retracted state, the nose and tail sections are either structurally coupled to one another at the nose and tail coupling surfaces or structurally coupled to at least one integrated module located between the nose and the tail sections.

    MODULAR CONTAINER TRANSPORT SYSTEMS
    7.
    发明申请
    MODULAR CONTAINER TRANSPORT SYSTEMS 有权

    公开(公告)号：US20210347559A1

    公开(公告)日：2021-11-11

    申请号：US17202167

    申请日：2021-03-15

    Applicant: Biosphere Aerospace, LLC

    Inventor： Elie Helou, Jr.

    IPC: B65D88/00 ,  B65D90/00 ,  B65D88/14 ,  B64D9/00 ,  B65D88/02 ,  B60P3/00 ,  B64C1/06 ,  B64C1/22 ,  B64C7/00

    Abstract: Disclosed are apparatus, systems, and methods, including a cargo transport system comprising a spine assembly, a container assembly, and an outer fairing. The spine assembly comprises a rigid spine and a plurality of mounts arranged on the rigid spine in a plurality of mount rows. The container assembly comprises a plurality of containers secured to the spine assembly using at least a subset of the plurality of mounts. The outer fairing at least partially encloses the container assembly. Each container of the plurality of containers comprises a plurality of fittings for securing the container to the spine assembly and/or another container of the container assembly. The container assembly is enclosed within a pressurization space for pressurizing the container assembly.

    MODULAR CONTAINER TRANSPORT SYSTEMS
    8.
    发明申请
    MODULAR CONTAINER TRANSPORT SYSTEMS 有权

    公开(公告)号：US20210221511A1

    公开(公告)日：2021-07-22

    申请号：US17222829

    申请日：2021-04-05

    Applicant: Biosphere Aerospace, LLC

    Inventor： Elie Helou, JR.

    IPC: B64D9/00 ,  B64C1/22 ,  B65D88/14 ,  B65D90/08 ,  B65D90/00 ,  B65D88/02

    Abstract: A cargo transport system comprising a spine assembly and a container assembly. The spine assembly comprises a rigid spine and a plurality of mounts arranged on the rigid spine in a plurality of mount rows. The container assembly comprises a plurality of containers and is secured to the spine assembly using at least a subset of the plurality of mounts. Each container of the plurality of containers comprises a plurality of fittings for securing the container to the spine assembly and/or another container of the container assembly. Each mount row extends along a width of the spine assembly, and the plurality of mount rows are spaced apart at regular distance intervals along a length of the spine.

    SPACE SHUTTLE ORBITER AND RETURN SYSTEM
    10.
    发明申请
    SPACE SHUTTLE ORBITER AND RETURN SYSTEM 审中-公开
    空间开关ORBITER和返回系统

    公开(公告)号：US20150284110A1

    公开(公告)日：2015-10-08

    申请号：US14736782

    申请日：2015-06-11

    Applicant: Biosphere Aerospace LLC

    Inventor： Elie Helou, JR.

    IPC: B64G1/00

    CPC classification number: B64G1/005 ,  B64G1/002 ,  B64G1/14 ,  B64G1/22 ,  B64G1/222 ,  B64G1/40 ,  B64G1/401 ,  B64G1/403 ,  B64G1/58 ,  B64G1/62 ,  B64G2001/1092

    Abstract: A launch system comprises a nose section comprising a nose coupling surface, a tail section comprising a tail coupling surface facing the nose coupling surface and a mast coupling the nose and tail sections. The mast is configured to expand and retract to displace the nose and tail sections within a range of distances from one another. In a retracted state, the nose and tail sections are either structurally coupled to one another at the nose and tail coupling surfaces or structurally coupled to at least one integrated module located between the nose and the tail sections.

    Abstract translation: 发射系统包括鼻部，其包括鼻部联接表面，尾部包括面向鼻部联接表面的尾部联接表面和连接鼻部和尾部的杆。 桅杆被配置成展开和缩回，以在彼此距离的距离范围内移动鼻部和尾部。 在缩回状态下，鼻部和尾部部分在结构上在鼻部和尾部联接表面处彼此耦合，或者结构上耦合到位于鼻部和尾部之间的至少一个集成模块。

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