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    Airship pitch trim and directional control system
    1.
    发明授权
    Airship pitch trim and directional control system 有权
    飞艇间距和方向控制系统

    公开(公告)号：US09567055B2

    公开(公告)日：2017-02-14

    申请号：US15164450

    申请日：2016-05-25

    申请人： Raven Industries, Inc.

    发明人： Michael Scott Smith ,  Randy E. Scott

    IPC分类号： B64B1/02 ,  B64B1/38 ,  B64B1/22 ,  B64B1/24 ,  B64B1/42 ,  G05D1/08 ,  B64B1/34 ,  B64D27/24 ,  B64D41/00

    CPC分类号： B64B1/38 ,  B64B1/22 ,  B64B1/24 ,  B64B1/34 ,  B64B1/42 ,  B64D27/24 ,  B64D2041/005 ,  G05D1/0808

    摘要： An example can include a pod detachably coupled to a hull. At least one thrust generator can be fixed to the pod. A power source can be mounted to the pod and slideable fore and aft. A power source actuator can be coupled between the pod and the power source to translate the location of the power source with respect to the pod. A sensor can be coupled to the pod to detect a pitch of the hull and provide a pitch signal. A controller can be coupled to one or more of the power source, the power source actuator, the first and second thrust generators and the sensor. The controller can maintain a pitch of the hull by translating the power source within the pod in association with the pitch signal.

    摘要翻译： 一个示例可以包括可拆卸地联接到船体的舱。 至少一个推力发生器可以固定到荚。 电源可以安装到荚上，并可前后滑动。 电源致动器可以耦合在容器和电源之间，以将电源相对于容器的位置转换。 传感器可以耦合到舱，以检测船体的桨距并提供俯仰信号。 控制器可以耦合到电源，电源致动器，第一和第二推力发生器和传感器中的一个或多个。 控制器可以通过与音高信号相关联地转换盒内的电源来维持船体的音调。

    BUOYANCY AERIAL VEHICLE
    3.
    发明申请
    BUOYANCY AERIAL VEHICLE 审中-公开

    公开(公告)号：US20200262536A1

    公开(公告)日：2020-08-20

    申请号：US16651686

    申请日：2018-09-28

    申请人： ATHENE WORKS LIMITED

    发明人： Nicholas DEAKIN

    IPC分类号： B64B1/38 ,  B64B1/20 ,  B64B1/12 ,  B64B1/62

    摘要： An aerial vehicle (1) in which forward motion is developed by changing the position of the buoyancy centre and the position of the centre of gravity of the aerial vehicle (1). The aerial vehicle (1) has an envelope (12) which is a body of revolution about a central axis (X-X). The envelope (12) comprises a film and contains a lighter than air gas and wings (13, 14) one each extending laterally either side of the envelope (12).

    AIRSHIP PITCH TRIM AND DIRECTIONAL CONTROL SYSTEM
    4.
    发明申请
    AIRSHIP PITCH TRIM AND DIRECTIONAL CONTROL SYSTEM 有权

    公开(公告)号：US20160264228A1

    公开(公告)日：2016-09-15

    申请号：US15164450

    申请日：2016-05-25

    申请人： Raven Industries, Inc.

    发明人： Michael Scott Smith ,  Randy E. Scott

    IPC分类号： B64B1/38 ,  B64B1/42 ,  B64B1/24 ,  G05D1/08

    CPC分类号： B64B1/38 ,  B64B1/22 ,  B64B1/24 ,  B64B1/34 ,  B64B1/42 ,  B64D27/24 ,  B64D2041/005 ,  G05D1/0808

    摘要： An example can include a pod detachably coupled to a hull. At least one thrust generator can be fixed to the pod. A power source can be mounted to the pod and slideable fore and aft. A power source actuator can be coupled between the pod and the power source to translate the location of the power source with respect to the pod. A sensor can be coupled to the pod to detect a pitch of the hull and provide a pitch signal. A controller can be coupled to one or more of the power source, the power source actuator, the first and second thrust generators and the sensor. The controller can maintain a pitch of the hull by translating the power source within the pod in association with the pitch signal.

    摘要翻译： 一个示例可以包括可拆卸地联接到船体的舱。 至少一个推力发生器可以固定到荚。 电源可以安装到荚上，并可前后滑动。 电源致动器可以耦合在容器和电源之间，以将电源相对于容器的位置转换。 传感器可以耦合到舱，以检测船体的桨距并提供俯仰信号。 控制器可以耦合到电源，电源致动器，第一和第二推力发生器和传感器中的一个或多个。 控制器可以通过与音高信号相关联地转换盒内的电源来维持船体的音调。

    Airship pitch trim and directional control system
    5.
    发明授权
    Airship pitch trim and directional control system 有权
    飞艇间距和方向控制系统

    公开(公告)号：US09352819B2

    公开(公告)日：2016-05-31

    申请号：US14209926

    申请日：2014-03-13

    申请人： Raven Industries, Inc.

    发明人： Michael Scott Smith ,  Randy E. Scott

    IPC分类号： B64B1/02 ,  B64B1/38 ,  B64B1/22

    CPC分类号： B64B1/38 ,  B64B1/22 ,  B64B1/24 ,  B64B1/34 ,  B64B1/42 ,  B64D27/24 ,  B64D2041/005 ,  G05D1/0808

    摘要： An example can include a pod detachably coupled to a hull. At least one thrust generator can be fixed to the pod. A power source can be mounted to the pod and slideable fore and aft. A power source actuator can be coupled between the pod and the power source to translate the location of the power source with respect to the pod. A sensor can be coupled to the pod to detect a pitch of the hull and provide a pitch signal. A controller can be coupled to one or more of the power source, the power source actuator, the first and second thrust generators and the sensor. The controller can maintain a pitch of the hull by translating the power source within the pod in association with the pitch signal.

    摘要翻译： 一个示例可以包括可拆卸地联接到船体的舱。 至少一个推力发生器可以固定到荚。 电源可以安装到荚上，并可前后滑动。 电源致动器可以耦合在容器和电源之间，以将电源相对于容器的位置转换。 传感器可以耦合到舱，以检测船体的桨距并提供俯仰信号。 控制器可以耦合到电源，电源致动器，第一和第二推力发生器和传感器中的一个或多个。 控制器可以通过与音高信号相关联地转换盒内的电源来维持船体的音调。

    Inertia aerostat
    6.
    发明公开
    Inertia aerostat 审中-公开

    公开(公告)号：US20230322353A1

    公开(公告)日：2023-10-12

    申请号：US17972653

    申请日：2022-10-25

    申请人： Guangyuan XU

    发明人： Guangyuan XU

    IPC分类号： B64B1/38 ,  B64B1/24

    CPC分类号： B64B1/38 ,  B64B1/24

    摘要： An inertia aerostat having a vacuum compartment and an inertial floating device provided in the vacuum compartment, the inertial floating device comprises a drive shaft, drive devices, recycle and power generation devices and axially symmetric EMD rotation bodies, fixing devices are respectively provided at both ends of the drive shaft, the fixing devices are connected with the vacuum compartment, the drive devices are sleeved over the drive shaft, the axially symmetric EMD rotation bodies are connected with the drive devices via wheel ribs, the recycle and power generation devices are sleeved over the drive devices; by providing the vacuum compartment and the inertial floating device, inertial centrifugal forces generated by high speed rotation of the axially symmetric EMD rotation bodies in a gravitational field can be used as conversion media between kinetic energy and gravitational potential energy so free floating of the aerostat in the gravitational field can be realized.

    Hybrid VTOL vehicle
    7.
    发明授权
    Hybrid VTOL vehicle 有权

    公开(公告)号：US10894591B2

    公开(公告)日：2021-01-19

    申请号：US15824748

    申请日：2017-11-28

    申请人： EGAN AIRSHIPS, INC.

    发明人： James C. Egan ,  Joel D. Egan

    IPC分类号： B64B1/20 ,  B64B1/14 ,  B64B1/22 ,  B64B1/28 ,  B64B1/30 ,  B64B1/38 ,  B64B1/58 ,  B64B1/70 ,  B64C39/02 ,  B64B1/34 ,  B64B1/60

    摘要： A hybrid VTOL vehicle having an envelope configured to provide hydrostatic buoyancy, a fuselage attached to the envelope and having at least one pair of wings extending from opposing sides thereof to produce dynamic lift through movement, and a thrust generation device on each wing and configured to rotate with each wing about an axis that is lateral to a longitudinal axis of the envelope to provide vertical takeoff or landing capabilities. Ideally, the envelope provides negative hydrostatic lift to enhance low-speed and on-the-ground stability. A vehicle comprising a first lift device capable of providing hydrostatic lift; a second lift device capable of providing dynamic lift through movement; and a system structured to generate thrust coupled to the second lift device, the second lift device and the thrust generation system capable of rotating together about an axis that is lateral to a longitudinal axis of the vehicle at angles at least in the range of 90 degrees to and including 180 degrees.

    Convertible airship
    9.
    发明授权
    Convertible airship 失效
    敞篷飞艇

    公开(公告)号：US3971533A

    公开(公告)日：1976-07-27

    申请号：US552793

    申请日：1975-02-25

    申请人： Saul I. Slater

    发明人： Saul I. Slater

    IPC分类号： B64B1/38

    CPC分类号： B64B1/38

    摘要： A flexible lighter-than-air gas-containing envelope carries at least one rigid structural member which provides a track for pivotal and slidable mounting of a gondola. The track extends along the underside of the airship from the nose section to a point aft of the midsection so that the gondola can be positioned from a point directly under the belly to one at the nose, causing the longitudinal axis of the envelope to rotate through 90.degree.. Remote controls actuate the rudders, ailerons and elevators as well as fully rotatable horizontal stabilizers and wings.

    摘要翻译： 柔性的比空气中的含气体的信封携带至少一个刚性结构构件，其提供用于枢转和可滑动地安装吊舱的轨道。 轨道沿着飞艇的下侧从鼻部延伸到中间部分的后方，使得吊舱可以从直接在腹部下方的点定位到鼻子处的一个位置，导致信封的纵向轴线旋转穿过 90°。 遥控器启动方向舵，副翼和电梯以及完全可旋转的水平稳定器和机翼。