Abstract:
Methods and apparatus for marine deployment according to various aspects of the present invention may operate in conjunction with a floatable housing adapted to be deployed by a marine vehicle. The floatable housing may be adapted to be launched from a marine vehicle and rise to the surface. Assets, such as an unmanned aerial vehicle, may be deployed from the surfaced floatable housing.
Abstract:
본 발명은 잠수함의 드론 시스템에 관한 것으로서, 본 발명의 일 실시예에 따르는 잠수함의 드론 시스템은 잠수함에 구비된 발사관을 이용하여 드론을 발사하는 잠수함의 드론 시스템으로서, 제1 드론을 내장하며, 잠수함의 수직발사관을 통해 사출되고, 사출 후 해수면 위로 제1 드론을 외부로 비상시키는 제1 캡슐형 드론, 및 제1 드론과 제1 연동 케이블로 연결되며, 제1 드론에 경로 및 운용 정보를 입력하는 제1 드론 통제장치를 포함한다.
Abstract:
Methods and apparatus for marine deployment according to various aspects of the present invention may operate in conjunction with a floatable housing adapted to be deployed by a marine vehicle. The floatable housing may be adapted to be launched from a marine vehicle and rise to the surface. Assets, such as an unmanned aerial vehicle, may be deployed from the surfaced floatable housing.
Abstract:
A leveling device (10, 100) for automatic platforms characterized in that it comprises - a movable part (11, 111) fixable to a platform; - a fixed part (12) fixable to a base suitable for supporting the platform; - actuating means adapted to move said movable part (11, 111) with respect to said fixed part (12); said fixed part (12) comprising a concave seat (13) and said movable part (11, 111) comprising a convex element (14) configured to engage said concave seat (13) in a sliding manner; said convex seat (13) and said convex element (14) being configured to couple so as to define an axis of rotation (A) with respect to which said movable part (11, 111) is rotatable with respect to said fixed part (12) to drive said actuating means.
Abstract:
A leveling device (10, 100) for automatic platforms characterized in that it comprises - a movable part (11, 111) fixable to a platform; - a fixed part (12) fixable to a base suitable for supporting the platform; - actuating means adapted to move said movable part (11, 111) with respect to said fixed part (12); said fixed part (12) comprising a concave seat (13) and said movable part (11, 111) comprising a convex element (14) configured to engage said concave seat (13) in a sliding manner; said convex seat (13) and said convex element (14) being configured to couple so as to define an axis of rotation (A) with respect to which said movable part (11, 111) is rotatable with respect to said fixed part (12) to drive said actuating means.
Abstract:
A rotary wing vehicle (1) includes a body structure having an elongated tubular backbone or core (40), and a counter-rotating coaxial rotor system (3, 5) having rotors with each rotor having a separate motor (54, 61) to drive the rotors about a common rotor axis of rotation (7), The rotor system is used to move the rotary wing vehicle (1) in directional flight.
Abstract:
Line capture devices for unmanned aircraft, and associated systems and methods are disclosed. A system in accordance with a particular embodiment includes a line capture device body having a line slot with an open end and a closed end. A retainer is positioned proximate to the line slot and has a rotor with a plurality of rotor arms positioned to extend at least partially across the line slot as the rotor rotates relative to the body. A joint rotatably couples the rotor to the body, and a ratchet device is operably coupled to the rotor to allow the rotor to rotate in a first direction and at least restrict the rotor arm from rotating in a second direction opposite the first. In other embodiments, the retainer can include other arrangements, for example, one or more wire-shaped elements.