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公开(公告)号：US20190248492A1
公开(公告)日：2019-08-15
申请号：US16322557
申请日：2017-07-26
CPC分类号： B64D1/02 , B64C3/40 , B64C3/56 , B64C9/08 , B64C27/24 , B64C27/37 , B64C27/50 , B64C39/024 , B64C2009/005 , B64C2201/021 , B64C2201/024 , B64C2201/08 , B64C2201/084 , B64C2201/102 , B64C2201/108 , B64C2201/12
摘要： An assembly comprising a drone (1) and at least one releasable load (37) mounted on the drone, the drone comprising an on-board data processing system, the releasable load (37) comprising at least one sensor delivering a piece of information that can be used to ascertain the path of same and actuators for controlling flight control surfaces allowing it to be oriented as it falls, being linked to the drone (1) by an optical fibre (70), the load and the drone being arranged to exchange information via the optical fibre while the load is falling, the load transmitting data originating from said at least one sensor and the drone transmitting data for controlling the actuators, established taking into account that received from the load, in order to guide the load towards a predefined target.
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公开(公告)号：US20230174224A1
公开(公告)日：2023-06-08
申请号：US17922081
申请日：2021-04-28
IPC分类号： B64C27/24 , B64C27/605 , B64D35/04 , B64C27/26
CPC分类号： B64C27/24 , B64C27/605 , B64D35/04 , B64C27/26
摘要： An aircraft including at least one wing system with two wings rigidly connected to a rotor provided with a swash plate control device. The wing system being able to change from a fixed wing configuration where the rotor is immobilised relative to the aircraft fuselage and the wings are oriented with their leading edge facing the direction of forward travel of the aircraft, to a rotating wing configuration where the rotor is rotated relative to the fuselage, and conversely, at least one of the wings is itself subjected, during the change-over from the fixed wing configuration to the rotating wing configuration, to a rotation on itself relative to the rotor in such a manner that the two wings of the wing system form blades having their leading edge oriented in the direction of rotation of the rotor.
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公开(公告)号：US20230002045A1
公开(公告)日：2023-01-05
申请号：US17778152
申请日：2020-11-17
摘要： A drone including a front section, a wing structure supported by a rotor located behind the front section, and a propeller at the rear. The wing structure including two wings rotating the rotor, the wing structure being able to move between a flight configuration, in which the rotor is immobile relative to the front section and the propulsion provided by the propeller, and a flight configuration with the wing structure rotating, in which the rotor is rotated relative to the front section, the rotor being connected to the front section with a possibility of orienting its axis of rotation relative thereto in order able to direct the drone in the rotary wing structure configuration by acting on said orientation.
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