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公开(公告)号：USD993076S1
公开(公告)日：2023-07-25
申请号：US29797020
申请日：2021-06-28
摘要： FIG. 1 is a front perspective view of an unmanned aircraft showing our new design;
FIG. 2 is a front view of an unmanned aircraft;
FIG. 3 is a back view of an unmanned aircraft;
FIG. 4 is a right side view of an unmanned aircraft.
FIG. 5 is a left side view of an unmanned aircraft;
FIG. 6 is a top view of an unmanned aircraft; and,
FIG. 7 is a bottom view of an unmanned aircraft.
The broken lines in the drawings showing elements of the unmanned aircraft represent unclaimed portions of the unmanned aircraft and form no part of the claimed design.-
公开(公告)号：USD1007366S1
公开(公告)日：2023-12-12
申请号：US29823375
申请日：2022-01-17
摘要： FIG. 1 is a front perspective view of an unmanned aircraft showing our new design;
FIG. 2 is a front view of an unmanned aircraft;
FIG. 3 is a back view of an unmanned aircraft;
FIG. 4 is a right side view of an unmanned aircraft.
FIG. 5 is a left side view of an unmanned aircraft;
FIG. 6 is a top view of an unmanned aircraft; and,
FIG. 7 is a bottom view of an unmanned aircraft.
The broken lines in the drawings showing elements of the unmanned aircraft form no part of the claimed design.-
公开(公告)号：US11834167B2
公开(公告)日：2023-12-05
申请号：US17245982
申请日：2021-04-30
发明人： Mikhail Blinkov , Curtis Leo , Stephen Morris
IPC分类号： B64C29/00 , B64D31/06 , B64D27/24 , B64U10/20 , B64U30/20 , B64U50/11 , B64U50/13 , B64U50/19 , B64D27/02
CPC分类号： B64C29/0025 , B64D27/24 , B64D31/06 , B64U10/20 , B64D2027/026 , B64U30/20 , B64U50/11 , B64U50/13 , B64U50/19
摘要： A VTOL drone aircraft can include a rechargeable battery, a primary processor, lift propellers, an internal combustion engine with a thrust propeller, a generator, and a power regulation controller. The generator can receive power from the internal combustion engine and deliver electrical power to the rechargeable battery, the lift propellers, or both. The power regulation controller can regulate dynamically power delivery from the internal combustion engine to the thrust propeller and the generator, and from the generator to the rechargeable battery based upon changing conditions during flight. The power regulation controller can prevent operation of the generator when peak power is needed from the internal combustion engine for the thrust propeller. The power regulation controller can also control a clutch coupled to the thrust propeller to regulate the delivery of power to the thrust propeller when the internal combustion engine is active.
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公开(公告)号：US11845530B2
公开(公告)日：2023-12-19
申请号：US17703815
申请日：2022-03-24
CPC分类号： B64C1/30 , B64C39/024 , B64U30/20
摘要： An unmanned aerial vehicle includes a fuselage having a first side and a second side, a first arm disposed on a first side of the fuselage, wherein the first arm is coupled to one or more first propellers, wherein the first arm is adapted to move between a first folded position in which the first arm is in a folded state inside the fuselage and a first extended position in which a first section of the first arm and the one or more first propellers are outside the fuselage, and a second arm disposed on the second side of the fuselage, wherein the second arm is coupled to one or more second propellers, wherein the second arm is adapted to move between a second folded position in which the second arm is in a folded state inside the fuselage and a second extended position in which a second section of the second arm and the one or more second propellers are outside the fuselage.
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公开(公告)号：USD1007364S1
公开(公告)日：2023-12-12
申请号：US29811286
申请日：2021-10-13
摘要： FIG. 1 is a front perspective view of an unmanned aircraft showing our new design;
FIG. 2 is a front view of an unmanned aircraft;
FIG. 3 is a back view of an unmanned aircraft;
FIG. 4 is a right side view of an unmanned aircraft.
FIG. 5 is a left side view of an unmanned aircraft;
FIG. 6 is a top view of an unmanned aircraft; and,
FIG. 7 is a bottom view of an unmanned aircraft.
The broken lines in the drawings showing elements ofthe unmanned aircraft form no part of the claimed design.-
公开(公告)号：USD996339S1
公开(公告)日：2023-08-22
申请号：US29779096
申请日：2021-04-16
摘要： FIG. 1 is a front left front perspective view of the aircraft showing our new design.
FIG. 2 is a front view thereof;
FIG. 3 is a back view thereof;
FIG. 4 is a left side view thereof.
FIG. 5 is a top view thereof; and,
FIG. 6 is a bottom view thereof.
The broken lines show elements of the aircraft that form no part of the claimed design.-
公开(公告)号：US11994876B2
公开(公告)日：2024-05-28
申请号：US17703811
申请日：2022-03-24
CPC分类号： G05D1/0669 , B64C39/024 , G08G5/003 , B64U70/80 , B64U2101/00
摘要： Methods, systems and apparatus for the deployment and retrieval of child UAVs from a V-TOL UAV Mothership. The Mothership may be piloted from a base station to one or more destination locations. At the destination location, one or more child UAVs may be deployed from a cargo bay module. The child UAVs perform tasks or complete a mission before coordinating their retrieval with the V-TOL UAV Mothership. The Mothership may plan an intercept course to retrieve the child UAVs in mid-flight or coordinate a hovering type retrieval with the child UAVs. The child UAVs are retrieved through an actuated frontal opening which provides access to the cargo bay without having to navigate through turbulence created beneath the hovering Mothership by the vertical thrust rotors.
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公开(公告)号：USD993827S1
公开(公告)日：2023-08-01
申请号：US29797019
申请日：2021-06-28
摘要： FIG. 1 is a front perspective view of a manned aircraft showing our new design;
FIG. 2 is a front view of a manned aircraft;
FIG. 3 is a back view of a manned aircraft;
FIG. 4 is a right side view of a manned aircraft;
FIG. 5 is a left side view of a manned aircraft;
FIG. 6 is a top view of a manned aircraft; and,
FIG. 7 is a bottom view of a manned aircraft.
The broken lines in the drawings showing elements of the manned aircraft represent unclaimed portions of the manned aircraft and form no part of the claimed design.-
公开(公告)号：US12071240B2
公开(公告)日：2024-08-27
申请号：US17246133
申请日：2021-04-30
发明人： Emily Agostino , Curtis Leo , Stephen Morris
IPC分类号： B64D1/22 , B64D1/10 , B64D37/00 , B64D47/08 , B64U10/20 , B64U20/40 , B64U20/87 , B64U101/30 , B64U101/60
CPC分类号： B64D1/22 , B64D1/10 , B64D37/005 , B64D47/08 , B64U10/20 , B64U20/40 , B64U20/87 , B64C2211/00 , B64U2101/30 , B64U2101/60
摘要： A dual use UAV or “drone” can include a battery and primary processor located at a fuselage, as well as two separate modular units removably coupled to the fuselage and in communication with the primary processor. The two separate modular units can interact with each other to provide an enhanced operation while the drone is in flight. One modular unit can be an ISR unit having a video camera, and the other modular unit can be a cargo unit. The enhanced operation can involve the ISR unit using its video camera to identify a delivery location for a cargo pod of the cargo unit. Alternative modular units can include a secondary ISR unit, a cargo fuel pod unit, or a robotic arm assembly. Standardized interfaces coupled to the fuselage can enable the ready removal of one modular unit and installation of another one.
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