UNMANNED AERIAL RESCUE SYSTEM
First Claim
1. An unmanned aerial system, comprising:
- a frame;
a landing member attached to the frame;
a propulsion system support member attached to the frame;
a propulsion system attached to the propulsion system support member;
a shroud attached to the frame;
a sealed equipment container attached to the frame;
a control system within the sealed equipment container;
a power source within the sealed equipment container; and
a sensor system within the sealed equipment container,wherein the controls system is configured to be powered by the power source and to control the propulsion system and the sensor system.
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Accused Products
Abstract
Embodiments of unmanned aerial rescue systems are disclosed, which may comprise: a frame or chassis, a landing member, a control system, a propulsion system, a propulsion system support member, a propulsion system orientation mechanism, a rotor shield or protector, a sealed equipment container, a cover or shroud, an equipment carrier, an equipment release mechanism, a navigation system, a sensor system, a sound system, a light system, a data communication system, an emergency equipment system, and a power management system. In some embodiments, a parabolic shroud increases the performance of sensor systems of the unmanned aerial rescue system, such as sound and light systems.
33 Citations
20 Claims
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1. An unmanned aerial system, comprising:
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a frame; a landing member attached to the frame; a propulsion system support member attached to the frame; a propulsion system attached to the propulsion system support member; a shroud attached to the frame; a sealed equipment container attached to the frame; a control system within the sealed equipment container; a power source within the sealed equipment container; and a sensor system within the sealed equipment container, wherein the controls system is configured to be powered by the power source and to control the propulsion system and the sensor system. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19)
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20. An unmanned aerial system, comprising:
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a frame; a plurality of landing members connected to the frame; an electronic control system; a plurality of electric motors, each electric motor of the plurality of electric motors connected to a rotor, each electric motor of the plurality of electric motors configured to be controlled by the electronic control system; a plurality of mesh rotor shields, each rotor shield of the plurality of rotor shields encompassing one of the plurality of electric motors and its connected rotor; a sealed equipment container connected to the frame and encompassing the electronic control system; a parabolic shroud connected to the frame; a plurality of external equipment carriers, each external equipment carrier of the plurality of external equipment carriers attached to the frame and configured to carry a piece of rescue equipment; an equipment release mechanism for each of the respective external equipment carriers, each equipment release mechanism configured to release a piece of rescue equipment from its respective external equipment carrier; a light system comprising at least one light emitter; a sound system comprising at least one sound capturing device and at least one sound emitter; a sensor system comprising at least one image capturing device; and a data communication system comprising at least one antenna and at least one transceiver, wherein the electronic control comprises; one or more processors; one or more memories comprising processor-executable software configured to be executed by the one or more processors.
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Specification