Self-righting aeronautical vehicle and method of use
A self-righting aeronautical vehicle comprising a hollowed frame and a lift mechanism. The exterior of the frame and center of gravity are adapted to self-right the vehicle. The frame can include sealed, hollowed sections for use in bodies of water. The frame can be spherical in shape enabling inspection of internal surface of partially or fully enclosed structures. Inspection equipment can be integrated into the vehicle and acquired data can be stored or wirelessly communicated to a server. A controlled or other mass can be pivotally assembled to a pivot axle spanning across the interior of the frame. The pivot axis can rotate about a vertical axis (an axis perpendicular to the elongated axis). The propulsion mechanisms can be adapted for use as a terrestrial vehicle when enclosed in a sealed spherical shell.
1. A method of inspecting a structure using an aeronautical inspection vehicle, the method comprising steps of:
obtaining the aeronautical inspection vehicle, the aeronautical inspection vehicle comprising:
a hollowed frame, the hollowed frame having a circular circumferential exterior surface,
at least one maneuvering and lift mechanism adapted to generate a lifting force, each of the at least one maneuvering and lift mechanism being assembled to a controller assembly, the controller assembly carried by a support element located within the interior of the hollowed frame,
a weighted mass assembled to one of (a) the hollowed frame and (b) the controller assembly in a manner enabling self-righting of the at least one maneuvering and lift mechanism during use, and
at least one inspection device for inspecting an object;
activating the aeronautical inspection vehicle;
placing the aeronautical inspection vehicle against a generally vertically oriented surface;
using the at least one maneuvering and lift mechanism to generate a lifting force, lifting the aeronautical inspection vehicle;
rolling the hollowed frame against the generally vertically oriented surface; and
acquiring inspection data.
2. A method of inspecting a structure using an aeronautical inspection vehicle as recited in claim 1 , the method further comprising a step of:
rotating the controller assembly respective to the hollowed frame about a first axis.
3. A method of inspecting a structure using an aeronautical inspection vehicle as recited in claim 1 , the method further comprising steps of:
rotating the controller assembly respective to the hollowed frame about a first axis; and
rotating the controller assembly respective to the hollowed frame about a second axis,
wherein the first axis and the second axis differ from one another.
4. A method of inspecting a structure using an aeronautical inspection vehicle as recited in claim 1 , the hollowed frame having a spherically shaped circumferential exterior surface,
the method further comprising a step of:
rotating the spherically shaped circumferential exterior surface along the generally vertically oriented surface.
5. A method of inspecting a structure using an aeronautical inspection vehicle as recited in claim 1 , the hollowed frame having a spherically shaped circumferential exterior surface, the aeronautical inspection vehicle further comprising a rotational mechanism adapted to rotate the controller assembly respective to the hollowed frame about a first axis and a second axis,
the method further comprising steps of:
rotating the controller assembly respective to the hollowed frame about a first axis; and
rotating the controller assembly respective to the hollowed frame about a second axis,
wherein the first axis and the second axis differ from one another.
6. A method of inspecting a structure using an aeronautical inspection vehicle as recited in claim 1 , the hollowed frame having a spherically shaped circumferential exterior surface, the aeronautical inspection vehicle further comprising a rotational mechanism adapted to rotate the controller assembly support element respective to the hollowed frame and a second rotational mechanism adapted to rotate the controller assembly respective to the controller assembly support element
the method further comprising a step of:
rotating at least one of following to maintain the at least one maneuvering and lift mechanism oriented to provide a substantially vertical lifting force to the hollowed frame:
(a) the controller assembly support element respective to the hollowed frame,
(b) the controller assembly respective to the controller assembly support element and
(c) the hollowed frame.
7. A method of inspecting a structure using an aeronautical inspection vehicle as recited in claim 1 , the method further comprising a step of:
using at least one of the following to inspect the object:
a digital camera,
an Infra-Red (IR) circuit,
an ultrasonic inspection circuit,
an X-ray circuit, and
an accelerometer,
an acoustic device,
a thermographer,
a pressure sensor,
a radiographic sensor,
a chemical detection device, and
an explosives detection device.
8. A method of inspecting a structure using an aeronautical inspection vehicle as recited in claim 1 , the method further comprising a step of:
inspecting at least one of:
piping,
a tank,
a fuel tank,
a water tank,
a cargo container,
a ship,
a train,
an airplane,
a rocket,
a spaceship,
a tunnel,
a building,
a bridge,
a cave, and
an elevator.
9. A method of inspecting a structure using an aeronautical inspection vehicle as recited in claim 1 , wherein the support member traverses the interior of the hollowed frame at a central location
the method further comprising at least one of the following steps:
rotating the support member respective to the hollowed frame to orient the controller assembly to provide a vertical lifting force; and
rotating the controller assembly about the support member to orient the controller assembly to provide a vertical lifting force.
10. A method of inspecting a structure using an aeronautical inspection vehicle as recited in claim 1 , each at least one maneuvering and lift mechanism and the weighted mass are in mechanical communication with one another, the method further comprising a step of:
orienting each at least one maneuvering and lift mechanism into a flight ready orientation by a pivoting motion driven by the weighted mass.
11. A method of inspecting a structure using an aeronautical inspection vehicle as recited in claim 1 , the method further comprising a step of:
self-righting the hollowed frame into a flight ready orientation when the aeronautical inspection vehicle lands on a generally planar horizontal surface, wherein the flight ready orientation orients the pivot axle in a generally horizontal orientation.
12. An aeronautical inspection vehicle, comprising:
a hollowed frame, the hollowed frame having a circular circumferential exterior surface;
at least one maneuvering and lift mechanism adapted to generate a lifting force, each of the at least one maneuvering and lift mechanism being assembled to a controller assembly, the controller assembly carried by a support element located within the interior of the hollowed frame;
a weighted mass assembled to one of (a) the hollowed frame and (b) the controller assembly in a manner enabling self-righting of the at least one maneuvering and lift mechanism during use; and
at least one inspection device for inspecting an object.
13. An aeronautical inspection vehicle as recited in claim 12 , wherein the at least one maneuvering and lift mechanism is entirely enclosed within the hollowed frame wherein the hollowed frame is configured to protect the at least one maneuvering and lift mechanism from damage when the hollowed frame contacts a surface.
14. An aeronautical inspection vehicle as recited in claim 12 , further comprising a rotation enabling mechanism enabling rotation of the controller assembly respective to the hollowed frame.
15. An aeronautical inspection vehicle as recited in claim 12 , further comprising a first rotation enabling mechanism enabling rotation of the controller assembly respective to the hollowed frame about a first axis; and
a second rotation enabling mechanism enabling rotation of the controller assembly respective to the hollowed frame about a second axis.
16. An aeronautical inspection vehicle as recited in claim 12 , wherein an exterior surface of the hollowed frame is spherical in shape.
17. An aeronautical inspection vehicle as recited in claim 12 , wherein the at least one inspection device is assembled to at least one of the controller assembly, the support member, and the hollowed frame.
18. An aeronautical inspection vehicle as recited in claim 12 , wherein the at least one inspection device is at least one of:
a digital camera,
an Infra-Red (IR) circuit,
an ultrasonic inspection circuit,
an X-ray circuit, and
an accelerometer,
an acoustic device,
a thermographer,
a pressure sensor, and
a radiographic sensor.
19. An aeronautical inspection vehicle as recited in claim 12 , further comprising at least one light emitting device, wherein the light emitting device is adapted to illuminate a region proximate the aeronautical inspection vehicle.
20. An aeronautical inspection vehicle as recited in claim 12 , each at least one maneuvering and lift mechanism provided as a pair of maneuvering and lift mechanisms, each pair of maneuvering and lift mechanisms employing counter rotating propellers.