An unmanned aerial vehicle (UAV) for landing and perching on a curved ferromagnetic surface is provided. The UAV includes a plurality of articulated legs. Each articulated leg includes: a magnet configured to magnetically attach to the curved ferromagnetic surface; and a magnetic foot for housing the magnet and configured to magnetically articulate towards and attach to the curved ferromagnetic surface using the magnet in a perpendicular orientation with respect to the curved ferromagnetic surface, in response to the UAV approaching the curved ferromagnetic surface, in order to land the UAV on the curved ferromagnetic surface and for the UAV to perch on the curved ferromagnetic surface after the landing. The magnetic foot is configured to remain magnetically attached to the curved ferromagnetic surface while the UAV is perched on the curved ferromagnetic surface.

Systems, methods, and sensor devices for fluid conduit inspection using passive magnetometry are provided. A method of inspecting a fluid conduit using passive magnetometry includes collecting magnetic flux data from inside the fluid conduit without actively magnetizing the fluid conduit, the magnetic flux data representing a residual magnetization of the fluid conduit, and identifying a conduit condition for the fluid conduit using the magnetic flux data. A computer system includes a memory for storing magnetic flux data collected from inside the fluid conduit without active magnetization of the fluid conduit, the magnetic flux data representing a residual magnetization of the fluid conduit; and a processor in communication with the memory and configured to generate an electronic representation of a conduit condition for the fluid conduit based on the magnetic flux data, wherein the electronic representation is stored in the memory.

A sensor device for measuring a rotational position of an element that is rotatable about an axis of rotation includes a sender member emitting a magnetic field and a plurality of receiving members receiving the magnetic field. Each of the receiving members has a pair of conductors that together delimit a pair of surrounded areas. Each of the surrounded areas tapers in and against a circumferential direction at ends of the surrounded areas.

According to an embodiment, an inspection system comprises: a moving body including a moving main body movable along a structure; a detector attached to the moving main body; a shape information storage unit for storing shape information indicating shape and size of the structure; an inspection location information storage unit for storing information of inspection locations to be inspected; an inspection item information storage unit for storing information of inspection items to be inspected; a moving body location detecting unit for detecting moving body location information indicating location of the moving body; a moving control unit for controlling movement of the moving body; and an inspection control unit for inspection.

A robotic vehicle for traversing surfaces comprises a chassis having a plurality of wheels mounted thereto. Two magnetic drive wheels are spaced apart in a lateral direction and rotate about a rotational axis while a stabilizing wheel is provided in front of or behind the two drive wheels. The drive wheels are configured to be driven independently, thereby driving and steering the vehicle along the surface. The vehicle also includes a sensor probe assembly that is supported by the chassis and configured to take measurements of the surface being traversed. In accordance with a salient aspect, the vehicle includes a probe normalization mechanism that is configured to determine the surface curvature and adjust the orientation of the probe transducer as a function of the curvature of the surface, thereby maintaining the probe at the preferred inspection angle irrespective of changes in the surface curvature with vehicle movement.

An unmanned aerial vehicle (UAV) for landing and perching on a curved ferromagnetic surface is provided. The UAV includes a plurality of articulated legs. Each articulated leg includes: a magnet configured to magnetically attach to the curved ferromagnetic surface; and a magnetic foot for housing the magnet and configured to magnetically articulate towards and attach to the curved ferromagnetic surface using the magnet in a perpendicular orientation with respect to the curved ferromagnetic surface, in response to the UAV approaching the curved ferromagnetic surface, in order to land the UAV on the curved ferromagnetic surface and for the UAV to perch on the curved ferromagnetic surface after the landing. The magnetic foot is configured to remain magnetically attached to the curved ferromagnetic surface while the UAV is perched on the curved ferromagnetic surface.

An unmanned aerial vehicle (UAV) includes a body constructed to enable the UAV to fly and three or more legs connected to the body and configured to land and perch the UAV on a curved ferromagnetic surface. Each leg includes a first portion connected to the body, a second portion including a magnet and configured to magnetically attach and maintain the magnetic attachment of the leg to the ferromagnetic surface during the landing and perching, and a passive articulation joint connecting the first and second portions and configured to passively articulate the second portion with respect to the first portion in response to the second portion approaching the ferromagnetic surface. The UAV further includes a releasable crawler including magnetic wheels which detach the crawler from the body during the perching and maneuver the crawler on the ferromagnetic surface while magnetically attaching the crawler to the ferromagnetic surface after detachment.

An unmanned aerial vehicle (UAV) autonomously perching on a curved surface from a starting position is provided. The UAV includes: a 3D depth camera configured to capture and output 3D point clouds of scenes from the UAV including the curved surface; a 2D LIDAR system configured to capture and output 2D slices of the scenes; and a control circuit. The control circuit is configured to: control the depth camera and the LIDAR system to capture the 3D point clouds and the 2D slices, respectively, of the scenes; input the captured 3D point clouds from the depth camera and the captured 2D slices from the LIDAR system; autonomously detect and localize the curved surface using the captured 3D point clouds and 2D slices; and autonomously direct the UAV from the starting position to a landing position on the curved surface based on the autonomous detection and localization of the curved surface.

A method of inspection or maintenance of a curved ferromagnetic surface using an unmanned aerial vehicle (UAV) having a releasable crawler is provided. The method includes: flying the UAV from an initial position to a pre-perching position in a vicinity of the ferromagnetic surface; autonomously perching the UAV on the ferromagnetic surface; maintaining magnetic attachment of the perched UAV to the ferromagnetic surface; releasing the crawler from the magnetically attached UAV onto the ferromagnetic surface; moving the crawler over the curved ferromagnetic surface while maintaining magnetic attachment of the released crawler to the ferromagnetic surface; inspecting or maintaining the ferromagnetic surface using the magnetically attached crawler; and re-docking the released crawler with the perched UAV.

A caliper tool for measuring a shape of a wellbore may include a sensor assembly and a movable measurement component including a hub and a measurement arm extending from the hub, and a magnetically-permeable target coupled to the hub and configured to rotate with the hub upon movement of the measurement arm. A sensor assembly includes primary coil and one or more secondary coils spaced apart from the primary coil, wherein output signals from the secondary coils facilitates measurement of the shape of the wellbore.