Abstract: An autonomous vehicle and a suspension for the autonomous vehicle are provided. The suspension may include first and second support legs pivotally coupled to a body of the autonomous vehicle at respective pivot points, and extending in opposing directions to contact a surface upon which the autonomous vehicle moves. A biasing element biases the support legs towards the surface. A coupler couples the support legs to cause pivotal movement of one of the support legs to be mirrored in the other support leg. The coupler may cause the support legs to maintain a centerline, which extends equidistantly between the pivot points and through a sensor mounted to an underside of the body, perpendicular to the surface as the support legs pivot during movement of the autonomous vehicle.

Abstract: An autonomous vehicle and a suspension for the autonomous vehicle are provided. The suspension may include first and second support legs pivotally coupled to a body of the autonomous vehicle at respective pivot points, and extending in opposing directions to contact a surface upon which the autonomous vehicle moves. A biasing element biases the support legs towards the surface. A coupler couples the support legs to cause pivotal movement of one of the support legs to be mirrored in the other support leg. The coupler may cause the support legs to maintain a centerline, which extends equidistantly between the pivot points and through a sensor mounted to an underside of the body, perpendicular to the surface as the support legs pivot during movement of the autonomous vehicle.

Abstract: A component inspection apparatus and a method for ultrasonic inspection of a component, including low pressure last stage steam turbine blades, are disclosed. The apparatus includes a guide member, a guide adapting member and scanning probes. The guide member includes a first surface and a distal second surface. The first surface is configured to adaptably mirror the shape of portions of the component to be inspected. The guide adapting member is capable of releasably attaching the second surface of the guide member. to be changeable as per the shape of the component. The scanning probes may be located on the guide adapting member in a manner configured to be movable along the second surface of the guide member to generate and receive ultrasonic waves used to inspect the component.

Abstract: A component inspection apparatus and a method for ultrasonic inspection of a component, including low pressure last stage steam turbine blades, are disclosed. The apparatus includes a guide member, a guide adapting member and scanning probes. The guide member includes a first surface and a distal second surface. The first surface is configured to adaptably mirror the shape of portions of the component to be inspected. The guide adapting member is capable of releasably attaching the second surface of the guide member.to be changeable as per the shape of the component. The scanning probes may be located on the guide adapting member in a manner configured to be movable along the second surface of the guide member to generate and receive ultrasonic waves used to inspect the component.