Abstract: A system including a landing location where a drone at least one of delivers and acquires a parcel, and a homing device to interact with the drone to guide the drone to the landing location independent of interaction from another source. The homing device guides the drone during the landing phase of a flight plan. A method is also disclosed.

Abstract: An object tracking assembly includes a plurality of tracking units that is each attachable to a respective object. Each of the tracking units is in communication with a location network for identifying a location of the tracking units and each of the tracking units broadcasts a tracking signal when the tracking units are actuated. A locating unit is provided and the locating unit broadcasts an actuate signal to each of the tracking units. Each of the tracking units broadcasts the tracking signal to the locating unit when the tracking units receives the actuate signal. The locating unit emits a location alert ranging between a minimum intensity and a maximum intensity corresponding to a distance between the locating unit and a respective one of the tracking units. In this way the locating unit communicates to the user the distance between the locating unit and the respective tracking unit.

Abstract: An object tracking assembly includes a plurality of tracking units that is each attachable to a respective object. Each of the tracking units is in communication with a location network for identifying a location of the tracking units and each of the tracking units broadcasts a tracking signal when the tracking units are actuated. A locating unit is provided and the locating unit broadcasts an actuate signal to each of the tracking units. Each of the tracking units broadcasts the tracking signal to the locating unit when the tracking units receives the actuate signal. The locating unit emits a location alert ranging between a minimum intensity and a maximum intensity corresponding to a distance between the locating unit and a respective one of the tracking units. In this way the locating unit communicates to the user the distance between the locating unit and the respective tracking unit.

Abstract: Systems for monitoring a component in a turbomachine can include a strain sensor comprising at least two reference points disposed on a surface of the component, and a data acquisition device connected to the turbomachine comprising a field of view, wherein the field of view is positioned to at least periodically capture the strain sensor on the component.

Abstract: Data acquisition devices for analyzing reference objects and systems for monitoring turbine component deformation are provided. A data acquisition device has a longitudinal axis and includes a lens assembly and an image capture device in communication with the lens assembly for receiving and processing light from the lens assembly to generate images. The data acquisition device further includes a light source and a light tube coupled at a rear end to the light source. The light tube extends along the longitudinal axis between a front end and the rear end, and is operable to transport light from the light source therethrough and emit the light from the front end. The data acquisition device further includes an actuator operable to activate the image capture device and the light source.

Abstract: Methods for monitoring a components include locating a plurality of machined surface features on the component, locating at least one reference point, and measuring a plurality of first distances between the plurality of machined surface features and the at least one reference point.

Abstract: Data acquisition devices for analyzing reference objects and systems for monitoring turbine component deformation are provided. A data acquisition device has a longitudinal axis and includes a lens assembly and an image capture device in communication with the lens assembly for receiving and processing light from the lens assembly to generate images. The data acquisition device further includes a light source and a light tube coupled at a rear end to the light source. The light tube extends along the longitudinal axis between a front end and the rear end, and is operable to transport light from the light source therethrough and emit the light from the front end. The data acquisition device further includes an actuator operable to activate the image capture device and the light source.

Abstract: Methods for determining strain on turbine components include providing a turbine component comprising a plurality of strain sensor reference features disposed along the turbine component separated from one another by a plurality of first distances at a first time, reading the plurality of strain sensor reference features at a second time to determine a plurality of second distances between the plurality of strain sensor reference features, and comparing the plurality of second distances to the plurality of first distances to determine a plurality of non-linear strain measurements between the plurality of strain sensor reference features.

Abstract: Traversable strain sensor readers for reading a plurality strain sensor reference features on a turbine component include a traversing system configured to traverse the traversable strain sensor reader along at least a portion of the turbine component, and a reader configured to read at least a portion of the plurality of strain sensor reference features while the traversing system traverses the traversable strain sensor reader along at least the portion of the turbine component.

Abstract: Methods for monitoring a components include locating a plurality of naturally occurring surface features on the component, locating at least one reference point, measuring a plurality of first distances between the plurality of naturally occurring surface features and the at least one reference point.

Abstract: Methods for monitoring a components include locating a plurality of naturally occurring surface features on the component, locating at least one reference point, measuring a plurality of first distances between the plurality of naturally occurring surface features and the at least one reference point.

Abstract: Methods for monitoring a components include locating a plurality of machined surface features on the component, locating at least one reference point, and measuring a plurality of first distances between the plurality of machined surface features and the at least one reference point.

Abstract: Components can include a substrate and an array-based strain sensor disposed on the substrate, wherein the array-based strain sensor comprises a plurality of reference features distributed along both a first axis and a second axis to form at least a two-dimensional array.

Abstract: Systems for monitoring a component in a turbomachine can include a strain sensor comprising at least two reference points disposed on a surface of the component, and a data acquisition device connected to the turbomachine comprising a field of view, wherein the field of view is positioned to at least periodically capture the strain sensor on the component.

Abstract: Components can comprise a substrate, an embedded strain sensor comprising at least two reference points disposed on the substrate, and an outer coating disposed over at least a portion of the embedded strain sensor.

Abstract: Traversable strain sensor readers for reading a plurality strain sensor reference features on a turbine component include a traversing system configured to traverse the traversable strain sensor reader along at least a portion of the turbine component, and a reader configured to read at least a portion of the plurality of strain sensor reference features while the traversing system traverses the traversable strain sensor reader along at least the portion of the turbine component.