Abstract: A method of data collection and reporting for a vehicle fleet includes defining a master reporting template at an original equipment manufacturer. The master reporting template includes one or more original equipment manufacturer report structures for original equipment manufacturer use. The master reporting template is communicated from the original equipment manufacturer to one or more vehicle operators. An inherited reporting template is defined at the vehicle operator including the one or more original equipment manufacturer report structures and one or more vehicle operator report structures for vehicle operator use. Data is collected from one or more vehicles of the vehicle fleet at a data hub via a data port at the one or more vehicles. The data collection is based on the contents of the inherited reporting template.

Abstract: A computer program product and method for performing position control on device members that have been identified as defective. The method may include providing a storage medium that stores data and programs used in processing images and a processing unit that processes the images, receiving, by the processing unit from an image capture device coupled to the processing unit, a set of images of a plurality of members inside of a device, detecting, by the processing unit, a defect in a first member of the plurality of members, and providing instructions to move the first member to an inspection position in the device. The device may be an engine and the members may be blades within the engine.

Abstract: A method and system for interactive aircraft maintenance procedures using a computer device is disclosed. The method comprises receiving an aircraft component operation request from a computing device, transmitting the aircraft component operation request to one or more aircraft components, receiving one or more aircraft component values based on the transmitting step, generating an aircraft status determination based on the receiving step at the computing device.

Abstract: An example avionic data communication method includes determining one or more available communication channels within a plurality of communication channel types, selecting one of the plurality of available communication channels using a channel controller, the channel controller configured to determine the quality of service of the available communication channels and to select one of the plurality of available communication channels having a cost threshold value that is not less than the cost threshold value of another channel type within the plurality of available channel types. The method further includes communicating data between an aircraft and a ground-based system using the selected one of the plurality of available channel types.

Abstract: An exemplary sensor for an aircraft includes a sensor mountable within an aircraft and operative to communicate wirelessly communications to a distributed aperture antenna. The sensor is operative to harvest energy from the aircraft to power the sensor.

Abstract: An example avionic data communication method includes determining one or more available communication channels within a plurality of communication channel types, selecting one of the plurality of available communication channels using a channel controller, the channel controller configured to determine the quality of service of the available communication channels and to select one of the plurality of available communication channels having a cost threshold value that is not less than the cost threshold value of another channel type within the plurality of available channel types. The method further includes communicating data between an aircraft and a ground-based system using the selected one of the plurality of available channel types.

Abstract: An example avionic data communication method includes establishing a plurality of available channels using a channel controller. The channel controller also establishes a quality of service for each of the plurality of available channels. The channel controller then selects one of the available channels. The quality of service of the selected channel is not less than the quality of service of another channel within the plurality of available channels. The method then communicates a type of data using the selected channel.

Abstract: A system and method for performing automated defect detection by utilizing data from prior inspections is disclosed. The system and method may include providing a image capture device for capturing and transmitting at least one current image of an object and providing a database for storing at least one prior image from prior inspections. The system and method may further include registering the at least one current image with the at least one prior image, comparing the registered at least one current image with the at least one prior image to determine a transformation therebetween and updating the database with the at least one current image.

Abstract: A computer program product and method for performing automated defect detection of blades within an engine is disclosed. The method may include providing a storage medium for storing data and programs used in processing video images, providing a processing unit for processing images, receiving from a borescope an initial set of images of a plurality of members inside of a device, and using the processing unit to apply Robust Principal Component Analysis to decompose the initial set of images into a first series of low rank component images and a second series of sparse component images, wherein there are at least two images in the initial series.

Abstract: A system and method for performing automated defect detection of blades within an engine is disclosed. The system and method may include an image capture device capable of capturing and transmitting images of a plurality of blades of an engine, creating a normal blade model of an undamaged one of the plurality of blades and determining defects within the plurality of blades by utilizing the normal blade model.

Abstract: A system and method for improving human-machine interface while performing automated defect detection is disclosed. The system and method may include an image capture device for capturing and transmitting data of an object, performing automated analysis of the data and reviewing results of the automated analysis by a human inspector and providing feedback. The system and method may further include refining the automated analysis of the data based upon the feedback of the human inspector.

Abstract: A system and method for performing automated defect detection using multiple image capture devices is disclosed. The system and method may include providing a plurality of image capture devices, the plurality of image capture devices capturing and transmitting a plurality of images of an object. The system and method may further include determining a feature correspondence between the plurality of images of the plurality of image capture devices, creating mosaiced images of the plurality of images if the feature correspondence is found or known and performing at least of an automated analysis and a manual inspection on the mosaiced images to find any defects in the object.

Abstract: A fault detection and diagnosis method for a gas turbine engines comprises collecting a sensor signal from an acoustic or vibrational sensor at the gas turbine engine, pre-processing the sensor signal to remove predictable background, and extracting a feature set from the sensor signal using Mel-Frequency Cepstral Coefficients (MFCC) algorithms and/or Code Excited Linear Prediction (CELP) algorithms. Fault and non-fault states are reported based on comparison between the feature set and a library of fault and non-fault feature profiles corresponding to fault and non-fault states of the gas turbine engine.

Abstract: An engine frame comprises an engine support structure and a communication device with a serial number and a wireless transceiver. The engine support structure is configured to support an engine for maintenance or transport. The communication device is configured to determine a location of the engine frame, and broadcast a report message including the location of the engine frame and the serial number to a remote server via the wireless transceiver.

Abstract: An aircraft component assembly has an aircraft component for an aircraft. A sensor is configured to monitor the aircraft component. A local wireless transmitter is provided for communication with a remote receiver. In addition, a local wireless receiver is provided for communication with the remote transmitter. A processor is in communication with the sensor. The processor is configured to control the sensor, the local wireless transmitter and the local wireless receiver. A power source is configured to generate energy proximate the installed aircraft component.

Abstract: A system and method for performing automated defect detection by utilizing data from prior inspections is disclosed. The system and method may include providing a image capture device for capturing and transmitting at least one current image of an object and providing a database for storing at least one prior image from prior inspections. The system and method may further include registering the at least one current image with the at least one prior image, comparing the registered at least one current image with the at least one prior image to determine a transformation therebetween and updating the database with the at least one current image.

Abstract: A system and method for performing automated defect detection using multiple image capture devices is disclosed. The system and method may include providing a plurality of image capture devices, the plurality of image capture devices capturing and transmitting a plurality of images of an object. The system and method may further include determining a feature correspondence between the plurality of images of the plurality of image capture devices, creating mosaiced images of the plurality of images if the feature correspondence is found or known and performing at least of an automated analysis and a manual inspection on the mosaiced images to find any defects in the object.

Abstract: A system and method for performing automated defect detection of blades within an engine is disclosed. The system and method may include an image capture device capable of capturing and transmitting images of a plurality of blades of an engine, creating a normal blade model of an undamaged one of the plurality of blades and determining defects within the plurality of blades by utilizing the normal blade model.

Abstract: A computer program product and method for performing automated defect detection of blades within an engine is disclosed. The method may include providing a storage medium for storing data and programs used in processing video images, providing a processing unit for processing images, receiving from a borescope an initial set of images of a plurality of members inside of a device, and using the processing unit to apply Robust Principal Component Analysis to decompose the initial set of images into a first series of low rank component images and a second series of sparse component images, wherein there are at least two images in the initial series.

Abstract: A computer program product and method for performing position control on device members that have been identified as defective. The method may include providing a storage medium that stores data and programs used in processing images and a processing unit that processes the images, receiving, by the processing unit from an image capture device coupled to the processing unit, a set of images of a plurality of members inside of a device, detecting, by the processing unit, a defect in a first member of the plurality of members, and providing instructions to move the first member to an inspection position in the device. The device may be an engine and the members may be blades within the engine.