Automated postflight troubleshooting sensor array
First Claim
Patent Images
1. A method for identifying anomalies for an aircraft, the method comprising:
- detecting a presence of the aircraft in a control area via monitoring, using a sensor system, the aircraft characterized by a first side, a second side, and a bottom;
responsive to the sensor system detecting the presence of the aircraft in the control area, identifying, using a number of array encoders, a speed of travel for the aircraft;
determining a scan rate for the aircraft using the speed of travel, wherein the scan rate is a number of electrical signal pulses sent to a number of cameras resulting in the number of cameras taking an exposure of at least a portion of the aircraft on each of the number of electrical signal pulses;
identifying, using a maintenance control system comprising a computer comprising an analysis process comprising an object identifier, the aircraft;
responsive to identifying the aircraft, identifying, using the analysis process and a scan priority database comprising a hierarchy of anomaly priorities, a number of scan priorities for the aircraft on the ground after a flight, wherein the number of scan priorities ranks different sections of the aircraft to be sought out during a scan based on information comprising operational maintenance information about the aircraft;
determining whether the analysis process received a datalink communication, identifying an anomaly with a section of the aircraft, from the aircraft during the flight;
assigning a first priority to the anomaly identified in the datalink communication, and responsive to receiving identification of multiple anomalies, identifying prioritization of the multiple anomalies received in the datalink communication based upon a hierarchy of anomaly priorities within a scan priority database communicating with the analysis process;
identifying prior scan results for the aircraft;
determining, using the analysis process and the prior scan results, whether an anomaly trend exists;
responsive to a determination that the anomaly trend exists, assigning a second priority to the anomaly trend;
determining, using a designated use for each sensor in the sensor system and a potential for degradation of each sensor influenced by dynamic conditions comprising;
a cloud coverage, an artificial illumination, a full moon light, a new moon darkness, a degree of sun brightness based on sun position due to season, a shadow, fog, smoke, sand, dust, rain, and snow, a number of redundant sensors in the sensor system used in scanning the aircraft;
responsive to identifying the number of scan priorities for the aircraft, scanning the aircraft, using the scan rate and a number of sensor components in an array in accordance with the number of scan priorities, the array including at least a horizontal array of sensors directed at the bottom of the aircraft and an angled array of sensors directed at the first side of the aircraft; and
responsive to scanning the aircraft, using the analysis process for forming scan results and determining whether a number of maintenance anomalies is present among a set of locations for the aircraft, the set comprising;
inside the aircraft, on an exterior surface of the aircraft, on an interior surface of the aircraft, and within a structure comprising the aircraft;
responsive to determining that the number of maintenance anomalies is present for the aircraft, generating a maintenance action to address the number of maintenance anomalies detected, transmitting the maintenance action to a maintenance unit, and executing the maintenance action on the aircraft.
1 Assignment
0 Petitions
Accused Products
Abstract
The advantageous embodiments provide an apparatus for identifying anomalies on an object comprising a sensor system and an analysis process. The sensor system is configured to detect a presence of the object, identify a speed of travel for the object, and determine a scan rate for the object using the speed of travel to generate scan results. The analysis process is configured to analyze the scan results and determine whether a number of maintenance anomalies are detected on the object using the scan results.
152 Citations
19 Claims
-
1. A method for identifying anomalies for an aircraft, the method comprising:
-
detecting a presence of the aircraft in a control area via monitoring, using a sensor system, the aircraft characterized by a first side, a second side, and a bottom; responsive to the sensor system detecting the presence of the aircraft in the control area, identifying, using a number of array encoders, a speed of travel for the aircraft; determining a scan rate for the aircraft using the speed of travel, wherein the scan rate is a number of electrical signal pulses sent to a number of cameras resulting in the number of cameras taking an exposure of at least a portion of the aircraft on each of the number of electrical signal pulses; identifying, using a maintenance control system comprising a computer comprising an analysis process comprising an object identifier, the aircraft; responsive to identifying the aircraft, identifying, using the analysis process and a scan priority database comprising a hierarchy of anomaly priorities, a number of scan priorities for the aircraft on the ground after a flight, wherein the number of scan priorities ranks different sections of the aircraft to be sought out during a scan based on information comprising operational maintenance information about the aircraft; determining whether the analysis process received a datalink communication, identifying an anomaly with a section of the aircraft, from the aircraft during the flight; assigning a first priority to the anomaly identified in the datalink communication, and responsive to receiving identification of multiple anomalies, identifying prioritization of the multiple anomalies received in the datalink communication based upon a hierarchy of anomaly priorities within a scan priority database communicating with the analysis process; identifying prior scan results for the aircraft; determining, using the analysis process and the prior scan results, whether an anomaly trend exists; responsive to a determination that the anomaly trend exists, assigning a second priority to the anomaly trend; determining, using a designated use for each sensor in the sensor system and a potential for degradation of each sensor influenced by dynamic conditions comprising;
a cloud coverage, an artificial illumination, a full moon light, a new moon darkness, a degree of sun brightness based on sun position due to season, a shadow, fog, smoke, sand, dust, rain, and snow, a number of redundant sensors in the sensor system used in scanning the aircraft;responsive to identifying the number of scan priorities for the aircraft, scanning the aircraft, using the scan rate and a number of sensor components in an array in accordance with the number of scan priorities, the array including at least a horizontal array of sensors directed at the bottom of the aircraft and an angled array of sensors directed at the first side of the aircraft; and responsive to scanning the aircraft, using the analysis process for forming scan results and determining whether a number of maintenance anomalies is present among a set of locations for the aircraft, the set comprising;
inside the aircraft, on an exterior surface of the aircraft, on an interior surface of the aircraft, and within a structure comprising the aircraft;responsive to determining that the number of maintenance anomalies is present for the aircraft, generating a maintenance action to address the number of maintenance anomalies detected, transmitting the maintenance action to a maintenance unit, and executing the maintenance action on the aircraft. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 10, 11, 13)
-
-
9. A method for identifying a scan rate for a scan of the object, the object having a first side, a second side, and a bottom, the method comprising:
-
detecting a presence of the object approaching a control area using a sensor system, the control area comprising an area that overlies a horizontal sensor array and is adjacent to a vertical sensor array and an angled sensor array, the vertical sensor array being at an angle of 90 degrees relative to the horizontal sensor array, and the angled sensor array being at an angle other than 90 degrees relative to the horizontal sensor array, the angled sensor array comprising a number of sensor components comprising;
an array encoder, a laser metrology system, a number of ultraviolet light sources, a number of ultraviolet receptors, a camera comprising a line scan technology, and a number of infrared sensors;determining whether a maintenance control system comprising a computer comprising an analysis process received a datalink communication, identifying an anomaly with a section of the object, from an aircraft during a flight; assigning a first priority to the anomaly identified in the datalink communication, and responsive to receiving identification of multiple anomalies, identifying prioritization of the multiple anomalies received in the datalink communication based upon a hierarchy of anomaly priorities within a scan priority database communicating with the analysis process; identifying prior scan results for the object; determining, using the analysis process and the prior scan results, whether an anomaly trend exists; assigning, responsive to a determination that the anomaly trend exists, a second priority to the anomaly trend; identifying preventative maintenance requirements; and assigning a third priority to preventative maintenance requirements; determining, using a designated use for each sensor in the sensor system and a potential for degradation of each sensor influenced by dynamic conditions comprising;
a cloud coverage, an artificial illumination, a full moon light, a new moon darkness, a degree of sun brightness based on sun position due to season, a shadow, fog, smoke, sand, dust, rain, and snow, a number of redundant sensors in the sensor system used in scanning the aircraft;detecting a speed of travel for the object via activating the array encoder; and monitoring the speed of travel for the object to determine the scan rate for the object, wherein the scan rate is a number of electrical signal pulses sent to a number of cameras to cause the number of cameras to take an exposure of the object on each of the number of electrical signal pulses, and generating scan results from the number of sensor components; responsive to the scan results, generating the maintenance action to address maintenance anomalies detected, transmitting the maintenance action to a maintenance unit, and executing the maintenance action on the object. - View Dependent Claims (12, 14, 15)
-
-
16. An apparatus for identifying anomalies for an object, the object comprising a first side, a second side, and a bottom, the apparatus comprising:
-
a sensor system configured; to detect a presence of the object in a control area; comprising a horizontal sensor array adjacent to a vertical sensor array and an angled sensor array, the vertical sensor array being at an angle of 90 degrees relative to the horizontal sensor array, and the angled sensor array being at an angle other than 90 degrees relative to the horizontal sensor array, such that the angled sensor array comprises a number of sensor components that comprises;
an array encoder, a laser metrology system, a number of ultraviolet light sources, a number of ultraviolet receptors, a camera comprising a line scan technology, and a number of infrared sensors;to identify a speed of travel for the object; and to determine, using the speed of travel, a scan rate for the sensor to scan the object to generate scan results, wherein the scan rate is a number of electrical signal pulses sent to a number of cameras to cause the number of cameras to take an exposure of the object on each of the number of electrical signal pulses and wherein the scan results are generated from a number of sensor components in accordance with a number of scan priorities; a maintenance control system that comprises a computer that comprises a scan priority database that comprises a hierarchy of anomaly priorities, such that the computer comprises an analysis process configured to; determine whether a maintenance control system that comprises the computer receives a datalink communication, that identifies an anomaly with a section of the object, from an aircraft during a flight; assign a first priority to the anomaly identified in the datalink communication, and responsive to receipt of identification of multiple anomalies, identify prioritization of the multiple anomalies received in the datalink communication based upon a hierarchy of anomaly priorities within a scan priority database that communicates with the analysis process; identify prior scan results for the aircraft; determine, based upon the analysis process and the prior scan results, whether an anomaly trend exists; responsive to a determination that the anomaly trend exists, assign a second priority to the anomaly trend; determine, based upon a designated use for each sensor in the sensor system and a potential for degradation of each sensor influenced by dynamic conditions that comprise;
a cloud coverage, an artificial illumination, a full moon light, a new moon darkness, a degree of sun brightness based on sun position due to season, a shadow, fog, smoke, sand, dust, rain, and snow, a number of redundant sensors in the sensor system used in scanning the aircraft;direct a prioritized scan of the object; analyze a result of the prioritized scan; and determine, based upon the result, a number of maintenance anomalies for the object; direct actions based upon the number of maintenance anomalies, such that a maintenance unit executes the actions on the object. - View Dependent Claims (17, 18, 19)
-
Specification