Reporting and prioritizing faults for aircraft downtime reduction
First Claim
1. A computer-implemented method for maintenance planning for an aircraft, the method comprising:
- measuring, using one or more sensors, conditions of the aircraft;
retrieving, via a processor, a data transmission comprising a plurality of component faults from an aircraft processor while the aircraft is in flight based at least in part on measurements from the one or more sensors;
constructing, via the processor executing a prediction engine, a predictive fault list based on the component faults, the predictive fault list having a plurality of weighted predictions of authentic component faults and nuisance component faults;
prioritizing, via the processor, the weighted predictions of authentic component faults;
generating, via the processor, a maintenance checklist prioritized based on the weighted prediction of authentic component faults; and
outputting, via an output processor, the prioritized maintenance checklist on an operatively connected maintenance planning device;
wherein constructing the predictive fault list comprises;
retrieving, via the processor, a part failure history for each sensor indicated in the plurality of component faults from the aircraft processor while the aircraft is in flight; and
evaluating, based on the part failure history, for each sensor associated with a particular sensor fault in the plurality of component faults from the aircraft processor, a relationship between
1) an aircraft flight path,
2) the particular sensor fault, and
3) a prediction hit or miss rate for the sensor associated with the sensor fault.
2 Assignments
0 Petitions
Accused Products
Abstract
Disclosed is a computer-implemented method for maintenance planning for an aircraft. The method includes retrieving, via a processor, a data transmission comprising a plurality of component faults from an aircraft processor while the aircraft is in flight. The processor executes, using a prediction engine, a predictive fault list based on the component faults. The predictive fault list includes a plurality of weighted predictions of authentic component faults and nuisance component faults. The processor prioritizes the weighted predictions of authentic component faults, and generates a maintenance checklist prioritized based on the weighted prediction of authentic component faults. The processor then outputs the prioritized maintenance checklist on an operatively connected maintenance planning device.
82 Citations
14 Claims
-
1. A computer-implemented method for maintenance planning for an aircraft, the method comprising:
-
measuring, using one or more sensors, conditions of the aircraft; retrieving, via a processor, a data transmission comprising a plurality of component faults from an aircraft processor while the aircraft is in flight based at least in part on measurements from the one or more sensors; constructing, via the processor executing a prediction engine, a predictive fault list based on the component faults, the predictive fault list having a plurality of weighted predictions of authentic component faults and nuisance component faults; prioritizing, via the processor, the weighted predictions of authentic component faults; generating, via the processor, a maintenance checklist prioritized based on the weighted prediction of authentic component faults; and outputting, via an output processor, the prioritized maintenance checklist on an operatively connected maintenance planning device; wherein constructing the predictive fault list comprises; retrieving, via the processor, a part failure history for each sensor indicated in the plurality of component faults from the aircraft processor while the aircraft is in flight; and evaluating, based on the part failure history, for each sensor associated with a particular sensor fault in the plurality of component faults from the aircraft processor, a relationship between
1) an aircraft flight path,
2) the particular sensor fault, and
3) a prediction hit or miss rate for the sensor associated with the sensor fault. - View Dependent Claims (2, 3, 4, 5)
-
-
6. A system for aircraft maintenance planning comprising:
-
one or more sensors configured to measure conditions of an aircraft; a processor configured to; retrieve a data transmission comprising a plurality of component faults from the aircraft processor while the aircraft is in flight based at least in part on measurement from the one or more sensors; construct, via a prediction engine, a predictive fault list based on the component faults, the predictive fault list having a plurality of weighted predictions of authentic component faults and nuisance component faults; prioritize, via the prediction engine, the weighted predictions of authentic component faults; generate a maintenance checklist prioritized based on the weighted prediction of authentic component faults; and output the prioritized maintenance checklist on an operatively connected maintenance planning device; wherein constructing the predictive fault list comprises; retrieving, via the processor, a part failure history for each sensor indicated in the plurality of component faults from the aircraft processor while the aircraft is in flight; and evaluating, based on the part failure history, for each sensor associated with a particular sensor fault in the plurality of component faults from the aircraft processor, a relationship between
1) an aircraft flight path,
2) the particular sensor fault, and
3) a prediction hit or miss rate for the sensor associated with the sensor fault. - View Dependent Claims (7, 8, 9)
-
-
10. A non-transitory computer readable medium comprising a computer program product configured to, when executed on a processor, perform a method for aircraft maintenance planning comprising:
-
one or more sensors configured to measure conditions of an aircraft, retrieving, via the processor, a data transmission comprising a plurality of component faults from an aircraft processor while the aircraft is in flight based at least in part on measurements from the one or more sensors; constructing, via the processor executing a prediction engine, a predictive fault list based on the component faults, the predictive fault list having a plurality of weighted predictions of authentic component faults and nuisance component faults; prioritizing, via the processor, the weighted predictions of authentic component faults; generating, via the processor, a maintenance checklist prioritized based on the weighted prediction of authentic component faults; and outputting, via an output processor, the prioritized maintenance checklist on an operatively connected maintenance planning device; wherein constructing the predictive fault list comprises; retrieving, via the processor, a part failure history for each sensor indicated in the plurality of component faults from the aircraft processor while the aircraft is in flight; and evaluating, based on the part failure history, for each sensor associated with a particular sensor fault in the plurality of component faults from the aircraft processor, a relationship between
1) an aircraft flight path,
2) the particular sensor fault, and
3) a prediction hit or miss rate for the sensor associated with the sensor fault. - View Dependent Claims (11, 12, 13, 14)
-
Specification