Aircraft prognostics health system
First Claim
1. A method of assessing reliability of a rotorcraft component, comprising:
- identifying, by a processor, aboard a rotorcraft, a first probability of failure of the rotorcraft component installed on the rotorcraft, the first probability of failure representing a probability of failure of the rotorcraft component prior to application of at least one load;
receiving, by the processor, from one or more sensors installed on the rotorcraft, one or more measurements representative of the at least one load applied against the rotorcraft component;
determining, by the processor, aboard the rotorcraft, a second probability of failure of the rotorcraft component based on the first probability of failure and the received one or more measurements representative of the at least one load applied against the rotorcraft component, the second probability of failure representing a probability of failure of the rotorcraft component after application of the at least one load;
determining, by the processor, an equivalent life by assessing a cumulative damage of a change of a probability of failure and then converting the change of the probability of failure back into a time domain;
subtracting, by the processor, a calculated used-life damage index from a baseline model to identify a variance and then credit the variance towards a remaining useful life of the rotorcraft component so as to extend the remaining useful life of the rotorcraft component; and
adjusting, by the processor, at least one of an operation and a maintenance of the rotorcraft based on the remaining useful life.
1 Assignment
0 Petitions
Accused Products
Abstract
According to one example embodiment, a method of assessing reliability of an aircraft component includes identifying, aboard an aircraft, a first probability of failure of the aircraft component installed on the aircraft. One or more measurements representative of at least one load applied against the aircraft component are received. Determined, aboard the aircraft, is a second probability of failure of the aircraft component based on the first probability of failure and the received one or more measurements representative of the at least one load applied against the aircraft component, the second probability of failure representing a probability of failure of the aircraft component after application of the at least one load.
37 Citations
20 Claims
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1. A method of assessing reliability of a rotorcraft component, comprising:
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identifying, by a processor, aboard a rotorcraft, a first probability of failure of the rotorcraft component installed on the rotorcraft, the first probability of failure representing a probability of failure of the rotorcraft component prior to application of at least one load; receiving, by the processor, from one or more sensors installed on the rotorcraft, one or more measurements representative of the at least one load applied against the rotorcraft component; determining, by the processor, aboard the rotorcraft, a second probability of failure of the rotorcraft component based on the first probability of failure and the received one or more measurements representative of the at least one load applied against the rotorcraft component, the second probability of failure representing a probability of failure of the rotorcraft component after application of the at least one load; determining, by the processor, an equivalent life by assessing a cumulative damage of a change of a probability of failure and then converting the change of the probability of failure back into a time domain; subtracting, by the processor, a calculated used-life damage index from a baseline model to identify a variance and then credit the variance towards a remaining useful life of the rotorcraft component so as to extend the remaining useful life of the rotorcraft component; and adjusting, by the processor, at least one of an operation and a maintenance of the rotorcraft based on the remaining useful life. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10)
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11. A system for assessing reliability of a rotorcraft component, comprising:
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a rotorcraft comprising a body, a power train coupled to the body and comprising a power source and a drive shaft coupled to the power source, a hub, a rotor blade coupled to the hub, and one or more sensors operable to provide a plurality of measurements; and a prognostics health system, including at least one processor, installed onboard the rotorcraft and operable to; identify, aboard the rotorcraft, a first probability of failure of the rotorcraft component installed on the rotorcraft, the first probability of failure representing a probability of failure of the rotorcraft component prior to application of at least one load; receive, from the one or more sensors installed on the rotorcraft, one or more measurements representative of the at least one load applied against the rotorcraft component; determine, aboard the rotorcraft, a second probability of failure of the rotorcraft component based on the first probability of failure and the received one or more measurements representative of the at least one load applied against the rotorcraft component, the second probability of failure representing a probability of failure of the rotorcraft component after application of the at least one load; determine an equivalent life by assessing a cumulative damage of a change of a probability of failure and then converting the change of the probability of failure back into a time domain; subtract a calculated used-life damage index from a baseline model to identify a variance and then credit the variance towards a remaining useful life of the aircraft component so as to extend the remaining useful life of the aircraft component; and adjust at least one of an operation and a maintenance of the aircraft based on the remaining useful life. - View Dependent Claims (12, 13, 14, 15, 16, 17, 18, 19, 20)
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Specification