Integrating design and field management of gas turbine engine components with a probabilistic model
First Claim
1. A gas turbine engine lifecycle decision assistance system for quantifying uncertainties during the lifecycle of one or more gas turbine engine components, the system comprising:
- a processor; and
one or more machine-accessible storage media coupled to the processor, the one or more machine-accessible storage media comprising;
a bidirectional probabilistic analysis subsystem comprising a probabilistic model of conditional dependencies between a plurality of random variables associated with a plurality of different sources of uncertainty in the gas turbine engine component lifecycle, wherein each source of uncertainty is associated with a random variable of the plurality of random variables, and wherein the probabilistic model includes an acyclic directed graph that includes a plurality of nodes and one or more edges, wherein each node corresponds to a random variable of the plurality of variables, and wherein each edge corresponds to a conditional dependency between a pair of random variables, the probabilistic model arranged to connect at least two of the plurality of different sources of uncertainty by a common random variable of the plurality of random variables, the bidirectional probabilistic analysis subsystem to, when executed by the processor;
compute a joint probability distribution for the probabilistic model;
periodically receive new evidence from one or more of the different sources of uncertainty over the course of the component lifecycle;
in response to the new evidence, re-compute the joint probability distribution;
determine a current phase of the gas turbine engine component lifecycle, wherein the current phase comprises a pre-production certification phase or a post-production certification phase;
communicate the re-computed joint probability distribution to a component design subsystem in response to determining the current phase is the pre-production certification phase; and
communicate the re-computed joint probability distribution to a field management subsystem in response to determining the current phase is the post-production certification phase, wherein the one or more machine-accessible storage media comprises the component design subsystem and/or the field management subsystem.
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Abstract
Embodiments of a gas turbine engine lifecycle decision assistant apply a probabilistic-based process founded on a Bayesian mathematical framework to intelligently combine analytical models, expert judgment, and data during the development and field management of gas turbine engines. The process integrates physics-based and high-fidelity models with data and expert judgment that evolves over the course of the gas turbine engine lifecycle. Among other things, embodiments of the gas turbine engine lifecycle decision assistant can improve future predictive models and understanding while at the same time reducing risk and uncertainty in the service management of existing products.
18 Citations
20 Claims
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1. A gas turbine engine lifecycle decision assistance system for quantifying uncertainties during the lifecycle of one or more gas turbine engine components, the system comprising:
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a processor; and one or more machine-accessible storage media coupled to the processor, the one or more machine-accessible storage media comprising; a bidirectional probabilistic analysis subsystem comprising a probabilistic model of conditional dependencies between a plurality of random variables associated with a plurality of different sources of uncertainty in the gas turbine engine component lifecycle, wherein each source of uncertainty is associated with a random variable of the plurality of random variables, and wherein the probabilistic model includes an acyclic directed graph that includes a plurality of nodes and one or more edges, wherein each node corresponds to a random variable of the plurality of variables, and wherein each edge corresponds to a conditional dependency between a pair of random variables, the probabilistic model arranged to connect at least two of the plurality of different sources of uncertainty by a common random variable of the plurality of random variables, the bidirectional probabilistic analysis subsystem to, when executed by the processor; compute a joint probability distribution for the probabilistic model; periodically receive new evidence from one or more of the different sources of uncertainty over the course of the component lifecycle; in response to the new evidence, re-compute the joint probability distribution; determine a current phase of the gas turbine engine component lifecycle, wherein the current phase comprises a pre-production certification phase or a post-production certification phase; communicate the re-computed joint probability distribution to a component design subsystem in response to determining the current phase is the pre-production certification phase; and communicate the re-computed joint probability distribution to a field management subsystem in response to determining the current phase is the post-production certification phase, wherein the one or more machine-accessible storage media comprises the component design subsystem and/or the field management subsystem. - View Dependent Claims (2, 3, 4, 5, 6, 7)
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8. A method for quantifying uncertainty during different phases of the lifecycle of a manufactured component, the method comprising, with at least one computing device:
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identifying at least two sources of uncertainty that are associated with different phases of the manufactured component lifecycle, wherein each source of uncertainty is associated with a random variable of a plurality of random variables; connecting the at least two sources of uncertainty by a common random variable of the plurality of random variables in a Bayesian network, wherein the Bayesian network includes an acyclic directed graph that includes a plurality of nodes and one or more edges, wherein each node corresponds to a random variable of the plurality of variables, and wherein each edge corresponds to a conditional dependency between a pair of random variables; computing a joint probability distribution for the Bayesian network using the common random variable and at least one random variable associated with each of the at least two sources of uncertainty; determining a current phase of the manufactured component lifecycle, wherein the current phase comprises a pre-production certification phase or a post-production certification phase; communicating the re-computed joint probability distribution to a component design subsystem in response to determining the current phase is the pre-production certification phase; and communicating the re-computed joint probability distribution to a field management subsystem in response to determining the current phase is the post-production certification phase. - View Dependent Claims (9, 10, 11, 12, 13, 14, 15, 16, 17)
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18. A gas turbine engine lifecycle decision assistant for quantifying uncertainties during the lifecycle of a gas turbine engine component, the gas turbine engine lifecycle decision assistant comprising:
- computer program instructions embodied in one or more machine-accessible storage media and executable by at least one processor to;
create a Bayesian network of conditional dependencies between a plurality of random variables associated with a plurality of different sources of uncertainty in the gas turbine engine component lifecycle, wherein each source of uncertainty is associated with a random variable of the plurality of random variables, and wherein the Bayesian network includes an acyclic directed graph that includes a plurality of nodes and one or more edges, wherein each node corresponds to a random variable of the plurality of variables, and wherein each edge corresponds to a conditional dependency between a pair of random variables, the Bayesian network arranged to connect at least two of the plurality of different sources of uncertainty by a common random variable of the plurality of random variables; compute a joint probability distribution for the Bayesian network; receive new evidence from one or more of the different sources of uncertainty over the course of the component lifecycle; in response to the new evidence, re-compute the joint probability distribution; determine a current phase of the gas turbine engine component lifecycle, wherein the current phase comprises a pre-production certification phase or a post-production certification phase; communicate the re-computed joint probability distribution to a component design subsystem in response to determining the current phase is the pre-production certification phase; and communicate the re-computed joint probability distribution to a field management subsystem in response to determining the current phase is the post-production certification phase. - View Dependent Claims (19, 20)
- computer program instructions embodied in one or more machine-accessible storage media and executable by at least one processor to;
Specification