ANSI AIAA S-102.2.2-2009 Performance-Based System Reliability Modeling Requirements.pdf
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1、 Standard ANSI/AIA S-102.2.2-2009 Performance-Based System Reliability Modeling Requirements AIA standards are copyrighted by the American Institute of Aeronautics and Astronautics (AIA), 1801 Alexander Bel Drive, Reston, VA 20191-434 USA. Al rights reserved. AIA grants you a license as folows: The
2、right to download an electronic file of this AIA standard for storage on one computer for purposes of viewing, and/or printing one copy of the AIA standard for individual use. Neither the electronic file nor the hard copy print may be reproduced in any way. In adition, the electronic file may not be
3、 distributed elsewhere over computer networks or otherwise. The hard copy print may only be distributed to other employees for their internal use within your organization. ANSI/AIA S-102.2.2-209 American National Standard Performance-Based System Reliability Modeling Requirements Sponsored by Americ
4、an Institute of Aeronautics and Astronautics Approved 17 November 208 American National Standards Institute Abstract This Standard provides the basis for developing performance-based System Reliability Modeling to develop mathematical or simulation models to be used for making numerical aportionment
5、s and reliability predictions based on the reliability characteristics and functional interdependencies for al configured items required to perform the mision. The requirements for contractors, the planing and reporting neds, along with the analytical tols are established. The linkage of this Standa
6、rd to the other standards in the new family of performance-based Reliability and Maintainability (R plan the activities to achieve a level of R apraise the performance an R and identify the activities necesary to improve the performance of an R b) The description of system operating modes and enviro
7、nments versus the mision timeline; c) The listing of functional components versus reliability values; d) The maturity and confidence level of the reliability value for each functional component; e) The indentured graphical system reliability model; f) The indentured system reliability predictions by
8、 functional components, mision-critical system functions, and aplicable levels of mision suces; g) The identification of hardware or functional elements of the system that are not included in the system reliability model, along with rationale for each elements exclusion from the model. 5 Detailed Re
9、quirements The folowing detailed requirements pertain to the performance-based System Reliability Modeling proces defined in Anex B. ANSI/AIA S-102.2.2-2009 8 5.1 System Design Data Colection Prior to begining the evaluation of system failure modes, the contractor shal colect suficient system design
10、 information to define al aplicable functional and physical characteristics of the system, and the reliability atributes that fal within the analytical ground rules to be specified by the contractor (se reference 9). The system design information shal include al system levels, mision phases, and env
11、ironments, and al normal, degraded, and contingency system odes that are aplicable to each mision phase. If a Capability Level 3 or higher System Reliability Modeling proces is required, this information shal be entered in the System Reliability Modeling database to alow cros-referencing functional
12、components against oficial design drawings. At a minimum, the contractors analytical ground rules shal include the identification of reliability atributes for al functional and physical components that aply to the capability level of the System Reliability Modeling proces under contract. Suficient e
13、nginering information shal be colected to determine the maturity and confidence level of the reliability value(s) used for each functional or physical component. 5.2 System Reliability Modeling Proces A reliability model shal be developed and maintained for the system or the system of systems (SoS)
14、if required. At a minimum, the model shal be developed to the functional component level, shal define the physical components asociated with each functional component, shal define the probability of failure/suces or hazard rate for each physical component, and shal provide the probability of ocurenc
15、e for each unaceptable failure severity clasification as defined in Table 1. If a Capability Level 2 System Reliability Modeling proces is required, the model also shal provide the probability of ocurence for unanticipated failures3for each unaceptable failure severity clasification as defined in Ta
16、ble 1. Reliability modeling techniques shal be used that provide separate outputs for: (1) the predicted reliability of each mision critical function, and (2) predicted reliability of the system, i.e., colective reliability of the subsystems, asemblies, components, and parts. The reliability models
17、shal be traceable to and cros-referenced to the latest aproved system design schematics, drawings, and specifications. The redundancy switching devices, i.e., relays and circuits shal be clearly identified in the reliability model where aplicable. The nomenclature used to identify items in reliabili
18、ty model shal be consistent with that used in the latest aproved system design schematics, drawings, and specifications. The system reliability model shal be updated, as neded, with enginering information resulting from FMECA, tests, aproved design changes, environmental studies, operations planing,
19、 and field experience. If a Capability Level 3 System Reliability Modeling proces is required, the reliability modeling data products shal be compatible with the Product FMECA/Hazards Analysis database, and the functional component reliability models shal include software and software to hardware in
20、terfaces, as necesary, to predict system reliability. 5.2.1 System Reliability Predictions The contractor shal construct a system reliability model to depict the intended utilization of the elements of the system to achieve mision suces. The system reliability model shal consist of a graphical syste
21、m reliability model or RBD that shows al of the series-paralel functional paths that are required for sucesful system operation. Each reliability block in the RBD shal have a description that includes the item identification that is traceable to design schematics or drawings, the aplicable mision ti
22、me and environment, the operating modes of the item acros the mision timeline, the asumptions used to develop the reliability block, and the references for locating the simulation or mathematical expresions used to obtain reliability values. For this standard, a single reliability block shal be used
23、 to represent a simulation instruction set, an event tre diagram, a fault tre diagram, a Markov diagram4, or a probability truth table, al of which have varied degres of complexity, ranging from representing a single component to hundreds of components. 3For this standard, unanticipated system failu
24、res are operational anomalies that are not documented in reliability analyses or test anomaly reports. 4Markov diagram is the comon name given to graphical representations of state transition models. ANSI/AIA S-102.2.2-2009 9 Table 1 AIA S-102 Failure Severity Clasification Failure Severity Clasific
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