ImageVerifierCode 换一换
格式:PDF , 页数:77 ,大小:776.27KB ,
资源ID:673010      下载积分:10000 积分
快捷下载
登录下载
邮箱/手机:
温馨提示:
如需开发票,请勿充值!快捷下载时,用户名和密码都是您填写的邮箱或者手机号,方便查询和重复下载(系统自动生成)。
如填写123,账号就是123,密码也是123。
特别说明:
请自助下载,系统不会自动发送文件的哦; 如果您已付费,想二次下载,请登录后访问:我的下载记录
支付方式: 支付宝扫码支付 微信扫码支付   
注意:如需开发票,请勿充值!
验证码:   换一换

加入VIP,免费下载
 

温馨提示:由于个人手机设置不同,如果发现不能下载,请复制以下地址【http://www.mydoc123.com/d-673010.html】到电脑端继续下载(重复下载不扣费)。

已注册用户请登录:
账号:
密码:
验证码:   换一换
  忘记密码?
三方登录: 微信登录  

下载须知

1: 本站所有资源如无特殊说明,都需要本地电脑安装OFFICE2007和PDF阅读器。
2: 试题试卷类文档,如果标题没有明确说明有答案则都视为没有答案,请知晓。
3: 文件的所有权益归上传用户所有。
4. 未经权益所有人同意不得将文件中的内容挪作商业或盈利用途。
5. 本站仅提供交流平台,并不能对任何下载内容负责。
6. 下载文件中如有侵权或不适当内容,请与我们联系,我们立即纠正。
7. 本站不保证下载资源的准确性、安全性和完整性, 同时也不承担用户因使用这些下载资源对自己和他人造成任何形式的伤害或损失。

版权提示 | 免责声明

本文(DIN EN 16602-30-02-2014 Space product assurance - Failure modes effects (and criticality) analysis (FMEA FMECA) English version EN 16602-30-02 2014《航天产品保证 失效模式和效应 (以及临界性) 分析 (FMEA .pdf)为本站会员(fatcommittee260)主动上传,麦多课文库仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。 若此文所含内容侵犯了您的版权或隐私,请立即通知麦多课文库(发送邮件至master@mydoc123.com或直接QQ联系客服),我们立即给予删除!

DIN EN 16602-30-02-2014 Space product assurance - Failure modes effects (and criticality) analysis (FMEA FMECA) English version EN 16602-30-02 2014《航天产品保证 失效模式和效应 (以及临界性) 分析 (FMEA .pdf

1、Dezember 2014DEUTSCHE NORM DIN-Normenausschuss Luft- und Raumfahrt (NL)Preisgruppe 26DIN Deutsches Institut fr Normung e. V. Jede Art der Vervielfltigung, auch auszugsweise, nur mit Genehmigung des DIN Deutsches Institut fr Normung e. V., Berlin, gestattet.ICS 49.140!% 1E-1 4 Occasional 1E-3 P 1E-1

2、3 Remote 1E-5 P 1E-3 2 Extremely remote P 1E-5 1 i. The quantitative approach shall be used when specific failure rates and probability of occurrence data are available. j. Data sources, approved by the customer, shall be listed. k. The data sources shall be the same as those used for the other depe

3、ndability analyses performed for the programme. EN 16602-30-02:2014 (E) DIN EN 16602-30-02:2014-12 23 l. The failure probabilities shall be ranked as per Table 5-2 and relevant entry (the PN) listed in the FMECA worksheet column. m. The CN for a specific failure mode shall be developed from the seve

4、rity of the failure effects and the probability of the failure mode occurrence. n. The CN shall be calculated as the product of the ranking assigned to each factor: CN = SN x PN. o. Failure modes having a high CN shall be given a higher priority in the implementation of the corrective actions than t

5、hose having a lower CN. 5.3 Identification of critical items a. An item shall be considered a critical item if: 1. a failure mode has failure consequences classified as catastrophic, or 2. a failure mode is classified as CN greater or equal to 6 in conformance with Table 5-3. NOTE The customer can t

6、ailor the criteria for critical item identification defining a failure mode as critical according to programme specific needs. Table 5-3: Criticality matrix Severity category SNs Probability level 10-510-310-11 PNs 1 2 3 4 catastrophic 4 4 8 12 16 critical 3 3 6 9 12 major 2 2 4 6 8 negligible 1 1 2

7、 3 4 5.4 FMECA report a. The results of the FMECA shall be documented in a FMECA report in conformance with the DRD in Annex A. EN 16602-30-02:2014 (E) DIN EN 16602-30-02:2014-12 24 6 FMEA/FMECA implementation requirements 6.1 General requirements a. Formal delivery of the FMEA/FMECA shall be in acc

8、ordance with the SOW. NOTE Generally the report is presented at all design reviews. b. In each phase, the FMEA/FMECA shall be reviewed, updated and changes recorded on a continuous basis to maintain the analysis current with the design evolution. NOTE For the project phase definition refer to ECSS-M

9、-ST-10. c. The means of recording the FMEA/FMECA shall be agreed by the customer. 6.2 Phase 0: Mission analysis or requirements identification In this phase the FMEA/FMECA is, typically, not performed. 6.3 Phase A: Feasibility a. The FMEA/FMECA shall assist the trade-off among the various possible d

10、esign concepts by assessing their impact on the project dependability and safety requirements. NOTE The analysis contributes to the overall risk evaluation of each design concept. The functional approach is generally used. b. The FMEA/FMECA shall make use of, as a minimum, the following inputs: 1. t

11、he mission requirements, in particular the dependability and safety requirements; 2. the design documentation of the different product concepts identified in phase 0; EN 16602-30-02:2014 (E) DIN EN 16602-30-02:2014-12 25 3. the hierarchical decomposition of the product functions. NOTE The function d

12、ecomposition is generally derived from the functional analysis. c. The FMEA/FMECA shall be performed to provide the following results: 1. evaluation of the conformance of each design concept function to the system dependability and safety requirements; 2. identification of critical failure scenarios

13、; 3. identification of needs of focused analyses; NOTE For example: fault tree. 4. identification of the features to be implemented for each analysed function in order to meet the system dependability and safety requirements. NOTE 1 Example of the identified features are: functional redundancies or

14、inhibits, possible alternative implementations. NOTE 2 A report for FMEA/FMECA is, typically, not required for phase A. 6.4 Phase B: Preliminary definition a. The FMEA/FMECA shall be performed either according to the functional approach (functional FMEA/FMECA) or to the hardware approach (hardware F

15、MEA/FMECA). NOTE A list of part failure modes is provided in Annex G. b. Rationale for selection of the approach shall be provided considering the following criteria: 1. available design data; 2. product complexity and level of integration; 3. criticality of the product or function; 4. segregation o

16、f function. c. The FMEA/FMECA shall: 1. support the trade-offs from the dependability and safety point of view; 2. support the definition of the requirements to be implemented in the product as redundancies, inhibits, operations to be followed to avoid hazards or loss of mission, and others, such as

17、 fail-safe, leak before burst, and maximum time allowable before compensation activation. d. The FMEA/FMECA shall make use of, as a minimum, the following inputs: 1. The mission requirements and the mission profile. EN 16602-30-02:2014 (E) DIN EN 16602-30-02:2014-12 26 2. The product specification,

18、considering in particular the dependability and safety requirements. NOTE Examples of product specifications are: system or subsystem specification and performance specification. 3. The current hierarchical decomposition of the product functions. NOTE The function decomposition is generally derived

19、from the functional analysis. 4. The design of the product architecture. NOTE Examples of product architecture are: design description, drawings and interfaces description. 5. Available information from the product safety analyses relevant to hazard causes and controls. 6. When applicable, available

20、 information from maintenance analysis relevant to replaceable unit definition. 7. When available, FMEA/FMECAs performed at lower integration levels. 8. For lower level FMEA/FMECAs, agreed list of parts failure modes 9. For FMECA, item failure rates from data sources agreed by the customer. e. The F

21、MEA/FMECA shall provide the following results: 1. Inputs for dependability and safety requirements to be allocated for implementing the prevention and compensation methods and for minimizing the single point failures and the identified critical failure scenarios. NOTE The dependability and safety re

22、quirements are in priority allocated to the product and lower levels. Recommendation to higher levels can be raised too. 2. Input to safety analyses: identification of hazardous consequences due to failures at lower levels and relevant identified prevention and compensation methods. 3. When applicab

23、le, input to maintainability analyses. NOTE Example of the input is the identification of replaceable units for meeting the dependability and safety requirements. 4. Input to software criticality analysis. NOTE Example of the input is the identification of software functional failure consequences. 5. Input to the critical function list or critical item list. NOTE Example of these inputs is the identification of the critical items as defined in clause 4.3 or 5.3. EN 16602-30-02:2014 (E) DIN EN 16602-30-02:2014-12

copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
备案/许可证编号:苏ICP备17064731号-1