SAE ARP 5120 : 2016
SAE ARP 5120 : 2016
AIRCRAFT GAS TURBINE ENGINE HEALTH MANAGEMENT SYSTEM DEVELOPMENT AND INTEGRATION GUIDE
SAE International
AIRCRAFT GAS TURBINE ENGINE HEALTH MANAGEMENT SYSTEM DEVELOPMENT AND INTEGRATION GUIDE
SAE International
1. SCOPE
2. REFERENCES
3. CONCEPTS AND CONSIDERATIONS
4. RECOMMENDED PRACTICES FOR DESIGN, DEVELOPMENT,
AND TEST
5. RECOMMENDED PRACTICES FOR IMPLEMENTATION
6. CONCLUSION
7. NOTES
APPENDIX A - HEALTH MANAGEMENT STANDARDS
APPENDIX B - SENSOR PARAMETER AND SIGNAL PERFORMANCE
REQUIREMENTS (SENSE/ACQUIRE)
APPENDIX C - EXAMPLE EGT MARGIN CALCULATION
APPENDIX D - DATA MANIPULATION DESIGN AND PERFORMANCE
REQUIREMENTS (ANALYSIS/ACT)
Gives recommended best practices, procedures, and technology to guide the physical and functional design, development, integration, verification, and validation of highly reliable Engine Health Management (EHM) systems for aircraft engines and Auxiliary Power Units (APUs).
Document Type | Standard |
Status | Current |
Publisher | SAE International |
Committee | E-32 |