1 / 8

RPI DSES-6070 HV7 Project Derk Philippona Fall 2008

RPI DSES-6070 HV7 Project Derk Philippona Fall 2008. Introduction: Description of the Problem Radar component failure data collected over a three year period on 241 Navy F/A-18 aircraft, taken from Blischke reference, were analyzed to provide a basis for making warranty decisions.

levia
Télécharger la présentation

RPI DSES-6070 HV7 Project Derk Philippona Fall 2008

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript


  1. RPI DSES-6070 HV7 Project Derk Philippona Fall 2008

  2. Introduction: Description of the ProblemRadar component failure data collected over a three year period on 241 Navy F/A-18 aircraft, taken from Blischke reference, were analyzedto provide a basis for making warranty decisions

  3. Methodologies: Summary Description • Data best fit failure distribution function identified with MINITAB • Expressions and plots for failure functions obtained with MAPLE • Constructed Monte Carlo model of data with EXCEL • Verified no benefit for age replacement policy with EXCEL model • Studied benefit of cold standby redundancy with MAPLE and EXCEL

  4. Results: Analysis / DiscussionExponential and Weibull distributions fit data well

  5. Results: Analysis / DiscussionReliability functions defined • F := 1-exp(-t/(223.653)); 1 - exp(-0.004471212101 t) • R := 1-F; exp(-0.004471212101 t) • f := diff (F, t); 0.004471212101 exp(-0.004471212101 t) • z := f/R; 0.004471212101 • MTTF := int (R, t = 0 .. infinity); 223.6530000

  6. Results: Analysis / DiscussionAge replacement policy does not reduce total cost(as expected with constant failure rate)

  7. Results: Analysis / DiscussionCold standby redundancy doubles MTTF • Rs := exp(-0.004471212101 t) + 0.004247651496 exp(-0.004471212101 t) t • evalf(subs(t = 223, Rs)); 0.7184390857 • evalf(subs(t = 223, R)); 0.3689551089 • MTTFs := int(Rs, t = 0 .. infinity); 436.1233500

  8. Conclusions: • Exponential distribution function fits failure data well • Failure rate is approximately constant; 4.47 failures / 1000 flight hours • MTTF is 223.65 flight hours • An age replacement policy does not reduce total cost, as expected with • a constant failure rate • Modifying the radar system to add a cold standby exciter and switch • could approximately double MTTF

More Related