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ARP - 5765 - updates - FAAWorkshop - 08102016 - 图文

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ARP5765 Rev. A :

Analytical Methods for Aircraft Seat Design and Evaluation

Prasanna Bhonge10 August 2016

Background

AC 20-146: Methodology for Dynamic Seat Certification by Analysis for Use in Parts 23, 25, 27, & 29 Airplanes and Rotorcrafts

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Signed in May 2003; allows simulation results to be used in support of seat certification

Provides high-level guidance on the validation of seat models

Defines the conditions under which computer modeling can be used in support of certification

ARP 5765

Analytical Methods for Aircraft Seat Design and Evaluation

Objectives

TheprimaryobjectivesoftheARPistoprovide?

Quantitativemethodtomeasureandevaluatethedegreeofcorrelationbetweenamodelandaphysicaltest

Bestmodelingpracticestoimprovetheaccuracyandpredictabilityofseatanalyses

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Technical Specialist from

Seat Suppliers?Weber / Zodiac?IPECO?Recaro?Sicma?B/E Aerospace?ContourA/C Manufacturers?Airbus?Cessna ?Embraer?BombardierSoftware?FTSS?TASS?ESI?Altair?LSTCRegulatory?FAA?EASAAcademic?NIAR SAE ARP 5765 Rev A –Published in Nov. 2015.

1.SCOPE2.REFERENCES

3.4.5.6.7.V-ATD CALIBRATION

SYSTEM VERIFICATION AND VALIDATION (REV A)MODEL USE (REV A)

DOCUMENTATION (REV A)BEST PRACTICES

APPENDIX

A: METHODOLOGY FOR THE COMPARISON OF TEST AND SIMULATION WAVEFORMS B: FAA -NIAR DATA SET FOR THE HYBRID II ATDC: FAA -NIAR DATA SET FOR THE FAA HYBRID III ATDD: SAMPLE HYBRID II V-ATD CALIBRATION REPORT

E: SYSTEM VERIFICATION AND VALIDATION EXAMPLES (REV A)

3.0 v-ATD Calibration

Goal: define the process for ensuring that v-ATDs match the

anthropometry and kinematic performance of a physical ATD for aviation-specific applications

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???

Mass and Geometry

Component Response (head, chest, knee, etc.)Pelvic Shape Evaluation (cushion interaction)

Dynamic Response : evaluate ATD performance for aircraft conditions

FF 2pt belt: extreme flail envelopeFF 3pt belt: torso twistFF 4pt belt: submariningDownload: vertical crash vector

Test Condition 2 (14 CFR XX.562) 2pt, 3pt, 4pt restraint system

Test Condition 1 (14 CFR XX.562)

ARP - 5765 - updates - FAAWorkshop - 08102016 - 图文

ARP5765Rev.A:AnalyticalMethodsforAircraftSeatDesignandEvaluationPrasannaBhonge10August2016BackgroundAC20-146:MethodologyforDynamicSeatCertificationb
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