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Impact Characteristics of Seat Back Mounted IFE Monitors - Basis for ARP6330
- Aerospace Standard
- AIR6908
- Issued
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This document provides background information, rationale, and data (both physical testing and computer simulations) used in defining the component test methods and similarity criteria described in SAE Aerospace Recommended Practice (ARP) 6330. ARP6330 defines multiple test methods uses to assess the effect of seat back mounted IFE monitor changes on blunt trauma to the head and post-impact sharp edge generation. The data generated is based on seat and IFE components installed on type A-T (transport airplane) certified aircraft. While not within the scope of ARP6330, generated test data for the possible future development of surrogate target evaluation methods is also included.
Rationale
This SAE Aerospace Information Report (AIR) documents the data and rationale used in the development of Aerospace Recommended Practice (ARP) 6330.
Recommended Content
| Aerospace Standard | Methods to Evaluate Impact Characteristics of Seat Back Mounted IFE Monitors |
| Aerospace Standard | Aircraft Seat Design Guidance and Clarifications |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| Unnamed Dataset 3 | ||
| Table 2 | HIC sensitivity study modified parameters | |
| Table A1 | Seat/IFE monitor configurations investigated | |
| Table B1 | Zodiac seats U.S. HIC test data | |
| Table B2 | B/E Aerospace HIC test data | |
| Table C1 | Configuration #2 test results - baseline monitor only | |
| Table C2 | Configuration #3 test results - baseline monitor only | |
| Table C3 | Configuration #5 test results | |
| Table D1 | Initial head impact velocity with seat back during HIC testing | |
| Table E1 | Configuration #5 test results | |
| Table E3 | Configuration #6 test results | |
| Unnamed Dataset 14 | ||
| Table G1 | Comparison of B/E aerospace FEM model and dynamic test HIC results | |
| Table G2 | B/E aerospace HCTD parametric study results | |
| Table G3 | B/E Aerospace row-to-row dynamic test parametric study results | |
| Unnamed Dataset 18 | ||
| Table G4 | Recaro row-to-row dynamic test parametric study results | |
| Unnamed Dataset 20 | ||
| Table G5 | Zodiac HCTD parametric study results with rigid bracket | |
| Table G6 | Zodiac HCTD parametric study results with bracket tilt locked | |
| Table G7 | Zodiac row-to-row dynamic test parametric study results | |
| Table G8 | Zodiac row-to-row dynamic test parametric study results (no glass erosion) | |
| Table H1 | Kinetic/internal strain energy attenuation - Recaro | |
| Table H2 | Seat back internal strain energy distribution - Recaro | |
| Table H3 | Monitor internal strain energy distribution - Recaro | |
| Table H4 | Effect of monitor change on seat back internal strain energy distribution - Recaro | |
| Table H5 | Effect of monitor change on monitor internal strain energy distribution - Recaro | |
| Table H6 | Kinetic/internal strain energy attenuation - Zodiac | |
| Table H7 | Seat back internal strain energy distribution - Zodiac | |
| Table H8 | Monitor internal strain energy distribution - Zodiac | |
| Table H9 | Effect of monitor change on seat back internal strain energy distribution (with glass erosion function) - Zodiac | |
| Table H10 | Effect of monitor change on seat back internal strain energy distribution (without glass erosion function) - Zodiac | |
| Table H11 | Effect of monitor change on monitor internal strain energy distribution - Zodiac | |
| Table H12 | Effect of monitor change on monitor internal strain energy distribution - Zodiac (no glass erosion) | |
| Table I1 | Impact location #1 test data | |
| Table I2 | Impact location #2 test data |
Issuing Committee
The Aerospace Council of SAE established the Aircraft Seat Committee (SEAT) in 1997 to address technical issues related to the design and/or performance of aircraft seating systems. The seating systems include crew, flight attendants, and passenger seats installed in Civil Rotorcraft, Transport Aircraft, and General Aviation Aircraft.
A list of the technical reports developed by the SEAT Committee can be obtained by searching on 'aircraft seat' and selecting 'standards', from the SAE Home Page. SEAT StandardsReference
| Number | Title |
|---|
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