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Development of 2 underseat energy absorbers for application to crashworthy passenger seats for general aviation aircraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Desjardins, S. P. Warrick, J. C. |
| Copyright Year | 1979 |
| Description | This report presents the methodology and results of a program conducted to develop two underseat energy absorber (E/A) concepts for application to nonadjustable crashworthy passenger seats for general aviation aircraft. One concept utilizes an inflated air bag, and the other, a convoluted sheet metal bellows. Prototypes of both were designed, built, and tested. Both concepts demonstrated the necessary features of an energy absorber (load-limiter); however, the air bag concept is particularly encouraging because of its light weight. Several seat frame concepts also were investigated as a means of resisting longitudinal and lateral loads and of guiding the primary vertical stroke of the underseat energy absorber. Further development of a seat system design using the underseat energy absorbers is recommended because they provide greatly enhanced crash survivability as compared with existing general aviation aircraft seats. |
| File Size | 4336738 |
| Page Count | 103 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840024297 |
| Archival Resource Key | ark:/13960/t3906xp4r |
| Language | English |
| Publisher Date | 1979-09-18 |
| Access Restriction | Open |
| Subject Keyword | Air Transportation And Safety Fabrication Stress Analysis Performance Tests Accident Prevention General Aviation Aircraft Design Analysis Energy Absorption Crashworthiness Air Bag Restraint Devices Loads Forces Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |