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Crash simulation parameter studies for a helicopter cockpit mock-up

Lützenburger, Marius (2007) Crash simulation parameter studies for a helicopter cockpit mock-up. DLR-Interner Bericht, Project Report. DLR-IB 435-2007/27, 24 S. (Unpublished)

Full text not available from this repository.

Abstract

Within the EU funded project ‘HeliSafe TA’ (2004 – 2007), DLR carried out crash simulations with MADYMO models of a helicopter cockpit mock-up. The models included the pilot seat with integrated energy absorption devices, the pilot (two different sizes: 50% / 95%-ile dummies) and also different safety belt systems. The models were verified by comparison to the respective results from sled tests which were carried out by a project partner (SRS). 15 different injury criteria are considered in the IRSIX calculation which is used in ‘HeliSafe TA’ to judge the injury risk of helicopter occupants. It was shown that for the here examined vertical load cases the IRSIX value is dominated by the maximum lumbar spine forces. Therefore, the optimisation of the characteristic of the seat energy absorbers is of upmost importance. In a sensitivity study, the influence of different belt related parameters – e.g. belt elongation, pretensioner load, TTF (time to fire), load limiter – was investigated. In a further parametric study, the influence of the misalignment of the seat legs (according to the respective FAA seat test regulations) was determined.

Item URL in elib:https://elib.dlr.de/52604/
Document Type:Monograph (DLR-Interner Bericht, Project Report)
Title:Crash simulation parameter studies for a helicopter cockpit mock-up
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Lützenburger, MariusUNSPECIFIEDUNSPECIFIED
Date:29 November 2007
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:24
Status:Unpublished
Keywords:Crash simulation, helicopter, MADYMO, Occupant safety
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Rotorcraft (old)
DLR - Research area:Aeronautics
DLR - Program:L RR - Rotorcraft Research
DLR - Research theme (Project):L - The Robust Rotorcraft (old)
Location: Stuttgart
Institutes and Institutions:Institute of Structures and Design > Structural Integrity
Deposited By: Lützenburger, Marius
Deposited On:07 Jan 2008
Last Modified:27 Apr 2009 14:36

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