Abstract
This paper describes the application of BATHfp to perform a detailed analysis of the bi-stable valve in the A340 landing gear absorber. During the development of the landing gear system, the shock abosorber was subjected to drop tests, during which a malfunction of the bi-stable valve was identified. A solution to the problem was found and incorporated before installation on the aircraft. Parametric variations are made in the simulation to identify the possible cause of the malfunction
| Original language | English |
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| Publication status | Published - Sep 1993 |
| Event | IMechE Aerospace Hydraulics and Systems Conference - Duration: 1 Sep 1993 → … |
Conference
| Conference | IMechE Aerospace Hydraulics and Systems Conference |
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| Period | 1/09/93 → … |