Review on the design of an aircraft crashworthy passenger seat

2022 ◽  
Vol 129 ◽  
pp. 100785
Author(s):  
M. Guida ◽  
G. Lamanna ◽  
F. Marulo ◽  
F. Caputo
Keyword(s):  
Ergonomics ◽  
2016 ◽  
Vol 60 (7) ◽  
pp. 889-911 ◽  
Author(s):  
Suzanne Hiemstra-van Mastrigt ◽  
Liesbeth Groenesteijn ◽  
Peter Vink ◽  
Lottie F. M. Kuijt-Evers

Author(s):  
E B Ratts ◽  
J W McElroy ◽  
W G Reed

In this paper, an experimental method to quantify the capability of an automotive seat to move heat and moisture away from the heat and water source is presented. To test the method, a test apparatus was constructed that generates heat and water vapour. The apparatus was placed on a seat cushion for a fixed time period. At the end of the period, heat and water transported were measured. These integrated values were used to quantify the seat's capability to move heat and moisture and ultimately to compare seats. By the impulse test method, the passenger seat had an effusivity of 94.7 W s1/2/m2 K. A non-ventilated seat transferred 5 W of thermal energy and an average of 0.36 g/min of water in 1800 s. A ventilated seat transferred 13.9 W of thermal energy and 0.70 g/min of water in 1800 s.


2021 ◽  
Author(s):  
Gabriel H. Campos

The premise of this work is to address aircraft seat comfort. This thesis presents the development of an automatic morphing backrest used to reduce pressure experienced by the passenger from the seat. Uncomfortable, high surface pressure zones on the backrest can be alleviated by decentralizing the occupant’s weight. The improved pressure distribution is intended to decrease discomfort during flight while taking different comfort/discomfort models into consideration. Pressure distribution data from the embedded sensor mat is used to compute the seat’s cushion deflection and corresponding backrest contour caused by the passenger’s weight. The surfaces of interest - the passenger’s back and the seat, are modelled and discretized. The discretized surface contact pressure is integrated into the hyperelastic contact model to determine the loading profile. From this, the current pressure distribution and the cushion’s surface change are computed and used in the control system to create the corresponding actuation of the surface.


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