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Optimal pressure comfort design for pilot helmets
- Source :
- Computer methods in biomechanics and biomedical engineering. 21(6)
- Publication Year :
- 2018
-
Abstract
- With the development of high-performance fighters, the function of pilot helmets is also constantly upgrading, and helmet-mounted display (HMD) has become a future development trend. To solve the inter-restriction between the eye position control and the pressure comfort under high overloads of pilot helmets, this paper optimizes the helmet design by building a head-helmet finite element model: (1) Under a 10 G overload, the deformation of helmet soft liner should not exceed 2 mm; and (2) The combination of liner materials used in various areas should satisfy the requirements of most comfortable head pressure distribution (Pfront: Ptop: Pside: Pback = 2:2:1:3). The study on 46 different combinations of materials finds that the helmet can meet both the eye position maintenance requirement under overloads and the requirement of comfortable pressure distribution when linear elastic materials with Young's modulus of 1000 pa, 55000 pa and 65000 pa are used for the side, top and front parts of the head, and nonlinear elastic hyperfoam material with two-fold stress variation is used for the head back area.
- Subjects :
- Optimal design
Rotation
Computer science
Finite Element Analysis
Biomedical Engineering
Bioengineering
02 engineering and technology
01 natural sciences
Automotive engineering
Stress variation
Elastic Modulus
0103 physical sciences
Pressure
Humans
010302 applied physics
Linear elasticity
Reproducibility of Results
General Medicine
Equipment Design
021001 nanoscience & nanotechnology
Soft liner
Finite element method
Computer Science Applications
Human-Computer Interaction
Pressure head
Pilots
Head (vessel)
Head Protective Devices
Stress, Mechanical
0210 nano-technology
Head
Subjects
Details
- ISSN :
- 14768259
- Volume :
- 21
- Issue :
- 6
- Database :
- OpenAIRE
- Journal :
- Computer methods in biomechanics and biomedical engineering
- Accession number :
- edsair.doi.dedup.....4de7ac28e6dc7e3016ab0e4f11ab3953