Abstract
The textile industry is an innovative field, a generator of competitive products, absolutely indispensable to many other fields (aeronautics, medicine, shipping, agriculture, environmental protection etc.)
In this philosophy, important researches have been carried out in order to develop new generations of textile products for strategic applications.
The paper presents important issues regarding: the role of helicopter thermal protection system as well as parachute recovery in the main system (supersonic aircraft); design of thermal protection woven structure for thermal protection of the helicopters as well as the woven structure for main parachute of recovery systems for landing of the supersonic aircraft, based on aerodynamic characteristics and areas of use; the main fabric structure characteristics used in the two systems; description of the phenomena occurring on the main parachute canopy at landing of the supersonic aircraft; structural analysis of the main parachute canopy of the aircraft deceleration system; the interdependence between the aerodynamic, geometric and mass characteristics of the considered systems and the characteristics of the fabric. The design and realization of these product types are based on the specific requirements imposed by its fields of application, which governs the system and the selection of components. Typical design and delivery criteria have been considered: safety in operation (the criterion of the greatest importance); mass and volume in order to efficiently use the loading value; stability; reproducibility of performance, etc.
This is a preview of subscription content, log in via an institution to check access.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Similar content being viewed by others
References
Lien, F.S., Kalitzin, G.: Computation of transonic flow with the v2-f turbulence model. Int. J. Heat Fluid Flow 22, 53–61 (2001)
Bogdanov, V.V., Zalogin, G.N., Zemlyanskii, B.A., et al.: Experimental study of the efficiency of flexible thermal protection of inflatable braking systems. Kosmonavt. Raketostr. 22, 22–32 (2001)
Pilyugin, N.N., Khlebnikov, V.S.: Development of a parachute system for deceleration of flying vehicles in supersonic regimes. J. Appl. Mech. Tech. Phys. 51(5), 623–632 (2010)
Acknowledgment
This scientific paper is funded by the Ministry of Research and Innovation within Program 1 - Development of the national RD system, Subprogram 1.2 - Institutional Performance - RDI excellence funding projects, Contract no. 6PFE/2018.
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2020 Springer Nature Switzerland AG
About this paper
Cite this paper
Mihai, C., Ene, A. (2020). Woven Fabrics Specially Designed for Thermal Protection and System Recovery of Air Vehicles. In: Di Bucchianico, G. (eds) Advances in Design for Inclusion. AHFE 2019. Advances in Intelligent Systems and Computing, vol 954. Springer, Cham. https://doi.org/10.1007/978-3-030-20444-0_47
Download citation
DOI: https://doi.org/10.1007/978-3-030-20444-0_47
Published:
Publisher Name: Springer, Cham
Print ISBN: 978-3-030-20443-3
Online ISBN: 978-3-030-20444-0
eBook Packages: EngineeringEngineering (R0)