Determination of the Protective Barrier Thickness of the Restraint System

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F13%3A00499847" target="_blank" >RIV/60162694:G43__/13:00499847 - isvavai.cz</a>

Výsledek na webu

<a href="http://vavtest.unob.cz/registr" target="_blank" >http://vavtest.unob.cz/registr</a>

DOI - Digital Object Identifier

—

Jazyk výsledku

angličtina

Název v původním jazyce

Determination of the Protective Barrier Thickness of the Restraint System

Popis výsledku v původním jazyce

The article presents the simulation analysis of the main elements of the restraint system. Such system provides a protection in case of accidental ejection of plug assembly during pressure testing of high-pressure valves. The aim of the analysis is to increase safety in the operating pressure tests at the manufacturer of valves facilities for given velocity and character of plug assembly. This article presents the estimation of the limit thickness of three possible barrier materials which can be used inthe construction of the restraint system elements. The analysis was performed using 2D Ansys Autodyn simulation model. Results of the analysis can be used as a basis for design of the restraint system capable to safely absorb the shock of flying body with the energy of tens to thousands of joules.

Název v anglickém jazyce

Determination of the Protective Barrier Thickness of the Restraint System

Popis výsledku anglicky

The article presents the simulation analysis of the main elements of the restraint system. Such system provides a protection in case of accidental ejection of plug assembly during pressure testing of high-pressure valves. The aim of the analysis is to increase safety in the operating pressure tests at the manufacturer of valves facilities for given velocity and character of plug assembly. This article presents the estimation of the limit thickness of three possible barrier materials which can be used inthe construction of the restraint system elements. The analysis was performed using 2D Ansys Autodyn simulation model. Results of the analysis can be used as a basis for design of the restraint system capable to safely absorb the shock of flying body with the energy of tens to thousands of joules.

Druh

J_x - Nezařazeno - Článek v odborném periodiku (Jimp, Jsc a Jost)

CEP obor

KA - Vojenství

OECD FORD obor

—

Projekt

—

Návaznosti

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Rok uplatnění

2013

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Název periodika

Advances in Military Technologies

ISSN

1802-2308

e-ISSN

—

Svazek periodika

Volume 8

Číslo periodika v rámci svazku

Issue 2

Stát vydavatele periodika

CZ - Česká republika

Počet stran výsledku

8

Strana od-do

63-70

Kód UT WoS článku

—

EID výsledku v databázi Scopus

—