Vše

Co hledáte?

Vše
Projekty
Výsledky výzkumu
Subjekty

Rychlé hledání

  • Projekty podpořené TA ČR
  • Významné projekty
  • Projekty s nejvyšší státní podporou
  • Aktuálně běžící projekty

Chytré vyhledávání

  • Takto najdu konkrétní +slovo
  • Takto z výsledků -slovo zcela vynechám
  • “Takto můžu najít celou frázi”

Study on the Additional Ballistic Protection for Military Transport Helicopters

Identifikátory výsledku

  • Kód výsledku v IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F26%3A00565907" target="_blank" >RIV/60162694:G43__/26:00565907 - isvavai.cz</a>

  • Výsledek na webu

    <a href="https://stumejournals.com/journals/tm/2025/2/47" target="_blank" >https://stumejournals.com/journals/tm/2025/2/47</a>

  • DOI - Digital Object Identifier

Alternativní jazyky

  • Jazyk výsledku

    angličtina

  • Název v původním jazyce

    Study on the Additional Ballistic Protection for Military Transport Helicopters

  • Popis výsledku v původním jazyce

    The article presents a comprehensive study on the enhancement of ballistic protection for the consumption fuel tank of the Mi-171 transport helicopter, which is deployed in conflict zones across various countries. The study examines the helicopter’s critical areas, evaluates the levels of ballistic protection, and proposes solutions for augmenting the consumption fuel tank’s protection against firing. Three variants of potential ballistic protection are suggested, utilizing commercially available armours: steel Hardox 450, aluminium alloy Al 7039, and titanium alloy Ti-6AL-4V. The analysis is conducted using the Ansys Workbench software, aiming to determine the required thickness of homogeneous armour to achieve ballistic level 2 according STANAG 4569, capable of withstanding penetration by 7.62 39 API BZ ammunition. The study estimates the ballistic limit thickness necessary to prevent perforation of the ballistic protection panel. The simulation procedure and the material models of the armours employed are thoroughly described. Additionally, the study evaluates the weight of the protection system to identify the material with the minimum weight, thereby preserving aircraft performance. Notably, the use of titanium alloy and steel results in the greatest reduction in the weight of the protective system, with their masses being nearly identical. In contrast, the aluminum alloy exhibits a mass that is approximately 11% higher. A method for installing the armours on the helicopter is also proposed. The findings of this study are valuable for analysing airframe structures that face ballistic threats during military operations or terrorist attacks. Proposals for further refinement and a shooting experiment are discussed to enhance the accuracy and effectiveness of the protection solutions.

  • Název v anglickém jazyce

    Study on the Additional Ballistic Protection for Military Transport Helicopters

  • Popis výsledku anglicky

    The article presents a comprehensive study on the enhancement of ballistic protection for the consumption fuel tank of the Mi-171 transport helicopter, which is deployed in conflict zones across various countries. The study examines the helicopter’s critical areas, evaluates the levels of ballistic protection, and proposes solutions for augmenting the consumption fuel tank’s protection against firing. Three variants of potential ballistic protection are suggested, utilizing commercially available armours: steel Hardox 450, aluminium alloy Al 7039, and titanium alloy Ti-6AL-4V. The analysis is conducted using the Ansys Workbench software, aiming to determine the required thickness of homogeneous armour to achieve ballistic level 2 according STANAG 4569, capable of withstanding penetration by 7.62 39 API BZ ammunition. The study estimates the ballistic limit thickness necessary to prevent perforation of the ballistic protection panel. The simulation procedure and the material models of the armours employed are thoroughly described. Additionally, the study evaluates the weight of the protection system to identify the material with the minimum weight, thereby preserving aircraft performance. Notably, the use of titanium alloy and steel results in the greatest reduction in the weight of the protective system, with their masses being nearly identical. In contrast, the aluminum alloy exhibits a mass that is approximately 11% higher. A method for installing the armours on the helicopter is also proposed. The findings of this study are valuable for analysing airframe structures that face ballistic threats during military operations or terrorist attacks. Proposals for further refinement and a shooting experiment are discussed to enhance the accuracy and effectiveness of the protection solutions.

Klasifikace

  • Druh

    J<sub>ost</sub> - Ostatní články v recenzovaných periodicích

  • CEP obor

  • OECD FORD obor

    20304 - Aerospace engineering

Návaznosti výsledku

  • Projekt

  • Návaznosti

    I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Ostatní

  • Rok uplatnění

    2025

  • Kód důvěrnosti údajů

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

Údaje specifické pro druh výsledku

  • Název periodika

    Trans Motauto World

  • ISSN

    2534-8493

  • e-ISSN

  • Svazek periodika

    10

  • Číslo periodika v rámci svazku

    2

  • Stát vydavatele periodika

    BG - Bulharská republika

  • Počet stran výsledku

    77

  • Strana od-do

    47-50

  • Kód UT WoS článku

  • EID výsledku v databázi Scopus