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Rotor Lock Test- H80 Turboprop Engine Extended Flight Testing

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F27174841%3A_____%2F16%3AN0000004" target="_blank" >RIV/27174841:_____/16:N0000004 - isvavai.cz</a>

  • Result on the web

  • DOI - Digital Object Identifier

Alternative languages

  • Result language

    angličtina

  • Original language name

    Rotor Lock Test- H80 Turboprop Engine Extended Flight Testing

  • Original language description

    Within the MOSTA project development phase 3/28 Flight tests – engine and subsequent certification validation of the H80 turboprop engine (out of MOSTA project), proof of continued rotor core rotation was sought. Instead of conducting an analysis, an actual engine test was conducted. The flying testbed aircraft instrumentation is described herein together with a novel probe design used for performance assessment. Key engine parameters are presented, clearly indicating that rotor lock requirements were met across the operating envelope. Enhanced engine operability is serving for the MOSTA project goals. Broader engine installation aspects are captured in earlier project publication [1].

  • Czech name

  • Czech description

Classification

  • Type

    J<sub>x</sub> - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)

  • CEP classification

    JU - Aeronautics, aerodynamics, aeroplanes

  • OECD FORD branch

Result continuities

  • Project

    <a href="/en/project/FR-TI2%2F557" target="_blank" >FR-TI2/557: Project MOSTA - Modernization Of Small Transport Aircraft to increase operation effectiveness and economy</a><br>

  • Continuities

    P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Others

  • Publication year

    2016

  • Confidentiality

    C - Předmět řešení projektu podléhá obchodnímu tajemství (§ 504 Občanského zákoníku), ale název projektu, cíle projektu a u ukončeného nebo zastaveného projektu zhodnocení výsledku řešení projektu (údaje P03, P04, P15, P19, P29, PN8) dodané do CEP, jsou upraveny tak, aby byly zveřejnitelné.

Data specific for result type

  • Name of the periodical

    Czech Aerospace Proceedings

  • ISSN

    1211-877x

  • e-ISSN

  • Volume of the periodical

    2016

  • Issue of the periodical within the volume

    2

  • Country of publishing house

    CZ - CZECH REPUBLIC

  • Number of pages

    3

  • Pages from-to

    12-14

  • UT code for WoS article

  • EID of the result in the Scopus database