All

What are you looking for?

All
Projects
Results
Organizations

Quick search

  • Projects supported by TA ČR
  • Excellent projects
  • Projects with the highest public support
  • Current projects

Smart search

  • That is how I find a specific +word
  • That is how I leave the -word out of the results
  • “That is how I can find the whole phrase”

Development of a drone for management of the linear structures

Public support

  • Provider

    Ministry of Industry and Trade

  • Programme

  • Call for proposals

  • Main participants

    LPS, letecké práce a služby, s.r.o.

  • Contest type

    OP - EU Operational Programme

  • Contract ID

    MPO 16357/17/61600/833

Alternative language

  • Project name in Czech

    Vývoj dronu pro kontrolu liniových staveb

  • Annotation in Czech

    Předmětem projektu je výzkum a vývoj na trhu zatím nedostupného bezpilotního prostředku - dronu - se zcela unikátními parametry v podobě prodloužené doby letu a s možností startu a přistání v omezeném prostoru. Pro takto technicky koncipované zařízení pak rovněž budou řešeny odpovídající řídící a monitorovací systémy a softwarová řešení k jejich civilní aplikaci.

Scientific branches

  • R&D category

    VV - Exeperimental development

  • CEP classification - main branch

    JU - Aeronautics, aerodynamics, aeroplanes

  • CEP - secondary branch

  • CEP - another secondary branch

  • OECD FORD - equivalent branches <br>(according to the <a href="http://www.vyzkum.cz/storage/att/E6EF7938F0E854BAE520AC119FB22E8D/Prevodnik_oboru_Frascati.pdf">converter</a>)

    20304 - Aerospace engineering

Completed project evaluation

  • Provider evaluation

    U - Uspěl podle zadání (s publikovanými či patentovanými výsledky atd.)

  • Project results evaluation

    As part of the project, a prototype of a small all-composite drone with a short take-off and landing was designed and verified by flight tests. During the development of the drone, known procedures and technologies were combined with new procedures such as solving stability problems of very thin sandwiches in airframe construction, verification of computational models with low Reynolds number, verification of 3D printing technology for primary structure production, control tasks of nonlinear flight control systems, etc. . Three performance parameters were primarily monitored, which were verified for the maximum considered take-off weight: - endurance of at least 2 hours in the take-off mode, ie in the mode where it moves like an airplane - vis, time of suspension and transition from suspension to horizontal flight and back to suspension - cruising speed greater than 60 km / h

Solution timeline

  • Realization period - beginning

    Sep 29, 2015

  • Realization period - end

    May 12, 2021

  • Project status

    U - Finished project

  • Latest support payment

    Dec 9, 2017

Data delivery to CEP

  • Confidentiality

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

  • Data delivery code

    CEP22-MPO-EG-U

  • Data delivery date

    May 24, 2022

Finance

  • Total approved costs

    20,663 thou. CZK

  • Public financial support

    7,589 thou. CZK

  • Other public sources

    0 thou. CZK

  • Non public and foreign sources

    3,258 thou. CZK