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1 677 (0,142s) •

Project

Dynamics in Aircraft Engineering Design and Analysis for Light Optimized Structures (7E11025)

. Establishing new procedures for the definition of loads to be used during aircraft designToday?s design and certification procedures of aircrafts are mainly based on conservative static loading which leads to add...

JU - Aeronautika, aerodynamika, letadla

  • 2011 - 2013
    • •
  • 1 302 tis. Kč
    • •
  • 1 302 tis. Kč
    • •
  • MŠMT
Project

FAMOS - frame aircraft monitoring system. (FD-K3/046)

Development and realization of the airborne equipment that enables to watch the loading of the frame of aircraft during its whole time of service. The obtained knowledge about loading of the structure enables more effective...

JU - Aeronautika, aerodynamika, letadla

  • 2003 - 2005
    • •
  • 10 219 tis. Kč
    • •
  • 5 025 tis. Kč
    • •
  • MPO
Project

Load monitoring system ELMS 601of aircraft turboprop engine WALTER M601. (FI-IM3/170)

The project is aimed on branch of aeronautical instrument technology. The aircraft turboprop engines WALTER M601 will be equipped by Load Monitoring System ELMS 601. By way of development this system will be provided monitoring and ...

JA - Elektronika a optoelektronika, elektrotechnika

  • 2006 - 2007
    • •
  • 6 839 tis. Kč
    • •
  • 1 907 tis. Kč
    • •
  • MPO
Project

Effect of cyclic loading with variable stress amplitude on fatigue behaviour of fibre-metal laminates (GP106/02/D147)

The proposed project is focused on the study of variable amplitude loading laminates, finding applications in the transport, especially in the aircraft industry. Untilnow, mostly fatigue behaviour at constant amplitude loading

JI - Kompositní materiály

  • 2002 - 2005
    • •
  • 135 tis. Kč
    • •
  • 135 tis. Kč
    • •
  • GA ČR
Project

Advanced prove method of strenght airwothines and life of landing gears of small aircraft. (FD-K3/047)

Application of new advanced proving experimental method of strength airworthiness and life landing gears of small aircraft into standard practice. The method is based on verified method of application of more accurate operational loads

JU - Aeronautika, aerodynamika, letadla

  • 2003 - 2005
    • •
  • 26 030 tis. Kč
    • •
  • 12 994 tis. Kč
    • •
  • MPO
Project

SALI – Software for Airframe Loading Investigation (TA03010399)

and will improve critical aircraft loading calculation. It will consequently reduce costs of development and modification of aircraft, will enhance air traffic safety aircraft model doesn´t correspond to the curre...

JU - Aeronautika, aerodynamika, letadla

  • 2013 - 2015
    • •
  • 14 629 tis. Kč
    • •
  • 7 063 tis. Kč
    • •
  • TA ČR
Project

*Research development and verification of methods for design and manufacturing technology of reinforced thermoplastics for different advanced applications (FR-TI1/463)

*Project goal is advanced methods for design and technology of manufacturing of reinforced thermoplastic parts for high loaded application. Development and testing of different types of parts for aircraft, transport vehicles and bio...

JI - Kompositní materiály

  • 2009 - 2012
    • •
  • 36 509 tis. Kč
    • •
  • 21 955 tis. Kč
    • •
  • MPO
Project

Innovative Linear Electro-Mechanical Actuators (FW01010148)

The shared goal of the consortium is within two years to develop, produce and verify electromechanical actuators of two different load ratings, intended to be used for primary flight control surfaces of CS-23 and Urban Air Mobility aircr...

Aerospace engineering

  • 2020 - 2022
    • •
  • 44 688 tis. Kč
    • •
  • 23 537 tis. Kč
    • •
  • TA ČR
Project

Proof of L-39NG airframe with tripled fatigue life (FW01010225)

Project primary aim is to proof the tripled fatigue life of the airframe of the L-39NG aircraft. L-39NGs airframe is made of advanced materials and production technologies. The fatigue life proof will also utilize extensive usage of structu...

Aerospace engineering

  • 2020 - 2023
    • •
  • 91 324 tis. Kč
    • •
  • 62 170 tis. Kč
    • •
  • TA ČR
Project

2nd Generation Active Wing – Active Flow- Loads & Noise control on next generation wing (7E13056)

and maturing highly promising flow control technologies for novel aircraft configurations to achieve a quantum leap in improving aircraft’s performance and thus reducing separation control applied in wing/pylon junction to improve ...

JU - Aeronautika, aerodynamika, letadla

  • 2013 - 2017
    • •
  • 5 607 tis. Kč
    • •
  • 5 607 tis. Kč
    • •
  • MŠMT
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