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MUTR SIGNED

Multipurpose test rig for transmissions gearboxes.

Total Cost €

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EC-Contrib. €

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Partnership

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 Outcomes and results

 MUTR project word cloud

Explore the words cloud of the MUTR project. It provides you a very rough idea of what is the project "MUTR" about.

aviation    experiences    demonstrator    elevated    pbs    compound    interconnection    temperatures    experimental    centre    combustor    gears    connected    iadp    compressor    impose    m601    rig    team    ge    fem    potentially    gearings    czech    cad    rigs    housings    turbine    uacute    proportional    torque    special    bites    bearing    internal    auxiliary    shaft    gas    segments    architecture    bevel    imposed    published    loader    supplied    aeronautical    cfd    pressure    radial    vzl    quill    device    aeronautics    suppose    manufacturers    objective    solvers    manufacture    1d    establishment    hydraulic    turboprop    frc    operation    gearboxes    lateral    participating    bench    velka    national    oil    lock    benches    engine    rotorcraft    ts100    propeller    losses    time    modern    space    shafting    mention    power    inserted    aircraft    pressures    vertical    arrius    covers    evaluation    static    frame    transmission    feed    cooperation    gearbox    m602    historically    equipped    cell    rotor    tp100    flow    back    stage    description    flanges    engines    components    rotation    drive    shafts    imput   

Project "MUTR" data sheet

The following table provides information about the project.

Coordinator		 VYZKUMNY A ZKUSEBNI LETECKY USTAV AS 

Organization address
address: LETNANY BERANOVYCH 130
city: PRAHA 18
postcode: 19000
website: www.vzlu.cz

contact info
title: n.a.
name: n.a.
surname: n.a.
function: n.a.
email: n.a.
telephone: n.a.
fax: n.a.
 Coordinator Country Czech Republic [CZ]
 Project website http://www.vzlu.cz
 Total cost 606˙400 €
 EC max contribution 606˙400 € (100%)
 Programme 1. H2020-EU.3.4.5.3. (IADP Fast Rotorcraft)
 Code Call H2020-CS2-CFP02-2015-01
 Funding Scheme CS2-IA
 Starting year 2016
 Duration (year-month-day) from 2016-09-01   to  2020-06-30

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    VYZKUMNY A ZKUSEBNI LETECKY USTAV AS CZ (PRAHA 18) coordinator 606˙400.00

Map

 Project objective

Objective of this proposal is to design, manufacture, test and support the adaptation of the test rig used to develop the Drive System for Compound Rotorcraft Demonstrator in the frame of IADP FRC. Based on the topic description published in this call our proposal suppose interconnection of the lateral rotor gearboxes via vertical transmission shafting, supported on two or three auxiliary bearing housings, in order to lock the two gearboxes together. The transmission shafting is connected to the lateral gearboxes by means of bevel gearings. Between flanges of the transmission shafting is inserted special hydraulic torque loader which make it possible to impose static or variable torque on gearboxes during operation/rotation according to a test program. The imposed torque is proportional to the pressure of the feed-in oil supplied to the device via quill shaft. Due to the back-to-back or face-to-face architecture, required power imput covers just losses in the gears and transmission shafting. Aeronautical Research and Test Establishment (VZLÚ) is a national centre for research, development and testing in aeronautics and space. VZLÚ and the potentially participating team has experiences with design of test benches for aircraft gas turbine engines (historically M601, M602) and its components like 2 stage 2 shafts radial flow compressor, to mention recent project, these are design of the test rigs for long term evaluation of aircraft turboprop gearboxes (Arrius 1D, TP100, TS100), test bench for turboprop engine with propeller, design of the internal technology for turboprop engine test cell, experimental system for testing of gas turbine combustor segments under elevated temperatures and pressures. Work team is well experienced and equipped with modern CAD technology, CFD and FEM solvers, and has long time cooperation experience with aircraft gearbox manufacturers (e.g. PBS Velka Bites, GE Aviation Czech).

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The information about "MUTR" are provided by the European Opendata Portal: CORDIS opendata.

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