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MUTR SIGNED

Multipurpose test rig for transmissions gearboxes.

Total Cost €

0

EC-Contrib. €

0

Partnership

0

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 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.

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

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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