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MUTR SIGNED

Multipurpose test rig for transmissions gearboxes.

Total Cost €

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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.

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

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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