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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.

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

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

Leaflet | Map data © OpenStreetMap contributors, CC-BY-SA, Imagery © Mapbox

 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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