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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.

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

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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