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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.

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

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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