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AMBEC SIGNED

Advanced Modelling Methodology for Bearing Chamber in Hot Environment

Total Cost €

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EC-Contrib. €

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Partnership

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Project "AMBEC" data sheet

The following table provides information about the project.

Coordinator
SCIENCE AND TECHNOLOGY CENTER IN UKRAINE 

Organization address
address: METALISTIV 7A
city: KYIV
postcode: 3057
website: n.a.

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 Ukraine [UA]
 Project website http://www.ambec.eu
 Total cost 1˙700˙668 €
 EC max contribution 1˙699˙668 € (100%)
 Programme 1. H2020-EU.3.4.5.5. (ITD Engines)
 Code Call H2020-CS2-CFP06-2017-01
 Funding Scheme CS2-RIA
 Starting year 2018
 Duration (year-month-day) from 2018-05-01   to  2021-04-30

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    SCIENCE AND TECHNOLOGY CENTER IN UKRAINE UA (KYIV) coordinator 4˙000.00
2    MOTOR SICH JSC UA (ZAPORIZHZHYA) participant 830˙000.00
3    ZAPOROZHYE MACHINE-BUILDING DESIGN BUREAU PROGRESS STATE ENTERPRISE NAMED AFTER ACADEMICIAN A.G. IVCHENKO UA (ZAPOROZHYE) participant 549˙543.00
4    NATIONAL AEROSPACE UNIVERSITY KHARKIV AVIATION INSTITUTE NAMED BY N ZUKOVSKIY UA (KHARKIV) participant 316˙125.00

Map

 Project objective

The AMBEC project aims to develop a reliable experimentally validated methodology able to calculate heat transfer coefficients and fluid distribution in different zones of bearing chamber. The methodology will be used for improvement of the design of compact bearing chambers in hot environment. Proposed concept consists in combination of advanced CFD simulation and experimental investigation of fluid flows and heat transfer phenomena in bearing chamber. The advantages of the proposed methodology consist in: - More accurate determination of oil film thickness and, consequently, heat exchange conditions and heat fluxes along the perimeter of the bearing chamber. Numerical simulation of oil film formation and motion will take into account the combined action of forces of interphase interaction, gravity and centrifugal effects. - More accurate determination of heat exchange between air and oil film. This problem will be solved taking into account possible rupture of liquid film onto the drops, their crushing and coagulation. These advantages fully meet call expectations, while proposed approaches and methodologies have been proven by AMBEC partners during previous extensive R&Ds. After project completion, the Topic Leader will obtain experimentally validated innovative methodology for analysis of heat transfer and fluid flows in the compact bearing chamber and recommendations for chamber design improvement. These outputs will feed the development of LP spool bearing chamber for UHPE Demonstrator for SMR aircraft in the frame of CS2 Engine ITD activities. Application of AMBEC methodology for aircraft engine design will ensure less oil flow rate, which will lead to reduction of power consumption by oil pumps and thus overall fuel savings. This will give European aeronautical industry an opportunity to better compete at global market and will contribute to greening of EU aviation.

 Deliverables

List of deliverables.
Literature review on multiphase flow characteristics and heat transfer phenomena in the bearing chamber Documents, reports 2019-06-19 16:48:51
Plan for Communication and Dissemination of project results Documents, reports 2019-06-19 16:48:51
Data Management Plan Open Research Data Pilot 2019-06-19 16:48:51

Take a look to the deliverables list in detail:  detailed list of AMBEC deliverables.

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The information about "AMBEC" are provided by the European Opendata Portal: CORDIS opendata.

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