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AMBEC SIGNED

Advanced Modelling Methodology for Bearing Chamber in Hot Environment

Total Cost €

EC-Contrib. €

Partnership

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Outcomes and
results

AMBEC project word cloud

Explore the words cloud of the AMBEC project. It provides you a very rough idea of what is the project "AMBEC" about.

onto coagulation aircraft oil flow numerical give compact flows environment calculate thickness liquid centrifugal phenomena fluid bearing rupture engine fluxes combined market investigation opportunity crushing air interphase meet heat drops consist demonstrator validated innovative transfer power chambers action frame ambec feed consequently exchange spool greening perimeter coefficients savings leader lp advantages obtain solved outputs global zones accurate itd recommendations experimental extensive compete chamber consumption smr completion simulation forces improvement rate aeronautical pumps ds gravity hot interaction combination uhpe expectations film cfd motion consists methodology experimentally cs2 industry fuel aviation proven

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 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.	UA (KYIV)	coordinator	4˙000.00
2	MOTOR SICH JSC MOTOR SICH JSC Organization address address: MOTOROBUDIVNYKIV AVENUE 15 city: ZAPORIZHZHYA postcode: 69068 website: www.motorsich.ru contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	UA (ZAPORIZHZHYA)	participant	830˙000.00
3	ZAPOROZHYE MACHINE-BUILDING DESIGN BUREAU PROGRESS STATE ENTERPRISE NAMED AFTER ACADEMICIAN A.G. IVCHENKO ZAPOROZHYE MACHINE-BUILDING DESIGN BUREAU PROGRESS STATE ENTERPRISE NAMED AFTER ACADEMICIAN A.G. IVCHENKO Organization address address: Ivanova street 2 city: ZAPOROZHYE postcode: 69068 website: www.ivchenko-progress.com contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	UA (ZAPOROZHYE)	participant	549˙543.00
4	NATIONAL AEROSPACE UNIVERSITY KHARKIV AVIATION INSTITUTE NAMED BY N ZUKOVSKIY NATIONAL AEROSPACE UNIVERSITY KHARKIV AVIATION INSTITUTE NAMED BY N ZUKOVSKIY Organization address address: CHKALOVA STR 17 city: KHARKIV postcode: 61070 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.	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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