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START SIGNED

inveSTigation of an ultrA compact Reverse flow combusTor

Total Cost €

EC-Contrib. €

Partnership

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Outcomes and
results

START project word cloud

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

liners maestro designed calculation evaluation optical cycle components reducing significantly manufactured carry gas hole numerical trl5 exit compact tests rules direct ge flow investigations emissions split explicit goals faced extensive simulations rig les methodology existent validate avio sfc cs2 combustion requiring additive verify validation weights strategy technologies turboprop annular cht series techniques manufacturing unsteady data prototypical performance innovative permit predictions itd full sat gathering model reverse rans infrared maps start combustors 2d liner positively hybrid combustor temperature thermal cfd efficiency engine behavior calculations meshing fidelity domain metal ultra aero flame

Project "START" data sheet

The following table provides information about the project.

Coordinator	UNIVERSITA DEGLI STUDI DI FIRENZE Organization address address: Piazza San Marco 4 city: Florence postcode: 50121 website: http://www.unifi.it 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	Italy [IT]
Total cost	640˙867 €
EC max contribution	640˙867 € (100%)
Programme	1. H2020-EU.3.4.5.5. (ITD Engines)
Code Call	H2020-CS2-CFP06-2017-01
Funding Scheme	CS2-IA
Starting year	2018
Duration (year-month-day)	from 2018-02-01 to 2020-07-31

Partnership

Take a look of project's partnership.

#	participants	country	role	EC contrib. [€]
1	UNIVERSITA DEGLI STUDI DI FIRENZE UNIVERSITA DEGLI STUDI DI FIRENZE Organization address address: Piazza San Marco 4 city: Florence postcode: 50121 website: http://www.unifi.it contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	IT (Florence)	coordinator	252˙317.00
2	CONSORZIO PER LO SVILUPPO DELLE AREE GEOTERMICHE CONSORZIO PER LO SVILUPPO DELLE AREE GEOTERMICHE Organization address address: Via tiberio gazzei 89 city: Radicondoli postcode: 53030 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.	IT (Radicondoli)	participant	388˙550.00

Map

Project objective

The main objective of START project is to carry out a series of advanced investigations on a prototypical reverse flow, ultra compact, combustor designed and manufactured by GE-Avio for turboprop engine as a part of the SAT ITD MAESTRO. The aim is to support the validation of the developed technologies and design rules by means of full annular combustion tests and high fidelity numerical simulations. Goals of START project will be addressed with the following steps: Verify a full additive combustor at real engine conditions in terms of combustor performance, by the measurement of emissions, gas exit temperature and liner metal temperature, through extensive full annular tests. Data will also permit validation of numerical modelling results. Improve the knowledge of combustor metal temperature and validation of aero-thermal predictions by gathering 2D temperature maps using InfraRed techniques across dedicated optical access on the full annular rig. Improve and further validate existent aero-thermal CFD modelling based on a two-step approach: RANS based CHT calculations for metal temperature and flow split predictions and LES (or Hybrid RANS-LES) calculations of the flame domain for combustor performance evaluation. Development of an innovative CFD approach based on unsteady CHT based on Hybrid RANS-LES, to allow direct calculation of aero-thermal and combustion performance behavior of the combustor. The methodology will also exploit and further validate dedicated strategy to model multi-hole liners without requiring the explicit meshing of each hole. START will greatly contribute to the goals of SAT initiative in CS2. The validation of innovative high fidelity CFD will significantly help the design of innovative combustors for addressing the target of SFC reduction faced with the increase of engine cycle efficiency. The validation of innovative additive manufacturing components at TRL5 will positively contribute to reach the objectives of reducing costs and weights.

Deliverables

List of deliverables.
Test specification	Documents, reports	2020-01-30 10:28:12
Innovative numerical models description	Documents, reports	2020-01-30 10:28:12

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

Publications

List of publications.
year	authors and title	journal	last update
2019	S. Paccati, D. Bertini, L. Mazzei, A. Andreini and S. Puggelli LARGE-EDDY SIMULATION OF A MODEL AERO-ENGINE SOOTING FLAME WITH A MULTIPHYSICS APPROACH published pages: , ISSN: , DOI:	Mediterrean Combustion Symposium 2019 - MCS11	2020-01-30

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