Explore the words cloud of the SABRE project. It provides you a very rough idea of what is the project "SABRE" about.
The following table provides information about the project.
Coordinator |
UNIVERSITY OF BRISTOL
Organization address contact info |
Coordinator Country | United Kingdom [UK] |
Project website | https://sabreproject.eu/ |
Total cost | 6˙033˙398 € |
EC max contribution | 6˙033˙398 € (100%) |
Programme |
1. H2020-EU.3.4. (SOCIETAL CHALLENGES - Smart, Green And Integrated Transport) |
Code Call | H2020-MG-2016-Two-Stages |
Funding Scheme | RIA |
Starting year | 2017 |
Duration (year-month-day) | from 2017-06-01 to 2020-11-30 |
Take a look of project's partnership.
# | ||||
---|---|---|---|---|
1 | UNIVERSITY OF BRISTOL | UK (BRISTOL) | coordinator | 1˙233˙541.00 |
2 | DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV | DE (KOELN) | participant | 1˙127˙555.00 |
3 | CENTRO ITALIANO RICERCHE AEROSPAZIALI SCPA | IT (CAPUA - CASERTA) | participant | 1˙100˙000.00 |
4 | TECHNISCHE UNIVERSITAET MUENCHEN | DE (MUENCHEN) | participant | 1˙098˙617.00 |
5 | SWANSEA UNIVERSITY | UK (SWANSEA) | participant | 779˙183.00 |
6 | TECHNISCHE UNIVERSITEIT DELFT | NL (DELFT) | participant | 694˙501.00 |
Shape Adaptive Blades for Rotorcraft Efficiency (SABRE) will develop ground-breaking new helicopter blade morphing technologies which will reduce helicopter fuel burn, CO2 and NOx emissions by 5-10%, while also reducing noise emissions. SABRE will help Europe achieve its ambitious aviation emissions goals while also sharpening its competitive edge in the rapidly growing international helicopter market. It will achieve this ambitious objective by removing one of the most fundamental limitations on helicopter performance: the need for rotor blades to have a single fixed geometry which is inherently a compromise between widely different operating conditions. SABRE envisions shape adaptive blades which can continuously change their shape to optimise performance in all conditions. SABRE has a tightly cross-linked, dual stream research approach with emissions-focused rotor performance analysis running concurrently with morphing technology development. The analysis stream will combine comprehensive rotor analysis, high-fidelity aerodynamic and structural solvers, detailed morphing mechanism models, and emissions models, creating the most detailed, transdisciplinary, and comprehensive model of its type. The technology development stream will mature a selected group of novel, beyond state-of-the-art, helicopter focused morphing concepts through a carefully considered program of modelling, design and experimental testing efforts. The achievable performance of the morphing concepts will be fed back into the emissions analysis, and the analysis stream will guide the development of the technologies towards configurations which minimize emissions. SABRE is highly ambitious in both its objectives and its approach. The project has strong industry support, and brings together the ideal consortium to achieve its objectives; with world-leading experts in rotorcraft and morphing structures backed up by a clear project plan, robust management procedures, and excellent facilities.
D3.7 Project leaflet to identified stakeholders | Websites, patent fillings, videos etc. | 2020-04-08 21:48:32 |
D2.4 Initial surrogate model of inertial twist and report | Other | 2020-04-08 21:48:31 |
D1.1 Selection of baseline rotor | Documents, reports | 2020-04-08 21:48:32 |
D1.4 S4 CA results on morphing performance | Documents, reports | 2020-04-08 21:48:32 |
D1.5 Initial morphing concept design targets | Documents, reports | 2020-04-08 21:48:32 |
D1.3 Decide common format for exchange of surrogate models | Documents, reports | 2020-04-08 21:48:31 |
D3.10 Report on dissemination and exploitation strategy | Documents, reports | 2020-04-08 21:48:32 |
D2.7 Initial surrogate model of FishBAC | Other | 2020-04-08 21:48:31 |
D3.3 SABRE Project Handbook | Websites, patent fillings, videos etc. | 2020-04-08 21:48:32 |
D2.16 Initial active tendon surrogate model | Other | 2020-04-08 21:48:32 |
D2.29 Interim report on negative stiffness design and optimisation | Documents, reports | 2020-04-08 21:48:32 |
D2.13 Initial surrogate model of variable chord extension | Other | 2020-04-08 21:48:31 |
D2.27 Whirl tower test proof load requirements | Documents, reports | 2020-04-08 21:48:32 |
D2.25 Wind tunnel test proof load requirements | Documents, reports | 2020-04-08 21:48:31 |
D3.6 Public website, LinkedIn profile, and ResearchGate profile set up | Websites, patent fillings, videos etc. | 2020-04-08 21:48:32 |
D1.12 Initial morphing concept CFD polars delivered to T1.2 | Documents, reports | 2020-04-08 21:48:31 |
D3.5 Intra consortium website set up for SABRE | Websites, patent fillings, videos etc. | 2020-04-08 21:48:31 |
D3.1 Partner List and copies of EC contract and Consortium Agreement. | Documents, reports | 2020-04-08 21:48:32 |
D3.4 SABRE Project Overview Presentation | Websites, patent fillings, videos etc. | 2020-04-08 21:48:31 |
D3.8 Phase 1 Reporting (Minutes of checkpoint meeting, Activity report) | Documents, reports | 2020-04-08 21:48:33 |
D3.9 Preliminary Design Review (PDR) | Documents, reports | 2020-04-08 21:48:32 |
D2.10 Initial surrogate model of TRIC concept | Other | 2020-04-08 21:48:31 |
D1.11 Surrogate model of emissions versus rotor power required | Other | 2020-04-08 21:48:31 |
D1.6 CFD/CSD coupled analysis running | Other | 2020-04-08 21:48:32 |
D3.2 Minutes of the Kick-Off meeting | Documents, reports | 2020-04-08 21:48:32 |
D1.10 Rotorcraft emissions model | Other | 2020-04-08 21:48:32 |
D1.2 Report on analytical adaptive rotor studies | Documents, reports | 2020-04-08 21:48:32 |
D2.1 Initial surrogate model of SMA active twist and report | Other | 2020-04-08 21:48:31 |
Take a look to the deliverables list in detail: detailed list of SABRE deliverables.
year | authors and title | journal | last update |
---|---|---|---|
2017 |
R. Dibble, BKS Woods, B. Titurus Static aeroelastic response of a rotor blade under internal axial loading published pages: , ISSN: , DOI: |
43rd European Rotorcraft Forum 12-14 September 2017 | 2020-04-08 |
2017 |
Benjamin King Sutton Woods The Aerodynamics of Active Camber published pages: , ISSN: , DOI: 10.13140/rg.2.2.14104.70405 |
28th ICAST conference 9-13 October 2017 | 2020-04-08 |
2018 |
K. Vidyarthi, M. Beuker, F. Yin, M. Voskuijl, M. Pavel Hoplite - a conceptual design environment for helicopters incorporatingmorphing rotor technology published pages: , ISSN: , DOI: |
44th European Rotorcraft Forum 18-21 September 2018 | 2020-04-08 |
2018 |
S Ameduri, A Concilio An SMA Torsion Actuator for Static Blade Twist published pages: , ISSN: , DOI: |
9th International Conference on Adaptive Structures and Technologies 1-4 October 2018 | 2020-04-08 |
2018 |
J Zhang, AD Shaw, MR Amoozgar, MI Friswell & BKS Woods Torsional Negative Stiffness Mechanism for Bidirectional Morphing Aircraft Actuation published pages: , ISSN: , DOI: |
6th Aircraft Structural Design Conference 9-11 October 2018 | 2020-04-08 |
2018 |
MR Amoozgar, AD Shaw, J Zhang & MI Friswell Twist morphing of a hingeless rotor blade using a moving mass published pages: , ISSN: , DOI: |
44th European Rotorcraft Forum 18-21 September 2018 | 2020-04-08 |
2018 |
MR Amoozgar, AD Shaw, J Zhang & MI Friswell Cross-sectional design of a composite rotor blade for twist morphing published pages: , ISSN: , DOI: |
6th Aircraft Structural Design Conference 9-11 October 2018 | 2020-04-08 |
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The information about "SABRE" are provided by the European Opendata Portal: CORDIS opendata.