C lean Sky 2 Information Day dedicated to the 6 th Call for Proposal (CfP06) JTI-CS2-2017-CFP06-REG-01-09 Innovative Low Power De-Icing System Brussels, 22 February 2017
REG-01-09 Topic Intro • Estimated Funding Topic Value: 1200k € • Duration: 36 months • Start date: Q1 2018 (indicative) • CfP short description: To design, develop and manufacture a demonstrator of Low Power De-Icing System, including the leading edge wing section. The demonstrator will be tested up to TRL 5 in an Ice Wind Tunnel (not part of this Topic); the Applicant shall also assure the support to testing activity for system performance validation. 2
REG-01-09 REG IADP WBS Overview R-IADP Related WPs Regional IADP WP 1 WP 3 WP 4 WP 0 WP 2 High Efficiency Demonstrations Demonstrations Management Technologies Regional A/C Analysis Development WP 3.1 WP 2.1 Airvehicle Flight Test Bed WP 2.2 (FTB#1) Adaptive Regional Avionics Electrical Wing WP 3.2 Fuselage/Cabin Ground WP 2.3 WP 2.4 Demonstrator Energy Optimized Innovative FCS Regional A/C WP 3.3 Flight Simulator WP 2.3.1 WP 2.3.3 WP 3.4 WP 2.3.2 Low Power Thermal Electrical LGS Iron Bird Management WIPS WP 3.5 WP 2.3.6 WP 2.3.4 WP 2.3.5 Innovative High Lift Advanced Electrical ECS Advanced EPGDS Propeller Turboprop (FTB#2) 3
REG-01-09 Scope of the work WP 2.3.1 Key Objectives & Technologies • Study of Low Power Wing Ice Protection System technologies including mechanical/electrical integration requirements & constraints • Modeling activities (thermal model not part of this topic) for system optimal sizing and performance validation • Certification approach for Regional A/C WIPS at early stage (new Appendix O condition) to be compliant with CS 25.1420 • Increasing TRL targets to 5 (in CS GRA hybrid technology only at TRL 2/3) IWT ACTIVITY FULL THERMAL ICE PROTECTION SYSTEM
REG-01-09 Scope of the work CfP Topic Activities: • High level requirements definition for system sizing and power budget estimation • Selection of system architecture identifying a low power solution most suitable for Regional A/C leading edge. An electro-thermal de-ice solution would be preferred, but the Applicant(s) can propose alternative ones (Preliminary Design Review - TRL3) • System detailed design (CDR) • Prototype manufacturing including: • Qualification/industrialization test-lab environment validation (TRL4) • Wing leading edge with technology embedded
REG-01-09 Tasks Ref. No. Title - Description Due Date Ice Impingement Analysis for system requirements T1 T0+9 definition Definition of system architecture and sizing of T2 complete ice protection system for Regional Aircraft T0+12 (Preliminary Design) T3 System detailed design T0+24 IPS Demonstrator components design, development, T4 T0+32 testing and delivery for IWT T5 Support IPS IWT demonstration and assessment T0+36 6
REG-01-09 Task 1: Ice Impingement Analysis for system requirements definition Based on defined wing profile, the Partner(s) shall perform and share analysis for impingement limits definition and ice accretion results. Studies performed shall target the system sizing vs ice certification requirements and integration studies. Main activities foreseen by this task are: • Ice impingement and shape analysis for low power de-icing system requirement definition • Preliminary system specification “Laminarity” concept for outboard wing will be shared with the selected Partner(s), to allow an harmonization of ice architecture with aerodynamic constraints. A trade-off will be carried out to compare wing configuration with and without laminar outboard concept, to evaluate relevant impact on ice architecture selection. 7
REG-01-09 Task 2: Definition of system architecture and sizing of complete ice protection system for Regional Aircraft (Preliminary Design) The Partner(s) shall perform the Preliminary Design of the low power de-icing system based on the requirements set by the TM and on ice impingement analysis results, defining system architecture and all necessary components. The Partner(s) shall provide all the information related to the chosen architecture, in terms of (at least): Performance Integration aspects Maintenance Safety failures Certification requirements This task ends with Preliminary Design Review (PDR). 8
REG-01-09 Task 3: System Detailed Design The Partner(s) shall perform the Detailed Design of the Low Power System: • Perform the detailed design of all the system components/equipment • Provide 2D drawings of all the components/equipment • Update weight report • Finalize the power & electrical load analysis • Provide a preliminary IWT plan & procedure • Test Article mechanical design All the technical information provided during the preliminary design phase shall be updated. This task ends with Critical Design Review (CDR). 9
REG-01-09 Task 4: IPS Demonstrator components design, development, testing and delivery for IWT The Partner(s) shall be responsible for the Test Article manufacturing and for the definition of the IWT test planning and procedure to demonstrate the effectiveness of the Low Power De- Icing System. The Partner(s) shall provide Test Article made of composite material including Low Power WIPS component (indicatively the wing section to be tested shall be the outboard with a chord-wise size of 1500 mm and span-wise size function of IWT test chamber size). Selected Candidate(s) shall define: • IPS configuration for test • Lab test instrumentation and IWT instrumentation specification • Control logic for test (e.g. D/I cycle activation, power regulation as function of ice accretion) • Detailed planning and procedure for the IWT • Test Article qualification to cover functional performance and environmental requirements With activities included inside this task, TRL 4 shall be reached. 10
REG-01-09 Task 5: Support IPS IWT demonstration and assessment The IWT test campaign will be finalized to testing the system integrated into the wing section sample in a range of operating points covering the critical conditions for the Regional A/C. The selected Partner(s), in concurrence with TM, shall prepare an IWT Test Program oriented to tests execution. The IWT tests will be performed in the context of a separate complementary activity (not part of this call). In this task the Partner(s) shall be responsible for: • Installing the demonstrator and instrumentation in the IWT • Record all the data after running in IWT • Write the IWT test plan and IWT test report • Update performance document for the complete system based on test results With activities included inside this task , TRL 5 shall be reached. 11
REG-01-09 Deliverables & Milestones 12
REG-01-09 Overall Planning Y1 Y2 Y3 T0+3 T0+6 T0+9 T0+12 T0+15 T0+18 T0+21 T0+24 T0+27 T0+30 T0+33 T0+36 T1- Ice Impingement Analysis for system requirements definition PDR T2-Definition of system architecture and sizing of complete ice protection system for RA CDR T3-System Detailed Design T4-IPS demonstrator and component design, development, testing and delivery for IWT T5-Support IPS, IWT Demonstration and Assessment Technology and Model Validation in IWT TRL ROADMAP TRL3 TRL4 TRL5 via CfP WP 2.3.1 Wing Ice Protection System via Complementary activities (not part of topic) 13
REG-01-09 Special skills, Capabilities, Certification expected from the Applicant(s) • Proven experience in the design and development of advanced technologies in the field of Anti-icing and De-icing Systems • Numerical tools availability to assess thermal performance in Appendix C and O conditions • Numerical tools availability to assess structure resistance under different kinds of steady and transient loads (thermal, mechanical, impact) • Validation of numerical tools against previously performed test campaigns (icing wind tunnel, structural testing, impacts) • Good experience and knowledge of aircraft icing issues • Proven experience in the use of design, analysis and configuration management tools of the aeronautical industry • IWT test rig experience • Proven IWT test running experience Applicant(s) should demonstrate experience in preparation and conduction of icing wind tunnel tests. 14
Q&A Any questions? Info-Call-CFP-2017-01@cleansky.eu Innovation Takes Off
C lean Sky 2 Information Day dedicated to the 6 th Call for Proposal (CfP06) JTI-CS2-2017-CFP06-REG-01-10 E 2 -EM Supervisor and Control Algorithms Brussels, 22 February 2017
REG-01-10 Topic Intro • Estimated Funding Topic Value: 800k € • Duration: 36 months • Start date: Q1 2018 (indicative) • SoW overview: – Technologies Development – Energy Optimized Regional A/C – Advanced Electrical Power Generation & Distribution System Decentralized EPDS Network concept A-EPGDS electrical architecture 17 CS2 Info Day CfP06, Brussels 22.Feb.2017
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