JTI-CS CFP06-REG-01-09

Transcription

1 Clean Sky 2 Information Day dedicated to the 6 th Call for Proposal (CfP06) JTI-CS CFP06-REG Innovative Low Power De-Icing System Brussels, 22 February 2017

2 Estimated Funding Topic Value: 1200k Duration: 36 months Start date: Q (indicative) CfP short description: REG Topic Intro 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

3 REG REG IADP WBS Overview R-IADP Related WPs Regional IADP WP 0 Management WP 1 High Efficiency Regional A/C WP 2 Technologies Development WP 3 Demonstrations WP 4 Demonstrations Analysis WP 2.1 Adaptive Electrical Wing WP 2.2 Regional Avionics WP 3.1 Airvehicle Flight Test Bed (FTB#1) WP 3.2 WP 2.3 Energy Optimized Regional A/C WP 2.4 Innovative FCS Fuselage/Cabin Ground Demonstrator WP 3.3 Flight Simulator WP Low Power WIPS WP Electrical LGS WP Thermal Management WP 3.4 Iron Bird WP Advanced EPGDS WP Electrical ECS WP Innovative Propeller WP 3.5 High Lift Advanced Turboprop (FTB#2) 3

4 WP Key Objectives & Technologies REG Scope of the work 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 Increasing TRL targets to 5 (in CS GRA hybrid technology only at TRL 2/3) IWT ACTIVITY FULL THERMAL ICE PROTECTION SYSTEM

5 CfP Topic Activities: REG Scope of the work 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

6 REG Tasks Ref. No. Title - Description Due Date T1 T2 Ice Impingement Analysis for system requirements definition Definition of system architecture and sizing of complete ice protection system for Regional Aircraft (Preliminary Design) T0+9 T0+12 T3 System detailed design T0+24 T4 IPS Demonstrator components design, development, testing and delivery for IWT T0+32 T5 Support IPS IWT demonstration and assessment T0+36 6

7 REG 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

8 REG 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

9 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 REG Task 3: System Detailed Design All the technical information provided during the preliminary design phase shall be updated. This task ends with Critical Design Review (CDR). 9

10 REG 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

11 REG 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

12 REG Deliverables & Milestones 12

13 REG Overall Planning T1- Ice Impingement Analysis for system requirements definition T2-Definition of system architecture and sizing of complete ice protection system for RA T3-System Detailed Design 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 PDR CDR 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 Wing Ice Protection System via Complementary activities (not part of topic) 13

14 REG 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

15 Q&A Any questions? Innovation Takes Off

16 Clean Sky 2 Information Day dedicated to the 6 th Call for Proposal (CfP06) JTI-CS CFP06-REG E 2 -EM Supervisor and Control Algorithms Brussels, 22 February 2017

17 REG Topic Intro Estimated Funding Topic Value: 800k Duration: 36 months Start date: Q (indicative) SoW overview: Technologies Development Energy Optimized Regional A/C Advanced Electrical Power Generation & Distribution System Decentralized EPDS Network concept A-EPGDS electrical architecture CS2 Info Day CfP06, Brussels 22.Feb

18 REG REG IADP WBS Framework R-IADP Related WPs Regional IADP WP 0 Management WP 1 High Efficiency Regional A/C WP 2 Technologies Development WP 3 Demonstrations WP 4 Demonstrations Analysis WP 2.1 Adaptive Electrical Wing WP 2.2 Regional Avionics WP 3.1 Airvehicle Flight Test Bed (FTB#1) WP 3.2 WP 2.3 Energy Optimized Regional A/C WP 2.4 Innovative FCS Fuselage/Cabin Ground Demonstrator WP 3.3 Flight Simulator WP Low Power WIPS WP Electrical LGS WP Thermal Management WP 3.4 Iron Bird WP Advanced EPGDS WP Electrical ECS WP Innovative Propeller CS2 Info Day CfP06, Brussels 22.Feb.2017 WP 3.5 High Lift Advanced Turboprop (FTB#2) 18

19 REG Objectives Main Goal: Centralized smart supervisory control for Enhanced Electrical Energy Management (E 2 -EM) strategy. Design, simulation, development, manufacturing, testing and integration of a controller embedding control logics for the innovative electrical distribution enabling technologies to be ground tested on the Regional A/C Iron Bird Demonstrator at Topic Manager lab facilities. Topic Context: TRL 5 validation of the Advanced Electrical Power Distribution System (A-EPDS) key elements are expected to be performed on Regional IRON BIRD on-ground demonstrator (relevant operative environment). CS2 Info Day CfP06, Brussels 22.Feb

20 REG Background Smart-Grid Conversion Network (SGN) CfP02 Smart Grid Conversion Network with DC/DC bi-way cellular converters (HV/LV automatic inversion) Substitution of normal monolithic with dynamic grouping of single cells (logically equivalent converters) Controller to optimally manage the power between the cells, and to select the operating mode (buck or boost) Energy Storage & Regeneration System (ESRS) CfP04 Energy Storage Device (ESD) based on supercapacitors Bi-way DC/DC converter connected to the ESD to manage the power flows EMA emulator as example of regenerative load Controller to manage the behavior of the DC/DC converter (buck or boost) and the operation set point CS2 Info Day CfP06, Brussels 22.Feb

21 REG Key Points (1/2) Enhanced Electrical Energy Management (E 2 -EM) DESIGN & MODELLING Higher level Centralized Smart Supervisory (CSS) hardware controller able to manage the SGN and ESRS lower level controllers to implement an optimal sharing of the available electrical power on-board during failures and/or overload conditions, thus not relying on main generators overload capabilities CSS control system to be fully interfaced with SGN and ESRS subsystems, as well as with the IRON BIRD, by appropriate communication protocols (equipment and test rig ICD s to be provided by TM at early stage of the Project) Formal mathematical approach is required for the CSS control logics design (for proof of correctness) Global E 2 -EM control and monitoring strategy to be modeled (at functional level) and tested in a simulation environment (architecture provided by TM) CS2 Info Day CfP06, Brussels 22.Feb

22 REG Key Points (2/2) Enhanced Electrical Energy Management (E 2 -EM) MANUFACTURING & TESTING CSS controller with embedded supervision logics shall be part of an hardware equipment, to be integrated onto Iron Bird and interfaced with SGN and ESRS via CAN network (preferred) Automatic or semi-automatic firmware translation is an asset, in order to minimize the chance of programming errors Hardware In the Loop techniques are required to provide evidence of CSS controller correct operations before integration on the Iron Bird Documentation (ICDs) required for correct electrical, mechanical and control interfaces with the electrical test rig, SGN and ESRS subsystems will be provided by TM at the early stage of the Project Qualification activities facilitating the preparation of the equipment for higher level TRL step will be an asset CS2 Info Day CfP06, Brussels 22.Feb

23 REG Tasks Tasks Ref. No. Title - Description Due Date KOM Task 1 Task 2 Task 3 Task 5 Task 6 Task 7 Task 8 Task 9 A Kick off meeting will be organized to review the technical requirements and the project logics and organization agreed with the partner during the negotiation phase. Requirements analysis: To review the customer requirements, and describe the equipment to be designed, manufactured, validated and provided to the customer for testing. System behaviour and energy management strategy definition: To analyse, design and theoretically proof the effectiveness of the energy management strategy. Software and mathematic tools are required to be used in order to prove the benefits and the formal properties of the designed system and energy management strategy. Preliminary Design: To validate the equipment requirements and check that equipment preliminary design is consistent with these requirements: architecture concept according to performance and safety requirements, sizing, interfaces definition, substantiation of design choice. Firmware definition and testing: To define the energy management strategy as a firmware for the computational core of the supervisor. Simulation based approaches shall be used for proving the firmware correctness in terms of energy management objectives achievement. Critical Design: To realize the detailed design (mechanical, electrical, thermal, ), realize detailed cad drawings, finalize safety analysis, prior to launch equipment manufacturing. Manufacturing: To manufacture the Supervisory equipment, following the CDR documentation. Testing and validation: To perform the final tests for validating the Energy management objectives achievement. Optimization and support: To analyse the feedbacks coming from the customer and provide further support for optimization activities. CS2 Info Day CfP06, Brussels 22.Feb.2017 T0 [T0 ; T0+ 3M] [T0 + 3M ; T0+ 9M] [T0 + 3M ; T0+ 12M] [T0 + 16M ; T0+ 21M] [T0 + 12M ; T0+ 24M] [T0 + 24M ; T0+ 30M] [T0 + 30M ; T0+ 34M] [T0 + 34M ; T0+ 36M] 23

24 REG Major Deliverables / Milestones Deliverables Ref. No. Title - Description Type* Due Date D1 D2 D3 D4 Analysis phase: Requirements matrix and support documentation E2-EM definition: Definition of energy management control strategy. Analysis of the results of the simulation models PDR: Preliminary Design Review and associated deliverables Firmware specification: Implementation of a preliminary firmware for energy management purposes R R/D R R T0 + 3M T0 + 9M T0 + 12M T0 + 21M D5 CDR: Critical Design Review and associated deliverables R T0 + 24M D6 D7 D8 Installation and commissioning: Delivery of the complete system with its associated documentation (preliminary DDP), installation and commissioning on site Validation final tests and DDP: Validation test report and final results (final DDP) Optimization and support: The CfP Supplier shall support the rig operations to correct potential faults during this probation period R/HW R/D R T0 + 30M T0 + 34M T0 + 36M Milestones (when appropriate) Ref. No. Title - Description Type* Due Date M1 Preliminary Design Review R T0 + 12M M2 Critical Design Review R T0 + 24M M3 Final results R T0 + 36M CS2 Info Day CfP06, Brussels 22.Feb

25 Q&A Any questions? Innovation Takes Off