GRC ITD TOPICS FOR CFP#12 - Clean · PDF fileOptimised helicopter fuselage design provided by...
Transcript of GRC ITD TOPICS FOR CFP#12 - Clean · PDF fileOptimised helicopter fuselage design provided by...
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Clean Sky Info Day on 7th call for proposals, 11 October 2010, Brussels
GRC ITD TOPICS FOR CFP#12
Giornata ACARE Italia
Torino, 17th May 2012
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GRC0: Management
GRC1:
Innovative
Rotor Blades
GRC3:
Integration of
Innovative
Electrical
Systems
GRC4:
Installation of a
Diesel Engine
on a Light
Helicopter
GRC5:
Environment-
Friendly Flight
Paths
EcoDesign for
Airframe
EcoDesign for
Systems
SGO / Energy
Management
Technology
Evaluator
GRC6:
EcoDesign
Demonstrators
(Rotorcraft )
GRC7: Preparation of T.E.
for Rotorcraft
GRC2:
Reduced Drag
of Airframe &
Dynamic
Systems
Engines /
SAGE 5
Technology Developments & Demonstrations
Contribution from/to
transversal ITDs
Green RotorCraft ITD - Giornata ACARE Italia – GRC Topics for CFP#12, 17th May 2012 Torino
Green RotorCraft ITD: Top Level WBS
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GRC - List of topics for CFP#12
5 topics split in 4 sub-projects
GRC1: Innovative Rotor Blades
Low weight, high energy efficient tooling for rotor blade manufacturing 710 k€
GRC2: Drag Reduction of Airframes and DynamicSystems
Wind tunnel tests on a common helicopter platform and contribution to its optimised aerodynamic design 800 k€
GRC3: Innovative Electrical Systems
Design and Implementation of a Load Simulator Rig and Ground Test Bench Adaptation Kit for a HEMAS Test Rig 1000 k€
GRC5: Environment-friendly Flight Paths
Sensoring and cockpit monitoring to reduce noise in manoeuvring flight 1500 k€
Curved SBAS-guided IFR procedures for low noise rotorcraft operations 580 k€
Green RotorCraft ITD - Giornata ACARE Italia – GRC Topics for CFP#12, 17th May 2012 Torino
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GRC1
Low weight, high energy efficient tooling for rotor blade manufacturing
Green RotorCraft ITD - Giornata ACARE Italia – GRC Topics for CFP#12, 17th May 2012 Torino
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Low weight, high energy efficient tooling for
rotor blade manufacturing
Status manufacturing of helicopter rotor blades with composite materials use
currently metallic moulds with self heated technology or external heating by heat presses or ovens
the mould weight for a light helicopter (~5,0 meters long) is likely above 5tons Curing temperature is, for rotor blades, above 135°C High energy consumption and poor handling capabilities
Path Change to new manufacturing processes (e. g. preforming and liquid
composite moulding, LCM) Use of innovative, energy efficient and light toolings for preforming and
injection with short turnaround times in industrial manufacturing
Green RotorCraft ITD - Giornata ACARE Italia – GRC Topics for CFP#12, 17th May 2012 Torino
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Objective Find new and innovative tooling for helicopter rotor blades manufacturing with
composite materials based on low energy and green aspects
Steps that should be performed by the applicant
Develop, design and manufacture of preform- and curing tools
Light and easy to handle Easy to heat up and cool down > short cycle times Less energy consumption / heat exchange device Heat up range up to 135°C curing or activation temperature Homogenous heat transfer and distribution Stiff and closed mould for injection (up to 3bar) Applicable to use with special impregnation technologies (e.g. LCM) Light, one sided, fast heatable preform tools
Green RotorCraft ITD - Giornata ACARE Italia – GRC Topics for CFP#12, 17th May 2012 Torino
Low weight, high energy efficient tooling for
rotor blade manufacturing
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Skills and capabilities required from the applicant (single organisation or consortium)
Knowledge to develop, design and manufacture new tooling concepts with respect to green aspects
Heat and energy management for toolings Able to collect LCA-data
As we intend to take a new approach regarding tooling design and manufacturing we are open to any proposal. A specific certification for aerospace and airworthiness items is not required from the possible applicants. Rotor blade manufacturing process details (e.g. position of injection line, preform technology,…) will be defined by topic manager.
Green RotorCraft ITD - Giornata ACARE Italia – GRC Topics for CFP#12, 17th May 2012 Torino
Low weight, high energy efficient tooling for
rotor blade manufacturing
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Project duration:
18months (January 2013 – June 2014)
Maximum Total Cost:
€ 710.000
Green RotorCraft ITD - Giornata ACARE Italia – GRC Topics for CFP#12, 17th May 2012 Torino
Low weight, high energy efficient tooling for
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GRC2
Wind tunnel tests on a common helicopter platform and contribution to its optimised
aerodynamic design
Green RotorCraft ITD - Giornata ACARE Italia – GRC Topics for CFP#12, 17th May 2012 Torino
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Wind tunnel tests on a
common helicopter platform
Title: Wind tunnel tests on a common helicopter platform and contribution to its optimized aerodynamic design
Expected start date : January 2013
Duration : 30 months
Green RotorCraft ITD - Giornata ACARE Italia – GRC Topics for CFP#12, 17th May 2012 Torino
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Objectives:
o Support of GRC consortium in benefit assessment process for a heavy-weight class H/C by:
Wind-tunnel tests of a reference helicopter fuselage
Wind-tunnel tests of optimised design of several
elements of the common helicopter fuselage
o The work comprises:
Design and manufacturing of some model components
Wind tunnel test preparation, execution and results post-processing
Background :
Optimised helicopter fuselage design provided by GRC consortium
Existing reference model components and wind-tunnel test results
Tasks :
Task 1 - Preparation of the Original and Optimised Models
Task 2 - Wind-Tunnel Tests on the Original and Optimised Configurations
Task 3 - CFD Analysis (optional) to address mount effects on fuselage aerodynamics
Reference fuselage
Green RotorCraft ITD - Giornata ACARE Italia – GRC Topics for CFP#12, 17th May 2012 Torino
Wind tunnel tests on a common helicopter platform
Scope
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Wind tunnel tests on a common helicopter platform
Expected activities (1/3)
Task 1: Preparation of the Original and Optimised Models
Manufacture additional components for the reference configuration
Sponsons, hub cap, blade stubs.
Manufacture optimised components
to be finalised during the numerical optimisation phase
Instrumentation of reference and optimised components
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Task 2: Wind-Tunnel Tests on the Original and Optimised Configurations
Perform wind-tunnel tests of the reference fuselage
Perform wind-tunnel tests of the optimised fuselage
Two set-up configurations
Strut configuration: for rotor head investigations (with/without rotation)
Upside down configuration: for fuselage backdoor ramp investigations
Main wind-tunnel requirements
Model size: L=4.097m, Sfrontral=0.55m²
Wind-tunnel speed > 40 m/s
fuselage angle of attack from -20° to +20°
rotating rotor-hub using suitable driving system (around 1000rpm expected) and monitoring system
Expected measurements
Global forces
Surface static pressure (~ 300 taps)
Surface unsteady pressure (~ 20 transducers)
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Wind tunnel tests on a common helicopter platform
Expected activities (2/3)
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Task 3: CFD Analysis (optional)
Numerical assessment of the drag reduction of the optimised design
Investigation of wind-tunnels effect (strut, walls)
Numerical/experimental correlations
Green RotorCraft ITD - Giornata ACARE Italia – GRC Topics for CFP#12, 17th May 2012 Torino
Wind tunnel tests on a common helicopter platform
Expected activities (3/3)
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Qualified and demonstrated skills in WT testing (appreciated previous experience in WT testing on helicopter configurations)
Wind Tunnel: wind speeds at least 40 m/s fuselage angle of attack from -20° to +20° (both mount systems) fuselage angle of side-slip from -20° to +20° (both mount systems) rotating rotor-hub using suitable driving system
Measurement capabilities global loads through an internal or external balance, all six components surface static pressures (~300 pressure taps in a full configuration) surface unsteady pressures (~20 unsteady pressure transducers in a full
configuration)
If the applicant offers CFD work in task 3, the following skills are encouraged mandatory
CFD code solving the RANS equations Optional
CFD code solving the URANS equations Moving body capabilities for rotating rotor head
Green RotorCraft ITD - Giornata ACARE Italia – GRC Topics for CFP#12, 17th May 2012 Torino
Wind tunnel tests on a common helicopter platform
Skills and capabilities required
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Expected planning, assuming (T0 at Jan. 2013)
Budget: 800 kEuros,
Expected start date : January 2013; Duration : 30 months
Evaluation: Detailed break-down for Tasks 1&2 recommended
Contractual aspects: Selected partner will be offered to enter the GRC consortium
N° Task Nr. Task Name
1 1 W T Test of the original geometry
2 1.1 Input01: CATIA file of the original model delivered to the Partner
3 1.2 Manufacturing of new elements
4 1.3 Input02 & Input03: Existing model delivered to the Partner
5 1.4 Model adjustment
6 1.5 Input05: Specifications for the original configuration wind-tunnel tests
7 1.6 Wind tunnel test of the original configuration
8 1.7 Data analysis
9 1.8 Input04: CATIA file of the optimised model delivered to the Partner
10 1.9 Manufacturing of the optimised components
11 1.10 Input06: Specifications for the optimised configuration wind-tunnel tests
12 1.11 Wind tunnel test of the optimised configuration
13 1.12 Data analysis and synthesis
14 2 CFD computations
15 2.1 Original configuration
16 2.2 Optimised configuration
17 2.3 Comparison with WT data and synthesis
03/01
03/01
03/12
Sep Nov Jan Mar Mai Jul Sep Nov Jan Mar Mai Jul Sep Nov Jan Mar Mai Jul Sep2012 2013 2014 2015
Green RotorCraft ITD - Giornata ACARE Italia – GRC Topics for CFP#12, 17th May 2012 Torino
Wind tunnel tests on a common helicopter platform
Planning and budget
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GRC3
Design and Implementation of a Load Simulator Rig and Ground Test Bench Adaptation Kit for a HEMAS Test Rig
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Design and Implementation of a Load Simulator Rig and Ground
Test Bench Adaptation Kit for a HEMAS Test Rig (1/4)
Topic background and rationale:
Electromechanic actuation is slowly replacing the hydraulic actuation
systems throughout the aviation industry.
To build a testing system composed by HEMAS for the simulation of main
rotor loads.
Test the HEMAS system inside a simulated aircraft architecture.
Related GRC3 objective: To develop a complete Adaptation Kit in order to
integrate the HEMAS equipment batch inside a simulated aircraft architecture .
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Summary task description:
Design, manufacturing and acceptance on site of a complete Adaptation Kit in
order to integrate the HEMAS equipment batch inside a simulated ground
aircraft architecture (ETB).
Commissioning and initial operation of the Adaptation Kit on two different
locations (Central Europe and Electrical Test Bench).
Support the rig operations to correct potential faults during the Clean Sky
Program Development.
Design and Implementation of a Load Simulator Rig and Ground
Test Bench Adaptation Kit for a HEMAS Test Rig (2/4)
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Background material & Information exchange:
Electrical test bench and electromechanic actuation specifications.
Information exchange with conventional tools and planned technical meetings.
Skills and capabilities required from the applicant: Experience in actuation test benches design, manufacture and installation is
an asset.
Design and Implementation of a Load Simulator Rig and Ground
Test Bench Adaptation Kit for a HEMAS Test Rig (3/4)
Green RotorCraft ITD - Giornata ACARE Italia – GRC Topics for CFP#12, 17th May 2012 Torino
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Project duration:
24 months (Jan. 2013 – Dec. 2014).
Maximum Total Cost:
€ 1.000.000
Design and Implementation of a Load Simulator Rig and Ground
Test Bench Adaptation Kit for a HEMAS Test Rig (4/4)
Green RotorCraft ITD - Giornata ACARE Italia – GRC Topics for CFP#12, 17th May 2012 Torino
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GRC5
Sensoring and cockpit monitoring to reduce noise in manoeuvring flight
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Development and Test of Novel Rotor Measurement Systems to
Estimate Manoeuvring Noise During Rotorcraft Approaches and
Departures (1/4)
Related GRC-5 objective: To develop innovative on-board systems allowing pilot to minimise noise annoyance during rotorcraft approaches and departures
Topic background and rationale: Helicopter noise depends on rotor speed, thrust and angle of attack (AOA) For in-flight noise monitoring, future systems will relay on crude estimates
of these quantities, as they are hard to measure accurately Inaccuracies are relevant in manoeuvring flight, when for instance rotor is
flapping (change of AOA) to decelerate the vehicle and actual thrust is hundreds of kilograms different from weight or other estimates
Manoeuvring flight is typical during rotorcraft approaches and departures
Need of innovative measurement systems to monitoring rotor state in-flight and accurately estimating rotorcraft radiated noise
Green RotorCraft ITD - Giornata ACARE Italia – GRC Topics for CFP#12, 17th May 2012 Torino
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Summary task description: Review of current and future technologies for rotor force and blade angle
measurement (D1) Definition of requirements of a Pilot Acoustic Indicator display to monitor
radiated noise (D2) Preliminary Design Review of measurement system, reporting design and
development activity (D3) Validation against flight data of CFD tools to predict noise in manoeuvring
flight (D4) Design and Implementation of Pilot Acoustic Indicator (D5) Critical Design Review of measurement system, reporting experimental
activity (D6) Application of unsteady noise prediction tool to study the effect of
perturbations on low-noise procedures (D7) Final demonstration of measurement system and pilot indicator (D8)
Development and Test of Novel Rotor Measurement Systems to
Estimate Manoeuvring Noise During Rotorcraft Approaches and
Departures (2/4)
Green RotorCraft ITD - Giornata ACARE Italia – GRC Topics for CFP#12, 17th May 2012 Torino
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Background material & Information exchange:
Suitable flight data for validation of tools and design of experiments
Vehicle system detailed design data, as required by the activity
Relevant material on rotor measurement systems
Skills and capabilities required from the applicant: Unsteady rotor noise prediction
Design, development and test of measurement systems
Airborne display systems
Experimental lab for structural and fatigue tests on the measurement system
Capability to comply with CS 27/29, MIL -810/RTCA DO-160, RTCA DO-254
GRC-05-006: Development and Test of Novel Rotor Measurement Systems to Estimate Manoeuvring Noise During Rotorcraft Approaches
and Departures (3/4)
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Project duration:
24 months (Jan 2013 – Dec 2014)
Maximum Total Cost:
€ 1.500.000
GRC-05-006: Development and Test of Novel Rotor Measurement Systems to Estimate Manoeuvring Noise During Rotorcraft Approaches
and Departures (4/4)
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GRC5
Curved SBAS-guided IFR procedures for low noise rotorcraft operations
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GRC-05-007: Curved SBAS-guided IFR procedures for low noise rotorcraft operations (1/5)
Related GRC-5 objective: To develop and test new rotorcraft-specific flight procedures to minimise noise impact in approaches and departures
Topic background and rationale:
Curved flight paths allow to avoid overfly of noise sensitive areas
For IFR procedures, curved flight paths shall be designed in compliance with RNP-AR ICAO specification
Current RNP-AR specification relies on barometric vertical guidance which is not suited for precise flight path optimisation in the vertical plane
SBAS (EGNOS in Europe) is the best guidance mean to optimise flight paths for noise reduction, both in the horizontal and vertical plane
Need to define and assess new types of curved IFR procedures relying on SBAS guidance to minimise noise impact
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GRC-05-007: Curved SBAS-guided IFR procedures for low noise rotorcraft operations (2/5)
Summary task description:
Review and analysis of ICAO design criteria for curved segments (D1)
Assessment of SBAS guidance benefits for curved segments (D2)
Definition of design criteria for curved segments under SBAS guidance with or without transition to LPV in last part of final approach (D4, D3)
Adaptation of proposed design criteria to Point-in-Space procedures ((D5)
Comparison of benefits / constraints of the different solutions for curved IFR rotorcraft procedures (D6)
Safety study for a generic curved Point-in-Space (PinS) procedure (D7)
Detailed design and implementation of a PinS SBAS-guided curved helicopter approach to an heliport (D8)
Dissemination and organisation of a User Forum (D9)
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GRC-05-007: Curved SBAS-guided IFR procedures for low noise rotorcraft operations (3/5)
Background material & Information exchange:
ICAO PBN and related navigation specifications (RNPx, RNP-AR)
Information exchanges with GARDEN (currently running CleanSky project)
Skills and capabilities required from the applicant: Full knowledge of ICAO air navigation regulations (PanOps, PBN manual, RNPx
and RNP-AR specifications) and foreseen evolutions
Detailed analysis of ICAO procedure design criteria:
Understanding of existing criteria and ability to propose new ones
Satellite navigation, in particular SBAS
Detailed design, charting and safety analysis of IFR procedures, in particular RNP-AR procedures including curved segments
Green RotorCraft ITD - Giornata ACARE Italia – GRC Topics for CFP#12, 17th May 2012 Torino
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GRC-05-007: Curved SBAS-guided IFR procedures for low noise rotorcraft operations (4/5)
Project duration:
24 months (Dec. 2012 – Nov. 2014)
Maximum Total Cost:
580 000 €
Green RotorCraft ITD - Giornata ACARE Italia – GRC Topics for CFP#12, 17th May 2012 Torino
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For further information:
www.cleansky.eu
Contact us
Green RotorCraft ITD - Giornata ACARE Italia – GRC Topics for CFP#12, 17th May 2012 Torino
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Green RotorCraft ITD - Giornata ACARE Italia – GRC Topics for CFP#12, 17th May 2012 Torino
BACK-UP SLIDES
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GRC0: Management
GRC1:
Innovative
Rotor Blades
GRC3:
Integration of
Innovative
Electrical
Systems
GRC4:
Installation of a
Diesel Engine
on a Light
Helicopter
GRC5:
Environment-
Friendly Flight
Paths
EcoDesign for
Airframe
EcoDesign for
Systems
SGO / Energy
Management
Technology
Evaluator
GRC6:
EcoDesign
Demonstrators
(Rotorcraft )
GRC7: Preparation of T.E.
for Rotorcraft
GRC2:
Reduced Drag
of Airframe &
Dynamic
Systems
Engines /
SAGE 5
Technology Developments & Demonstrations
Contribution from/to
transversal ITDs
Green RotorCraft ITD - Giornata ACARE Italia – GRC Topics for CFP#12, 17th May 2012 Torino
GRC: Top Level WBS
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Green RotorCraft ITD - Giornata ACARE Italia – GRC Topics for CFP#12, 17th May 2012 Torino
1. Innovative Rotor Blades
Active and passive technologies to reduce rotor power consumption and acoustic signature
2. Drag Reduction of Airframes and DynamicSystems
Passive and active flow controls for helicopter and tiltorotor components
Efficiency improvement (pressure losses) and noise emission reduction of engine intake
3. Innovative Electrical Systems
Replacement of hydraulic systems on rotorcraft by electrically-powered systems
Reduction of carbon emissions and improved electrical power system efficiency.
4. Diesel Engine
Integration of a Diesel engine on a light helicopter to reduce CO2 emissions.
5. Environment-Friendly Flight Paths
Noise abatement with optimized flight procedures in VFR & IFR including ATM constraints
Fuel consumption and pollutant emissions reduction through a mission profile optimization
6. EcoDesign
Exploitation of eco-friendly technologies to specific rotorcraft components
7. Technical Evaluator for Rotorcraft
Interface to Technology Evaluator for assessing actual impact of rotorcraft technologies
GRC: Technological objectives
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Giornata ACARE Italia – GRC Topics for CFP#12, 17th May 2012 Torino
Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4
GRC1 - Innovative Rotor Bades
TRL Progress
GRC2 - Drag Reduction
TRL Progress
GRC3 - Inn. Electrical Systems
TRL Progress
HEMAS for FCS & utilities
Helicopter Electrical Systems
Electrical Tail Rotor
GRC4 - Diesel Engine on a light H/C
TRL Progress
GRC5 - Environment Friendly Flight Paths
TRL Progress
GRC6 - Eco-Design for Helicopters
TRL Progress
H/C design, test and validation
Passive Rotor Blade
Drag Reduction
(Hub & Fuselage)
Engine Installation
Engine Development
Active Rotor Blade
2014 2015 20162008 2009 2010 2011 2012 2013
Test & Evaluation
Technology Review
Full-scale blade design
Preliminary Design Detailed Design Ground Test
2 CoDR PDR CDR 4 5
Whirl Tower test
Ground test: full scale rotor blade
Design & manufacturing Whirl Tower test
Technology Review
Manufacturing
Preliminary Design Detailed Design Final TestsCoDR PDR CDR
sub-assembly design & validation (WTT)
3 6
Flight test (Hub)
WTT (fuselage)
Numerical aerodynamics optimization Design & manufacturing Flight test
H/C Requirements Equipments & Systems development /from SGO & ED) Ground Test
3 4SR
6
WTT
Test
Test
Test
(Copper Bird on EDS)
H/C pre-design, engine requirements Preliminary Design, detailed design, developmt. Ground Test
Engine Design Development
FlightTest
SR
2
2 3 CoDR PDRCDR 5 6
Test
Test
H/C adaptation design & development Test
<= depending on budget
Def.phase: flight rules analysis, requirement & tools Tools development for in-flight
environmental measures
Procedure & Guidance Systems Development
SR
2 3
PDR CDR
5 6
CoDR
Flight Test
Design
3PDR
Manufacturing Recycling
4CDR
3
2 4 5
5
2 5 6
GRC-ITD Demonstration schedule
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GRC-ITD Environmental Goals
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Green RotorCraft ITD - Giornata ACARE Italia – GRC Topics for CFP#12, 17th May 2012 Torino
© 2012 by the CleanSky JU / Green Rotorcraft ITD (GRC) Members: AgustaWestland, Eurocopter,
Liebherr-Aerospace, Hispano-Suiza, Thales Avionics Electrical Systems, Wytwornia Sprzetu
Komunikacyjnego PZL Swidnik, Office National d'Etudes et de Recherches Aérospatiales, Deutsches
Zentrum für Luft- und Raumfahrt, Centro Italiano Ricerche Aerospaziali, SELEX Sistemi Integrati,
Airborne Composites, Alphei Pueschel Roesler - Akustik Technologie Goettingen, Eurocarbon, Fibre
Optic Sensors and Sensing Systems, LMS International, Microflown Technologies, Micromega Dynamics,
Stichting Nationaal Lucht- en Ruimtevaartlaboratorium, Technische Universiteit Delft, Universiteit
Twente,
All rights reserved. This presentation material is provided for information of parties/persons invited to
the meeting as indicated herewith. No information contained in this material may be disclosed to any
other party/person, nor reproduced in whole or in part, nor used without the prior written consent of
the specific GRC member(s) to which the information belong(s).
Clean Sky JU / Green RotorCraft ITD