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Innovation Takes Off 15/09/2015
Clean Sky 2 Information Day dedicated to the
2nd Call for Proposals (CFP02)
Innovation Takes Off
FAST ROTORCRAFT IADP (LifeRCraft)
Airbus Helicopters Philippe CABRIT, Brussels, 3d September 2015
Juan Manuel JIMENEZ, Sevilla , 15th September 2015 François TOULMAY, Rzeszow, 22th September 2015
15/09/2015
TRANSPORT RANGE & PRODUCTIVITY
Unprepared Area Helideck
Door-to-Door
Large Airport
Regional Airport
Heliport Local airfield
Local Transport Short range Medium Range Long Range
Helicopter
Turboprop
Turbofan & CROR
FRC – Filling the Mobility Gap
EMS, SAR, Coast guard Disaster relief Oil & Gas offshore
Corporate Transport Air Taxi
MISSIONS AIRFIELD
TRANSPORT RANGE & PRODUCTIVITY
Unprepared Area Helideck
Door-to-Door
Large Airport
Regional Airport
Heliport Local airfield
Local Transport Short range Medium Range Long Range
Helicopter
Compound R/C
Tilt-Rotor A/C
Turboprop
Turbofan & CROR
FRC – Filling the Mobility Gap
EMS, SAR, Coast guard Disaster relief Oil & Gas offshore
Corporate Transport Air Taxi
MISSIONS AIRFIELD
Unique capabilities:
Hover/Vertical flight: as good as helicopter
Cruise speed exceeding 220 kt (410 km/h)
(*) VTOL: Vertical Take-Off & Landing
LifeRCraft (1) - The Compound Rotorcraft A new game–changing rotorcraft
NB: images may not reflect CS2 demonstrator sizing & components (for illustration purpose only)
Not an airplane, better than a helicopter:
a compound VTOL* architecture that retains
the best of both aircraft types
Continue with LifeRCraft to prepare a
competitive product
(1) LifeRCraft= Low Impact, Fast & Efficient RotorCraft.
Thanks to a comprehensive demonstration that will:
De-risk the integration of this new configuration thru the supply chain
Pave the way for development & marketing prior non-EU competitors to secure market share of European rotorcraft industry.
Enabling to meet expectations for door-to-door mobility, environment protection, citizens’ health & safety:
Shorter time for Rescue & Emergency, Air Taxi
Acoustic footprint & CO2 emission lower than helicopter
Eco-friendly materials, greener life cycle
15/09/2015
Example of benefit: Emergency Medical
Service - Full Coverage within 1 hour
140 Kts
Range
in 1 hour
Required rescue bases:
-7 to 8 bases with conventional H/C (main land only)
03/02/2015
Example of benefit: Emergency Medical
Service - Full Coverage within 1 hour
140 Kts
Range
in 1 hour
Required rescue bases:
-7 to 8 bases with conventional H/C (main land only)
220Kts
Required rescue bases:
-7 to 8 bases with conventional H/C (main land only)
- 4 to 5 bases with compound R/C (land & islands)
03/02/2015
LifeRCraft - The Compound Rotorcraft Major Challenges
Weight, weight, and weight… Even more crucial than for helicopters, why?
Additional components: wing and lateral rotors
Strong engines & power train
Aerodynamic efficiency: Also crucial!
Cruise: low drag, high Lift-to-Drag ratio
Hover/ vertical flight: efficiency & manoeuvrability
Cost efficiency: Must outperform helicopter
Operating cost (per kg payload/km)
Recurring cost
NB: images may not reflect actual demonstrator sizing & components (for illustration purpose only)
Unique opportunity to mature innovative technologies up to TRL 6 and showcase them for future compound and helicopter products
15/09/2015
15/09/2015
WP2.2: Airframe Structure (AHD)
WP2.4: Lifting rotor (AH)
WP2.12: Flight control, AFCS, nav systems (AH)
WP2.3:Landing system (AH)
WP2.6: Mechanical drive: MGB, LGB, shafts (AH - AHP)
WP2.8: Electrical system: power
generation, distribution
& storage (AH - AHD)
Wing (WP B-1.1) (AHD)
Tail boom & tail surfaces
(WP B-4.1) (AHE)
WP7: Power plant: Engines - adaptation & installation (AH)
WP2.1: Project management & integration activities (AH)
In ITD Airframe
WP2.5: Lateral rotors (AH)
WP2.9: Actuators (AH)
WP2.11: Cabin & Mission Equipment (AH – AHD)
WP2.10: Avionics & Sensors (AH)
WP2.13: Validation, verification demonstration: ground tests, flying demonstrator (AH)
WP numbers are referring to FRC
project:
MGB: Main Gearbox
LGB: Lateral Gearbox
CS2 LifeRCraft Work breakdown LifeRCraft WBS
CALL FOR PARTNER nb 2: TOPICS FOR LIFERCRAFT
15/09/2015
Topics proposed by Airbus Helicopters for the call for partner n° 2 :
Within Airframe ITD:
• AIR-02-13: Prototype Manufacturing Tooling for Single Parts Manufacturing of the Rotorless tail for LifeRCraftAssembly tooling (tail fuselage)
• AIR-02-14: Prototype Tooling for Sub-Assembly, Final Assembly and Transport of the Rotorless tail for the Compound RC
Within FRC IADP:
• FRC 02-09 Light weight, impact resistant, canopy for fast compound rotorcraft
• FRC-02-10: Multipurpose test rig for transmission gearboxes
• FRC-02-11: Design and Realization of equipped engine compartments for a fast compound rotorcraft
• FRC-02-12: Fuel bladder tanks for a fast compound rotorcraft
• FRC-02-13: HVDC Generator
• FRC-02-14: Bird strike - Erosion resistant and fast maintainable windshields
AIR-02-13: Prototype Manufacturing Tooling for Single Parts Manufacturing of the Rotorless tail for LifeRCraft
• Leading Companies: Airbus Helicopters España + AERNNOVA Consortium
• Indicative Funding Value, duration: 0,75 M€ ; 34 Months
• Type of Action: IA • Overview:
– The aim of this Call for Partner is to develop, design, manufacture and deliver to the CoP of the CfCP AIR-02-02, the prototype manufacturing tooling's for all single parts of the LifeRCraft Rotorless Tail that belong to the WP_B4.1 “Rotorless Tail for LifeRCraft”
– The development of this tooling should be innovative in order to implement the best performances in the following fields:
• Low Cost Materials
• Eco-design
• Energy savings
• Manufacturing processes simplification-Production time savings.
– Always ensuring that each one of the single parts manufactured with the prototype tooling fit with the Aeronautical quality standards
15/09/2015
AIR-02-14: Prototype Tooling for Sub-Assembly, Final Assembly and Transport of the Rotorless tail for the Compound RC
• Leading Companies: Airbus Helicopters España + AERNNOVA Consortium
• Indicative Funding Value, duration: 0,35 M€ ; 32 Months
• Type of Action: IA • Overview:
– The aim of this Call for Partner is to develop, design, manufacture and deliver to the Leader and/or the CoP of the CfCP AIR-02-02, all the prototype Assembly, Sub-Assembly and Transportation tooling needed to pre-assemble, assemble and transport the Compound RC Rotorless Tail.
– The development of this tooling should be innovative in order to implement the best performances in the following fields:
• Low Cost/ Natural Materials
• Eco-design
• Energy savings
• Assembly processes simplification-Assembly time savings
• Simplify Transportation processes
15/09/2015
FRC-02-09: Light weight, impact resistant, canopy for fast compound rotorcraft
• Leading Companies: Airbus Helicopters Deutschland
• Indicative Funding Value, duration: 1 M€ ; 50 Months
• Type of Action: IA
Sketches & Dimensions
Dimensions are indicative and will be specified after partner selection
Overview: The primary structure to be designed and produced constitutes the fuselage front section from radar-transparent nose and cockpit section to junction with the central fuselage. It does not include the doors (responsibility of partner selected through Call 1) and the windshields (other subject of the present call: FRC02-14). This structure will be integrated in the LifeRCraft rotorcraft flying demonstrator. Main challenges are to demonstrate light weight and bird strike resistance according to airworthiness requirement and to reach TRL6 at the end of the demonstration.
This fuselage module will interfaced with the main airframe developed by Core-Partner Romanian Cluster (INCAS + IAR Brasov) and the Cockpit doors developed by Austrian-German Cluster, as well as the windscreens.
15/09/2015
FRC-02-10: Multipurpose test rig for transmission gearboxes
• Overview: The aim of this Call for Partners is to design, manufacture, test and support the adaptation of the test rig used to develop the Drive System for the Compound Rotorcraft Demonstrator in the frame of IADP FRC.
Rig adaptation includes:
– Main module which simulates the twin engine power feeding
– - Two lateral modules which simulate the lateral rotor gearboxes power consumption
– Main Gearbox installation platform
The rig is installed in Marignane (France)
• Leading Companies: Airbus Helicopters
• Indicative Funding Value, duration: 0,8 M€ ; 44 Months
• Type of Action: IA
15/09/2015
FRC-02-11: Design and Realization of equipped engine compartments for a fast compound rotorcraft
• Leading Companies: Airbus Helicopters and Airbus helicopters Deustchland
• Indicative Funding Value, duration: 1,250 M€ ; 42 Months
• Type of Action: IA
• Overview: The aim of this Call for Proposals is to develop and manufacture the main elements constituting the engine compartments of the High Speed Rotorcraft (Upper Cowlings, Air Intake, Exhaust Ejector …).
The engine compartment module will be interfaced with the main airframe developed by Core-Partner in charge of the fuselage (Romanian Cluster: INCAS + IAR Brasov)
Dimensions are indicative and will be specified after partner selection 15/09/2015
FRC-02-12: Fuel bladder tanks for a fast compound rotorcraft
• Leading Companies: Airbus helicopters Deustchland
• Indicative Funding Value, duration: 0,800 M€ ; 48 Months
• Type of Action: IA • Overview:
Design, Development, manufacturing and tests of 5 fuel tank bladders (number TBC) for the high speed compound helicopter.
These bladders shall be CS29 compliant (crashworthy)
The fuel tanks will be developed in cooperation with the Core-Partner in charge of the fuselage (Romanian Cluster: INCAS + IAR Brasov)
Number of cells, dimensions and volume are indicative and will be specified after partner selection 15/09/2015
FRC-02-13: HVDC Generator
• Leading Companies: Airbus Helicopters
• Indicative Funding Value, duration: 1,200 M€ ; 42 Months
• Type of Action: IA
• Overview: Development of High Voltage Direct current generator to be driven by rotorcraft main gearbox:
– 270 VDC
– Large speed range, nominal 12000 rpm
– 20 kw (+ pre-sizing for 40 kw)
Two Components: • Regulator or Generator control unit • Electrical Generator: Rotating machine with integrated converter
15/09/2015
FRC-02-14: Bird strike - Erosion resistant and fast maintainable windshields
• Leading Companies: Airbus Helicopters
• Indicative Funding Value, duration: 0,600 M€ ; 50 Months
• Type of Action: IA • Overview:
Complete set of lightweight windshields to be developed, manufactured and tested
Opportunity to develop a lightweight innovative windshield fulfilling the requirement of a non-pressurized high speed rotorcraft aircraft:
– Bird strike resistant (CS29),
– Low drag,
– Compatible with water repellent treatment…)
– De-fogging capability
– Compatibility with electrical anti-icing.
The windshields will be installed on the canopy subject of the topic FRC 02-09
15/09/2015
LifeRCraft - The Compound Rotorcraft
Main tasks to be performed by the partner
Packages for partnership
Main activities for these packages include:
General design and interfaces according to the Airbus Helicopters specification (Plateau phase and common design offices with AH and/or the relevant Core partner will be planned)
Choice of technologies to be validated by Airbus Helicopters,
Detail design and component/subsystem development under full Partner’s responsibility, including the following activities:
• Optimisation of Weight and Recurring cost (excepted for FRC02-10 and AIR 02-13 and AIR 02-14)
• Compliance with environmental requirements to be insured
• Certification requirement have to be considered for design , but demonstration will be limited to flight clearance (excepted for FRC02-10 and AIR 02-13 and AIR 02-14)
• Manufacturing of parts and assembly of component/subsystem for integration demonstration (as specified for each topic )
• Lab tests (optional) & substantiations for flight clearance (except for FRC-02-10),
• Support to integration tests (ground and flight demonstration),
• Analysis of tests results.
15/09/2015
Questions ?
Any questions on the 2nd Call for Proposals can be addressed to the following mailbox:
Last deadline to submit your questions: 15th October 2015
Thank you !
15/09/2015
Thank You
7
Disclaimer
The selection of Partners is based on Horizon 2020 Rules for Participation, the rules for submission of proposals, evaluation and
selection of Partners as adopted by the Governing Board of Clean Sky 2 JU and as published on the JU’s website.
The content of this presentation is not legally binding. This presentation wishes to provide an overview of the call and rules.
The proposed content/approach is based on the consultation with the “National States Representative Group” and the “Task
Force “ of the Clean Sky 2 Programme.
