Brussels, 22 nd February 2017 This document is the property of one or - - PowerPoint PPT Presentation
Clean Sky 2 AIRFRAME ITD Call for Proposals #6 Brussels, 22 nd February 2017 This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
Brussels, 22nd February 2017
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
Re-think the a/c architecture Re-think the fuselage Re-think the wing Re-think the control Re-think the cabin
Smart Fixed Wing Aircraft
2
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
Weight New Materials Manufacturing Cost Drag Maintenance
More Efficient Airframes
Cabin
Efficiency of the engineering & manufacturing process
Time to Market (lead Time)
High Performance & Energy Efficiency High Versatility & Cost Efficiency
Innovative Aircraft Architecture Advanced Laminarity High Speed Airframe Novel Control Novel travel experience Next generation
wing Optimized high lift configs. Advanced integrated structures Advanced Fuselage
REG
IADP/Integrated Demonstrators
FRC LPA AIR Bizjet SAT
the prospect of changing step by 2030+
Noise
FRC AIR Bizjet SAT LPA REG
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
Dassault – SAAB - Airbus DS
4
IADPs & SAT provide General Requirements Airframe technologies development up to TRL5/6 TRL6+ demonstrations in IADPs and SAT Leonardo
Leonardo Airbus Helicopters
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
5
5 Technology Streams 4 Technology Streams Co-Leaders: DAv, SAAB
Leaders: Airbus, Fraunhofer CP: NACOR, GAINS, ecoTECH, CASTLE, MANTA
Co-Leaders: Airbus D&S S.A.U. (CASA)
Leaders: Airbus, FNM-VEL, FNM-HD/AW,
AH, Fraunhofer, SAAB, Evektor, Piaggio
CP: NACOR, OUTCOME, ASTRAL, SHERLOC, OPTICOMS, PASSARO, SAT-AM, CASTLE, LIFTT(?)
TS A-0: Management & Interface TS A-1: Innovative Aircraft Architecture TS A-2: Advanced Laminarity TS A-3: High Speed Airframe TS A-4: Novel Control TS A-5: Novel travel experience TS B-0: Management & Interface TS B-1: Next Generation
box TS B-2: Optimized high lift configurations TS B-3: Advanced Integrated Structures TS B-4: Advanced Fuselage
WP A-0.1 WP A-1.1 WP A-2.1 WP A-3.1 WP A-4.1 WP A-5.1 WP B-0.1 WP B-1.1 WP B-2.1 WP B-3.1 WP B-4.1Overall Management Optimal engine integration on rear fuselage Laminar nacelle Multidisciplinary wing for high & low speed Smart mobile control surfaces Ergonomic flexible cabin Overall Management
Wing for incremental lift & transmission shaft integration
High wing / large Tprop nacelle configuration Advanced Integration of
Rotor-less tail for Fast Rotorcraft
WP A-0.2 WP A-1.2 WP A-2.2 WP A-3.2 WP A-4.2 WP A-5.2 WP B-0.2 WP B-1.2 WP B-2.2 WP B-3.2 WP B-4.2Business Aviation OAD & config. Mgt CROR & UHBR configurations NLF smart integrated wing Tailored front fuselage Active load control Office Centered Cabin SAT OAD & configuration Mgt More affordable composite structures High lift wing All electrical wing Pressurized fuselage for Fast Rotorcraft
WP A-0.3 WP A-1.3 WP A-2.3 WP A-3.3 WP B-0.3 WP B-1.3 WP B-3.3 WP B-4.3LPA OAD & config. Mgt Novel high performance configuration Extended laminarity Innovative shapes & structure RotorCraft OAD & configuration Mgt More efficient wings technologies Highly integrated cockpit More affordable composite fuselage
WP A-0.4 WP A-1.4 WP A-3.4 WP B-0.4 WP B-1.4 WP B-3.4 WP B-4.4Eco-Design TA Link Virtual modelling for certification Eco-Design for airframe Regional a/c OAD & config. Mgt Flow & shape control More affordable small a/c manufacturing Low weight, low cost cabin
WP B-0.5 WP B-3.5Eco-Design TA Link Advanced integration of
New materials & manufacturing A - High Performance and Energy Efficiency B - High Versatility and Cost Efficiency
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
Share of funding foreseen Participants to date Countries involved to date Leader 16.7% 4* 4 Part. Leaders 23.2% 13* 6 Core Partners 30.0% 76* 12 Partners 30.1% 124 16 *incl. Affiliates and Third Parties
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
7
Identificatio n Code CfP Title WP/Task
Project HPE AIR-01-25 Improvement of the aerodynamic loads prediction at high Reynolds number
A-1.4
AIR-01-26 Development of innovative and optimized stiffeners run-out for overall panel weight saving
A-3.1
AIR-01-27 Innovative solutions for metallic ribs or fittings introduced in a composite box to optimally deal with thermo- mechanical effects
A-3.1
AIR-01-28 Bigger cockpit windshields and associated trade-off between “plugged” design and “load-bearing” design
A-3.2
AIR-01-29 Optimisation of Friction Stir Welding (FSW) and Laser Beam Welding (LBW) for assembly of structural aircraft parts
A-3.3
Project HVC AIR-01-39 Ice tunnel Model & test for Induction system + Ice tunnel Model & test for Heat Transport system
B-2.1/B- 3.2
AIR-01-40 Infusion manufacturing methodolodies for Aircraft complex composite components.
B-2.2
AIR-01-41 All Electric Wing: Integrated electronics for actuator data and power management for Morphing Leading Edge activities
B-1.4 / B- 3.2
AIR-01-42 Lay-up tools for Helicopter Shells
B-3.3.10
AIR-01-43 Materials & Process : Low Cost Optical Wave Guide for Damage Detection & Data Transfer
B-3.3.2
AIR-01-44 Adjustable high loaded rod
B-3.3.2
AIR-01-45 Development and deployment of PLM Tools for A/C Ground Functional testing with Eco-design criteria.
B-3.6
AIR-01-46 Auto testing technologies and more automated factories for Aircraft validation test process
B-3.6
AIR-01-47 Part specific process optimization in SLM
B-3.6
AIR-01-48 Development and validation of a portable, automated and jigless system for drilling and assembly of fuselage joints
B-4.3
AIR-01-49 Development and validation of a self-adaptive system for automated assembly of major composite aerostructures
B-4.3
AIR-01-50 Design and manufacturing of innovative toolings for large curved fuselage panel
B-4.3
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
8 Optimal engine integration on rear fuselage UHBR & CROR configuration Novel high performance configuration Virtual modelling for Certification
WP A-1.4
TS A-1: Innovative Aircraft Architecture
AIB
WP A-1.1 WP A-1.2 WP A-1.3
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
9
Multidisciplinary wing for high & low speed Tailored front fuselage Innovative shapes & structure Eco-Design for Airframe
WP A-3.4
TS A-3: High Speed Airframe
DAV
WP A-3.1 WP A-3.2 WP A-3.3
BJ COMPOSITE WING ROOT
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
10
Multidisciplinary wing for high & low speed Tailored front fuselage Innovative shapes & structure Eco-Design for Airframe
WP A-3.4
TS A-3: High Speed Airframe
DAV
WP A-3.1 WP A-3.2 WP A-3.3
BJ COMPOSITE WING ROOT
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
11 11
Multidisciplinary wing for high & low speed Tailored front fuselage Innovative shapes & structure Eco-Design for Airframe
WP A-3.4
TS A-3: High Speed Airframe
DAV
WP A-3.1 WP A-3.2 WP A-3.3
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
12 12 12
Multidisciplinary wing for high & low speed Tailored front fuselage Innovative shapes & structure Eco-Design for Airframe
WP A-3.4
TS A-3: High Speed Airframe
DAV
WP A-3.1 WP A-3.2 WP A-3.3
DOOR DEMONSTRATOR
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
13
High lift wing TS B-2: Optimized high lift configurations
WP B-2.2
CASA, PAI, EVE
CASA
WP B-2.1
High wing / large Tprop nacelle configuration
CASA
WP B-3.4
More affordable small A/C manufacturing
EVE
WP B-3.3
Advanced integrated cockpit
CASA, Airbus, FHG
TS B-3: Advanced Integrated Structures
CASA
WP B-3.2
All electrical wing
CASA, FHG
Anti Ice Loop Heat Pipe Nacelle Demonstrator Anti Ice Induction Leading Edge
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
14
High lift wing TS B-2: Optimized high lift configurations
WP B-2.2 WP B-2.2.1
Advanced composite external wing box
CASA CASA, PAI, EVE
CASA
WP B-2.1
High wing / large Tprop nacelle configuration
CASA
DOOR DEMONSTRATOR
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
15
WP B-3.4
More affordable small A/C manufacturing
EVE
WP B-3.3
Advanced integrated cockpit
CASA, Airbus, FHG
TS B-3: Advanced Integrated Structures
CASA
WP B-3.2
All electrical wing
CASA, FHG
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
16
WP B-3.4
More affordable small A/C manufacturing
EVE
WP B-3.3
Advanced integrated cockpit
CASA, Airbus, FHG
TS B-3: Advanced Integrated Structures
CASA
WP B-3.2
All electrical wing
CASA, FHG
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
17
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
18
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
19
New materials and manufacturing
WP B-3.4
More affordable small A/C manufacturing
WP B-3.5
Advanced int. of systems in small A/C
WP B-3.6 WP B-3.3
Advanced integrated cockpit TS B-3: Advanced Integrated Structures
CASA
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
20
New materials and manufacturing
WP B-3.4
More affordable small A/C manufacturing
WP B-3.5
Advanced int. of systems in small A/C
WP B-3.6 WP B-3.3
Advanced integrated cockpit TS B-3: Advanced Integrated Structures
CASA
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
21
New materials and manufacturing
WP B-3.4
More affordable small A/C manufacturing
WP B-3.5
Advanced int. of systems in small A/C
WP B-3.6 WP B-3.3
Advanced integrated cockpit TS B-3: Advanced Integrated Structures
CASA
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
22
WP B-4.4
TS B-4: Advanced Fuselage
FNM VEL Affordable low weight, human centered cabin
WP B-4.1 WP B-4.2 WP B-4.3
Roto-less tail for Fast Rotorcraft Pressurized fuselage for Fast Rotorcraft More affordable composite fuselage
Full Scale Fuselage Structural Ground Demo
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
23 23
WP B-4.4
TS B-4: Advanced Fuselage
FNM VEL Affordable low weight, human centered cabin
WP B-4.1 WP B-4.2 WP B-4.3
Roto-less tail for Fast Rotorcraft Pressurized fuselage for Fast Rotorcraft More affordable composite fuselage
Full Scale Fuselage Structural Ground Demo
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
24
WP B-4.4
TS B-4: Advanced Fuselage
FNM VEL Affordable low weight, human centered cabin
WP B-4.1 WP B-4.2 WP B-4.3
Roto-less tail for Fast Rotorcraft Pressurized fuselage for Fast Rotorcraft More affordable composite fuselage
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
Capability: The portable equipment shall be able to perform drilling and hole check for Composite regional aircraft fuselage longitudinal and orbital joints. Reference components are shown in pictures.
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
The advanced technologies development for an automated drilling system on the Regional TurboProp fuselage shall be driven by the following key factors: increase of integration, reduction of assembly flow, reduction of assembling costs and increase of automation..
Equipment shall be designed as an integrated system of the three main components: drilling and measuring head, head moving equipment (both X and Y axis, moving on the fuselage, at specific locations for panels joint) and positioning and alignment system.
After design, a Test Plan for each of the three main components shall be produced by the Applicant, listing and describing all the tests that have to be conducted to develop the process.
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
Equipment shall satisfy all design requirements. Tests required by plans shall be conducted during the equipment construction, thus supporting and orienting the development of the automatic equipment.
A pre-acceptance phase shall be conducted before equipment shipping to the Topic Manager plant in
An acceptance task, similar but more in depth than pre-acceptance, shall be performed after final installation in the Topic Manager facility. A full-size demonstrator shall be successfully drilled, checked and assembled in order to validate the Equipment capabilities (6 longitudinal joints, 1 orbital joint).
Equipment shall be tested on the final planned demonstrator. The partner shall provide the required operational and engineering support for drilling and assembly
Maintenance, technical assistance and spare parts shall be guaranteed by the partner until the completion of all the activities planned (2 full complete demonstrators, 12 panels).
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
components assembly, by a documented experience in participating in actual aeronautical
programs for CN machines.
structures.
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
This solution will be applied for the assembly of stiffened panel skins, frames, window frames and door surround components. Recognition of actual position and shape of sub structure is performed by a dedicated camera system, so that a specific algorithm will elaborate the 3D model holes pattern on the basis of the actual structure position and profile. Camera system and algorithm shall be able to perform visual and dimensional checks by matching the actual data with requirements and providing report. Reference components is shown in figure 1.
Figure 1 -generic stiffened after frame/ shear tie clips installation.
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
The advanced technologies development for an automated drilling system on the Regional TurboProp fuselage shall be driven by the following key factors: increase of integration, reduction of assembly flow, reduction of assembling costs and increase of automation..
Equipment shall be an integrated system of the three main components: drilling and fastening (sealing and insertion) head, moving equipment and vision, analysis, positioning and alignment system,
After design, a Test Plan for each of the three main components shall be produced by the Applicant, listing and describing all the tests that have to be conducted to develop the process.
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
Equipment shall satisfy all design requirements. Tests required by plans shall be conducted during the equipment construction, thus supporting and orienting the development of the automatic equipment.
A pre-acceptance phase shall be conducted before equipment shipping to the Topic Manager plant in
An acceptance task, similar but more in depth than pre-acceptance, shall be performed after final installation in the Topic Manager facility. A full-size demonstrator shall be successfully drilled, checked and assembled in order to validate the Equipment capabilities (6 panels assembly).
Equipment shall be tested on the final planned demonstrator. The partner shall provide the required operational and engineering support for drilling and assembly
Maintenance, technical assistance and spare parts shall be guaranteed by the partner until the completion of all the activities planned (2 full complete demonstrators, 12 panels).
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval
Last deadline to submit your questions: 29th March 2017
This document is the property of one or more Parties to the Clean Sky 2 AIRFRAME ITD consortium and shall not be distributed or reproduced without their formal approval