Horizon 2020 (2014 - 2020)

Thermoplastic fuselage repair process integrated on manufacturing line

Last update: Feb 8, 2023 Last update: Feb 8, 2023

Details

Location:EU 27, Switzerland
EU 27, Switzerland
Contracting authority type:Development Institution
Status:Awarded
Budget: EUR 34,800,000
Award ceiling:N/A
Award floor:N/A
Sector:Air & Aviation
Eligible applicants:Unrestricted / Unspecified
Eligible citizenships:Afghanistan, Albania, Algeria, A ...
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Afghanistan, Albania, Algeria, American Samoa, Angola, Anguilla, Argentina, Armenia, Aruba, Austria, Azerbaijan, Azores, Bangladesh, Belarus, Belgium, Belize, Benin, Bermuda, Bhutan, Bolivia, Bosnia and Herzegovina, Botswana, British Virgin Islands, Bulgaria, Burkina Faso, Burundi, Cambodia, Cameroon, Canary Islands, Cape Verde, Caribbean Netherlands, Cayman Islands, Central African Republic, Chad, Chile, Colombia, Comoros, Congo, Costa Rica, Cote d'Ivoire, Croatia, Cuba, Cyprus, Czech Republic, Dem. Rep. Congo, Denmark, Djibouti, Dominica, Commonwealth of, Dominican Republic, Ecuador, Egypt, El Salvador, Eritrea, Estonia, Eswatini (Swaziland), Ethiopia, Falkland Islands, Faroe Islands, Fiji, Finland, France, French Polynesia, French Southern Territory, Gabon, Gambia, Georgia, Germany, Ghana, Greece, Greenland, Grenada, Guatemala, Guinea, Guinea-Bissau, Guyana, Haiti, Honduras, Hungary, Iceland, Indonesia, Iran, Iraq, Ireland, Israel, Italy, Jamaica, Jordan, Kazakhstan, Kenya, Kiribati, Kosovo, Kyrgyzstan, Laos, Latvia, Lebanon, Lesotho, Liberia, Libya, Lithuania, Luxembourg, Madagascar, Malawi, Malaysia, Maldives, Mali, Malta, Marshall Islands, Mauritania, Mauritius, Micronesia, Moldova, Mongolia, Montenegro, Montserrat, Morocco, Mozambique, Myanmar, Namibia, Nepal, Netherlands, New Caledonia, Nicaragua, Niger, Nigeria, North Korea, North Macedonia, Norway, Pakistan, Palau, Palestine / West Bank & Gaza, Panama, Papua New Guinea, Paraguay, Peru, Philippines, Pitcairn, Poland, Portugal, Romania, Rwanda, Saint Helena, Saint Kitts and Nevis, Saint Lucia, Saint Vincent and the Grenadines, Samoa, Sao Tome and Principe, Senegal, Serbia, Seychelles, Sierra Leone, Slovakia, Slovenia, Solomon Islands, Somalia, South Africa, South Sudan, Spain, Sri Lanka, St. Pierre and Miquelon, Sudan, Suriname, Sweden, Switzerland, Syria, Tajikistan, Tanzania, Thailand, Timor-Leste, Togo, Tonga, Tunisia, Turkey, Turkmenistan, Turks and Caicos, Tuvalu, Uganda, UK, Ukraine, Uruguay, Uzbekistan, Vanuatu, Venezuela, Vietnam, Wallis and Futuna, Yemen, Zambia, Zimbabwe
Date posted: Jan 17, 2020

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Description

Call Updates

Apr 15, 2020 5:35:25 PM

Release 4 of the Questions & Answers document was added on 15 April 2020. See the "Additional Documents" section below.

Apr 6, 2020 4:54:15 PM

Becuase of the Covid-19 situation, the deadline for all topics in this call have been extended by 2 weeks from 28 April to 12 May 2020 at 17.00.00 (Brussels local time).

Mar 26, 2020 6:42:05 PM

Release 3 of the Questions & Answers document was added on 26 March 2020. See the "Additional Documents" section below.

Feb 20, 2020 4:56:58 PM

Release 2 of the Questions & Answers document was added on 20 February 2020. See the "Additional Documents" section below.

Jan 28, 2020 12:30:03 AM

The submission session is now available for: JTI-CS2-2020-CfP11-LPA-02-37(CS2-IA)


Thermoplastic fuselage repair process integrated on manufacturing line

ID: JTI-CS2-2020-CfP11-LPA-02-37
Type of action: CS2-IA Innovation action
Deadline Model : single-stage
Planned opening date: 28 January 2020
Deadline: 28 April 2020 17:00:00 Brussels time

Horizon 2020

Work programme: H2020-JTI-CLEANSKY-2020-2021
Work programme year: H2020-JTI-CLEANSKY-2020-2021
Call name: Clean Sky 2 Call for Proposals 11
Call ID: H2020-CS2-CFP11-2020-01

Specific Challenge:Development of new technologies for in-house repair (rework) for structural and non-structural applications on Single Part, Major Component Assembly and Final Assembly Line level. Two general concepts shall be investigated in parallel:
• Welded thermoplastic Pre-consolidated Repair-Patch with parent material
• In-Situ Layer-by-Layer Integration of Repair Patch
The developed approaches have to be demonstrated on representative structural detail level, taking account the local design and thermal distribution into the structure related to typical design of fuselage structures. Please refer to the full topic descriptions document published in this call.

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