NSLGP | non-structural landing gear parts made of composite

Summary
The objective of this proposal is to develop, manufacture and test non-structural landing gear parts for helicopter and aircrafts based on advance carbon fiber material system, the proposal introduce the methods, capabilities and resources of IAI and CirComp to fulfill the proposal requirements such as weight reduction, low cost production, and capability of the parts to sustain in harsh environmental, This proposal include activities of improving of the automated manufacture process, weight reduction by design optimization, assembly simplification and describe the certification process, innovation activities and common aims of IAI and CirComp are also introduce .
The proposal describes also the expected impact during those activities, project structure, implementation and communication activities in this project
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More information & hyperlinks
Web resources: https://cordis.europa.eu/project/id/737721
Start date: 01-02-2017
End date: 31-07-2019
Total budget - Public funding: 627 436,25 Euro - 439 205,00 Euro
Cordis data

Original description

The objective of this proposal is to develop, manufacture and test non-structural landing gear parts for helicopter and aircrafts based on advance carbon fiber material system, the proposal introduce the methods, capabilities and resources of IAI and CirComp to fulfill the proposal requirements such as weight reduction, low cost production, and capability of the parts to sustain in harsh environmental, This proposal include activities of improving of the automated manufacture process, weight reduction by design optimization, assembly simplification and describe the certification process, innovation activities and common aims of IAI and CirComp are also introduce .
The proposal describes also the expected impact during those activities, project structure, implementation and communication activities in this project

Status

CLOSED

Call topic

JTI-CS2-2016-CFP03-SYS-03-05

Update Date

27-10-2022
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