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Quick Disconnect System

Project description

Innovative quick disconnect system for energy-optimised aircraft

The EU-funded QUICK project will design, develop, manufacture and test a disconnect system to be installed on future energy-optimised aircraft. The project will exploit the world-leading expertise in mechanical, electrical and control engineering focused on aerospace applications at the University of Nottingham (UNOTT) to develop an innovative, highly robust and reliable fault detection and mechanical isolation system. This system will reduce the risks from potentially highly dissipative failure modes required by the upcoming high-performance electrical power generation technologies. UNOTT’s innovative design and prototyping capabilities, internal quality control and commercial experience will support the development of the QUICK system.

Objective

The Quick Disconnect System (QUICK) project brings the world leading expertise in mechanical, electrical and control engineering focused on aerospace applications at the University of Nottingham (UNOTT) to design, develop, manufacture, test and qualify up to demonstrator test levels, a quick disconnect system intended to be installed on future energy-optimised aircraft. A novel, highly robust and reliable fault detection and mechanical isolation system will be developed aimed at reducing the risks associated with potentially highly dissipative failure modes that high-performance electrical power generator technologies will require in the near future.
Delivery of the QUICK system will be supported by UNOTT’s innovative design and prototyping capabilities and underpinned by UNOTT’s internal quality control (QC) and commercial experience. UNOTT has a proven record of working across the range of technology readiness levels (TRL), from fundamental research up to flight demonstrators for aircraft technologies, up to TRL 6. This includes the required simulations and physical hardware testing. UNOTT has world leading laboratory-based test facilities for electrical and mechanical systems including, electrical machines (EM), power electronics (PE) and aircraft electrical systems (see Section BII). Such examples include
• Electric taxiing motor, realised up to TRL5
• FIRS3T power electronics for stop/start systems, realised up to TRL7
• AEGART starter-generator and associated PE, realised up to TRL5
• HEMAS actuator systems, realised up to TRL5
• Helicopter landing gear equipment for extraction/retraction and steering
• Various power generations products

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Keywords

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Programme(s)

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Topic(s)

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Funding Scheme

Funding scheme (or “Type of Action”) inside a programme with common features. It specifies: the scope of what is funded; the reimbursement rate; specific evaluation criteria to qualify for funding; and the use of simplified forms of costs like lump sums.

IA - Innovation action

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Call for proposal

Procedure for inviting applicants to submit project proposals, with the aim of receiving EU funding.

(opens in new window) H2020-CS2-CFP07-2017-02

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Coordinator

THE UNIVERSITY OF NOTTINGHAM
Net EU contribution

Net EU financial contribution. The sum of money that the participant receives, deducted by the EU contribution to its linked third party. It considers the distribution of the EU financial contribution between direct beneficiaries of the project and other types of participants, like third-party participants.

€ 599 386,25
Address
University Park
NG7 2RD Nottingham
United Kingdom

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Region
East Midlands (England) Derbyshire and Nottinghamshire Nottingham
Activity type
Higher or Secondary Education Establishments
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Total cost

The total costs incurred by this organisation to participate in the project, including direct and indirect costs. This amount is a subset of the overall project budget.

€ 599 386,25
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