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Engine Mounting System EMS for Ground Test Turboprop Engine Demonstrator

In aircraft, one of the primary sources of vibration is the power plant. Engine vibration could lead to unnecessary expenses for replacing damaged components, cabin noise, crew and passenger discomfort, and structural fatigue. Hut... ver más

03/07/2021

Hutchinson

571K€

Presupuesto del proyecto: 571K€

Líder del proyecto

BARRY CONTROL AEROSPACE No se ha especificado una descripción o un objeto social para esta compañía.

TRL 4-5

Fecha límite participación Sin fecha límite de participación.

Ver 2 Participantes

Financiación concedida El organismo H2020 notifico la concesión del proyecto el día 2021-07-03

JTI-CS2-2015-CFP02-ENG-01-04: Engine Mounting System (EMS) for Gr...

I+D

Cerrada hace 9 años

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Información adicional privada

No hay información privada compartida para este proyecto. Habla con el coordinador.

2 Participantes

Hutchinson

399.53K€ | Lider

PAULSTRA

44.38K€ | Participante

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Duración del proyecto: 59 meses Fecha Inicio: 2016-07-12
Fecha Fin: 2021-07-03

Líder del proyecto

BARRY CONTROL AEROSPACE No se ha especificado una descripción o un objeto social para esta compañía.

TRL 4-5

Presupuesto del proyecto 571K€

Fecha límite de participación Sin fecha límite de participación.

Descripción del proyecto In aircraft, one of the primary sources of vibration is the power plant. Engine vibration could lead to unnecessary expenses for replacing damaged components, cabin noise, crew and passenger discomfort, and structural fatigue. Hutchinson is the major supplier of aircraft main Power plant and APU Vibration Isolation Systems. The Engine Vibration Isolation Systems – EVIS project main objective is to achieve improved engine mounting system in terms of technology and associated process enabling higher level of comfort for passengers. Throughout all the proposed developments a dedicated Cost and weight reduction optimization approach will be implemented so as to enable improved performances in comparison to existing engine mounting system. So as to provide an innovative, lightweight, low-cost EVIS for the related TP Demonstrator engine, Hutchinson proposes to carry out the expected work for two distinctive concepts: • Concept 1: Cost efficiency concept based on the adaptation of existing engine mounts, • Concept 2: Full technical concept based on specifically developed engine mounts. Both Concepts will be investigated through the same usual V-shape approach for systems integration as detailed below: • Establish technical specifications of the engine mounts • Use and adapt/tune if necessary existing engine mounts for the first delivery • Analyze first test campaign results to optimize the EVIS design • Manufacture and deliver optimized EVIS • Analyze second test campaign results Hutchinson will then fully contribute through the above whole process to assist the Topic in evaluating and selecting the most efficient and effective engine suspension system for the TP Demonstrator engine.

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