LORD OPEN-ROTOR S2

LORD Engine Mounting System for the SAGE2 Open-Rotor demonstrator

 Coordinatore LORD SUISSE SARL 

 Organization address address: CHEMIN DU PAVILLON 2
city: LE GRAND SACONNEX
postcode: 1218

contact info
Titolo: Mr.
Nome: Lucien
Cognome: Audibert
Email: send email
Telefono: +33 6 77 28 23 14
Fax: +33 9 56 09 11 29

 Nazionalità Coordinatore Switzerland [CH]
 Totale costo 2˙594˙991 €
 EC contributo 1˙297˙495 €
 Programma FP7-JTI
Specific Programme "Cooperation": Joint Technology Initiatives
 Code Call SP1-JTI-CS-2012-03
 Funding Scheme JTI-CS
 Anno di inizio 2013
 Periodo (anno-mese-giorno) 2013-09-01   -   2016-08-31

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    LORD SUISSE SARL

 Organization address address: CHEMIN DU PAVILLON 2
city: LE GRAND SACONNEX
postcode: 1218

contact info
Titolo: Mr.
Nome: Lucien
Cognome: Audibert
Email: send email
Telefono: +33 6 77 28 23 14
Fax: +33 9 56 09 11 29

CH (LE GRAND SACONNEX) coordinator 1˙297˙495.50

Mappa

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 Word cloud

Esplora la "nuvola delle parole (Word Cloud) per avere un'idea di massima del progetto.

lord    engine    mounting    mount    isolation    details   

 Obiettivo del progetto (Objective)

'This response to the SAGE-02 call details the proposed approach to an engine mounting system for the open-rotor demonstrator. The goal of the program is to define the requirements of the mounting system, design and develop the system so that it meets the requirements and can be optimized and validated on an engine ground test. The mount system structural and vibration isolation requirements will be established early in the design phase. This will be done through trade studies, incorporating the many years of experience of LORD in designing and developing aircraft engine isolation systems. The technology used for the system will be adapted from current elastomeric, metallic and Fluidlastic engine mount systems to the requirements of this engine. Manufacture of components will use LORD aerospace quality system. Bench testing will be conducted at LORD using methods established for certification testing of engine mount systems. Details on how LORD will utilize, adapt and extend current technology to meet the requirements of the program are shown in the work package response.'

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