Patent details

Basic Information

Publication number:

EP2459445

PCT Application Number:

PCT/FR/2010/051617

Type:

European Patent Granted for LU

Legal Status:

Lapsed

Application number:

EP107629529

PCT Publication Number:

WO/2011/012822

First applicant's nationality:

Translation Language:

EPO Publication Language:

French

English Title of Invention:

ENGINE ASSEMBLY FOR AN AIRCRAFT OF WHICH THE ATTACHMENT STRUT COMPRISES A STRUCTURAL CASE FORMING AN INTERNAL RADIAL DELIMITATION OF THE SECONDARY FLOW

French Title of Invention:

ENSEMBLE MOTEUR POUR AERONEF DONT LE MAT D'ACCROCHAGE COMPREND UNE ENVELOPPE STRUCTURALE FORMANT DELIMITATION RADIALE INTERNE DU FLUX SECONDAIRE

German Title of Invention:

MOTORBAUGRUPPE FÜR EIN FLUGZEUG MIT EINER ANBRINGUNGSSTREBE MIT EINEM STRUKTURELLEN GEHÄUSE ZUR FORMUNG EINER INTERNEN RADIALEN BEGRENZUNG DES SEKUNDÄRFLUSSES

SPC Number:

Dates

Filing date:

29/07/2010

Grant date:

11/12/2013

EP Publication Date:

11/12/2013

PCT Publication Date:

03/02/2011

Claims Translation Received Date:

Translations Received Date (B1 EP Publication):

Translations Received Date (B2 EP Publication):

Translations Received Date (B3 EP Publication):

Publication date:

06/06/2012

EP B1 Publication Date:

11/12/2013

EP B2 Publication Date:

EP B3 Publication Date:

Lapsed date:

29/07/2014

Expiration date:

29/07/2030

Renunciation date:

Revocation date:

Annulment date:

Owner

From:

29/07/2010

 

 

Name:

Airbus Operations

Address:

(société Par Actions Simplifiée) 316 Route de Bayonne, 31060 Toulouse, France (FR)

Inventor

Name:

LAFONT Laurent

Address:

France (FR)

Priority

Priority Number:

0955425

Priority Date:

31/07/2009

Priority Country:

France (FR)

Classification

Main IPC Class:

F02K 1/70;

Filing date	Document type	Number of pages