Patent details

EP2873813 Title: Gas turbine engine turbine blade tip active clearance control system and method

Basic Information

Publication number:
EP2873813
PCT Application Number:
Type:
European Patent Granted for LU
Legal Status:
Lapsed
Application number:
EP141892927
PCT Publication Number:
First applicant's nationality:
Translation Language:
EPO Publication Language:
English
English Title of Invention:
Gas turbine engine turbine blade tip active clearance control system and method
French Title of Invention:
Moteur à turbine à gaz à contrôle actif de jeu d'extrémité d'aube de turbine, système et procédé de commande
German Title of Invention:
System und Verfahren zur aktiven Regelung des Schaufelspitzenspiels von Gasturbinenmotorturbinen
SPC Number:

Dates

Filing date:
16/10/2014
Grant date:
21/09/2016
EP Publication Date:
21/09/2016
PCT Publication Date:
Claims Translation Received Date:
Translations Received Date (B1 EP Publication):
Translations Received Date (B2 EP Publication):
Translations Received Date (B3 EP Publication):
Publication date:
20/05/2015
EP B1 Publication Date:
21/09/2016
EP B2 Publication Date:
EP B3 Publication Date:
Lapsed date:
16/10/2016
Expiration date:
16/10/2034
Renunciation date:
Revocation date:
Annulment date:

Owner

From:
16/10/2014
 
 

Name:
Honeywell International Inc.
Address:
115 Tabor Road, Morris Plains, NJ 07950, United States (US)

Inventor

1

Name:
Gage Raymond
Address:
United States (US)

2

Name:
Barrett Rich
Address:
United States (US)

3

Name:
Tillman Don
Address:
United States (US)

Priority

Priority Number:
201314082755
Priority Date:
18/11/2013
Priority Country:
United States (US)

Classification

Main IPC Class:
F01D 11/20;

Annual Fees

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