GAS TURBINE ENGINE INLET TEMPERATURE SENSOR CONFIGURATION AND CORRESPONDING METHOD

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EP 3 249 199 B8

(12)	CORRECTED EUROPEAN PATENT SPECIFICATION
	Note: Bibliography reflects the latest situation

(15)	Correction information:
	Corrected version no 1 (W1 B1)

(48)	Corrigendum issued on:
	17.03.2021 Bulletin 2021/11

(45)	Mention of the grant of the patent:
	23.12.2020 Bulletin 2020/52

(21)	Application number: 17172882.7

(22)	Date of filing: 24.05.2017

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International Patent Classification (IPC):

F02C 7/04^(2006.01)
F02C 9/28^(2006.01)

G01K 13/02^(2021.01)
G01K 7/42^(2006.01)

(54)	GAS TURBINE ENGINE INLET TEMPERATURE SENSOR CONFIGURATION AND CORRESPONDING METHOD GASTURBINENTRIEBWERKEINLASSTEMPERATURSENSORKONFIGURATION SOWIE DAZUGEHÖRIGES VERFAHREN CONFIGURATION DE CAPTEUR DE TEMPÉRATURE D'ADMISSION DE MOTEUR À TURBINE À GAZ ET PROCÉDÉ CORRESPONDANT

(84)	Designated Contracting States:
	AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

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Priority:

24.05.2016 US 201615162727

(43)	Date of publication of application:
	29.11.2017 Bulletin 2017/48

(60)	Divisional application:
	20216482.8

(73)	Proprietor: Raytheon Technologies Corporation
	Farmington, CT 06032 (US)

(72)	Inventor:
	FEULNER, Matthew R. West Hartford, CT Connecticut 06119 (US)

(74)	Representative: Dehns
	St. Bride's House 10 Salisbury Square London EC4Y 8JD London EC4Y 8JD (GB)

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References cited: :

EP-A1- 3 139 143
US-A- 5 080 496
US-B2- 7 974 812

WO-A1-2014/100081
US-A1- 2011 077 895

Note: Within nine months from the publication of the mention of the grant of the European patent, any person may give notice to the European Patent Office of opposition to the European patent granted. Notice of opposition shall be filed in a written reasoned statement. It shall not be deemed to have been filed until the opposition fee has been paid. (Art. 99(1) European Patent Convention).