AXIAL FLOW COMPRESSOR FOR A GAS TURBINE ENGINE

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EP 3 231 994 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:
	31.03.2021 Bulletin 2021/13

(45)	Mention of the grant of the patent:
	06.01.2021 Bulletin 2021/01

(21)	Application number: 17155262.3

(22)	Date of filing: 08.02.2017

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International Patent Classification (IPC):

F01D 5/08^(2006.01)

(54)	AXIAL FLOW COMPRESSOR FOR A GAS TURBINE ENGINE AXIALVERDICHTER EINES GASTURBINENTRIEBWERKS COMPRESSEUR À DÉBIT AXIAL POUR UN MOTEUR À TURBINE À GAZ

(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:

08.04.2016 US 201615094583

(43)	Date of publication of application:
	18.10.2017 Bulletin 2017/42

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

(72)	Inventor:
	WALL, Jordan T. Middletown, CT 06457 (US)

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

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References cited: :

WO-A2-2015/138031
US-A- 4 657 482
US-A1- 2015 308 341

FR-A1- 2 881 794
US-A- 5 297 386

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).