TURBINE ENGINE WITH A BLADE

Number of patents in Portfolio can not be more than 2000

United States of America Patent

APP PUB NO 20240254885A1
SERIAL NO

18599470

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Abstract

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A blade for a turbine engine with a wall separating a cooling fluid flow and a hot gas fluid flow and having a heated surface along which the hot gas fluid flow flows and a cooled surface facing the cooling fluid flow. A plurality of cooling holes each having a passage extending between an inlet at the cooled surface and an outlet at the heated surface. The outlet extending between an upstream end and a downstream end with respect to the hot gas fluid flow to define a distance, the passage defining a centerline forming a first angle (θ) with the heated surface.

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Patent Owner(s)

Patent OwnerAddress
GENERAL ELECTRIC COMPANYSCHENECTADY NY

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Feldmann, Kevin Robert Mason, US 29 151
Gallier, Kirk Douglas Liberty Township, US 43 160
Osgood, Daniel Endecott Loveland, US 63 54
Perry, Andrew David Cincinnati, US 5 0
Rausch, Jonathan Michael West Chester, US 7 26
Webster, Zachary Daniel Cincinnati, US 67 130

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