Compressor airfoil

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United States of America Patent

PATENT NO 9920642
SERIAL NO

14195430

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Abstract

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Aspects of the present invention relate to systems and methods of a vane design utilizing welding techniques. The present invention concerns a method for preventing cracking within a vane assembly utilizing full penetration welding. Additional embodiments concern a vane design that, when assembled with another vane, comprises an axial slot that prevents cracking within a vane assembly.

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Patent Owner(s)

Patent OwnerAddress
H2 IP UK LIMITED27 OLD GLOUCESTER STREET LONDON WC1N 3AX

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Miller, Edward Len Jupiter, US 6 50
Orsatti, Richard Jupiter, US 1 0

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