System and method for manufacture of abrasive coating

US10060273B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10060273-B2
Application numberUS-201514687651-A
CountryUS
Kind codeB2
Filing dateApr 15, 2015
Priority dateApr 15, 2015
Publication dateAug 28, 2018
Grant dateAug 28, 2018

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A component for a gas turbine engine includes an airfoil section including a free end and an abrasive coating sprayed onto the free end, the abrasive coating including a polymer matrix and an abrasive filler, the abrasive filler between about 50%-75% by volume of the abrasive coating.

First claim

Opening claim text (preview).

What is claimed: 1. A fan blade, comprising: an airfoil section of a fan blade for a gas turbine engine, the fan blade including a free end; and a sprayed on abrasive coating bonded to the free end, the abrasive coating comprising a polymer matrix and an abrasive filler, the abrasive filler between about 50%-75% by volume of the abrasive coating wherein the filler comprises hollow glass microspheres. 2. The component as recited in claim 1 , wherein the polymer matrix provides about 3%-10% volume of the abrasive coating once cured. 3. The fan blade as recited in claim 1 , wherein the abrasive filler is zirconia. 4. The fan blade as recited in claim 1 , wherein the abrasive filler has an average particle size of 220 mesh. 5. The fan blade as recited in claim 1 , wherein the polymer matrix outgases during elevated temperature curing. 6. The fan blade as recited in claim 1 , wherein the polymer matrix maintains porosity between grit particles of the abrasive filler. 7. The fan blade as recited in claim 1 , wherein the polymer matrix includes at least one of an epoxy, polyimide, polyurethane, cyanoacrylate, acrylic, and combinations thereof. 8. The fan blade as recited in claim 7 , wherein the abrasive filler includes at least one of zirconia, alumina, silica, cubic boron nitride (CBN), and combinations thereof. 9. The fan blade as recited in claim 1 , wherein the abrasive filler is of a volume of the abrasive coating such that capillary action facilitates retention of the polymer matrix between particles of the abrasive filler. 10. The fan blade as recited in claim 9 , wherein the free end comprises a distal end and an extension around a sides of said airfoil section. 11. The fan blade as recited in claim 1 , wherein capillary action facilitates retention of the polymer matrix between particles of the abrasive filler. 12. The fan blade as recited in claim 1 , wherein the fan blade is a polymer composite upon which the abrasive coating is sprayed. 13. The fan blade as recited in claim 1 , wherein the fan blade is a polymer coated aluminum upon which the abrasive coating is sprayed. 14. The fan blade as recited in claim 1 , wherein the free end comprises a distal end. 15. The fan blade as recited in claim 1 , wherein the polymer matrix is not utilized to carry the abrasive filler during spraying. 16. A fan blade, comprising: an airfoil section of a fan blade for a gas turbine engine, the fan blade including a free end; and a sprayed on abrasive coating bonded to the free end, the abrasive coating comprising a polymer matrix and an abrasive filler, the abrasive filler between about 50%-75% by volume of the abrasive coating, the polymer matrix comprises about 3%-10% of the volume of the abrasive coating when cured wherein the filler comprises hollow glass microspheres. 17. The fan blade as recited in claim 16 , wherein the abrasive filler is zirconia. 18. The fan blade as recited in claim 17 , wherein the abrasive filler has an average particle size of 220 mesh. 19. The fan blade as recited in claim 16 , wherein the polymer matrix includes at least one of an epoxy, polyimide, polyurethane, cyanoacrylate, acrylic, and combinations thereof. 20. The fan blade as recited in claim 19 , wherein the abrasive filler includes at least one of zirconia, alumina, silica, cubic boron nitride (CBN), and combinations thereof.

Assignees

Inventors

Classifications

  • Applying different liquids or other fluent materials simultaneously · CPC title

  • Applying particulate materials (B05D1/06, B05D1/10 take precedence) · CPC title

  • Synthetic polymers, e.g. plastics; Rubber · CPC title

  • Zirconium · CPC title

  • F01D5/288Primary

    Protective coatings for blades · CPC title

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Frequently asked questions

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What does patent US10060273B2 cover?
A component for a gas turbine engine includes an airfoil section including a free end and an abrasive coating sprayed onto the free end, the abrasive coating including a polymer matrix and an abrasive filler, the abrasive filler between about 50%-75% by volume of the abrasive coating.
Who is the assignee on this patent?
United Technologies Corp
What technology area does this patent fall under?
Primary CPC classification F01D5/288. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Aug 28 2018 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).