Diode electrical ground for fan blades

Patent metadata

Field	Value
Publication number	US-9394805-B2
Application number	US-201213714779-A
Country	US
Kind code	B2
Filing date	Dec 14, 2012
Priority date	Sep 27, 2012
Publication date	Jul 19, 2016
Grant date	Jul 19, 2016

Abstract

A rotor has a rotor body with at least one slot receiving a blade. The blade has an outer surface, at least at some areas, formed of a first material and having an airfoil extending from a dovetail. The dovetail is received in the slot. A diode is in contact with a portion of the dovetail formed of a second material that is more electrically conductive than the first material. The diode is in contact with a rotating element that rotates with the rotor. The rotating element is formed of a third material. The first material is less electrically conductive than the third material. The diode and the rotating element together form a ground path from the portion of the dovetail into the rotor. An engine and a fan blade are also disclosed.

First claim

The invention claimed is:

1. A rotor for use in a gas turbine engine comprising:
a rotor body having at least one slot receiving a blade;
said blade having an outer surface, at least at some areas, formed of a first material and having an airfoil extending from a dovetail, said dovetail received in said slot; and
a diode in contact with a portion of said dovetail, said portion formed of a second material that is more electrically conductive than said first material, and said diode being in contact with a rotating element that rotates with said rotor, said rotating element being formed of a third material, and said first material being less electrically conductive than said third material, said diode and said rotating element together forming a ground path from said portion of said dovetail into said rotor.

2. The rotor as set forth in claim 1 , wherein said first material includes an outer coating that is relatively non-conductive compared to said second and third materials.

3. The rotor set forth in claim 2 , wherein said second material is aluminum, and said third material includes titanium.

4. The rotor as set forth in claim 2 , wherein said diode contacts said portion of said dovetail at an area of said dovetail where said outer coating has not been deposited.

5. The rotor as set forth in claim 1 , wherein said diode blocks flow of electric charge from said rotating element into said portion of said dovetail.

6. The rotor as set forth in claim 1 , wherein said rotating element is separate from said rotor.

7. The rotor as set forth in claim 6 , wherein said rotating element is a lock ring which secures said blade within said rotor, said grounding element contacts said lock ring, and said lock ring contacts said rotor to provide said grounding path.

8. The rotor as set forth in claim 1 , wherein said rotor is a fan rotor and said blade is a fan blade.

9. A gas turbine engine comprising:
a fan section, a compressor section, a combustor section, and at least one turbine rotor, said at least one turbine rotor driving a compressor rotor, and said at least one turbine rotor also driving a fan rotor of said fan section through a gear reduction;
said fan rotor having at least one fan blade having an outer surface, at least at some areas, formed of a first material and having an airfoil extending from a dovetail, said dovetail received in a slot in said fan rotor; and
a diode in contact with a portion of said dovetail, said portion formed of a second material that is more electrically conductive than said first material, and said diode being in contact with a rotating element that rotates with said fan rotor, said rotating element being formed of a third material, and said first material being less electrically conductive than said third material, said diode and said rotating element together forming a ground path from said portion of said dovetail into said rotor.

10. The gas turbine engine as set forth in claim 9 , wherein said first material includes an outer coating that is relatively non-conductive compared to said second and third materials.

11. The gas turbine engine as set forth in claim 10 , wherein said second material is aluminum, and said third material includes titanium.

12. The gas turbine engine as set forth in claim 10 , wherein said diode contacts said portion of said dovetail at an area of said dovetail where said outer coating has been masked to not be deposited.

13. The gas turbine engine as set forth in claim 9 , wherein said diode blocks flow of electric charge from said rotating element into said portion of said dovetail.

14. The gas turbine engine as set forth in claim 9 , wherein said rotating element is separate from said fan rotor.

15. The gas turbine engine as set forth in claim 14 , wherein said rotating element is a lock ring which secures said fan blade within said fan rotor, said grounding element contacts said lock ring, and said lock ring contacts said rotor to provide said grounding path.

16. A fan blade and grounding element comprising:
a fan blade having an outer surface, at least at some areas, formed of a first material and having an airfoil extending from a dovetail; and
a diode in contact with a portion of said dovetail, said portion formed of a second material that is more electrically conductive than said first material, such that said diode will contact a rotating element when said fan blade is received in a rotor to provide a ground path from said portion of said dovetail into the rotor.

17. The fan blade as set forth in claim 16 , wherein said first material includes an outer coating that is relatively non-conductive compared to said second material.

18. The fan blade as set forth in claim 17 , wherein said second material is aluminum.

19. The fan blade set forth in claim 17 , wherein said diode contacts said portion of said dovetail at an area of said dovetail where said outer coating has been masked to not be deposited.

20. The fan blade as set forth in claim 16 , wherein said diode blocks flow of electric charge from said rotating element into said portion of said dovetail.

Assignees

• United Technologies Corp

Inventors

• Hansen James O
• Garosshen Thomas J
• Watson Thomas J

Classifications

• F01D25/00 Primary

  Component parts, details, or accessories, not provided for in, or of interest apart from, other groups · CPC title

• Y02T50/671

  Cross-Sectional Technologies · mapped topic

• F01D5/30

  Fixing blades to rotors; Blade roots {; Blade spacers} · CPC title

• F01D25/007

  Preventing corrosion · CPC title

• B64D45/02 Primary

  Lightning protectors; Static dischargers · CPC title