Leading edge sheath manufacturing method

Patent metadata

Field	Value
Publication number	US-10081082-B2
Application number	US-201314768633-A
Country	US
Kind code	B2
Filing date	Dec 16, 2013
Priority date	Mar 15, 2013
Publication date	Sep 25, 2018
Grant date	Sep 25, 2018

Abstract

A method for manufacturing a protective sheath for a fan blade leading edge is described. The method may comprise generating a preform plate from a stock plate wherein the preform plate has a flattened surface and an inclined surface having a spike flanked by a first side and a second side. The method may further comprise bending the first side and the second side away from the spike to generate a sheath intermediate followed by generating the protective sheath from the sheath intermediate by shaping an outer surface and an inner surface of the sheath intermediate to match the contour of the fan blade leading edge.

First claim

What is claimed is:

1. A method for manufacturing a protective sheath for a fan blade leading edge comprising:
generating a preform plate from an input stock plate, the preform plate having a flat surface and an inclined surface, the inclined surface having a spike extending away from the inclined surface, the preform plate further including a first side and a second side flanking the spike;
bending the first side and the second side away from the spike to generate a sheath intermediate, wherein the sheath intermediate is generated from the preform plate without discarding any material of the preform plate; and
generating the protective sheath from the sheath intermediate by shaping an outer surface and an inner surface of the sheath intermediate to match the contour of the fan blade leading edge.

2. The method according to claim 1 , wherein the shaped inner surface forms an inner diameter slot configured to receive the fan blade leading edge.

3. A method for manufacturing a protective sheath for a fan blade leading edge comprising:
generating a preform plate from an input stock plate, the preform plate having a flat surface and an inclined surface, the inclined surface having a spike extending away from the inclined surface, the preform plate further including a first side and a second side flanking the spike;
bending the first side and the second side away from the spike to generate a sheath intermediate;
generating the protective sheath from the sheath intermediate by shaping an outer surface and an inner surface of the sheath intermediate to match the contour of the fan blade leading edge, wherein the shaped inner surface forms an inner diameter slot configured to receive the fan blade leading edge, and wherein generating the protective sheath from the sheath intermediate is performed by a superplastic forming process.

4. The method according to claim 3 , wherein the superplastic forming process comprises:
placing the sheath intermediate over a mandrel in the shape of the fan blade leading edge;
heating the sheath intermediate to a temperature conducive to superplastic deformation; and
using a tool to shape the outer surface and the inner surface of the sheath intermediate to match the contour of the fan blade leading edge.

5. The method according to claim 3 , wherein bending the first side and second side is performed by a cold forming process over a mandrel.

6. The method according to claim 5 , wherein the cold forming process is performed at room temperature.

7. The method according to claim 3 , wherein bending the first side and the second side is performed by a warm forming process over a mandrel.

8. The method according to claim 7 , wherein the warm forming process is performed between about 200° C. and about 1500° C.

9. The method according to claim 3 , wherein generating the preform plate from the stock plate is performed by a contour roll plate technique.

10. The method according to claim 3 , wherein generating the preform plate from the stock plate is performed by a method selected from the group consisting of a contour roll plate technique, conventional machining, and hot forging.

11. The method according to claim 10 , further comprising the step of bonding the protective sheath to the fan blade using at least one adhesive.

12. The method according to claim 10 , wherein the protective sheath is formed from titanium.

13. A method for manufacturing a protective sheath for a fan blade leading edge using a preform plate as input stock material, the preform plate having a flat surface and an inclined surface, the inclined surface having a spike extending away from the inclined surface, the spike being bordered by a first side and a second side, said method comprising:
bending the first side and the second side away from the spike to introduce a bend into the flat surface and to generate a sheath intermediate, wherein the sheath intermediate is generated from the preform plate without discarding any material of the preform plate; and
generating the protective sheath from the sheath intermediate by shaping an outer surface and an inner surface of the sheath intermediate to match the contour of the fan blade leading edge, the shaped inner surface forming an inner diameter slot configured to receive the fan blade leading edge.

14. The method according to claim 13 , wherein the preform plate is generated from a stock plate by a contour roll plate technique.

15. The method according to claim 13 , wherein the preform plate is generated from a stock plate by a method selected from the group consisting of a contour roll plate technique, conventional machining, and hot forging.

16. A method for manufacturing a protective sheath for a fan blade leading edge using a preform plate as input stock material, the preform plate having a flat surface and an inclined surface, the inclined surface having a spike extending away from the inclined surface, the spike being bordered by a first side and a second side, said method comprising:
bending the first side and the second side away from the spike to introduce a bend into the flat surface and to generate a sheath intermediate; and
generating the protective sheath from the sheath intermediate by shaping an outer surface and an inner surface of the sheath intermediate to match the contour of the fan blade leading edge, the shaped inner surface forming an inner diameter slot configured to receive the fan blade leading edge, wherein generating the protective sheath from the sheath intermediate is performed by a superplastic forming process.

17. The method according to claim 16 , wherein the superplastic forming process comprises the steps of:
placing the sheath intermediate over a mandrel in the shape of the fan blade leading edge;
heating the sheath intermediate to a temperature conducive to superplastic deformation; and
using a tool to shape the outer surface and the inner surface of the sheath intermediate to match the contour of the fan blade leading edge.

18. The method according to claim 16 , wherein bending the first side and the second side is performed by a cold forming process over a mandrel.

19. The method according to claim 16 , wherein bending the first end and the second end is performed by a warm forming process over a mandrel.

20. A fan blade protective sheath having an outer surface and an inner diameter slot configured to receive a fan blade leading edge, the outer surface and the inner diameter slot having a shape that conforms to the shape of the fan blade leading edge, the fan blade protective sheath formed by a method comprising:
generating a preform plate from an input stock plate, the preform plate having a flat surface and an inclined surface, the inclined surface having a spike extending away from the inclined surface, the preform plate further including a first side and a second side flanking the spike;
bending the first side and the second side away from the spike to generate a sheath intermediate; and
generating the protective sheath from the sheath intermediate by shaping an outer surface and an inner surface of the sheath intermediate to match the contour of the fan blade leading edge, the shaped inner surface forming the inner diameter slot, wherein the sheath intermediate is generated from the preform plate without discarding any material of the preform plate.

Assignees

• United Technologies Corp

Inventors

• Hansen James O
• Furrer David Ulrich

Classifications

• B23P15/04 Primary

  turbine or like blades from several pieces · CPC title

• F01D5/288

  Protective coatings for blades · CPC title

• F05D2240/303

  related to the leading edge of a rotor blade · CPC title

• B21D53/78

  propeller blades; turbine blades · CPC title

• B21H7/00

  Making articles not provided for in the preceding groups, e.g. agricultural tools, dinner forks, knives, spoons (nails, pins B21G3/30) · CPC title