Manufacturing method

Patent metadata

Field	Value
Publication number	US-11267096-B2
Application number	US-201916691655-A
Country	US
Kind code	B2
Filing date	Nov 22, 2019
Priority date	Dec 13, 2018
Publication date	Mar 8, 2022
Grant date	Mar 8, 2022

Abstract

A method of manufacturing a component is provided. The method includes performing a machining operation by moving a rotating, abrasive grinding tool along a feed direction to remove material from the component. At least the part of the component from which the material is removed is formed of composite material. The abrasive grinding tool follows a trochoidal path along the feed direction.

First claim

We claim:

1. A method of manufacturing a component, the method including:
performing a machining operation by moving a rotating, abrasive grinding tool along a feed direction to remove material from the component;
wherein at least the part of the component from which the material is removed is formed of composite material, and wherein the abrasive grinding tool follows a trochoidal path along the feed direction,
wherein the composite material is a ceramic matrix composite material,
wherein the trochoidal path has a step over t, which is the distance in the feed direction between two equivalent points on adjacent loops of the trochoidal path, such that:

t
<

(

d
2

)

2

-

(

(

d
2

)

-
ae

)

2

-

(

(

d
2

)

-
g

)

2

-

(

(

d
2

)

-
ae

)

2

where d is the diameter of the tool, ae is the depth of cut made by the tool, and g is the maximum distance by which abrasive grit particles protrude from the surface of the tool,
wherein the component is a seal segment of a gas turbine engine, and the machining operation forms a groove in the seal segment.

2. The method according to claim 1 , wherein the trochoidal path lies in a plane and the abrasive grinding tool rotates about a rotation axis which is perpendicular to the plane.

3. The method according to claim 1 , wherein the rotation of the abrasive grinding tool is directed such that the surface of the tool in contact with the component rotates towards the a most recently cut surface of the component.

4. The method according to claim 1 , wherein the trochoidal path contains loops having a loop radius r, which in terms of the tool diameter d of the abrasive grinding tool has a value which, to within ±10%, is determined by the expression:

r
=

(

(

d
0.7

)

-
d

)

⁢

0.5
.

5. The method according to claim 1 , wherein the machining operation includes forming a slot in the component.

6. The method according to claim 5 , wherein:
d<0.7w
where d is the diameter of the tool and w is the width of the slot measured perpendicularly to the feed direction.

7. The method according to claim 1 , wherein the machining operation includes removing an external face of the component.

Assignees

• Rolls Royce Plc

Inventors

• NOVOVIC Donka
• Kelsey James
• Curtis David T

Classifications

• B24B19/14 Primary

  for grinding turbine blades, propeller blades or the like (using grinding belts B24B21/16) · CPC title

• B24B19/09 Primary

  for grinding trochoidal surfaces, e.g. in rotor housings of Wankel engines · CPC title