IP Library Granted Patent US 9,802,288
Granted Patent B2
US 9,802,288 · App. 14/741,056 · Granted Oct 31, 2017

Machining system having a tool for finishing airfoils

Inventors: John P. Rizzo, Jr. (Vernon, CT); Alan C. Barron (Jupiter, FL); Joel H. Wagner (Wethersfield, CT)
Assignee: United Technologies Corporation
B24B19/14B24B17/00B24B19/009B24B19/26B24B27/0038B24B49/12B24B49/14B24B49/16B25J11/0065F01D5/005F01D5/141F05D2220/32F05D2230/14Y02T50/673
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Quick Facts
Patent No.
US 9,802,288
App. No.
14/741,056
Granted
Oct 31, 2017
Kind
B2
Abstract

An abrasive profiling tool that may be part of a robotic machining system for machining a trailing edge of an airfoil, includes a shank extending along a rotational axis, a bearing guide rotationally secured to a distal end of the shank for riding upon the airfoil; and an abrasive profiler projecting radially and rigidly outward from the shank for grinding at least the trailing edge as the shank rotates. The profiler may include a round-over portion for grinding the trailing edge and a chamfered blending portion for grinding adjacent surfaces of the airfoil to produce a smooth transition from the adjacent surfaces and to the trailing edge.

Claims (28)

1. A tool for machining an edge of an airfoil, the tool comprising:

a shank extending along a rotational axis, and including a distal end;

a bearing guide rotationally secured to the distal end for riding upon the airfoil; and

an abrasive profiler projecting radially and rigidly outward from the shank for grinding at least the edge as the shank rotates;

wherein the profiler includes a chamfered blending portion extending axially between a first end adjacent to the bearing guide and a second end, the first end having a first diameter that is equal to or less than a diameter of the bearing guide, and the second end having a second diameter that is greater than the diameter of the bearing guide and the first diameter.

2. The tool set forth in claim 1 , wherein the profiler includes a round-over portion adjacent to the second end for rounding the edge.

3. The tool set forth in claim 2 , wherein the profiler includes an abrasive coating.

4. A tool for machining a trailing edge of an airfoil, the tool comprising:

a shank extending along a rotational axis, and including a distal end;

an abrasive profiler projecting radially and rigidly outward from the shank for grinding the trailing edge as the shank rotates; and

a bearing guide rotationally secured to the distal end of the shank for riding upon the airfoil;

wherein the profiler includes a chamfered portion extending axially between a distal first end and a second end, the first end having a first diameter that is less than a second diameter of the second end;

wherein the profiler includes a round-over portion adjacent to the second end for rounding the trailing edge; and

wherein the bearing guide has a diameter that is equal to or greater than the first diameter.

5. The tool set forth in claim 4 , wherein the profiler includes abrasive grains for cutting.

6. A machining system for shaping a trailing edge of an airfoil, the system comprising:

a tool including a shank extending along a rotational axis-end, an abrasive profiler projecting radially and rigidly outward from the shank for grinding at least the trailing edge as the shank rotates, and a bearing guide rotationally secured to a distal end of the shank for riding upon the airfoil;

a robot having an arm engaged to the shank;

wherein the robot is constructed and arranged to apply a specified force between the tool and the airfoil;

wherein the profiler includes a chamfered portion extending axially between a distal first end and a second end, the first end having a first diameter that is less than a second diameter of the second end;

wherein the profiler includes a round-over portion adjacent to the second end for rounding the trailing edge; and

wherein the bearing guide has a diameter that is equal to or greater than the first diameter.

7. The machining system set forth in claim 6 further comprising:

a force feedback device.

8. The machining system set forth in claim 7 further comprising:

an optical sensor.

9. The machining system set forth in claim 7 further comprising:

a thermal, infrared, sensor.

Assignments (4)
CHANGE OF NAME Recorded Jul 27, 2023
From: RAYTHEON TECHNOLOGIES CORPORATION
To: RTX CORPORATION
Reel/Frame 064714/0001 →
CORRECTIVE ASSIGNMENT TO CORRECT THE AND REMOVE PATENT APPLICATION NUMBER 11886281 AND ADD PATENT APPLICATION NUMBER 14846874. TO CORRECT THE RECEIVING PARTY ADDRESS PREVIOUSLY RECORDED AT REEL: 054062 FRAME: 0001. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF ADDRESS. Recorded Mar 4, 2021
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 055659/0001 →
CHANGE OF NAME Recorded Sep 4, 2020
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 054062/0001 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 16, 2015
From: RIZZO, JOHN P., JR.; BARRON, ALAN C.; WAGNER, JOEL H.
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 035846/0956 →
Continuity (2)
Provisional Application 62012654 · Jun 16, 2014
Related Publication 20150360338A1 · Dec 17, 2015