IP Library Granted Patent US 10,913,122
Granted Patent B2
US 10,913,122 · App. 16/207,816 · Granted Feb 9, 2021

Forming tool for leading edge of turbine blades

Inventors: Eric Fromerth (Manchester, CT); Daniel J Wright (Glastonbury, CT); Chung Y. Wu (Middletown, CT)
Assignee: Raytheon Technologies Corporation
B23C3/18B23C5/10B23P15/02B24B9/00B24B19/14B24D5/02B23C2210/084B23C2215/44B23C2224/36B23C2226/31B23C2228/10
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Quick Facts
Patent No.
US 10,913,122
App. No.
16/207,816
Granted
Feb 9, 2021
Kind
B2
Abstract

A forming tool for forming leading edges of turbine blades is disclosed. In various embodiments, a forming tool may comprise a cylindrically-shaped body having a notch around the circumference of the cylindrically-shaped body. The notch may be positioned perpendicularly to a center axis of the cylindrically-shaped body. Further, the notch may have a notch contour with an upper notch contour and a lower notch contour, and where the notch contour is a relief of a selected turbine blade leading edge. The forming tool may be a grinding tool or a cutting tool. Moreover, a forming process may comprise forming, by a forming tool, a first portion of a turbine blade leading edge with a rough edge result, and forming, by a milling cutter, a second portion of the turbine blade leading edge with a rough edge result.

Claims (10)

1. A forming process comprising:

forming, by a forming tool, a first portion of a turbine blade leading edge in rough condition;

forming, by a milling cutter, a second portion of the turbine blade leading edge in rough condition; wherein:

the forming tool has a notch around a circumference of a cylindrically-shaped body,

a notch contour of the notch is a relief of a selected turbine blade leading edge, and

the forming tool is a cutting forming tool comprising at least four flutes at an interior point of the notch.

2. The forming process of claim 1 , wherein the first portion of the turbine blade leading edge is an edge tip area.

3. The forming process of claim 1 , wherein a turbine blade including the turbine blade leading edge is independent from at least one of a second turbine blade and a support structure during the forming process.

4. The forming process of claim 1 , further comprising providing, by the forming tool, support to an edge tip area of the turbine blade leading edge to reduce vibration during the forming process.

5. The forming process of claim 4 , wherein the forming tool makes contact on least two surfaces of the turbine blade leading edge during the forming process.

Assignments (5)
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 Jan 4, 2021
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 054891/0802 →
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 Dec 3, 2018
From: FROMERTH, ERIC; WRIGHT, DANIEL J.; WU, CHUNG Y.
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 047660/0319 →
Continuity (3)
Division 15032000 · Apr 25, 2016
Continuation PCTUS2015012461 · Jan 22, 2015
Related Publication 20190099815A1 · Apr 4, 2019