IP Library Granted Patent US 10,329,033
Granted Patent B2
US 10,329,033 · App. 15/543,269 · Granted Jun 25, 2019

Cold spray method to join or in certain cases strengthen metals

Inventors: JinKyu Choi (Trumbull, CT); Aaron T. Nardi (East Granby, CT); Michael A. Klecka (Vernon, CT); Robert Guillemette (Durham, CT); Jeffrey Michael Mendoza (Manchester, CT)
Assignee: SIKORSKY AIRCRAFT CORPORATION
B64F5/40B22F7/06B23P6/00B23P6/04C23C24/04F01D5/005B22F2003/247B22F2007/068B23P2700/01F05D2230/10F05D2230/30Y02T50/672
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Quick Facts
Patent No.
US 10,329,033
App. No.
15/543,269
Granted
Jun 25, 2019
Kind
B2
Abstract

A method of repairing or, in certain cases, strengthening a metallic substrate at a damage site is provided and includes removing material from the substrate around the damage site to form a recess, and cold spraying particulate material into the recess to form a bead of deposited material.

Claims (23)

1. A method of repairing or, in certain cases, strengthening a metallic substrate at a damage site, comprising:

removing material from the substrate around the damage site to form a recess having chamfered edges and rounded corners; and

cold spraying particulate material into the recess to form a bead of deposited material.

2. The method according to claim 1 , wherein a ratio of cross-sectional areas of the bead and the substrate is greater than a ratio of a strength of the substrate to a strength of the bead.

3. The method according to claim 1 , wherein a ratio of a total bond area between the bead and the substrate to the cross-sectional area of the substrate is greater than a ratio of the strength of the substrate to a bond strength between the bead and the substrate.

4. The method according to claim 1 , wherein the bead comprises rounded corners having a radius of at least 0.5 times an exit diameter of a nozzle from which the particulate material is cold sprayed.

5. The method according to claim 1 , further comprising machining the bead to planarize the bead.

6. The method according to claim 1 , further comprising machining the bead to smooth the bead.

7. The method according to claim 1 , further comprising:

clamping a doubler to the substrate at the damage site;

machining the doubler; and

machining the bead to planarize the bead.

8. The method according to claim 1 , wherein the removing of the material from the substrate comprises forming a tapered recess in the substrate.

9. The method according to claim 8 , wherein an angling of the recess is defined in accordance with a type of the particulate material and a velocity of the cold spraying.

10. An in situ method of repairing or, in certain cases, strengthening an aluminum substrate at a damage site, comprising:

removing material from the substrate around the damage site to form a tapered recess having chamfered edges and rounded corners and narrow and wide ends at first and second opposite sides of the substrate, respectively;

clamping a doubler to the first side of the substrate at the damage site; and

cold spraying particulate material into the recess against the doubler to form a bead.

11. The method according to claim 10 , further comprising inspecting the substrate to identify the damage site.

12. The method according to claim 10 , further comprising:

machining the doubler; and

machining the bead to planarize the bead.

13. The method according to claim 10 , wherein an angling of the chamfered edges is defined in accordance with a type of the particulate material and a velocity of the cold spraying.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 13, 2017
From: CHOI, JINKYU; NARDI, AARON T.; KLECKA, MICHAEL A.; GUILLEMETTE, ROBERT; MENDOZA, JEFFREY MICHAEL
To: SIKORSKY AIRCRAFT CORPORATION
Reel/Frame 042994/0351 →
Continuity (2)
Provisional Application 62104426 · Jan 16, 2015
Related Publication 20170369187A1 · Dec 28, 2017