IP Library Granted Patent US 10,677,529
Granted Patent B2
US 10,677,529 · App. 15/624,524 · Granted Jun 9, 2020

Vacuum forming method

Inventors: Andrew Pirie (Gardena, CA); Ignacio Hernandez (Gardena, CA)
Assignee: DUCOMMUN AEROSTRUCTURES, INC.
F27D7/06B21D5/02B21D11/203B21D53/92C21D1/30C22F1/02C22F1/183F27D5/00F27D5/0006F27D2007/066
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Quick Facts
Patent No.
US 10,677,529
App. No.
15/624,524
Granted
Jun 9, 2020
Kind
B2
Abstract

A method for forming large titanium parts includes forming bends into a titanium plate for form a bent part. The bent part is then roll-formed to form contours into the bent part. The surfaces of the contoured part are rough-machined, and the part is then secured to a bladed form fixture. The bladed form fixture comprises a plurality of header boards that secure the part to the fixture. The fixture part is placed in a thermal vacuum furnace and a stress-relieving operation is performed. The part is removed from the fixture and final machining takes place.

Claims (30)

1. A method for forming large titanium parts, the method comprising:

forming bends into a titanium plate to form a bent part;

roll-forming contours into the bent part to form a contoured part;

rough-machining the surfaces of the contoured part to form a rough-machined part;

securing the rough-machined part to a bladed form fixture to form a fixtured part, the bladed form fixture comprising a plurality of header boards extending upwardly from a base, an upper surface of each of the header boards dimensioned to engage with a lower surface of the rough-machined part;

vacuum stress-relieving the fixtured part to form a stress-relieved part;

removing the stress-relieved part from the bladed form fixture;

final-machining the stress-relieved part.

2. The method of claim 1 , wherein the plurality of header boards are spaced apart from one another substantially equidistantly.

3. The method of claim 2 , wherein the plurality of header boards are spaced apart from one another a minimum distance of between 3 and 7% of a finished length of the part.

4. The method of claim 1 , wherein the bladed form fixture further comprises a plurality of clamps engaged with upper corners of the header boards, each clamp configured to securely clamp the rough-machined part to one of the header boards.

5. The method of claim 4 , wherein the plurality of clamps comprise C-clamps and each header board has a pair of the clamps on each opposed upper corner of the header board.

6. The method of claim 5 , wherein one of the pair of clamps is disposed on a front side of the header board and one of the pair of clamps is disposed on a rear side of the header board.

7. The method of claim 1 , wherein each header board is formed from titanium.

8. The method of claim 7 , wherein each header board is connected to the base via titanium runners that extend longitudinally down the base.

9. The method of claim 8 , wherein each runner is connected to the base via a restraint plate that extends over a width of the runner and is fastened to the base outside of the width of the runner, such that the runner is configured to expand and contract without being restrained longitudinally by the base.

10. A method for forming large titanium parts, the method comprising:

rough-machining the surfaces of a titanium part to form a rough-machined part;

securing the rough-machined part to a bladed form fixture to form a fixtured part, the bladed form fixture comprising a plurality of header boards extending upwardly from a base, an upper surface of each of the header boards dimensioned to engage with a lower surface of the rough-machined part;

vacuum stress-relieving the fixtured part to form a stress-relieved part;

removing the stress-relieved part from the bladed form fixture;

final-machining the stress-relieved part.

11. The method of claim 10 , further comprising forming bends into the titanium part to form a bent part, before the bent part is rough-machined.

12. The method of claim 11 , further comprising roll-forming contours into the bent part to form a contoured part, before the contoured part is rough-machined.

13. The method of claim 10 , wherein the bladed form fixture further comprises a plurality of clamps engaged with upper corners of the header boards, each clamp configured to securely clamp the rough-machined part to one of the header boards.

14. The method of claim 13 , wherein the plurality of clamps comprise C-clamps and each header board has a pair of the clamps on each opposed upper corner of the header board.

15. The method of claim 14 , wherein one of the pair of clamps is disposed on a front side of the header board and one of the pair of clamps is disposed on a rear side of the header board.

16. The method of claim 10 , wherein each header board is formed from titanium.

17. The method of claim 16 , wherein each header board is connected to the base via titanium runners that extend longitudinally down the base.

18. The method of claim 17 , wherein each runners is connected to the base via a restraint plate that extends over a width of the runner and is fastened to the base outside of the width of the runner, such that the runner is configured to expand and contract without being restrained longitudinally by the base.

Assignments (3)
NOTICE OF GRANT OF SECURITY INTEREST IN PATENTS Recorded Jul 14, 2022
From: DUCOMMUN AEROSTRUCTURES, INC.
To: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 060653/0562 →
NOTICE OF GRANT OF SECURITY INTEREST IN PATENTS Recorded Nov 27, 2018
From: DUCOMMUN AEROSTRUCTURES, INC.
To: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 047648/0544 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 16, 2017
From: PIRIE, ANDREW; HERNANDEZ, IGNACIO
To: DUCOMMUN AEROSTRUCTURES, INC.
Reel/Frame 042731/0429 →
Continuity (2)
Provisional Application 62350559 · Jun 15, 2016
Related Publication 20170363355A1 · Dec 21, 2017