IP Library Granted Patent US 12,343,798
Granted Patent B2
US 12,343,798 · App. 18/178,771 · Granted Jul 1, 2025

Multi-material structures and methods

Inventors: Jonathan D. Embler (Santa Ana, CA); William E. O'Connor (Santa Monica, CA); Tobias Schaedler (Oak Park, CA); Eric C. Clough (Santa Monica, CA); Raymond Nguyen (Anaheim, CA); Sonia Zacher (Santa Monica, CA)
Assignee: The Boeing Company
B22F10/43B22F10/38B22F10/60B22F2301/205B22F2303/05B22F2303/40
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 12,343,798
App. No.
18/178,771
Granted
Jul 1, 2025
Kind
B2
Abstract

A multi-material structure includes a refractory portion with a metal or metal alloy of at least one of niobium (Nb), molybdenum (Mo), tantalum (Ta), tungsten (W), rhenium (Re), iridium (Ir), vanadium (V), and ruthenium (Ru). A structural portion is metallurgically joined with the refractory portion. The structural portion includes a titanium (Ti) alloy. At least one of the refractory and structural portions is additively manufactured.

Claims (29)

1. A multi-material structure comprising:

a machined refractory portion provided in a finished configuration, the refractory portion comprising at least one of niobium (Nb), molybdenum (Mo), tantalum (Ta), tungsten (W), rhenium (Re), iridium (Ir), vanadium (V), and ruthenium (Ru);

an additively manufactured structural portion comprising a titanium alloy, wherein the additively manufactured structural portion further comprises a core having an open cell structure; and

an interface portion metallurgically joining the machined refractory portion and the additively manufactured structural portion.

2. The multi-material structure of claim 1 wherein the refractory portion comprises a body centered cubic metal alloy.

3. The multi-material structure of claim 1 wherein the additively manufactured structural portion comprises a titanium alloy in a phase of at least one of a near-alpha, alpha-beta, near-beta, beta, and gamma.

4. The multi-material structure of claim 1 wherein the additively manufactured structural portion comprises at least one of Ti-6Al-4V, Ti-6Al-2Sn-4Zr-2Mo, and TiAl.

5. The multi-material structure of claim 1 wherein the interface comprises a mixed composition metallurgically joining the refractory portion and the additively manufactured structural portion.

6. The multi-material structure of claim 1 wherein the interface comprises a mixed composition powder deposited onto the refractory portion by additive manufacturing.

7. The multi-material structure of claim 1 wherein the interface comprises a graded composition.

8. The multi-material structure of claim 1 wherein the interface comprises a plurality of layers.

9. The multi-material structure of claim 8 wherein the plurality of layers define a compositional gradient.

10. The multi-material structure of claim 1 wherein the interface comprises titanium.

11. The multi-material structure of claim 1 wherein the interface comprises niobium.

12. The multi-material structure of claim 1 wherein the interface portion is a continuous solid structure formed by additive manufacturing.

13. A multi-material structure comprising:

a machined refractory portion provided in a finished configuration;

an additively manufactured structural portion having a physical characteristic different from a physical characteristic of the refractory portion, wherein the additively manufactured structural portion comprises a core having an open cell structure; and

an interface portion metallurgically joining the machined refractory portion and the additively manufactured structural portion.

14. The multi-material structure of claim 13 wherein the refractory portion comprises at least one of niobium (Nb), molybdenum (Mo), tantalum (Ta), tungsten (W), rhenium (Re), iridium (Ir), vanadium (V), and ruthenium (Ru), and alloys thereof.

15. The multi-material structure of claim 13 wherein the refractory portion comprises a niobium (Nb) alloy.

16. The multi-material structure of claim 13 wherein the structural portion comprises at least one of Ti-6Al-4V, Ti-6Al-2Sn-4Zr-2Mo, and TiAl.

17. The multi-material structure of claim 13 wherein the structural portion comprises a titanium alloy in a phase of at least one of a near-alpha, alpha-beta, near-beta, beta, and gamma.

18. The multi-material structure of claim 13 wherein the interface portion is a continuous solid structure formed by additive manufacturing.

19. A multi-material structure comprising:

a machined refractory portion provided in a finished configuration, the machined refractory portion comprising a body centered cubic metal alloy comprising at least one of niobium (Nb), molybdenum (Mo), tantalum (Ta), tungsten (W), rhenium (Re), iridium (Ir), vanadium (V), and ruthenium (Ru);

an additively manufactured structural portion comprising a titanium alloy in a phase of at least one of a near-alpha, alpha-beta, near-beta, beta, and gamma, wherein the additively manufactured structural portion comprises at least one of Ti-6Al-4V, Ti-6Al-2Sn-4Zr-2Mo, and TiAl, wherein the additively manufactured structural portion comprises a core having an open cell structure; and

an interface portion metallurgically joining the machined refractory portion and the additively manufactured structural portion.

20. The multi-material structure of claim 19 wherein the interface portion is a continuous solid structure formed by additive manufacturing.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 6, 2023
From: EMBLER, JONATHAN D.; O'CONNOR, WILLIAM E.; SCHAEDLER, TOBIAS; CLOUGH, ERIC C.; NGUYEN, RAYMOND; ZACHER, SONIA
To: THE BOEING COMPANY
Reel/Frame 062958/0436 →
Continuity (2)
Provisional Application 63367062 · Jun 27, 2022
Related Publication 20230415236A1 · Dec 28, 2023
References Cited (10)
US 10857628B2 · Mann · 2020 [cited by applicant]
US 10926480B2 · Yousefiani et al. · 2021 [cited by applicant]
US 11255641B2 · Zamorano Senderos et al. · 2022 [cited by applicant]
US 20080078482A1 · Cotton · 2008 [cited by examiner]
US 20190233924A1 · Parrish et al. · 2019 [cited by applicant]
US 20200248285A1 · Rajan et al. · 2020 [cited by applicant]
US 20220023942A1 · Sungail et al. · 2022 [cited by applicant]
EP 3216547 · 2017 [cited by applicant]
WO WO2013112217 · 2013 [cited by applicant]
European Patent Office, International Search Report and Written Opinion, Intl. App. No. PCT/US2023/068759 (Oct. 9, 2023). [cited by applicant]
Cited By (1)
US 12,649,407