US4117970A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Method for fabrication of honeycomb structures
Assignee: Boeing North American Inc
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Filing: 1976-11-16
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Granted: 1978-10-03
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Expires: 1996-11-16
Abstract
Abstract A method for fabrication of honeycomb metallic structures combining superplastic forming and metallurgical bonding wherein a face sheet is formed and bonded to another face sheet and a core to form the desired structure. A metal honeycomb core is positioned between the first and second metal face sheets. The first face sheet, which has superplastic characteristics, is brought to within a temperature range suitable for superplastic forming. A pressure loading is applied to the first face sheet causing it to deform against the core and second metal face sheet. The face sheets and core are maintained under coordinated temperature-pressure-time duration conditions to produce metallurgical bonding to one another to form the desired honeycomb structure.
Inventors
- 👤 C. Howard Hamilton
- 👤 Leonard A. Ascani, Jr.
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-05 00:43
CPC Classifications
B; B21; B21D; B21D26/00; B21D26/02; B21D26/053; B21D26/055; B23; B23K; B23K20/00; B23K20/14
Claims Analysis
Total Claims: 15
Claim 1
Independent Claim
166 words
A method for making a honeycomb metallic structure in a single operation comprising the steps of: positioning a metal honeycomb core, a first metal blank, and a second metal blank within a hollow forming apparatus for the duration of the method, the first metal blank having superplastic characteristics, the first metal blank and the second metal blank each having opposed principal surfaces; positioning the core between the first metal blank and the second metal blank; bringing the first metal blank to within a temperature range suitable for superplastic forming of the first metal blank; applying a pressure loading across the principal surfaces of the first metal blank causing the first metal blank to deform superplastically against, and into intimate contact with, the core and the second metal blank; and maintaining the first metal blank, the second metal blank, and the core under coordinated temperature-pressure-time duration conditions sufficient to produce metallurgical bonding of the first metal blank, the second metal blank, and the core to one another.
Claim 2
Independent Claim
166 words
A method for making a honeycomb metallic structure in a single operation comprising the steps of: positioning a metal honeycomb core, a first metal blank, and a second metal blank within a hollow forming apparatus for the duration of the method, the first metal blank having superplastic characteristics, the first metal blank and the second metal blank each having opposed principal surfaces; positioning the core between the first metal blank and the second metal blank; bringing the first metal blank to within a temperature range suitable for superplastic forming of the first metal blank; applying a pressure loading across the principal surfaces of the first metal blank causing the first metal blank to deform superplastically against, and into intimate contact with, the core and the second metal blank; and maintaining the first metal blank, the second metal blank, and the core under coordinated temperature-pressure-time duration conditions sufficient to produce metallurgical bonding of the first metal blank, the second metal blank, and the core to one another.
Claim 3
Dependent Claim
35 words
The method of claim 1 wherein said positioning of the core between the first metal blank and the second metal blank is such that the core is in contacting relationship with said second metal blank.
Claim 4
Dependent Claim
40 words
The method of claim 1 wherein the positioning of the core between the first metal blank and the second metal blank is such that the core is in contacting relationship with the first metal blank and the second metal blank.
Claim 5
Dependent Claim
12 words
The method of claim 1 wherein the metallurgical bonding is diffusion bonding.
Claim 6
Dependent Claim
19 words
The method of claim 1 wherein the temperature range suitable for superplastic forming is also suitable for metallurgical bonding.
Claim 7
Dependent Claim
29 words
The method of claim 1 wherein the pressure loading used for superplastic forming said first metal blank is of sufficient magnitude for the metallurgical bonding of said maintaining step.
Claim 8
Dependent Claim
29 words
The method of claim 5 wherein the pressure loading used for superplastic forming said first metal blank is of sufficient magnitude for the metallurgical bonding of said maintaining step.
Claim 9
Dependent Claim
48 words
The method of claim 4 wherein the hollow forming apparatus defines a cavity, and also including the step of positioning the first metal blank to divide the cavity into first and second chambers, and wherein the core and the second metal blank are located in the second chamber.
Claim 10
Dependent Claim
75 words
The method of claim 8 also including the step of providing an inert gas environment in the cavity, and wherein the pressure loading across the principal surfaces of the first metal blank comprises a greater pressure of inert gas in the first chamber relative to the second chamber and the second chamber is vented to allow for efflux of inert gas as the metal blank deforms and thereby reduces the size of the second chamber.
Claim 11
Dependent Claim
32 words
The method of claim 8 wherein the pressure loading across the principal surfaces of the first metal blank comprises maintaining a fluid pressure differential between the first chamber and the second chamber.
Claim 12
Dependent Claim
63 words
The method of claim 4 wherein the second metal blank has superplastic properties, and wherein the second metal blank is also brought to within a temperature range suitable for superplastic forming, and also including the step of: applying pressure to the second metal blank by the first metal blank to cause at least a portion of the second metal blank to expand superplastically.
Claim 13
Dependent Claim
32 words
The method of claim 4 wherein the applying the pressure loading to the first metal blank is such that the first metal blank deforms against the core without significantly deforming the core.
Claim 14
Dependent Claim
13 words
The method of claim 4 wherein the first metal blank is a preform.
Claim 15
Dependent Claim
11 words
The method of claim 1 wherein the metallurgical bonding is brazing.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1981-10-02 | 1982-04-03 | 1982-10-03 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1985-10-02 | 1986-04-03 | 1986-10-03 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1989-10-02 | 1990-04-03 | 1990-10-03 | $7700.00 | Window Closed / Lapsed |