US4622445A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Method of inductively brazing honeycomb panels
Assignee: Boeing Co
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Filing: 1984-09-28
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Granted: 1986-11-11
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Expires: 2004-09-28
Abstract
Abstract A process for brazing a metal face sheet to a honeycomb core to form a composite member. A brazing alloy is placed between the face sheet and the core. Rigid thermal insulation is used to press the face sheet against the core while heating the structure with induction heating for a time just sufficient to melt the brazing alloy. The portion being brazed is covered by an inert gas when it is at elevated temperatures. The rapid heating and cooling of the brazing alloy by induction heating joins the face sheet to the core without excessive energy consumption or the need for a complex vacuum system.
Inventors
- 👤 Marc R. Matsen
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-02 03:39
CPC Classifications
B; B23; B23K; B23K1/00; B23K1/002; B23K1/0008; B23K1/0014
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
114 words
A process for brazing at least one face sheet to a honeycomb core panel, said process comprising the steps of: (a) placing a brazing alloy between said face sheet and said core; (b) placing a heat resistant, rigid, thermal insulating member on said face sheet; (c) pressing said face sheet against said brazing alloy and said honeycomb core panel; (d) covering the portion of the face sheet and core panel to be brazed with an inert gas; (e) applying heat to said alloy within said portion sufficient to increase the temperature of said alloy above its melting point by induction heating; and (f) cooling said brazing alloy to a temperature below its melting point.
Claim 2
Dependent Claim
114 words
A process for brazing at least one face sheet to a honeycomb core panel, said process comprising the steps of: (a) placing a brazing alloy between said face sheet and said core; (b) placing a heat resistant, rigid, thermal insulating member on said face sheet; (c) pressing said face sheet against said brazing alloy and said honeycomb core panel; (d) covering the portion of the face sheet and core panel to be brazed with an inert gas; (e) applying heat to said alloy within said portion sufficient to increase the temperature of said alloy above its melting point by induction heating; and (f) cooling said brazing alloy to a temperature below its melting point.
Claim 3
Dependent Claim
16 words
The process of claim 1 wherein said brazing alloy is in the form of a foil.
Claim 4
Dependent Claim
16 words
The process of claim 1 wherein said brazing alloy is in the form of metal powder.
Claim 5
Dependent Claim
37 words
The process of claim 3 wherein said core panel has two opposite faces disposed to have face sheets adhered thereto, said process includes the step of adhering powdered brazing alloy to the faces of said core panel.
Claim 6
Dependent Claim
178 words
A process for brazing at least one face sheet to a honeycomb core panel, said process comprising the steps of: (a) placing a brazing alloy between said face sheet and said core panel; (b) placing a heat resistant, rigid, thermal insulating member on a portion of said face sheet; (c) pressing said face sheet against said brazing alloy and said core panel with pressure from said insulating member; (d) covering said portion of said face sheet and said core panel to be brazed with an inert gas; (e) applying heat to a portion of said brazing alloy beneath said insulating member by activating an induction heater, said heat being sufficient to increase the temperature of said alloy above its melting point; (f) deactivating said induction heater and allowing molten brazing alloy to solidify; (g) releasing pressure applied by said insulating sheet; (h) advancing said core panel and said face sheet such that an unbrazed portion is beneath said insulating member; and (i) repeating steps (c)-(g) until the desired amount of face sheet is brazed to said honeycomb core.
Claim 7
Dependent Claim
178 words
A process for brazing at least one face sheet to a honeycomb core panel, said process comprising the steps of: (a) placing a brazing alloy between said face sheet and said core panel; (b) placing a heat resistant, rigid, thermal insulating member on a portion of said face sheet; (c) pressing said face sheet against said brazing alloy and said core panel with pressure from said insulating member; (d) covering said portion of said face sheet and said core panel to be brazed with an inert gas; (e) applying heat to a portion of said brazing alloy beneath said insulating member by activating an induction heater, said heat being sufficient to increase the temperature of said alloy above its melting point; (f) deactivating said induction heater and allowing molten brazing alloy to solidify; (g) releasing pressure applied by said insulating sheet; (h) advancing said core panel and said face sheet such that an unbrazed portion is beneath said insulating member; and (i) repeating steps (c)-(g) until the desired amount of face sheet is brazed to said honeycomb core.
Claim 8
Dependent Claim
16 words
The process of claim 5 wherein said brazing alloy is in the form of a foil.
Claim 9
Dependent Claim
16 words
The process of claim 5 wherein said brazing alloy is in the form of metal powder.
Claim 10
Dependent Claim
37 words
The process of claim 7 wherein said core panel has two opposite faces disposed to have face sheets adhered thereto, said process includes the step of adhering powdered brazing alloy to the faces of said core panel.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1989-11-10 | 1990-05-12 | 1990-11-11 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1993-11-10 | 1994-05-12 | 1994-11-11 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1997-11-10 | 1998-05-12 | 1998-11-11 | $7700.00 | Window Closed / Lapsed |