US4294419A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Airframe assembly and process
Assignee: VAC ACQUISITION CORP
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Filing: 1979-01-22
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Granted: 1981-10-13
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Expires: 1999-01-22
Abstract
Abstract Disclosed is a process for fabrication and assembly of airframes and airframe components utilizing the principles of diffusion bonding and superplastic forming. A preform blank or blank sheet of material capable of being superplastically formed and diffusion bonded is attached to an airframe body or casing by diffusion bonding and superplastically deformed to form a structural airframe component. The superplastically formed structural component may be diffusion bonded to other airframe components and the superplastic forming and diffusion bonding steps may be performed simultaneously or successively to progressively fabricate and assembly an airframe having unique structural geometries and characteristics without conventional machining or welding of component parts.
Inventors
- 👤 Jack A. Fouse
- 👤 Sherwood W. McClaren, III
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-05 06:27
CPC Classifications
B; B21; B21D; B21D26/00; B21D26/02; B21D26/053; B21D26/055; B64; B64C; B64C1/00; B64C1/06; B64C1/061; B64U; B64U20/00; B64U20/10; B64C2001/0054; B64C2001/0081; B64U2101/00; B64U2101/15; Y; Y02; Y02T; Y02T50/00; Y02T50/40
Claims Analysis
Total Claims: 11
Claim 1
Independent Claim
134 words
The method of assembling a portion of an airframe having a minimum radar cross section comprising the steps of: (a) diffusion bonding the periphery of a preform capable of being superplastically formed and diffusion bonded onto the outer surface of a substantially cylindrical casing, (b) placing said cylindrical casing in a mold having a cavity therein substantially conforming to the external dimension of a structural air duct, said cavity enclosing said preform and said mold supporting a wing structure with the wing root face forming a portion of said cavity, and (c) heating said preform to a superplastic forming and diffusion bonding temperature and applying sufficient pressure across said preform to superplastically deform said preform to conform to the dimensions of said mold and diffusion bond said deformed preform to said wing root face.
Claim 2
Independent Claim
134 words
The method of assembling a portion of an airframe having a minimum radar cross section comprising the steps of: (a) diffusion bonding the periphery of a preform capable of being superplastically formed and diffusion bonded onto the outer surface of a substantially cylindrical casing, (b) placing said cylindrical casing in a mold having a cavity therein substantially conforming to the external dimension of a structural air duct, said cavity enclosing said preform and said mold supporting a wing structure with the wing root face forming a portion of said cavity, and (c) heating said preform to a superplastic forming and diffusion bonding temperature and applying sufficient pressure across said preform to superplastically deform said preform to conform to the dimensions of said mold and diffusion bond said deformed preform to said wing root face.
Claim 3
Dependent Claim
38 words
The method set forth in claim 1 wherein said preform and said casing are placed in said mold and the periphery of said preform is diffusion bonded to said casing immediately prior to superplastic deforming of said preform.
Claim 4
Dependent Claim
29 words
The method set forth in claim 1 including the step of diffusion bonding additional airframe components to said casing simultaneously with diffusion bonding of said preform to said casing.
Claim 5
Dependent Claim
21 words
The method set forth in claim 1 wherein said preform is superplastically formed into an air duct having non-linear asymmetrical dimensions.
Claim 6
Dependent Claim
20 words
The method set forth in claim 4 wherein the inlet of said duct is formed into a non-planar asymmetrical geometry.
Claim 7
Dependent Claim
9 words
The product made by the method of claim 1.
Claim 8
Independent Claim
122 words
The method of forming and assembling a portion of an airframe having minimum radar cross section comprising the steps of: (a) diffusion bonding at least a portion of a preform capable of being superplastically formed and diffusion bonded to a first structural component of an airframe, the first structural component comprising a substantially cylindrical casing structure, (b) placing said cylindrical, first structural component and preform in a mold having a cavity therein substantially conforming to the external configuration of a second structural component of said airframe, said cavity enclosing said preform, and (c) heating said preform to a superplastic forming and diffusion bonding temperature and applying sufficient pressure across said preform to superplastically deform said preform to conform to the mold cavity.
Claim 9
Independent Claim
122 words
The method of forming and assembling a portion of an airframe having minimum radar cross section comprising the steps of: (a) diffusion bonding at least a portion of a preform capable of being superplastically formed and diffusion bonded to a first structural component of an airframe, the first structural component comprising a substantially cylindrical casing structure, (b) placing said cylindrical, first structural component and preform in a mold having a cavity therein substantially conforming to the external configuration of a second structural component of said airframe, said cavity enclosing said preform, and (c) heating said preform to a superplastic forming and diffusion bonding temperature and applying sufficient pressure across said preform to superplastically deform said preform to conform to the mold cavity.
Claim 10
Dependent Claim
30 words
The method set forth in claim 7 wherein said structural components are placed in a forming and assembly mold and the diffusion bonding and superplastic forming steps are performed simultaneously.
Claim 11
Dependent Claim
64 words
The method set forth in claim 7, wherein said mold supports a third airframe structural component having a surface forming a portion of said cavity, the step of applying sufficient pressure across said preform to superplastically deform said preform comprising applying sufficient pressure to diffusion bond said deformed preform to said surface of the third airframe structural component forming a portion of said cavity.
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) | 1984-10-12 | 1985-04-13 | 1985-10-13 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1988-10-12 | 1989-04-13 | 1989-10-13 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1992-10-12 | 1993-04-13 | 1993-10-13 | $7700.00 | Window Closed / Lapsed |