Formed structural assembly and associated preform and method

• US 7,967,240 B2
• Filed: 03/16/2007
• Issued: 06/28/2011
• Est. Priority Date: 10/21/2004
• Status: Expired due to Fees

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Sanders, Daniel G., Ramsey, Gregory L., Foutch, David W., Booker, Garry A., Will, Jeff D., Leon, Luis
• Primary Examiner(s): Speer; Timothy M
• Assistant Examiner(s): Krupicka; Adam C
• Application Number:
  US11/687,244
• Publication Number:
  US 20070175968A1
• Time in Patent Office: 1,565 Days
• Field of Search: None
• US Class Current: 244/53.00B
• CPC Class Codes: B21D 26/055 Blanks having super-plastic properties
• CPC Class Codes: B23K 20/122 using a non-consumable tool, e.g. friction stir welding
• CPC Class Codes: B23K 2103/10 Aluminium or alloys thereof
• CPC Class Codes: B23K 2103/14 Titanium or alloys thereof
• CPC Class Codes: Y10T 428/12368 Struck-out portion type
• CPC Class Codes: Y10T 428/13 Hollow or container type article [e.g., tube, vase, etc.]
• CPC Class Codes: Y10T 428/24273 including aperture

Abstract

A superplastically formed structural assembly is provided, as is an associated preform and method for forming such an assembly. The assembly includes a skin member and a support member that are joined to define a space between the members and between the joints. The assembly can be produced by joining the members in a flat configuration, and then forming the resulting preform to a predetermined shape of the structural assembly. The support member defines at least one aperture in communication with the space between the members. Thus, the skin member can be formed by delivering a pressurized fluid through the support member to the skin member, e.g., to superplastically form the skin member against a die that defines a contour surface corresponding in shape to the predetermined configuration of the assembly. The support member can extend in a substantially direct configuration between opposing portions of the skin member.

Claims

1. A nacelle assembly, comprising:

an inlet of a nacelle comprising a structural assembly, wherein the structural assembly comprises;

a skin member;

a support member joined to the skin member by first and second annular joints such that the skin member and the support member define an annular space, the first joint extending annularly proximate to an outer periphery of the annular space and the second joint extending annularly proximate to an inner periphery of the annular space,

wherein the support member extends in a substantially direct configuration between opposing portions of the skin member such that the annular space is defined between the skin and support members and between the first and second joints, and the support member defines a plurality of apertures extending through the support member to the annular space; and

a film comprised of a sol-gel material disposed on at least a portion of a surface of the skin member; and

a remainder of the nacelle bonded to the inlet,

wherein the film of the sol-gel material is disposed on that portion of the inlet that is bonded to the remainder of the nacelle in order to join the inlet and the remainder of the nacelle.

2. A nacelle assembly according to claim 1 wherein the skin member is superplastically formed from a flat configuration.

3. A nacelle assembly according to claim 1 wherein each of the first and second joints comprises at least one of the group consisting of a laser weld joint, a friction stir weld joint, a resistance weld joint, and a diffusion bond joint.

4. A nacelle assembly according to claim 1 wherein the support member defines a bulkhead within the inlet.

5. A nacelle assembly according to claim 1 wherein at least one of the joints defines a sinusoidal pattern.

6. A nacelle assembly according to claim 1 wherein at least one of the skin and support members comprises titanium, and wherein the remainder of the nacelle comprises a composite material.

7. A nacelle assembly according to claim 1 wherein each of the skin and support members is a unitary member.

8. A nacelle assembly according to claim 1 wherein the skin and support members comprise different titanium alloys.

9. A nacelle assembly according to claim 1 wherein the skin member defines a nonuniform thickness with that portion of the skin member that extends between the first and second joints being thinner than that portion of the skin member that does not extend between the first and second joints.

10. A nacelle assembly according to claim 1 wherein the inlet is bonded to the remainder of the nacelle independent of any mechanical fasteners.