IP Library › Granted Patent US 8,157,469
Granted Patent B2
US 8,157,469 · App. 11/562,605 · Granted Apr 17, 2012

Composite structural member and method for producing the same

Assignee: The Boeing Company
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Quick Facts
Patent No.
US 8,157,469
App. No.
11/562,605
Granted
Apr 17, 2012
Kind
B2
Abstract

A composite structural member is provided. The structural member includes a tubular shaft having a mating region of stiffness, and possibly thickness, greater than another region of said shaft. The shaft defines a lumen, and a fitting is disposed in the lumen. The fitting has a coupling region that defines at least one recessed portion bounded by one or more non-recessed portions, and the mating region mates with the coupling region of said fitting. As such, the shaft and fitting are mechanically restrained from at least some relative movement due to interference of the shaft and the fitting. A sleeve may be coupled to said shaft, for example, by including a tubular inner surface that proximately surrounds at least part of said shaft and mating region, for discouraging expansion of the mating region of said shaft.

Claims (23)

1. A composite structural member comprising:

a metallic fitting including a coupling region and an outwardly extending shoulder, the coupling region defining at least one recessed portion bounded by one or more non-recessed portions;

a tubular shaft having a mating region of stiffness greater than another region of said shaft and defining a lumen, said fitting being disposed in the lumen such that the mating region mates with the coupling region of said fitting, said tubular shaft including both the mating region and the another region being formed of a common fiber-reinforced material with the mating region including fibers that are provided such that the mating region has increased stiffness for radial expansion relative to the another region of said shaft; and

a sleeve coupled to said shaft for discouraging expansion of the mating region of said shaft, said sleeve comprising first and second portions with the first portion having smaller internal dimensions than the second portion to thereby define a shoulder extending outwardly from the first portion to the second portion, said sleeve positioned relative to the fitting such that the shoulder of the sleeve abuts the shoulder of the fitting as a result of the internal dimensions of the first portion of the sleeve being smaller than outer dimensions of the shoulder of the fitting with the fitting extending into the second portion and impeding movement of the first portion over the shoulder of the fitting,

wherein said shaft and fitting are mechanically restrained from at least some relative movement due to interference of said shaft and said fitting.

2. A composite structural member according to claim 1 , wherein the recessed portion extends circumferentially around said fitting to form a neck.

3. A composite structural member according to claim 1 , further comprising adhesive disposed between the coupling region of said fitting and the mating region of said shaft.

4. A composite structural member according to claim 1 , wherein said shaft has increased thickness in the mating region relative to the another region of said shaft.

5. A composite structural member according to claim 1 , wherein said sleeve is formed of a metallic material.

6. A composite structural member according to claim 1 , wherein said shaft has an increased thickness in the mating region relative to the another region of said shaft and said sleeve has a tubular inner surface that proximately surrounds at least part of said shaft, including at least part of the mating region.

7. A composite structural member according to claim 6 , further comprising adhesive disposed between said shaft and sleeve.

8. A composite structural member according to claim 7 , wherein said shaft and fitting and the tubular inner surface of said sleeve are tapered.

9. A composite structural member according to claim 7 , wherein the inner surface of said sleeve is substantially parallel with an outer surface of said shaft.

10. A composite structural member according to claim 1 , further comprising a core disposed in at least part of the lumen of said shaft.

11. A composite structural member according to claim 1 , wherein the mating region includes an increased percentage of fibers oriented substantially circumferentially relative to the another region of said shaft.

12. A composite structural member according to claim 1 , wherein said shaft is comprised of resin-based material.

13. A composite structural member comprising:

a metallic fitting including a coupling region and an outwardly extending shoulder, the coupling region defining at least one of a protrusion or a recessed portion bounded by one or more non-recessed portions;

a tubular shaft having a mating region and defining a lumen, said shaft including the mating region being comprised of a common material including reinforcing fibers and being configured to have a greater percentage of substantially circumferential fibers in the mating region than in another region of said shaft, such that the mating region has increased stiffness for radial expansion relative to the another region of said shaft; and

a sleeve coupled to said shaft for discouraging expansion of the mating region of said shaft, said sleeve comprising first and second portions with the first portion having smaller internal dimensions than the second portion to thereby define a shoulder extending outwardly from the first portion to the second portion, said sleeve positioned relative to the fitting such that the shoulder of the sleeve abuts the shoulder of the fitting as a result of the internal dimensions of the first portion of the sleeve being smaller than outer dimensions of the shoulder of the fitting with the fitting extending into the second portion and impeding movement of the first portion over the shoulder of the fitting,

wherein said fitting is disposed in the lumen of said shaft such that the mating region of said shaft mates with the coupling region of said fitting and said shaft and fitting are mechanically restrained from at least some relative movement due to interference of said shaft and said fitting.

14. A structural member according to claim 13 , wherein the coupling region is radially asymmetrical.

15. A structural member according to claim 13 , wherein said sleeve is formed of a metallic material.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 22, 2006
From: KENNEDY, DENNIS K.
To: THE BOEING COMPANY
Reel/Frame 018547/0130 →
Continuity (1)
Related Publication 20080118303A1 · May 22, 2008