Composite strut and method of making same

• US 20050056117A1
• Filed: 06/25/2004
• Published: 03/17/2005
• Est. Priority Date: 07/22/2003
• Status: Abandoned Application

• Current Assignee: Kaiser Compositek, Inc. (BAE Systems Plc)
• Original Assignee: Kaiser Compositek, Inc. (BAE Systems Plc)
• Inventors: Jones, Brian
• Application Number:
  US10/877,132
• Publication Number:
  US 20050056117A1
• Time in Patent Office: Days
• US Class Current: 74/579.R
• CPC Class Codes: B29C 33/485 cores or mandrels collapsible mandrels for shaping tube ends B29C57/02; collapsible mandrels for winding and joining B29C53/824
• CPC Class Codes: B29C 33/52 soluble or fusible in particular used in injection moulding B29C45/4457
• CPC Class Codes: B29C 70/32 on a rotating mould, former or core
• CPC Class Codes: B29C 70/382 Automated fiber placement [AFP]
• CPC Class Codes: B29C 70/86 Incorporated in coherent impregnated reinforcing layers, e.g. by winding
• CPC Class Codes: B29L 2031/75 Shafts
• CPC Class Codes: B64C 1/06 Frames; Stringers; Longerons ; Fuselage sections
• CPC Class Codes: F16C 7/026 made of fibre reinforced resin
• CPC Class Codes: Y02T 50/40 Weight reduction
• CPC Class Codes: Y10T 74/2142 Pitmans and connecting rods

Abstract

A filament wound strut as well as a method of making the strut. The filament wound strut has a cylindrical section merging into ends through tapered end sections and which ends may be forked or otherwise arranged to receive a lug fitting. The flat ends are provided with a specially designed pre-form having a generally oval shape, and which is formed by filament reinforcement in a racetrack format surrounding a quasi-isotropic laminate. In accordance with this construction, the wound structure will react to tension loads and the inner laminate reacts to compression loads, while improving the load transfer through edge bearing and shear. A method of producing the strut is also provided in which filament materials are wound about a mandrel which is disassemblable and removable from the strut body formed thereon.

Claims

1. A load bearing strut formed primarily of a reinforced plastic composite and reacting tension and compression loading as well as minimizing effects of edge bearing and shear loading, said strut comprising:

a) an elongate section comprised of a reinforced composite material;

b) at least one terminal end section on an end of said elongate section; and

c) a load transfer insert in said end section formed of a quasi-isotropic material surrounded by a fiber reinforcing strip and having a portion therein for conducting load transference, such that the laminate reacts compression loads and the fiber reinforcing strip reacts tension loads reducing the prospect of failure by edge bearing and shear.

2. The load bearing strut of claim 1 further characterized in that said end section has a shape different than that of said elongate section and having portions which merge into a shape of the elongate section so that the two sections become effectively contiguous.

3. The load bearing strut of claim 1 further characterized in that said elongate section has a cylindrically shaped portion for a substantial portion of its length and that said terminal end section is a toric section.

4. The load bearing strut of claim 3 further characterized in that said end section has a pair of oppositely disposed surfaces and a portion which merges into a cylindrically shaped elongate section.

5. The load bearing strut of claim 1 further characterized in that said load transfer insert has a somewhat oval shape with a pair of opposite flat surfaces and that the portion therein for conducting load transference is located closer to one end of said oval-shaped portion.

6. The load bearing strut of claim 1 further characterized in that said strut is covered by an outer layer of fiber reinforcing material such that the elongate section and the end section are covered by the fiber reinforcing material wound thereabout.

9. The load bearing strut of claim 1 further characterized in that said opposite faces of said end portion are formed of an insert core material and said end section is provided with a peripheral band of reinforcing material wound thereon.

7. A load bearing strut formed primarily of a reinforced plastic composite material and capable of reacting tension and compression loads while minimizing the effects of edge bearing and shear loading, said strut comprising:

a) an elongate section having a rounded portion thereon and being comprised of at least a reinforced composite material;

b) at least one terminal end section on said elongate section and having a portion which merges into the rounded shape of said elongate section and also a relatively flat plate-like section thereon and which plate-like section has flat opposed surfaces; and

c) a load transfer insert in said terminal end section and having an insert core section surrounded by fiber reinforcing material, said load transfer insert also having a portion therein adjacent one end portion thereof for conducting load transference, such that the laminate reacts compression loads and the fiber reinforcing strip reacts tension loads while reducing loads which would result in edge bearing and shear.

8. The load bearing strut of claim 7 further characterized in that said end section has a shape different than that of said elongate section and having portions which merge into a shape of the elongate section so that the two sections become effectively contiguous.

10. The load bearing strut of claim 7 further characterized in that the entire strut is wound with filament reinforcing material.

11. A process for producing a load bearing strut capable of reacting to tension and compression loads while minimizing shear and edge bearing loads, said process comprising:

a) wrapping a peripheral edge of a preformed member with a filamentary reinforcing material to produce a load transfer insert;

b) locating a load transfer point in an end of an elongate member and with the elongate member and load transfer insert having the overall shape of the strut to be produced;

c) inserting the load transfer insert in proximity to one end of said elongate member; and

d) wrapping filament reinforcing material about said elongate member and said end of the elongate member having the load transfer insert therein to provide a load bearing strut.

12. The process for producing the load bearing strut of claim 11 further characterized in that the insert is somewhat oval shaped and the process comprises wrapping the filament in a somewhat oval pattern.

13. The process for producing the load bearing strut of claim 12 further characterized in that said insert is formed of a quasi-isostropic material.

14. The process for producing a load bearing strut of claim 12 further characterized in that said process comprises inserting said load transfer insert into an end plate secured to an elongate member, and winding filament reinforcing material about said end plate and said elongate portion.

15. A process for forming a composite body on a mandrel in such manner that the mandrel can be removed from the body without any destructive effect on the body, said method comprising:

a) providing components necessary to render a removable mandrel;

b) arranging such components to constitute a mandrel having a shape and size approximating that of the composite body to be formed;

c) applying a resin impregnated composite material to said mandrel and allowing for curing of the resin to provide a hardened composite body; and

d) physically causing removal of said mandrel from said body as formed without any destructive effect on the body.

16. The process for forming a composite body of claim 15 further characterized in that said body is a strut body having an elongate center section and a pair of end sections thereon.

17. The process for forming a composite body of claim 15 wherein said process further comprises:

a) the step of providing components to render a removable mandrel comprises providing a plurality of rigid component parts which are assemblable to render that removable mandrel; and

b) the step of physically causing removal of said mandrel further comprises effectively disassembling the rigid component parts by pulling one of the component parts out of the composite body and thereafter pulling any remaining component parts out of the body of the mandrel.

18. The process for forming a composite body of claim 17 further characterized in that said process further comprises:

a) using at least three component parts forming part of said mandrel and which are stacked together in an arrangement to have a shape similar to the composite body to be formed; and

b) the step of physically causing removal of said mandrel from said body comprises pulling a center component part out of an end of the composite body thus formed, allowing for collapsing of the remaining two component parts and thereafter pulling the remaining two component parts out of an end of the composite body.

19. An assembly for forming a mandrel upon which a composite body having an elongate body section and end section on said elongate body, said assembly comprising:

a) a first mandrel component;

b) a second mandrel component assemblable with said first mandrel component to form a mandrel upon which resin impregnated composite material can be applied;

c) said first and second mandrel components being formed of a material upon which a curing of the resin can take place; and

d) at least said first mandrel component having a transverse end capable of being physically engaged and pulled out of the composite body as formed.

20. The assembly for forming the mandrel of claim 19 further characterized in that said assembly comprises:

a) a third mandrel component assemblable with said first and second mandrel components to form a mandrel upon which the resin impregnated composite material can be applied; and

b) said first mandrel component being located intermediate said second and third mandrel components.

21. The assembly for forming the mandrel of claim 20 further characterized in that said assembly comprises end sections which are attachable to the arrangement of mandrel components as arranged to form the mandrel so that the composite body which is formed will have end sections thereon and where the end plates forming part of the mandrel can thereafter be removed.

22. The assembly for forming the mandrel of claim 20 further characterized in that said composite body is formed on said mandrel by filament winding a resin impregnatable filament strand upon said body.

23. The assembly for forming the mandrel of claim 22 further characterized in that said mandrel components are arranged so that the composite body thus formed thereon will have at least one open end thereon.