Workpiece support

6598866
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Inventors

Helm, Stephen P.
Hoggatt, Brian A.
Moore, Brian

Application #

741911

Filed

Dec-22-2000

Published

Jul-29-2003

Current US Class

029/897.2
269/21
269/266
269/43

International Classes

B25B 011/00

Field of Search

269/21 269/266 269/296 269/297 269/298 269/299 269/300 269/301 269/287 269/43 29/897.2 29/525.06 29/429 29/722 29/407.05 72/60

Assignee

BAE Systems PLC (Farnborough, GB)

Examiners

Hail, III; Joseph J.

Attorney, Agent or Firm

Nixon & Vanderhye P.C.

US Patent References

4381104   Stringer clamp
4527783   Universal contoure...
4894903   Assembly jig and...
4995146   Assembly jig and...
5144825   Elevated temperatu...
5249785   Reconfigurable hol...
5482409   Part positioning an...
5615483   Method of assembli...
6029352   Wing panel assem...

Referenced by:

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Citation

Cite This Patent

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Abstract
A modular workpiece support reconfigurable to support a number of similar, but different profiled workpieces (such as the leading edge skin sections of an aircraft wing) comprises a base 32 defining a number of stations along the component. Each station comprises a clamp block 34, and a frame element 38 of predetermined profile may be clamped in the clamp block in either of two different orientations (for hand and opposite). Each frame element includes a number of suction cups 40, the suction being controlled by a valve 42. The workpiece support may be rapidly reconfigured for a symmetric component simply by unclamping and rotating the frame element through 180.degree.. The workpiece support may also be reconfigured for different profiles by selecting the appropriate frame elements from a library thereof.
 
Claims
What is claimed is:

1. A workpiece support for supporting a workpiece of a given profile, and being reconfigurable to support a workpiece of a different profile, said workpiece support including:

a base means having a plurality of anchorage means at spaced intervals;

a plurality of station frame elements removably secured to said plurality of anchorage means for providing support for a given workpiece over an extended area at spaced stations, and

attachment means associated with each of said station frame elements for securing the workpiece to said workpiece support,

wherein each of said anchorage means permits each respective station frame element to be secured to said base means in either of two different angular working orientations.



Description
BACKGROUND OF THE INVENTION

1. Field of the Invention

This invention relates to workpiece supports for supporting a workpiece and, in particular, but not exclusively, to a workpiece support for supporting a workpiece during a machining or routing operation.

2. Discussion of Prior Art

There are many applications where it is required to support one of a number of workpieces of different profiles during a machining or routing operation. For example, the leading edge skin of a typical commercial aircraft wing is made up of about a dozen sections of the same general shape but of different detailed profile. In an existing proposal, a sheet element is stretch-formed over a stretch-form of the required three-dimensional profile. After this initial forming the component is routed out of the stretch-formed skin. The stretch-forming and routing operations include six different stages as set out in FIGS. 1(a) to (f) of the accompanying drawings. Initially the margins 12 of the skin 10 are clamped in the jaws of a stretch form machine and then stretch-formed around a profile to -give the required shape. At this stage, although the overall profile of the skin is formed, the component itself still needs to be cut out of the stretch-formed skin using e.g. a CNC routing machine, and it is essential that the skin be accurately located prior to the routing operation. Thus in stage 2 the stretch-formed surplus is removed and pilot holes 14 are drilled in the opposite edges of the workpiece 10 which are enlarged to form location or component clamping holes. In stages 3 and 4 the trimmed workpiece 10 is applied to a routing fixture 16 which has a series of manually operated toggle clamps 18 which engage in the component clamping holes 14 and pull the workpiece accurately into alignment on the routing fixture 16. The profile is then routed leaving tags 20. In stage 5 the workpiece 10 is removed from the routing fixture 16, and in stage 6 the component is snipped out of the workpiece 10, detagged and deburred.
 
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