Clamp for clamping a workpiece

Information

  • Patent Grant
  • 6619642
  • Patent Number
    6,619,642
  • Date Filed
    Monday, August 13, 2001
    22 years ago
  • Date Issued
    Tuesday, September 16, 2003
    20 years ago
Abstract
A clamp for clamping a workpiece such as a forging of an aerofoil component comprises a support body 24 to which a clamping member 26 is hinged. The clamping member 26 has a workpiece clamping element 54 having pads 58 for engagement with the workpiece. The workpiece clamping element 54 is pivotable relatively to the clamping member 26 by means of a ball and socket connection including a ball element 40. This enables the workpiece clamping element 54 to self-align with the profile of the workpiece, for example with a surface of the blade 6 of the aerofoil component.In an alterative embodiment, the workpiece clamping element 54 is formed integrally with the clamping member 26, but is connected thereto by a necked region of the clamping member 26 which permits flexure of the workpiece clamping element 54 relatively to the clamping member 26.
Description




FIELD OF THE INVENTION




This invention relates to a clamp for clamping a workpiece, and is particularly, although not exclusively, concerned with a clamp for clamping an aerofoiled component for machining purposes.




BACKGROUND OF THE INVENTION AND PRIOR ART




The secure clamping of aerofoiled components presents difficulties because the aerofoil sections do not have flat, parallel surfaces. Also, aerofoil components formed by forging have dimensional and shape differences from one another which means that a clamping structure shaped to fit perfectly with one component will not fit perfectly with another. Such imperfect fits can result in inadequate clamping and/or marking of the aerofoil surface.




A forged aerofoil component, for example a compressor rotor blade of a gas turbine engine, must undergo various operations after forging in order to remove forging flash and forging locating pips, to form blade edge and root profiles and to tip the blade to the required length. To perform these operations, the component must be held securely while exposing those parts on which the operations are to be performed. Hand polishing, followed by a vibro-polishing operation, is commonly used to form the desired circular profiles of blade chordal edges, but this often results in the chordal edges having flats or facets which, while within engineering tolerances, do not provide optimum aerodynamic performance, resulting in a loss of efficiency of the compressor module. It is thus desirable for the aerofoil finishing operations to be performed by machine, which requires secure fixing of the component while the machining and polishing operations are performed.




An object of the present invention is to provide a clamp which is able to support a workpiece having variable profiles and dimensions.




A further object of the present invention is to provide a clamp with a workpiece clamping element which is pivotable to adapt to the surface profile of a clamped workpiece.




A yet further object of the present invention is to provide a clamp which provides firm support to parts of a component during the performance of machining and polishing operations.




SUMMARY OF THE INVENTION




According to the present invention there is provided a clamp for clamping a workpiece, the clamp comprising:




a support body;




a workpiece supporting element mounted on the support body:




a clamping member mounted on the support body for displacement towards and away from the support body;




a workpiece clamping element mounted on the clamping member;




securing means adapted to retain the clamping member in a clamping position in which, in use, the workpiece clamping element applies a clamping force to a workpiece clamped between the workpiece clamping element and the workpiece supporting element; and




connecting means which connects the workpiece clamping element to the clamping member for pivoting displacement relatively to the clamping member about axes lying in a plane extending transversely of the line of action of the clamping force, and for linear movement relatively to the clamping member in a direction substantially transverse to the line of action of the clamping force, whereby the workpiece clamping element is self-aligning with the surface of a clamped workpiece.




Because the workpiece clamping element is self-aligning, it is able to adapt to variations in surface profile and dimensions of the clamped workpiece, for example a forged aerofoil component.




The pivoting displacement of the workpiece clamping element may be limited, for example by contact between the workpiece clamping element and the clamping member.




In one embodiment in accordance with the present invention, the pivoting displacement is achieved by means of a ball and socket connection. The ball and socket connection may comprise a part-spherical ball element mounted on the clamping member, which engages a socket formed in the workpiece clamping element. Separate means, for example a transverse pin, may be provided to retain the workpiece clamping element on the clamping member.




Resilient means may be provided for biasing the workpiece clamping element into engagement with a face of the workpiece, the biasing force extending transversely of the line of action of the clamping force.




In an alternative embodiment, the pivoting displacement of the workpiece clamping element may be provided by connecting the workpiece clamping element to the clamping member by means of a resilient connecting element. This connecting element may comprise a necked region between the clamping member and the workpiece clamping element, the clamping member, the necked region and the workpiece clamping element then being integral with each other. The connecting element may be situated generally centrally of the workpiece clamping element.




Around the connecting element, the workpiece clamping element may be separated from the clamping member by machined slots, closure of the slots upon deflection of the workpiece clamping element limiting the extent of displacement of the workpiece clamping element relatively to the clamping member.




The clamp may include at least one locating element, spaced from the workpiece supporting element and the workpiece clamping element, for engagement with a surface profile of the workpiece to locate the workpiece within the clamp. The locating element may comprise a recess for receiving a protrusion or pip on the workpiece.




The support body may be mounted on a fixture for removable fitting to a machine tool or other workpiece processing equipment.











BRIEF DESCRIPTION OF THE DRAWINGS




For a better understanding of the present invention, and to show how it may be carried into effect, reference will now be made, by way of example, to the accompanying drawings, in which:





FIG. 1

shows a forged workpiece in the form of an aerofoil component;





FIG. 2

is a partly sectioned side view of a clamp holding the component of

FIG. 1

;





FIG. 3

is an enlarged sectional view of part of the clamp indicated by an arrow III in

FIG. 2

;





FIG. 4

is a view taken in the direction of the arrow IV in

FIG. 3

;





FIG. 5

is a sectioned side view of another clamp holding the aerofoil component of

FIG. 1

, following processing in the clamp of

FIG. 2

;





FIG. 6

is a view taken generally on line VI—VI in

FIG. 5

;





FIG. 7

is a top view of the clamp shown in

FIG. 5

, with the clamping member omitted; and





FIG. 8

is a partially sectioned view corresponding to FIG.


5


.











DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS




The workpiece


2


shown in

FIG. 1

comprises an aerofoil component


4


having a blade


6


and a root


8


. The component


4


is surrounded by a region of forging flash


10


. The forging flash


10


has a tip end


14


, a tip location pip


16


and a root location pip


18


.




The workpiece


2


must undergo several operations in order to finish the aerofoil component


4


. Thus, the forging flash


10


must be removed, along with the location pips


16


an


18


, the root


8


must be machined to a desired configuration, and the blade


6


must have its chordal edges


20


and tip


24


machined to the required dimensions and profiles.




To perform these operations, the aerofoil component must be clamped firmly so that it is prevented from moving under the machining forces. This clamping is achieved by means of the clamps shown in

FIGS. 2

to


4


, and

FIGS. 5

to


8


. The clamp shown in

FIGS. 2

to


4


is employed to hold the workpiece during finishing of the blade chordal edges


20


, while the clamp shown in

FIGS. 5

to


8


is employed during machining of the root


8


.




Referring first to the clamp shown in

FIGS. 2

to


4


, this comprises a support body


124


to which a clamping member


126


is hinged for movement about a hinge axis


128


. The support body


124


is secured to an EROWA base fixing


130


having a spigot


132


for releasable fitment to, for example, a machine tool for performing operations on the workpiece


2


.




The support body


124


has a workpiece supporting element


134


which is formed integrally with the support body


124


. The clamping member


126


has a workpiece clamping element


138


which is formed integrally with the clamping member


126


. The connection between the clamping member


126


and the workpiece clamping element


138


is shown more clearly in FIG.


5


. The clamping member


126


at its end region adjacent the workpiece clamping element


138


has a generally rectangular cross-section. Slots


140


having a relatively narrow outer region


142


(having a width, for example, of 0.25 mm) and a wider inner region


144


(having a width, for example, of 0.5 mm) extend inwardly from all four sides of the clamping member


126


, leaving a central connecting element or pillar


146


connecting the clamping member


126


to the workpiece clamping element


138


. This pillar may, for example, have a cross-sectional area which is not greater than 20 mm


2


, for example it may have a square cross-section with a side of 4 mm.




The slots


140


may be formed by electrical discharge wire cutting.




The slots


140


permit resilient pivoting of the workpiece clamping element


138


about the pillar


146


. The pivoting movement is limited by closure of the narrow regions


142


of the slots


140


, so that the maximum pivoting angle of the workpiece clamping element


138


is not greater than 2°, for example it may be 1.5°.




The workpiece clamping element


138


and the workpiece supporting element


134


each have two pads


158


and


160


respectively, for engagement with the blade


6


of an aerofoil component


2


. Each pad


158


extends the full length of the respective workpiece supporting element


134


and workpiece clamping element


138


, and engages the component


2


close to the respective chordal edge of the blade


6


.




A stud


162


is secured to the support body


124


and extends through an opening


164


in the clamping member


126


. A nut


166


engages the top end of the stud


162


and can be tightened to exert the required clamping force between the workpiece supporting element


134


and the workpiece clamping element


138


.




The support body has two locating elements


168


and


170


, which are spring-loaded upwardly, as seen in

FIG. 4

, by means of springs


172


and


174


. The locating elements


168


and


170


have V-shaped recesses


176


and


178


at their upper ends, which, in use, receive the locating pips


18


and


16


of the aerofoil component (FIG.


1


).




A spring-loaded domed platform location pin


180


is provided in the workpiece supporting element


134


for abutment with the annulus surface of the root


8


from which the blade


6


extends. Although not shown, a separate clamping device may be provided for retaining the tip pip


16


in the locating recess


178


.




For use, as shown in

FIG. 4

, the aerofoil component


2


is positioned on the workpiece supporting element


134


and located by engagement of the locating pips


16


and


18


in the recesses


176


and


178


. The position of the workpiece


4


in the lengthwise direction of the blade


6


is established by the location pin


180


. The clamping member


126


is then lowered to bring the workpiece clamping element


138


into engagement with the upper side of the blade


6


, and the nut


166


is tightened to clamp the blade


6


between the workpiece supporting element


134


and the workpiece clamping element


138


. Variations in the profile and dimensions of the blade


6


are accommodated by flexure of the pillar


146


, allowing the workpiece clamping element


138


to align itself with the profile of the upper surface of the blade


6


. When the workpiece


2


is clamped, machining, profiling and polishing of the blade chordal edges can be performed. While in the clamp of

FIGS. 2

to


4


, the blade


6


may be tipped to length, and the locating pip


16


removed. However, it is alternatively possible for this operation to be performed separately.




The workpiece


2


is then transferred to the clamp shown in

FIGS. 5

to


8


, which comprises a support body


24


to which a clamping member


26


is hinged for movement about a hinge axis


28


. The support body


24


and the clamping member


26


are formed from aluminium. The support body


24


is secured to an EROWA base fixing


30


having a spigot


32


for releasable fitment to, for example, a machine tool for performing operations on the workpiece


2


.




The support body


24


has a steel workpiece supporting element


34


secured to it by means of machine screws


36


. The clamping member


26


has a steel workpiece clamping element


38


which is located relatively to the clamping member


26


by means of a ball and socket connection comprising a part-spherical ball element


40


cooperating with a hardened hemi-spherical recess


42


(

FIG. 6

) formed in the workpiece clamping element


38


. The ball element


40


is secured to the clamping member


26


by a machine screw


44


, in such a way that there is limited freedom of movement of the ball element


40


in the general direction towards and away from the root


8


of the clamped aerofoil component


2


.




It will be appreciated that the ball element


40


does not retain the workpiece clamping element


38


on the clamping member


26


. This function is performed by a pin


46


which is secured within the clamping member


26


by a grub screw


48


. The pin


46


extends with a clearance through a bore


50


formed in the clamping element


38


.




The clearance between the pin


46


and the bore


50


, and the freedom of movement of the ball element


40


, permit limited pivotal displacement of the workpiece clamping element


38


relatively to the clamping member


26


about the axes defined by the ball element


40


, as well as limited linear displacement.




A spring


52


acts between the clamping member


26


and the workpiece clamping element


38


to bias the workpiece clamping element


38


in a direction which is generally transverse of the line of action of the clamping force exerted by the workpiece clamping element


38


in the direction of the workpiece supporting element


34


. Thus, with reference to

FIG. 2

, the workpiece clamping element


38


is biased towards the annular surface of the root


8


of the aerofoil component


4


shown clamped between the workpiece supporting element


34


and the workpiece clamping element


38


. This brings a hardened support pad


54


, provided on the workpiece clamping element


38


, into contact with the annulus surface of the root


8


from which the blade


6


extends. A similar hardened pad


56


is provided on the workpiece supporting element


34


.




The ball element


40


has a flat guide surface


70


which engages a complementary surface


72


formed on the clamping member


26


. The surface


72


, as shown in

FIG. 2

, is slightly angularly offset (for example by 3°) from the plane extending perpendicular to the line of action of the clamping force exerted by the clamping member


26


. The result of this is that the clamping force applies a wedging action on the workpiece clamping element


38


so assisting the spring


52


in biasing the workpiece clamping element


38


into contact, via the pad


54


, with the annulus surface of the root


8


of the workpiece


2


.




The workpiece clamping element


38


and the workpiece supporting element


34


each have four hardened blade-engaging pads, with two adjacent each chordal edge of the blade


6


, as shown in FIG.


6


. These pads are plated with cubic boron nitride (CBN) that serves to prevent slip between the pads


158


and


160


and the blade


6


.




A pair of jaws


182


,


184


are secured to the workpiece supporting element


34


. The jaw


182


is a fixed jaw and is rigidly fixed to the workpiece supporting element


34


by screws


186


. The jaw


184


is a movable jaw and is retained on the workpiece supporting element


34


by screws


188


. There is a clearance between these screws


188


and the holes in the movable jaw


184


in which they are received, which permits limited movement of the movable jaw


184


towards and away from the fixed jaw


182


. The movable jaw


184


is biased towards the fixed jaw


182


by means of a leaf spring


190


which is fixed at one end to the workpiece supporting element


34


and bears resiliently at its other end on a side face of the movable jaw


184


.




A retaining bar


192


is resiliently mounted on the support body


24


. The bar


192


extends from a journal


194


which is pivotably mounted on the support body


24


by bearings


196


. An operating lever


198


depends from the journal


194


and is acted upon by a spring


200


.




To install the workpiece


2


in the clamp shown in

FIGS. 5

to


8


, the bar


192


is raised and the blade


6


is laid under it on to the pads


60


on the workpiece supporting element


34


. To assist this, the jaw


184


is displaced away from the jaw


182


, and, when released, is moved by the leaf spring


190


to engage the adjacent chordal edge


20


of the blade


6


to push the blade


6


into contact, at the opposite chordal edge, with the fixed jaw


182


. The bar


192


is released, and is biased by the spring


200


, acting through the lever


198


, to contact the upper edge of the blade


6


so as to provide a preliminary holding force on the workpiece


2


. The workpiece clamping element


38


is then lowered to bring the pads


58


into contact with the upper surface of the blade, these pads straddling the bar


192


.




A stud


62


is secured to the support body


24


and extends through an opening


64


in the clamping member


26


. A nut


66


engages the top end of the stud


62


and can be tightened to exert the required clamping force between the workpiece supporting element


34


and the workpiece clamping element


38


.




As shown in

FIGS. 5 and 6

, the forged workpiece of

FIG. 1

is held by the clamp with the root


8


exposed for machining. Thus the pads


58


on the workpiece clamping element


38


and the pads


60


on the workpiece supporting element


34


engage opposite faces of the blade


6


and grip the blade


6


firmly under the action of the nut


66


on the stud


62


. During clamping, the ball and socket connection provided by the ball element


40


and the hemi-spherical socket


42


permit the pads


58


on the workpiece supporting element


38


to align themselves with the contacted surface of the blade


6


so that an adequate clamping pressure can be applied to the blade


6


without marking it. The CBN plating on the pads


58


and


60


avoids slippage of the blade


6


so that the workpiece


2


will remain held securely during machining operations on the root


8


. Additional support is provided by the pads


54


and


56


. When installing the workpiece in the clamp, the annulus surface of the root


8


is abutted against the pad


56


on the fixed workpiece supporting element


34


, the workpiece clamping element


38


then being biased by the spring


52


and the wedging action of the surfaces


70


and


72


to bring the pad


54


into abutment with the annulus surface.




The workpiece supporting element


34


has a recess


68


to accommodate the tip locating pip


16


if it has not been removed in a previous operation.




It will be appreciated that various modifications can be made to the clamps shown in

FIGS. 2

to


8


to suit particular applications. For example, although four pads are shown on each of the workpiece clamping elements


38


,


138


and the workpiece supporting elements


34


,


134


, satisfactory results may be achieved with, for example, three pads on each element.




Also, a single support body


24


,


124


could be provided with separate workpiece supporting elements


34


,


134


and corresponding separate clamping members


26


,


126


so that a workpiece can be re-positioned on the same fixture to present appropriate parts of the workpiece for machining at different stages of operation.



Claims
  • 1. A clamp for clamping a workpiece, the clamp comprising:a support body; a workpiece supporting element mounted on the support body: a clamping member mounted on the support body for displacement towards and away from the support body; a workpiece clamping element mounted on the clamping member; securing means adapted to retain the clamping member in a clamping position in which, in use, the workpiece clamping element applies a clamping force to a workpiece clamped between the workpiece clamping element and the workpiece supporting element; connecting means which connects the workpiece clamping element to the clamping member for pivoting displacement relatively to the clamping member about axes lying in a plane extending transversely of the line of action of the clamping force, and for linear movement relatively to the clamping member in a direction substantially transverse to the line of action of the clamping force, whereby the workpiece clamping element is self-aligning with the surface of a clamped workpiece, the connecting means having a ball and socket connection which includes a part-spherical ball element mounted on the clamping member and a socket formed in the workpiece clamping element, the part-spherical ball element engaging the socket; and a retaining pin which engages the workpiece clamping member and which extends with clearance through a bore in the workpiece clamping element for retaining the workpiece clamping element on the workpiece clamping member.
  • 2. A clamp as claimed in claim 1, in which the pivoting displacement of the workpiece clamping element is limited by contact between the workpiece clamping element and the clamping member.
  • 3. A clamp as claimed in claim 1, in which the clamping member is hinged to the support body.
  • 4. A clamp as claimed in claim 1, in which resilient means is provided for biasing the workpiece clamping element relatively to the clamping member in the direction of linear movement.
  • 5. A clamp as claimed in claim 4, in which the workpiece clamping element has an abutment face for engagement with a surface of a workpiece under the action of the resilient means.
  • 6. A clamp as claimed in claim 5, in which the workpiece supporting element has an abutment face for engagement with a surface of a workpiece, the abutment face of the workpiece supporting element being fixed with respect to the workpiece supporting member.
  • 7. A clamp as claimed in claim 1, in which the support body is on a fixture which is adapted for releasable fitting to a machine tool.
  • 8. A clamp as claimed in claim 1, which is adapted to receive a workpiece in the form of an aerofoil component.
  • 9. A clamp for clamping a workpiece, the clamp comprising:a support body; a workpiece supporting element mounted on the support body: a clamping member mounted on the support body for displacement towards and away from the support body; a workpiece clamping element mounted on the clamping member; securing means adapted to retain the clamping member in a clamping position in which, in use, the workpiece clamping element applies a clamping force to a workpiece clamped between the workpiece clamping element and the workpiece supporting element; and connecting means which connects the workpiece clamping element to the clamping member for pivoting displacement relatively to the clamping member about axes lying in a plane extending transversely of the line of action of the clamping force, the connecting means comprising a necked region formed integrally with and extending between the clamping member and the workpiece clamping element, the workpiece clamping element projecting on all sides beyond the necked region, whereby the workpiece clamping element is self-aligning with the surface of a clamped workpiece.
  • 10. A clamp as claimed in claim 9, in which the pivoting displacement of the workpiece clamping element is limited by contact between the workpiece clamping element and the clamping member.
  • 11. A clamp as claimed in claim 9, in which the clamping member is hinged to the support body.
  • 12. A clamp as claimed in claim 9, in which the necked region is defined by slots extending inwardly from the outer surface of the clamping member.
  • 13. A clamp as claimed in claim 9, in which each slot has a width which is not greater than 0.5 mm.
  • 14. A clamp as claimed in claim 9, in which the cross-sectional area of the necked region is not greater than 20 mm2.
  • 15. A clamp as claimed in claim 9, in which the maximum pivoting angle of the workpiece clamping element relatively to the workpiece clamping member is not greater than 2°.
  • 16. A clamp as claimed in claim 9, in which the support body comprises a locating element which is spaced from the workpiece supporting element, which locating element is adapted to engage a region of the workpiece to locate the workpiece on the support body.
  • 17. A clamp as claimed in claim 16, in which the locating element comprises a recess adapted to receive a protrusion on the workpiece.
  • 18. A clamp as claimed in claim 9, in which the support body is mounted on a fixture which is adapted for releasable fitting to a machine tool.
  • 19. A clamp as claimed in claim 9, which is adapted to receive a workpiece in the form of an aerofoil component.
  • 20. A method of performing operations on a workpiece, which method comprises:securing the workpiece in a clamp comprising: a support body; a workpiece supporting element mounted on the support body: a clamping member mounted on the support body for displacement towards and away from the support body; a workpiece clamping element mounted on the clamping member; securing means adapted to retain the clamping member in a clamping position in which the workpiece clamping element applies a clamping force to the workpiece clamped between the workpiece clamping element and the workpiece supporting element; and connecting means which connects the workpiece clamping element to the clamping member for pivoting displacement relatively to the clamping member about axes lying in a plane extending transversely of the line of action of the clamping force, and for linear movement relatively to the clamping member in a direction substantially transverse to the line of action of the clamping force, whereby the workpiece clamping element is self-aligning with the surface of a clamped workpiece, the connecting means having a ball and socket connection which includes a part-spherical ball element mounted on the clamping member and a socket formed in the workpiece clamping element, the part-spherical ball element engaging the socket: and a retaining pin which engages the workpiece clamping member and which extends with clearance through a bore in the workpiece clamping element for retaining the workpiece clamping element on the workpiece clamping member; and performing the operation on the clamped workpiece.
  • 21. A method of performing operations on a workpiece, which method comprises:securing the workpiece in a clamp comprising: a support body; a workpiece supporting element mounted on the support body: a clamping member mounted on the support body for displacement towards and away from the support body; a workpiece clamping element mounted on the clamping member; securing means adapted to retain the clamping member in a clamping position in which the workpiece clamping element applies a clamping force to the workpiece clamped between the workpiece clamping element and the workpiece supporting element; and connecting means which connects the workpiece clamping element to the clamping member for pivoting displacement relatively to the clamping member about axes lying in a plane extending transversely of the line of action of the clamping force, the connecting means comprising a necked region formed integrally with and extending between the clamping member and the workpiece clamping element, the workpiece clamping element projecting on all sides beyond the necked region, whereby the workpiece clamping element aligns with the surface of the clamped workpiece; and performing the operations on the clamped workpiece.
Priority Claims (1)
Number Date Country Kind
0020220 Aug 2000 GB
US Referenced Citations (6)
Number Name Date Kind
661322 Ranz Nov 1900 A
999979 Fisher Aug 1911 A
3495867 Avery Feb 1970 A
4240621 Daddato Dec 1980 A
4623157 Rohs Nov 1986 A
4632375 Yang Dec 1986 A
Foreign Referenced Citations (2)
Number Date Country
0 739 683 Oct 1996 EP
1 289 541 Mar 1970 GB