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Publication numberUS3803898 A
Publication typeGrant
Publication dateApr 16, 1974
Filing dateAug 2, 1972
Priority dateAug 2, 1972
Publication numberUS 3803898 A, US 3803898A, US-A-3803898, US3803898 A, US3803898A
InventorsE Speakman
Original AssigneeMc Donnell Douglas Corp
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Ring pad stress coining tooling
US 3803898 A
Abstract
Tools to plastically deform a portion of a structural member into one or a pair of flat bottomed grooves to generate residual compressive stresses in the member adjacent a discontinuity therein which improve the fatigue strength of the structural member.
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Description  (OCR text may contain errors)

United States Patent [1 1 Speakman RING PAD STRESS COINING TOOLING [75] Inventor: Eugene R. Speakman, Fullerton,

Calif.

[73] Assignee: McDonell Douglas Corporation,

Santa Monica, Calif.

[22] Filed: Aug. 2, 1972 [21] Appl. No.: 277,358

[52] US. Cl 72/416, 72/446, 72/470 [51] Int. Cl B2ld 37/10 [58] Field of Search 72/377, 416, 470, 446, 72/476; 29/155 R, 155 C, 457, 446; 113/1 F,

[56] References Cited UNITED STATES PATENTS 2,760,263 8/1956 Geertsen 72/377 Apr. 16, 1974 3,041,989 7/1962 Tanner 72/476 3,406,555 10/1968 Fuchs 72/377 3,355,930 12/1967 Fedorov 72/377 Primary Examiner-Charles W. Lanham Assistant Examiner-Robert M. Rogers Attorney, Agent, or Firm-George W. Finch; Walter J. Jason; Donald L. Royer [5 7] ABSTRACT Tools to plastically deform a portion of a structural member into one or a pair of flat bottomed grooves to generate residual compressive stresses in the member adjacent a discontinuity therein which improve the fatigue strength of the structural member.

7 Claims, 7 Drawing Figures 'PNENTEUAPR 16 I974 I 31303898 sum 1 or 2 HE, E

RING PAD STRESS COINING TOOLING CROSS REFERENCE TO RELATED PATENTS This application relates to the subject matter of U. S. Pat. No. 3,110,086 entitled Coining Structural Parts by Austin Phillips and U. S. Pat. No. 3,434,327 entitled Stress Coining by Eugene R. Speakman. Reference is made to the information therein as though fully set forth hereinbelow.

BACKGROUND OF THE INVENTION the strengths for such parts under static load is insuffi-.

cient to enable design of such parts when they are expected to be subjected tofluctuating loads. This is because such parts tend to fail in fatigue even though the stress approaching the ultimate breaking load is normally never experienced in actual service. Ring groove and pad coining methods for improving the fatigue strength of parts having apertures therethrough are shown in the referenced patents. Both of the patents disclose means which establish a field of residual compressive stress about the aperture, which stress tends to measurably increase the fatigue life of the part. Unfortunately, both methods have disadvantages that preclude their universal use. For example, the ring groove coining 'method, as disclosed in U.S. Pat. No. 3,110,086, when used on materials below 0.065 inch thickness, tends to generate an internal shear crack in the grooved area which is unacceptable. Also, precise control of the depth of the groove is important in the ring groove method since a shallow groove results in less than optimum fatigue improvement and a deep groove can result in a doughnut-shaped punch out. In the production situation, the desired way to control the depth of the groove is by controlling the force applied to the grooving die. However, because of the shape of the dies, the groove depth can vary greatly with the same applied force. In the pad coining method disclosed in U.S. Pat. No. 3,434,327, the pilots from each die contact each other preventing coining of material in thicknesses below 0.090 inch. At the same time a substantial amount of material adjacent the aperture is plastically deformed so the aperture closes up, sometimes seizing the die pilots in the aperture. As a result, the pilots must be made undersize to compensate for aperture closure. It is therefore difficult to assure that the pad coining is concentric with the aperture. Also both prior art coining methods require extremely high force levels, especially when the material being coined is steel or titanium. The high force levels effectively eliminate the use of portable tools, which means that retrofit or repair of -a part requires its removal to a shop area.

In modern aircraft which are of fail-safe design, it is conventional practice to use thin sacrificial doublers for the attachment of leading edges or access doors to the structuralv spar cap flanges which support them. The sacrificial doublers are attached at one edge to the spar cap flanges with interference attachments to assure an adequate fatigue life for the spar cap flanges. The op-' posite edges of the doublers include clearance holes and adjacent floating nut plates to enable easy attachment of the leading edge or access doors to the doublers Since the doublers are attached to the spar cap with interference attachments, the same stress levels present in the spar cap flanges are also present in the doublers. The uncoined clearance holes in such doublers have a very low fatigue life and cracks result in a relatively short service time. Although a crack in a doubler is of secondary importance because it cannot cause a disasterous primary failure, the cracks are bothersome and expensive since their existence requires regular replacement of the doublers based on relatively few flight hours for the aircraft. Therefore, means for increasing the fatigue life of such doublers which tend to be relatively thin have been required.

SUMMARY OF THE INVENTION The present ring pad stress coining method was developed to fill the gaps in the prior art fatigue strength improvement methods with aluminum, steel and titanium from one-half inch thick down to foil gauges being of primary interest. The method is comprised of plastically compressing a substantially flat bottomed ring. of material in one or both side surfaces of a part generally concentric with an aperture or discontinuity in the part. The tooling to perform the ring pad coining has a die surface which includes a flat portion with adjacent curved edge portions. This shape provides a relatively and the part which enables relatively precise depth control by control of the force applied thereto. The total depth required to generate the desired volume of residual compression stress and to provide the desired fatigue strength is reduced by such shape so that usually the total coining force can be generated by means of portable tools. The tooling can also include a resilient pilot which assures the coined ring pad is maintained concentric with the aperture it surrounds. The pilot retracts as the die is brought into engagement with the workpiece so the pilot never is locked in the aperture by the plastic deformation of the material around the aperture.

It is therefore the object of the present invention to provide means for improving the fatigue strength of relatively thin structural parts having apertures therein.

Another object of the present invention is to provide a ring pad stress coining tool which is easy to use.

Another object is to provide means for improving the fatigue strength of a metal part quickly and economically.

Another object is to provide ring pad stress coining tooling which can be used with conventional portable production equipment to improve the fatigue strength ofmetal parts having apertures therethrough.

Another object is to provide means for improving the expected fatigue life of used parts having apertures therethrough or for restoring fatigue strength to apertured parts in which failures have started to occur.

Another, object is to provide means for forming a controlled concentric groove to generate a region of residual compressive stress about the periphery of an aperture in a structural member to improve the fatigue strength of the structural member.

These and other objects and advantages of the present invention will become apparent after considering the following detailed specification which covers preferred embodiments thereof in conjunction with the accompanying drawings.

BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is an exploded pictorial view showing apparatus to provide ring pad stress coining;

FIG. 2 is a partial cross-sectional view of ring pad stress coining tooling after ring pad coining a workpiece;

FIG. 3 is an enlarged cross-sectional view showing the shaping details of a typical ring pad stress coining die in engagement with a workpiece;

FIG. 4 is a view depicting a stress pattern of an apertured and ring pad coined structural member showing lines of stress therein;

FIG. 5 is a perspective view of the workpiece of FIG. 2 after a ring pad coining operation, the workpiece being shown with a floating nut plate riveted thereto;

FIG. 6 is a partial cross-sectional view of a ring pad stress coining tool for coining a conical structural member; and

FIG. 7 is a partial cross-sectional view of the tool of FIG. 6 in use.

DESCRIPTION OF THE SHOWN EMBODIMENTS Referring to the drawings more particularlyby reference numbers, number 10 in FIG. 1 refers to a ring pad coining tool for performing ring pad coining according to the present invention. The tool 10 includes a ring pad coining die 12 having a resilient pilot 14 mounted centrally therein. Attachment means 16 are provided on the opposite end of the tool 10 from the die 12 to provide means for attaching the tool 10 to suitable force applying means which are shown symbolically in FIG. 1 by cylinders 18 and 20. The force applying means may be any of a widely known group of tools including a rivet gun in which case the cylinder 20 represents a bucking member, and a C-clamp type squeezer in which case a second coining tool 22 may be connected by its attachment means 24 to the cylinder 20. If used, the tool 22 has a coining die 26 similar to die 12 but lacks a pilot member since C-clamp type squeezers act to maintain the dies 12 and 26 in axial and perpendicular alignment. The pilot 14 of the tool 10 is used to assure the proper concentric alignment of the dies 12 and 26 with the aperture 28 in the workpiece 30 in which the coining is to take place. FIG. 2 shows this axial and perpendicular alignment more clearly.

Before coining, the aperture 28 is usually prepared by having its edges broken about 0.010 t 0.005 inch at 45 fl. This results in frustroconical surfaces 32, one of which engages the pilot 14 as the tool 10 is brought against the workpiece 30. If multiple layers of material are being coined simultaneously, the frustroconical surfaces 32 need only be formed at the outer surfaces of the apertures through the stackup.

The pilot 14 includes a rounded frustroconical end portion 34 which acts as the guiding surface and a cylindrical portion 36 which rides on an inner circumferential surface 38 of the die 12. The pilot 14 as aforesaid is resiliently mounted to the die 12 and such mounting means are shown as a spring 40 which extends into apertures 42 and 44 in the pilot l4 and the die 12 respectively. The diameter of the spring 40 is chosen so that it frictionally and resiliently engages the surfaces of the apertures 42 and 44, thereby retaining the pilot 14 to the tool 10. Once the pilot 14 has engaged the break 32 of the aperture 28, it retracts as the die 12 is forced into engagement with the workpiece 30, thereby assuring that the die 12 is concentric with the aperture 28.

As show-n in FIG. 3, the die 12, which is doughnutshaped, has a coining surface 46 comprised of first and second radius portions 48 and 50 of a predetermined radius 52 with a flat portion 54 therebetween. The relative dimensions of the radius 52 and the flat portion 54 are shown in Table I for tools for coining holes of the indicated size. The optional die 26 has a similar die surface 56.

TABLE I Hole diameter D out D in F R to coin .l80-.229 .462 .2750 .033 .030 .230-.29l .523 .3370 .033 .030 .292-.354 .586 .4000 .033 .030 .355-.4l6 .648 .4620 .033 .030

When the dies 12 and 26 are constructed, great care is used to assure that the surfaces 46 and 56 thereof are given a mirror finish since any irregularity in the die surface results in a degradation of optimal levels of fatigue strength improvement. It is then usual to further assure that the surfaces 46 and 56 are smooth by chrome plating them. When in use, the die surfaces 46 and 56 are also protected by applying heavy cutting oil metal-working lubricant such as Pems 300 manufactured by Pemco Inc., Los Angeles, California, so the die surfaces 46 and 56 are not galled or otherwise damaged when they are forced into the workpiece during the coining operation. The lubricant also reduces the friction between the dies 12 and 26 and the workpiece 30 so the temperature of the workpiece 30 is not raised substantially. Excessive heating is undesirable because it causes reduction of the residual compressive stress which must remain in the workpiece 30 to improve its fatigue strength. The lubricant also assures a more consistent result when the force applied to the dies 12 and 26 is the regulated force to control the depth of penetration of the dies to form the depressed ring pad.

The groove or grooves generated by the tool 10 and when employed, the tool 22, follow the shape of the coining dies 12 and 26 so a concentric ring 58 or rings 58 and 60 having flat bottoms 62 and 64 with curved edge portions 66 result when the tools 10 and 22 are forced into the workpiece 30. This is because the dies 12 and 26 are driven with sufficient force to plastically deform the workpiece 30. As a rule of thumb, the amount of plastic deformation should equal the elastic deformation so the average workpiece rebound is onehalf the total elastic and plastic deformation. The described shape of ring pad grooves has proved to be advantageous especially in thin gauges of material since it produces the desired residual compressive stress which is shown diagrammatically by the vector arrows 68 and 70 in FIG. 3. As can be seen, the present method results in two general types of induced compressive stress. The stress represented by arrows 68 is internal surface to surface compressive stress akin to the stress generated by the prior art pad coining method while the stress represented by arrows 70 is radial and circumferencial stress akin to the stress generated by the prior art ring groove coining method. It is the combined residual compressive stresses created by the present stress coining method which provides greatly improved fatigue strength for thin workpieces 30 having apertures 28 therethrough.

A possible explanation of the fatigue strength improvement is shown in FIG. 4 which is a stress diagram of the workpiece 30 having an aperture 28 about which the ring pad coining operation has been performed.

Stress lines 72 depict the stress pattern of the workpiece 30 showing the effect of the ring padstress coin.-

ing operation. It should be noted that the lines of stress 72 do not converge on the aperture but seem to be fenced out instead tending to flow around the aperture similar to an aerodynamic flow pattern. In open noncoined holes, the lines of stress t end to converge toward the center of the aperture 28 to concentrate 'tests had an R factor equal to +2, that is, the stresses were cycled from percent to the indicated load.

T A B L E 11 Material Ring Pad Depth Coining Cycles & Load to Thickness Reqd Actual, (lbs) Failure .010 667,000 "No Failure As can be seen from Table 11, the actual depth of the coined ring pad varied little with a given coining force. This proved coining force is an acceptacle way to control the present method. The novel shape of the coining dies 12 and 26 makes control by force control practical. This is because the flat portion 54 causes high force resistive levels within the workpiece 30 which tend to limit further penetration by the die 12 and the curved also tending to limit the depth of penetration of the coining die.

Since the required amount of force applied to the tool 10 to obtain'the desired penetration and thereby the depth of the coined pad depends in large measure upon the material to be coined and the treatments that the material may have sustained, it is usual practice when coining a new type of production part to make a test specimen setup using the same hole size, thickness, alloy and temper as for the production part. What is thought to be the correct force is then applied to the die or dies across the specimen and the depth of the ring pad groove is measured. Final force adjustments are then made as necessary to establish the required coin depth. Once set up, the coining tool 10 can be used to coin the production parts and the coining can be quality assured very simply by merely measuring the depth and observing the smoothness and symmetry of the ring pad groove. The depth of the groove can be directly related to the amount of fatigue strength improvement while smoothness and symmetry are a measure of the care taken during the coining operation. When a rivet gun and bucking member are used to coin only one side of a workpiece, it is usual practice to use a rivet gun with an unrestricted air inlet and full air line pressure and then apply enough blows to obtain the required depth of the ring pad groove.

FIG. 5 shows a typical application of the present ring pad coining method wherein a floating nut plate 74 is attached by rivets 76 and 78 to the coined workpiece 30 behind the aperture 28. In such an application it is extremely convenient that the present method can be employed closely adjacent to the aperture 28 so that a standard floating nut plate 74 can be used and so the rivets 76 and 78 located as shown do not interfer with the groove 60 or 58.

FIGS. 6 and 7 show a ring pad coining tool 80 of a modified form which was developed to improve the fatigue strength about cooling apertures 82 in jet engine bearing sumps 84. The sump 84 includes a conical section 86 through which the apertures 82 extend. The tool 80 is comprised of a pair of stress coining dies 88 and 90, the die 88 being threadably mountable to a shaft 92 while the die 90 is slidably mountable thereon. The die surfaces 94 and 96 of the dies 88 and 90 respectively, have a cross-sectional shape like that shown in FIG. 3 for tool but the die surfaces 94 and 96 are curved as shown by the radii 98 and 100 to correspond generally to the conical surfaces of the sump 84 about the cooling apertures 82. A pilot member 102 is provided between the dies 88 and 90 to assure that when the die surfaces 94 and 96 contact the sump 84, they are generally concentric with the cooling aperture 82. The pilot member 102 is also slidably mountable on the shaft 92.

To use the tool 80, the die 90 and the pilot member 102 are mounted on the shaft 92. The shaft 92 is then extended from the outside of the sump 84 through one of the cooling apertures 82 and the die 88 is threaded onto the end of the shaft 92 with the pilot member 102 in engagement with the aperture wall 103 to properly position the tool 80 with respect to the aperture 82. Indicator means such as marks 104 and 105 and wrench flats 106 and 107 are provided on the dies 88 and 90 so the dies can be aligned with each other and with the sump 84 by using a U-shaped double end wrench 108. This assures the curvatures of the die surfaces 94 and 96 correspond to the curvatures of the sump 84. The shaft 92 also includes means 109 for engaging a pulling tool. By applying a predetennined force with the pulling tool between the shaft 92 and an abutment surface 110 on the die 90 in the directions shown by arrows 112 and 114, the desired plastic deformation of the su'mp 84 is accomplished to create the aforesaid residual compressive stresses about the aperture 82. The tool 80 is removed by releasing the force and disengaging the die 88 from the shaft 92. Fatigue tests on sample specimens have shown that use of the tool 80 greatly increases the fatigue strength of sumps 84, the fatigue tests being performed at over 600F which is the normal maximum operating temperature for bearing sumps such as sump 84.

Thus, there have been shown and described novel tools for increasing the fatigue strength of workpieces having discontinuities therein which fulfill all the objects and advantages sought before. Many changes, modifications, variations and other usesand applications of the subject invention will, however, become apparent to those skilled in the art after considering this specification and the accompanying drawings. All such changes, modifications, alterations and other uses and applications which do not depart from the spirit and scope of the invention are deemed to be covered by the invention which is limited only by the claims which follow.

What is claimed is:

l. Tooling for improving the fatigue strength of a structural member having first and second surfaces and a discontinuity in at least said first surface, said tooling including:

a first die member having a ring shaped die surface for engagement and deformation of the first surface of the structural member and means adapted to engage means for driving said die surface into the first surface, said die surface having a crosssection which includes a linear section generally perpendicular to the direction said die surface is driven and curved sections on opposite sides of said linear section extending from tangents thereto;

a pilot member adapted to engage the discontinuity and to space said die surface therefrom; and

means connecting said pilot member to said first die member whereby said pilot member can move with I respect to said die member.

2. The tooling defined in claim 1 wherein said pilot member has a frustro-conical portion for engaging the discontinuity and a cylindrical portion, said first die member having an inner cylindrical wall defining a depression therein, said cylindrical portion of said pilot member being in engagement with said inner cylindrical wall to restrain movement of said pilot with respect to said first die member to directions parallel to the direction said first die member is driven.

3. The tooling defined in claim 2 including:

a second die member having a die surface for engagement and deformation of the second surface of the structural member and means adapted to'engage means for driving said die surface of said second die member into the second surface, said die surface of said second die member having a crosssection which includes a linear section generally perpendicular to the direction said second die member die surface is driven and curved sections on opposite sides of said linear section extending from tangents thereto.

4. The tooling defined in claim 3 wherein the curved sections of said die member die surface cross-section have radii which are less than the length of said linear section of said second die member die surface crosssection.

5. Tooling for improving the fatigue strength of a structural member having first and second surfaces and a discontinuity in at leastsaid first surface, said tooling including:

a first die member having a die surface for engagement and deformation of the first surface of the structural member and means adapted to engage means for driving said die surface into the first sur face, said die surface having a cross-section which includes a linear section generally perpendicular to the direction said die surface is driven and curved sections on opposite sides of said linerar section extending from tangents thereto;

a pilot member adapted to engage the discontinuity and to space said die surface therefrom;

means connecting said pilot member to said first die member whereby said pilot member can move with respect to said die member;

a second die member having a die surface for engagement and deformation of the second surface of the structural member and means adapted to engage means for driving said die surface of said second die member into the second surface, said die surface of said second die member having a crosssection which includes a linear section generally perpendicular to the direction said second die member die surface is driven and curved sections on opposite sides of said linear section extending from tangents thereto; and

a shaft adapted to engage and restrain said second die member, said shaft including means adapted to have force applied thereto, said pilot member being mounted on said shaft, said pilot member being ring shaped and having an inner and outer wall, said outer wall being shaped to engage said force applied thereto of said shaft. discontinuity and said inner wall being shaped to 6. The tooling defined in claim 5 wherein said pilot engage said shaft, said first die member being slidmember is slidably mounted on said shaft. ably mounted on said shaft and having an abutment 7. The tooling defined in claim 5 wherein said first surface, the driving means for said die members ap- 5 and second die members include radial alignment plying force between said abutment surface of said means. first die member and said means adapted to have

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Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US4391358 *Nov 5, 1980Jul 5, 1983Haeger Virgil JHardware press and punch apparatus
US4578984 *Mar 5, 1984Apr 1, 1986Uddeholm Strip Steel AktiebolagMachine for deforming the gullets of saw blades to improve resistance to fatigue stress
US6209381 *Jul 7, 1999Apr 3, 2001Kuroda Precision IndustriesMethod and system for chamfering and press therefor
US6230537Sep 22, 1999May 15, 2001Stresswave, Inc.Method and apparatus for producing beneficial stresses around apertures by use of focused stress waves, and improved fatigue life products made by the method
US6389865Mar 16, 1999May 21, 2002Stresswave, Inc.Method and apparatus for producing beneficial stresses around apertures by use of focused stress waves
US6615636 *May 15, 2001Sep 9, 2003Stresswave, Inc.Method and apparatus for improving the fatigue life of components and structures using the stresswave process
US6711928Sep 22, 2000Mar 30, 2004Stresswave, Inc.Method and apparatus for producing beneficial stresses around apertures, and improved fatigue life products made by the method
US6742376Feb 9, 2001Jun 1, 2004Stresswave, Inc.Method and apparatus for manufacturing structures with improved fatigue life
US7047786Jan 30, 2002May 23, 2006Stresswave, Inc.Method and apparatus for improving the fatigue life of components and structures
US7131310Jun 1, 2004Nov 7, 2006Stresswave, Inc.Method for manufacturing improved fatigue life structures, and structures made via the method
WO2002024372A1 *Sep 24, 2001Mar 28, 2002Eric T EasterbrookMethod and apparatus for improving the fatigue life of components and structures
Classifications
U.S. Classification72/416, 72/446, 72/470
International ClassificationB44B5/00, B21D37/00, B21J5/00
Cooperative ClassificationB44B5/00, B23P9/025, B21D37/00, B21J5/00
European ClassificationB23P9/02A, B44B5/00, B21D37/00, B21J5/00