US20030116924A1 - Stress-induced connecting assembly - Google Patents
Stress-induced connecting assembly Download PDFInfo
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- US20030116924A1 US20030116924A1 US10/288,385 US28838502A US2003116924A1 US 20030116924 A1 US20030116924 A1 US 20030116924A1 US 28838502 A US28838502 A US 28838502A US 2003116924 A1 US2003116924 A1 US 2003116924A1
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- component
- assembly
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- axis
- elastic
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/02—Sealings between relatively-stationary surfaces
- F16J15/06—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces
- F16J15/08—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with exclusively metal packing
- F16J15/0887—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with exclusively metal packing the sealing effect being obtained by elastic deformation of the packing
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/02—Sealings between relatively-stationary surfaces
- F16J15/06—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces
- F16J15/064—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces the packing combining the sealing function with other functions
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/02—Sealings between relatively-stationary surfaces
- F16J15/06—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces
- F16J15/08—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with exclusively metal packing
- F16J15/0806—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with exclusively metal packing characterised by material or surface treatment
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/16—Sealings between relatively-moving surfaces
- F16J15/164—Sealings between relatively-moving surfaces the sealing action depending on movements; pressure difference, temperature or presence of leaking fluid
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B3/00—Measuring instruments characterised by the use of mechanical techniques
- G01B3/22—Feeler-pin gauges, e.g. dial gauges
- G01B3/28—Depth gauges
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S277/00—Seal for a joint or juncture
- Y10S277/935—Seal made of a particular material
- Y10S277/939—Containing metal
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S285/00—Pipe joints or couplings
- Y10S285/909—Fluorocarbons and memory plastics
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Gasket Seals (AREA)
- Insertion Pins And Rivets (AREA)
- Quick-Acting Or Multi-Walled Pipe Joints (AREA)
Abstract
A connecting assembly is disclosed having a first component defining an opening, a second component adapted to be retained together with the first component and a connector component made of a super-elastic alloy. Relative motion between at least two of the components causes a super-elastic activation of the connector wherein the activation simultaneously retains the components together with the connector interposed jointly there between. Preferably the connector component is pre-assembled to one of the first and second components. More preferably, the first component is pre-assembled with the connector and the second component is moved relative to the pre-assembled components to activate the super-elastic alloy of the connector. Alternatively, the second component is pre-assembled with the connector and the first component is moved relative to the pre-assembled components to activate the super-elastic alloy of the connector. In another alternative assembly, the first and second components are pre-assembled and relative motion occurs between the connector and the pre-assembled components.
Description
- This application is a continuation of application Ser. No. 09/523,719 filed Mar. 11, 2000, which is a continuation in part of Ser. No.09/311,938, filed May 14, 1999.
- The present invention relates generally to metallic connectors and metallic shape memory seals, that is, devices that join together multiple parts by means of an interposed member, particularly connectors having one or more elements made of material that possesses super-elastic properties. The present connectors and seals are suitable for high-performance industrial and medical applications involving different ranges of operating temperatures and component materials being connected/sealed.
- The present inventor has previously published application Ser. No. WO 00/70244 entitled “Stress Induced Seal” on Nov. 23, 2000.
- The use of metallic super-elastic alloys, such as Ni—Ti (nitinol) and other bi- or tri-metal alloys, has been documented in a variety of technical applications, including fasteners, connectors, gaskets, clamps and seals. Many such uses have required temperature in order to activate the material and change its physical state, while others have used mechanical forces that impart stress to cause a super-elastic physical deformation in the material. Still others have employed a combination of temperature and mechanical stress causing a shape memory effect to function in a desired product. As will be seen, however, not all shape memory materials are pseudo-elastic, because not all exhibit super-elastic behavior at their operating temperatures. Of particular concern to the instant inventor is the application of the super-elastic material to connectors and seals. The use of non-corrosive, metallic super-elastic material offers a decided advantage in high performance connecting assemblies, versus more traditional assemblies requiring threaded fasteners, springs, clamps or other holding or securing mechanisms. Particularly, super-elastic alloys can withstand more wear than materials used in conventional connectors, due to harder surface characteristics. They can also withstand extreme vibrations and not loosen due to their elastic pre-loaded condition, without the use of conventional adhesives to hold the assembled components and/or the connector itself together. Adhesives used with conventional connectors make them very difficult to disassemble, whereas it is generally possible to make a super-elastic connector completely reversible. The use of non-corrosive, metallic shape memory material offers a decided advantage in high performance sealing environments, versus pliable synthetic rubber or silicone materials, in their ability to withstand a more substantial sealing load under extremes of pressure and temperature while not drying up the way rubbers and silicones can.
- U.S. Pat. Nos. 5,395,193 and 5,584,631 to Krumme et al., discuss the use of nickel-titanium shape memory retainers in an optimized elastic condition that have super-elastic or pseudo-elastic properties. These fasteners are said to be useful for eyeglass assembly; they are placed onto a pin to retain components together. However, this use does not contemplate an interposed connector. In U.S. Pat. Nos. 5,395,193 and 5,584,631, also co-invented by Krumme, the aforementioned optimized elastic materials are further incorporated in a Belleville fastener said to be useful in eyeglass frames.
- U.S. Pat. No. 5, 683,404 to Johnson, entitled “Clamp and Method for its Use”, further discusses shape memory materials that are “pseudo-elastic”, defining these materials in terms of their ability to exhibit super-elastic/pseudo-elastic recovery characteristics at room temperature. Such materials are said to deform from an austenitic crystal structure to a stress-induced structure postulated to be martensitic in nature, returning thence to the austenitic state when the stress is removed. The alternate crystal structures described give the alloy super-elastic or pseudo-elastic properties. Poisson's Ratio for nitinol is about 0.3, but this ratio significantly increases up to approximately 0.5 or more when the shape memory alloy is stretched beyond its initial elastic limit. It is at this point that stress-induced martensite is said to occur, i.e., the point beyond which the material is permanently deformed and thus incapable of returning to its initial austenitic shape. A special tool is employed by Johnson to impart an external stretching force that deforms the material which force is then released to cause the material to return to its original condition. While the device is stretched, a member is captured by it and securely clamped when the stretching force is released. This device is intended for use in clamping and does not contemplate traditional connecting operations of the kind addressed by the present invention. Another use envisioned by Johnson is in connecting the modular components of a medical device, as described in his U.S. Pat. No. 5,858,020, by subjecting a thimble component made of shape memory material to an external stretching stimulus to elongate and thereby reduce its transverse dimension. Upon release of the stretching force, this component returns towards its original rest dimension, contacting and imparting a force on another component. This is a sequential stretching and relaxation of the super-elastic material rather than a simultaneous activation and retention operation. Also, special structures are necessary on the thimble to allow the stretching force to be imparted.
- U.S. Pat. No. 4,896,955 to Zider and Krumme, entitled “Eyeglass Frame Including Shape Memory Elements”, characterizes the use of nickel-titanium shape memory alloys that have super-elastic or pseudo-elastic properties. In criticizing these materials, it is said that the effective useful temperature range for such purely pseudo-elastic components in eyeglass frames is too narrow. This limitation was further said to be remedied by fabrication of such components from materials having “optimized elasticity” properties, that is, work-hardened shape memory alloys.
- In U.S. Pat. No. 5,197,720 to Renz, et al., a work piece is held within a clamping tool by an expansion element made of shape memory material that is activated by mechanical force. In this way, torque is transmitted through the shape memory member. This device is useful for bringing parts together for holding the work piece in order to perform an operation. It does not, however contemplate a use as a connector or a seal. U.S. Pat. No. 5,190,546 to Jervis discloses insertion into a broken bone cavity of a split member made of shape memory material using a super-elastic alloy. The split member holds the walls of the bone cavity when radial compressive forces acting on it are released. In order for the radial compressive force to reduce the diameter, the component must be split, allowing the reduction in dimension for insertion. It does not act as an interposed member in a connecting assembly nor does it exhibit sealing behavior.
- Others have sought to utilize the properties of shape memory materials as locking, connector and bearing elements, e.g., U.S. Pat. Nos. 5,507,826 to Besselink, et al., 5,779,281 to Kapgan, et al., and 5,067,827 to Arnold, respectively; however, such approaches have required temperature to be applied during use. U.S. Pat. Nos. 5,277,435 to Kramer, et al. and 5,876,434 to Flomenblit, et al similarly has relied upon temperature to activate the shape memory effect. Such dependence on extrinsic activation by temperature introduces an added process step and may further be disadvantageous in certain other applications.
- U.S. Pat. No.5,842,312 to Krumme, et al., entitled, “Hysteretic Damping Apparati and Methods”, employs shape memory tension elements to provide energy dissipation. Such elements can be placed between building structures, etc., which are subject to vibration, serving to absorb the energy created by their relative movement. However, this patent does not contemplate the vibration dampening effect of a super-elastic material in the formation of a connector or a seal. None of the above-mentioned prior approaches have contemplated the formation of an effective seal such as envisioned by the present inventor. Moreover, the aforementioned Renz, et al patent, although transmitting torque through a work piece, does not contemplate doing so while forming a seal. Further, a key feature of certain seals is their ability to accommodate changes of differing kinds in the members being sealed, such as thermal expansion. Pliable rubbers and silicones, for example, have this characteristic; however, the operating demands are decidedly different in high performance metallic sealing applications.
- Prior approaches to the formation of seals from shape memory alloys will now be addressed. Reference is now made to U.S. Pat. No. 5,862,995 to Wu, entitled, “High Pressure Fluid Passage Sealing for Internal Combustion Engine Fuel Injectors and Method of Making Same”. In this patent, a shape memory alloy plug is inserted into an open end of a fuel passage, undergoing a metallurgical phase change from martensite to austenite to effect a seal with the passage. This is done by pre-straining the plug when it is cooled within a temperature range of—minus 100 to minus 80 degrees Celsius. U.S. Pat. No. 5,226,683 to Julien, et al, entitled, “Reusable Metallic Seal Using Memory Metal”, employs an annulus of binary metal in the martensite state that is positioned for use, then heated above a transition temperature to an austenite state for removal and reuse. In U.S. Pat. No. 4,281,841 to Kim, et al, entitled, “O-Ring Sealing Arrangements for Ultra-High Vacuum Systems”, a heat-recoverable tube is chilled to its martensitic state, then deformed, and returned to its austenitic state by means of temperature activation.
- However, all of the above attempts involved temperature changes to a shape memory material. The material is initially in an austenitic state, then chilled to a martensitic physical state where it becomes malleable, i.e., not elastic. It is important to note that this process step occurred before a seal was formed. The material was subsequently formed into an intermediate shape and placed into the sealing assembly. The temperature was raised above the austenite transition temperature where the material recovered towards its original austenitic shape and size, effecting a seal.
- Accordingly, there is a need to form a durable metallic, non-corrosive seal or plug, beginning with a shape memory material in its austenitic state and inducing a super-elastic behavior via stress-induction to form an effective high performance seal.
- There is a further need to form a seal that decreases the temperature sensitivity of a component made from a shape memory material.
- Accordingly, there is a need to form a connecting assembly using a durable metallic, non-corrosive connector assembly, which are simple to install using relative motion to activate the assembly.
- There is a further need to form a secure connection between components that minimizes the micro-motional wear characteristics of the assembly, enhancing its useful life.
- There is another need to form a fastened assembly that does not require temperature for its activation.
- There is still a further need to form a stress-induced seal/connector using a pre-tensioned shape memory alloy that adjusts for differences in thermal coefficients of expansion or contraction of dissimilar materials comprising those components being sealed/connected.
- There is still a further need to form a pre-tensioned seal/connector that allows for vibration dampening, transmitted through a sealed member.
- There is still a further need to form a pre-tensioned seal that allows for torque to be transmitted through a sealed member.
- There is still a further need for a connector with elastic properties that allow more forgiving tolerances during manufacturing of the assembly components.
- According to the present invention, a seal forming connecting assembly has at least two components. A first component defines a given shape with a cross section having a first dimension. A second component defines a second given shape having a cross section which is continuous with at least a second dimension sized with interference to the first dimension, the second component being made of a super-elastic alloy. One of the first and second components includes an opening that corresponds to its associated cross-section wherein relative motion causes the first dimension to contact the second dimension, imparting a force to super-elastically expand or contract the second dimension, allowing them to be jointly retained.
- According to an embodiment of the present invention, a connecting assembly has a first component defining an opening, a second component adapted to be retained together with the first component and a connector component made of a super-elastic alloy. Relative motion between at least two of the components causes a super-elastic activation of the connector wherein the activation simultaneously retains the components together with the connector interposed jointly there between.
- In a preferred embodiment of the present invention, the connector component is pre-assembled to one of the first and second components. More preferably, the first component is pre-assembled with the connector the second component is moved relative to the pre-assembled components to activate the super-elastic alloy of the connector. Alternatively, the second component is pre-assembled with the connector and the first component is moved relative to the pre-assembled components to activate the super-elastic alloy of the connector.
- In another preferred embodiment, the first and second components are pre-assembled and relative motion occurs between the connector and the pre-assembled components.
- In yet another embodiment of the present invention, the opening defines an axis and relative motion occurs along the axis; alternatively, the relative motion could occur normal to the axis.
- In still another embodiment of the present invention, the components are rigidly retained.
- In still yet another embodiment of the present invention, the connection forms a seal.
- An advantage of an embodiment of the present invention is that a super-elastic alloy, e.g., nickel-titanium has an oxide layer presenting a stronger wear surface than other traditional connectors. Moreover, the connector component is elastic in nature, allowing it to act as a vibration-dampening member that prevents the assembly from loosening. Also, the components of the present assembly are more forgiving of manufacturing tolerances. These connectors are entirely reversible.
- Another advantage of an embodiment of the present invention is that a connection is effected by simple relative motion, not requiring threaded fasteners; springs, clamps or other holding or securing mechanisms. This feature allows the connectors to be operable in a much smaller working space, further avoiding the complexity associated with traditional connection devices.
- A further advantage of an embodiment of the present invention is that the super-elastic properties are not dependent on temperature to impart the activation force required to effect such a connection.
- Other objects and advantages will be appreciated by those skilled in the art, by resort to the appended Drawings having reference numerals that correspond to the ensuing Description of one or more embodiments of the invention wherein the following Figures are further elucidated.
- FIG. 1 is an exploded external side view of a ball and a super-elastic component (i.e., a washer), shown prior to assembly, illustrating the super-elastic effect operative in the present invention;
- FIG. 2 is a sequential view of FIG. 1, showing the ball fully engaged with the washer to form a connection;
- FIG. 3 is a further sequential view of FIG. 2, showing the ball pushed entirely through the washer;
- FIG. 4A is a top plan view of the washer of FIG. 3;
- FIG. 4B is a top plan view of an alternative, open sided washer;
- FIG. 5 is side view of a connector assembly of the invention showing a first component with an opening, a second component in the form of a ball, and a connector component (shown in phantom) in the form of a washer, prior to assembly;
- FIG. 6 is a sequential view of FIG. 5 showing the components assembled (shown partially in phantom);
- FIG. 7 is a side view of a connecting assembly similar to that shown in FIG. 5 with an alternative second component in the form of a pin;
- FIG. 8 is a side view of a connecting assembly of the present invention, prior to activation by an external force, showing a first component with a collet activating a pre-assembled connector component (washer shown in phantom) to retain the second component (i.e., pin partially shown in phantom);
- FIG. 9 is a sequential view of FIG. 8 showing the components retained together upon activation of connector component (shown in phantom) by an external force applied to the collet;
- FIG. 10 is a perspective view of an open sided connecting assembly of the present invention, showing a first component and a connector component pre-assembled prior to activation of the connector by a second component i.e., ball;
- FIG. 11 is a sequential front view of FIG. 10 showing the components retained together upon activation of the connector (shown in phantom) by relative motion of the ball;
- FIG. 12 is a side view of FIG. 11;
- FIG. 13 shows a perspective view of a connecting assembly of the present invention with a first body component pre-assembled with a second pin component prior to activation of multiple connector tube components to retain the pre-assembled components;
- FIG. 14 is a sequential top view of FIG. 13, showing the assembly with its components connected;
- FIG. 15 is a cross-sectional view taken substantially along lines15-15 of FIG. 14, showing deformation of the super-elastic connector tubes;
- FIG. 16 is an exploded side view, partially in cross section, of a preferred fastener seal of the present invention, showing a super-elastic cover plate prior to engagement over a bolt head in a counter-bore; and
- FIG. 17 is a sequential view of FIG. 16, showing the plate installed over the fastener head.
- Referring to FIGS.1-3, the operative super-elastic properties employed by the present inventor are illustrated. In FIGS. 4A-4B, alternative super-elastic washers used in an experimental assembly are generally shown at 10. The remaining FIGS. 5-15 depict preferred embodiments of a connecting assembly of the instant invention.
- Referring again to FIGS.1-3, a first component of
assembly 10 is aball 12 defining a given spherical shape with a cross sectional diameter having a first dimension Dl. A second component consists ofwasher 14 defining a second given shape, in this case annular, having a cross section which is continuous with at least a second dimension D2 sized with interference to the first dimension Dl. One of the first 12 and second 14 components, i.e.,washer 14 in FIGS. 1-3, includes anopening 16 with an entrance edge orlip 18 that is sized to correspond to its associated continuous cross-section, i.e., the inner diameter D2. In FIG. 2, relative motion indicated byarrow 13 ofball 12 with first dimension Dl causes it to contact the second dimension D2 ofwasher 14, imparting a force to super-elastically expand the second dimension, allowing the ball and washer to be jointly retained with one another. - Referring still to FIGS.1-3 first dimension DI is preferably greater than second dimension D2 and the relative motion of the first 12 and second 14 component causes the second dimension to expand. Although not shown in these Figures, the
assembly 10 may be provided with means for creating therelative motion 13; however, it is possible to impart the necessary force to assemble thecomponents -
Washer 14 is preferably an integral member made of a super-elastic alloy, preferably nitinol, and more preferably SE508 nitinol. This material is described in “Nitinol SE508 Data Sheet”, and is available from Nitinol Devices & Components, Inc., located in Fremont, Calif. All of the super-elastic components referred to herein preferably are made of Nitinol SE508. - Experiment 1
-
Washer 14 of FIGS. 1-3 was placed in a mechanical clamping structure (not shown) at room temperature prior to forming theexperimental assembly 10.Ball 12 was made of polished stainless steel, with a uniform spherical diameter D1 of 0.375 inches. The initial resting dimensions ofwasher 14 were as follows: inner diameter D2=0.360; outer diameter D3=0.550; thickness T1=0.050.Washer 14 was placed under the press with its axial movement constrained by a support plate having an aperture (further not shown) underlyingopening 16, the plate limiting the downward motion of the washer.Ball 12 was placed at the entrance to opening 16 and the press engaged to move the ball downward, forcing it into the opening. The super-elastic material ofwasher 14 was activated byball 12 in response to the expansion of its inner diameter D2, by interference with the diameter D1 of the ball, up to a maximum insertion of the ball as shown in FIG. 2. The outer diameter D3 ofwasher 14 was then measured withball 12 thus inserted and it was observed to increase 0.014 inches to a new diameter D2 of 0.564 inches. That is, the outer diameter D3 ofwasher 14 expanded 0.014 inches, in nearly direct proportion to the difference between the ball diameter D1 and the inner diameter D2 of the washer. Neither the diameter D1 ofball 12 nor thickness T1 ofwasher 14 were observed to change.Ball 12 was then pushed completely through the inner diameter D2 ofwasher 12, whereupon the dimensions of the washer were measured as follows: outer diameter D3=0.556; and inner diameter=0.367. Therefore, some of the deformation was of a “plastic” nature, that is, the dimensions ofwasher 14 were permanently altered. Because the super-elastic material was in the austenitic state, there was no return to the extent of such plastic deformation. The 1-2% stated elastic capacity was thus exceeded, and so the plastic deformation ensued to the extent it was beyond this elastic capacity. In order to verify the results observed above, I repeated this experiment with a different washer having substantially the same dimensions and observed similar results. - Experiment 2
- The
same ball 12 andwasher 14 from the initial run of Experiment 1 was used to form theassembly 10. I postulated that the maximum plastic deformation had already occurred and, thus, would not further change. It was expected that thewasher 14 would preserve its super-elastic properties and continue to admitball 12 intoopening 16, therefore expanding the resting dimensions of the washer in the manner observed for the initial run of Experiment 1. I observed that the inner D2 and outer D3 diameters ofwasher 14 measurably expanded to practically the same dimensions as was observed before, not greater or less. Whenball 12 was pushed throughopening 16, the same dimensions were observed as at the conclusion of the initial run of Experiment 1. A uniform band or swath 17 (FIG. 3) was observed upon passage ofball 12 through washer 14 (FIG. 3), in the circumferential area of diameter D1 corresponding to its contact with the super-elastic material of the inner diameter D2. This indicates that an even seal was effectively formed in a substantial area surrounding the circumference ofball 12, rather than a narrow line of contact. Thus it is concluded that the super-elastic material deformed in response to the stress-activated seal formation by the relative motion, conforming to the contour ofball 12. - With further reference to FIGS.1-3, either of the first 12 and second 14 components the
experimental assembly 10 had a tapered lead to facilitate activation of the super-elastic alloy.Lip 18 of opening 16 may have a chamfered entrance edge (not shown), functioning as a lead-in that makes easier the insertion of the first dimension D1 into the second dimension D2. - Returning to FIG. 4B and with reference to FIGS.10-12, a connector component in the form of an alternative washer is shown at 314 with an
opening 316. Thiswasher 314 is configured for use in the connector assembly generally shown at 310 as will be described below. - In FIGS.5-6, a connection assembly is generally shown at 110. A
ball 112 and awasher 114 are similar to those shown by FIGS. 1-3, except they are activated within a third component represented by abody 120 having an opening consisting of a through-bore 121 with a counter-bore 122 within which the washer is placed.Washer 114 has anopening 116. Through-bore 121 has a central axis A which, preferably, also passes through the center ofopening 116. Theball 112 is moved in the direction indicated byarrow 113 along axis A, that is, relative axial motion, into opening 116 (FIG. 6) inducing an internal stress in theconnector causing opening 116 to super-elastically expand in the direction of divergingarrows 124. Likewise the outer diameter D3 expands to engage and form a connection againstcounter-bore 122. Because the outer diameter of washer D3, when engaged withcounter-bore 122, exerts an inward radial force shown by arrows 126, the inner diameter D2 further contracts and exerts additional force onball 112. FIG. 7 is similar to FIGS. 5-6 but for the substitution ofpin 111 forball 112. - The components can be connected in various ways either by pre-assembling two of the components as shown in FIGS. 8 and 10 then assembling these with the third in a final assembly as in FIGS. 9 and 11-12. Tolerances can be chosen, as will be appreciated by those skilled in the art, so that there is an initial interference fit between components so that they can be temporarily held together in preparation for the final assembly. Alternatively, the tolerances could be chosen so that, while in the pre-assembled state, the components are loosely placed into position in preparation for final assembly as shown in FIGS. 5-7.
- In FIGS.8-9, a connecting assembly is generally shown at 210 with a first component in the form of a
body 220 including acollet 219. A second component in the form ofpin 211 and a connector component in the form of awasher 214 are provided, similar to those shown in FIG. 7.Body 220 has an opening consisting of abore 221 with a counter-bore 222 within whichwasher 214 is placed. Similar to FIGS. 1-7,washer 214 has anopening 216.Bore 221 has a central axis A which, preferably, also passes through the center ofopening 216.Pin 211 is pre-assembled in a loose-fitting relationship withinopening 216.Collet 219 is radially compressed in the direction indicated byarrow 213 along axis A, that is, relative motion is in a direction normal to axis A thereby inducing an internal stress inconnector 214 causingopening 116 to super-elastically contract effecting the connection. Inherently, when thesuper-elastic component 214 is activated bycollet 219, the outside dimension D3 (shown for example in FIG. 1) of the super-elastic component elastically contracts, effecting a connection between the collet and the super-elastic component. The connection betweencollet 219 andsuper-elastic component 214 is effected prior to the connection between the collet andpin 211. Various means could be employed toradially compress collet 219 in a direction normal to axis A, e.g., the slide ablyadjustable sleeve 230 of FIGS. 8-9, as will be appreciated by those skilled in the art. It is to be understood that the term “relative motion” encompasses the axial motion described in conjunction with FIGS. 1-7, as well as the radial compression ofcollet 219 in FIGS. 8-9 which results in motion of the collet in a direction normal to axis A relative to bore 221. - In FIGS.10-12, a connecting assembly is generally shown at 310. A connector component represented by a
washer 314, is pre-assembled with a first component represented by abody 320.Body 320 has an opening consisting of an open through-bore 321 with agroove 323 within which thewasher 314 is placed.Washer 314 has anopening 316. Through-bore 321 has a central axis A which, preferably, also passes through the center ofopening 316. Aball 312 is moved in the direction indicated byarrow 313 along axis A, that is, relative axial motion, intoopening 316. Alternativelyball 312 can be moved in a direction indicated byarrow 315 normal to axis A, into theopening 316. Asball 312 enterswasher opening 316, it induces an internal stress inwasher 314, causing the opening to super-elastically expand engaging thegroove 323 effecting a connection.Body 320 preferably has abase 324 and ashaft 326 projecting therefrom. - In FIGS.13-15, a connecting assembly is generally shown at 410. A
first component body 420 has a throughbore 421 defining an axis A. A second component shown as apin 411 is pre-assembled within thebore 421 in a loosely fitting relationship. Connector component represented by at least one, preferably a pair ofpegs 414, are aligned with throughholes 428 in thebody 420. The throughholes 428 run normal to axis A and pass partially into the throughbore 421. Thepegs 414 are inserted in the direction ofarrows 405 into the throughholes 428 in thebody 420. As thepegs 414 are inserted in an interposed relationship to thebody 420 and the pin 411 a super-elastic response is induced in thepegs 414 effecting a connection. In an alternative thepegs 414 can be per-assembled in the throughholes 428 in thebody 420. Then, thepin 411 is moved axially within the throughbore 421 bringing it into contact with thepegs 414 effecting a connection. - The fastening seal assembly is shown in FIGS.16-17. A
washer 614 made of super-elastic material is used to seal afastener 628 received within a threadedaperture 664 formed in abody 620. Thebody 620 has anopening 616 leading into a counter-bore 622 within which both thehead 632 of tightenedfastener 628 and thewasher 614 are received, as in FIG. 17. The outside diameter of thewasher 614 can be sized larger than the ID of the counter-bore 622. Inherently then, when thewasher 614 is moved in an axial direction into interfering contact with the counter-bore 622, the interference causes a super-elastic activation in thewasher 614. Thewasher 614 then contracts allowing the washer to connect against the counter-bore 622. At the same time the stress activation also causes the inner diameter of thewasher 614 to contract. Hence, activation of the super-elastic material of thewasher 614 by tightening ofbolt 628 into threadedaperture 664 causes outward radial stress that locks its outer diameter againstcounter-bore 622. The stress activation also causes the inner diameter ofwasher 614 to contract where it is desirable to have it grip the threadedshaft 634, in the case (not shown) where the washer is located beneathhead 632 and pre-assembled withfastener 628 prior to insertion into theopening 616. That is, for use as a locking seal washer. - While one or more preferred embodiments of the present invention have been described, it should be understood that various changes, adaptations and modifications may be made without departing from the spirit of the invention and the scope of the appended claims:
Claims (24)
- 36. A connecting assembly comprising,a first component defining a bore, anda washer component made of a super-elastic alloy, whereuponrelative motion between the components causes an interference between the washer and the bore creating a super-elastic activation in the washer, the activation simultaneously connecting the components together in an operatively fixed relative position.
- 37. The assembly of
claim 36 wherein the bore defines an axis, and the washer defines an axis. - 38. The assembly of
claim 37 wherein the axes are positioned in alignment. - 39. The assembly of
claim 38 wherein the relative motion occurs in a direction parallel to the axes. - 40. The assembly of
claim 36 further comprises a third component that is retained with the assembly as the connection is effected. - 41. The assembly of
claim 40 wherein the third component is mobile within the assembly. - 42. The assembly of
claim 36 wherein the washer component is nitinol. - 43. The assembly of
claim 36 wherein the super-elastic properties of the washer are exhibited within the operating temperature range of the assembly. - 44. The assembly of
claim 36 wherein the washer effects a seal. - 45. A connecting assembly comprising,a first component with a body defining a bore with an axis, presenting a radially compressible or deformable portion, anda second component made of a super-elastic alloy with a hole defining an axis, whereuponrelative motion between the first component and the second component causes a super-elastic activation in the second component, the activation simultaneously connecting the components together in an operatively fixed relative position.
- 46. The assembly of
claim 45 wherein the bore axis and the second component axis are aligned. - 47. The assembly of
claim 46 wherein the relative motion occurs in a direction substantially perpendicular to the axes. - 48. The assembly of
claim 45 wherein the radially compressible or deformable portion is enabled by slits formed in the body. - 49. The assembly of
claim 48 further comprising a sleeve component defining an axis aligned with the bore axis. - 50. The assembly of
claim 49 wherein relative axial motion between the sleeve components and the radially compressible or deformable portion cause the radially compressible or deformable portion to move in a substantially perpendicular direction to the bore axis. - 51. The assembly of
claim 50 wherein the motion of the radially compressible or deformable portion causes the super-elastic activation. - 52. The assembly of
claim 45 wherein the second component is nitinol. - 53. The assembly of
claim 45 wherein the super-elastic properties of the second component are exhibited within the operating temperature range of the assembly. - 54. A connecting assembly comprising,a first component with a body defining a bore with an axis, the body having slits to enable a portion to be radially compressible,a second component made of a super-elastic nitinol alloy with a hole defining an axis aligned with the bore axis, anda third sleeve component defining an axis aligned with the bore axis, whereuponrelative motion between the sleeve component and the radially compressible portion cause the radially compressible portion to move in a direction substantially normal to the bore axis contacting the nitinol component causing a super-elastic activation, the activation simultaneously connecting the components together in an operatively fixed relative position.
- 55. The assembly of
claim 54 wherein the super-elastic properties of the nitinol are exhibited within the operating temperature range of the assembly. - 56. A connecting assembly comprising,a first component with a body defining a bore with an axis, presenting a radially compressible portion; anda second component made of a super-elastic alloy with an axis, whereuponrelative motion between the first component and the second component causes a super-elastic activation in the second component, the activation simultaneously connecting the components together in an operatively fixed relative position.
- 57. A connecting assembly comprising,a first component with a body defining a bore with an axis, presenting a radially compressible portion; anda second component made of a super-elastic alloy with an axis, whereuponrelative motion between the first component and the second component causes a super-elastic activation in the second component, the activation simultaneously connecting the components together in an operatively fixed relative position.
- 58. A connecting assembly comprising,a first component with a body defining a bore with an axis, including a collet with slits; anda second component made of a super-elastic alloy with a hole defining an axis, whereuponrelative motion between the first component and the second component causes a super-elastic activation in the second component, the activation simultaneously connecting the components together in an operatively fixed relative position.
- 59. The connecting assembly of
claim 58 wherein the slits allow the collet to be radially compressible.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/288,385 US20030116924A1 (en) | 1999-05-14 | 2002-11-05 | Stress-induced connecting assembly |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US31193899A | 1999-05-14 | 1999-05-14 | |
US09/523,719 US6257593B1 (en) | 1999-05-14 | 2000-03-11 | Stress induced interposed connector |
US09/860,918 US6513814B2 (en) | 1999-05-14 | 2001-05-18 | Stress induced connecting assembly |
US10/288,385 US20030116924A1 (en) | 1999-05-14 | 2002-11-05 | Stress-induced connecting assembly |
Related Parent Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US09/860,918 Continuation US6513814B2 (en) | 1999-05-14 | 2001-05-18 | Stress induced connecting assembly |
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US20030116924A1 true US20030116924A1 (en) | 2003-06-26 |
Family
ID=24086182
Family Applications (3)
Application Number | Title | Priority Date | Filing Date |
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US09/523,719 Expired - Lifetime US6257593B1 (en) | 1999-05-14 | 2000-03-11 | Stress induced interposed connector |
US09/860,918 Expired - Lifetime US6513814B2 (en) | 1999-05-14 | 2001-05-18 | Stress induced connecting assembly |
US10/288,385 Abandoned US20030116924A1 (en) | 1999-05-14 | 2002-11-05 | Stress-induced connecting assembly |
Family Applications Before (2)
Application Number | Title | Priority Date | Filing Date |
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US09/523,719 Expired - Lifetime US6257593B1 (en) | 1999-05-14 | 2000-03-11 | Stress induced interposed connector |
US09/860,918 Expired - Lifetime US6513814B2 (en) | 1999-05-14 | 2001-05-18 | Stress induced connecting assembly |
Country Status (4)
Country | Link |
---|---|
US (3) | US6257593B1 (en) |
CN (1) | CN1416512A (en) |
AU (1) | AU2001249172A1 (en) |
WO (1) | WO2001069108A1 (en) |
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US20170315598A1 (en) * | 2016-03-16 | 2017-11-02 | Microsoft Technology Licensing, Llc | Thermal management system including an elastically deformable phase change device |
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-
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-
2001
- 2001-03-12 CN CN01806417A patent/CN1416512A/en active Pending
- 2001-03-12 WO PCT/US2001/007950 patent/WO2001069108A1/en not_active Application Discontinuation
- 2001-03-12 AU AU2001249172A patent/AU2001249172A1/en not_active Abandoned
- 2001-05-18 US US09/860,918 patent/US6513814B2/en not_active Expired - Lifetime
-
2002
- 2002-11-05 US US10/288,385 patent/US20030116924A1/en not_active Abandoned
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20140361499A1 (en) * | 2013-06-11 | 2014-12-11 | General Electric Company | Shape memory alloy intersegment seals |
US20170315598A1 (en) * | 2016-03-16 | 2017-11-02 | Microsoft Technology Licensing, Llc | Thermal management system including an elastically deformable phase change device |
US10656688B2 (en) * | 2016-03-16 | 2020-05-19 | Microsoft Technology Licensing, Llc | Thermal management system including an elastically deformable phase change device |
Also Published As
Publication number | Publication date |
---|---|
US6257593B1 (en) | 2001-07-10 |
AU2001249172A1 (en) | 2001-09-24 |
WO2001069108A1 (en) | 2001-09-20 |
US6513814B2 (en) | 2003-02-04 |
US20010028148A1 (en) | 2001-10-11 |
CN1416512A (en) | 2003-05-07 |
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Legal Events
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STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |